tm 9 1425 450 12 tow 2 weapon system

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TM 9-1425-450-12 TECHNICAL MANUAL OPERATOR AND ORGANIZATIONAL MAINTENANCE MANUAL FOR TOW 2 WEAPON SYSTEM GUIDED MISSILE SYSTEM M220A2 (TOW 2 HEAVY ANTITANK/ ASSAULT WEAPON SYSTEM) WARNING This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C. Sec 2751, et. seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401, et. seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25. DISTRIBUTION STATEMENT D – Distribution authorized to Department of Defense and DoD contractors only due to critical technology. This determination was made October 1986. Other requests shall be referred to: Project Manager, CCWS Project Office, SFAE-MSL-CWS-O, Redstone Arsenal, AL 35898-5750. DESTRUCTION NOTICE – Destroy by any method that will prevent disclosure of contents or reconstruction of the document. HEADQUARTERS, DEPARTMENT OF THE ARMY 25 May 1983 PCN 349 142060 00

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Page 1: TM 9 1425 450 12 TOW 2 Weapon System

TM 9-1425-450-12

TECHNICAL MANUAL

OPERATOR AND ORGANIZATIONAL MAINTENANCE MANUAL

FOR

TOW 2 WEAPON SYSTEM GUIDED MISSILE SYSTEM

M220A2 (TOW 2 HEAVY ANTITANK/

ASSAULT WEAPON SYSTEM)

WARNING This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C. Sec 2751, et. seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401, et. seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

DISTRIBUTION STATEMENT D – Distribution authorized to Department of Defense and DoD contractors only due to critical technology. This determination was made October 1986. Other requests shall be referred to: Project Manager, CCWS Project Office, SFAE-MSL-CWS-O, Redstone Arsenal, AL 35898-5750.

DESTRUCTION NOTICE – Destroy by any method that will prevent disclosure of contents or reconstruction of the document.

HEADQUARTERS, DEPARTMENT OF THE ARMY 25 May 1983

PCN 349 142060 00

danny.mitchell
Text Box
This copy is a reprint which includes current pages from Changes 1-13.
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WARNING

WARNING

TM 9-1425-450-12

DANGEROUS VOLTAGE

HIGH VOLTAGE is used in this system. Death or injury can result if you do notobserve the safety precautions given in this manual.

LOW VOLTAGE can also be dangerous. DON’T be misled by this term. Potentials as lowas 50 volts may cause death under certain circumstances.

SERIOUS EYE DAMAGE can occur if too much light is seen through day sight tracker.Do not look at sun or bright lights through day sight tracker.

If eye damage occurs, cover eyes and get medical help right away.

a

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WARNING

WARNING

TM 9-1425-450-12

SOLVENT AND ALCOHOL WILL BURN

Solvent and alcohol can explode and cause death or serious injury. BE SURE tofollow these precautions for the safety of personnel.

Keep it away from open flame,

Use only in area where there is plenty of fresh air.

Try not to get solvent on your bare skin.

If solvent gets in your eyes, wash them with plenty of water and get medicalhelp right away.

After using solvent, wash carefully so that there is no solvent on your bareskin.

The anti-reflective coating on night sight infrared optics contains thorium fluoridewhich is slightly radioactive. The only potential hazard involves ingestion(swallowing or inhaling) of this coating material. Dispose of broken lenses, etc.,in accordance with AR 385-11.

b

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WARNING

TM 9-1425-450-12

A lithium battery is used in this equipment, and is potentiallyhazardous if misused or tampered with. The battery containspressurized sulfur dioxide gas which is toxic. The followingprecautions must be strictly observed to prevent possibleinjury to personnel or damage to equipment:

Do not heat, incinerate, crush, puncture, disassemble, orotherwise abuse the battery in any way that may cause it torupture.

Do not short-circuit the battery, test for capacity, or attemptto recharge.

Do not use any battery showing signs of damage, such as bulging,swelling, disfigurement, a brown liquid in the plastic wrap, ora swollen plastic wrap.

Do not bypass internal fuse or replace with a fuse of adifferent rating.

Do not store battery in unused equipment for more than 30 days.

Do not dispose of lithium batteries with ordinary trash/refuse.Turn in batteries to your local Defense Reutilization andMarketing Office.

Turn off the equipment immediately if you detect the batterycompartment becoming unduly hot, hear battery venting (hissingsound), or smell irritating sulfur dioxide gas. Remove anddispose of the battery only after it is cool to touch.

In the event of a fire near a lithium battery, rapid cooling ofthe battery is important. Flood the equipment with water oruse a carbon dioxide extinguisher. Control of the equipmentfire and cooling may prevent the battery from venting andpotentially exposing lithium metal. In the event that lithiummetal becomes involved in fire, the use of a graphite basedClass D fire extinguisher is recommended, such as Lith-X orMet-L-X. Do not use a Halon type fire extinguisher on alithium battery fire.

Remove the battery when the voltage drops below 20 volts underload (or equipment does not operate properly) and replace witha new battery.

If there is a safety incident, or if you believe a safetyhazard exists, notify your local safety officer.

Change 5 c

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WARNING

WARNING

WARNING

TM 9-1425-450-12

PAINT, PRIMER, AND THINNERARE TOXIC AND FLAMMABLE

They must be used with extreme care.

Do not get them on skin. Wear eyeprotection and rubber gloves when using.

Avoid prolonged or repeated breathing ofvapors. Use only in well ventilated area.

Keep away from heat and open flames.If injury occurs, get medical help right away.

Never open one end of cargo/loader’s dooron HMMWV without first insuring that oppo-site end is securely closed. Not doing sowill cause both ends to open at the sametime causing injury to personnel, damageto equipment, or mission abort.

Cargo/loader’s door on HMMWV must beclosed and securely 1 atched at bothends before firing a missile. Firinga missile with door not secure willcause injury to personnel, damage toequipment, or mission abort.

d Change 5

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WARNING

TM 9-1425-450-12

Serious injury to personnel could result if crewmembers are inis fired.

Make sure that

firing danger zones when missile

all personnel are clear of firingdanger zones before doing missile loading procedure.

Make sure crew is out of firing danger zonesbefore pressing trigger.

All crew members stay in their firing positionsuntil missile hits target or explodes.

Ear damage can occur when missile is fired.All personnel within 50 meters of launchermust wear ear plugs (V-51R or equal).

For complete danger zone information and rangesafety guidelines, refer to AR 385-62.

Change 5 e

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WARNING

WARNING

WARNING

TM 9-1425-450-12

If forward slope at launch site is greater than30 degrees (300), injury to personnel and damageto equipment may occur when missile is fired. Ifsideways slope is greater than 10 degrees (100),adequate tracking may be impossible.

Do not fire missile over or in the direction ofelectrical wires. If command-link wires contacta live high voltage power line, injury to person-nel and damage to equipment may occur.

When launcher is mounted on a vehicle, positionvehicle so front or rear of vehicle is in linewith target. If launcher is loaded, keep missilepointed toward target area at all times. Observefiring angle limitations when firing over frontor rear of vehicle (para 2-66 and 2-78). If mis-sile fails to launch, hand off malfunctionedmissile to either left or right side of vehicleso missile always points downrange.

f Change 6

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TM 9-1425-450-12 C13

Change ) HEADQUARTERS ) DEPARTMENT OF THE ARMY NO. 13 ) Washington, D.C. 14 September 2004

Operator and Organizational Maintenance Manual

for

TOW 2 WEAPON SYSTEM, GUIDED MISSILE SYSTEM M220A2

(TOW 2 HEAVY ANTITANK/ASSAULT WEAPON SYSTEM)

WARNING This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C. Sec 2751, et. seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401, et. seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

DISTRIBUTION STATEMENT D – Distribution authorized to Department of Defense and DoD contractors only to protect critical technical data on systems or hardware. This determination was made October 1986. Other requests shall be referred to: Project Manager, CCWS Project Office, SFAE-MSL-CWS-O, Redstone Arsenal, AL 35898-5750.

DESTRUCTION NOTICE – Destroy by any method that will prevent disclosure of contents or reconstruction of the document.

OZONE DEPLETING CHEMICAL INFORMATION

This document has been reviewed for the presence of Class I Ozone Depleting Chemicals by the Engineering, Environment, and Logistics Oversight Office. As of Base Document through Change 11, dated 25 May 1983, all references to Class I Ozone Depleting Chemicals have been removed from this document by substitution with chemicals that do not cause atmospheric ozone depletion.

TM 9-1425-450-12, 25 May 1983, is changed as follows:

1. The pages affected by this change, appearing in the following listing, are to be inserted in the manual. New or changed text is indicated by a vertical bar in the margin of the page. Where a completed paragraph, chapter, section, or appendix is changed or added, a vertical line is placed in the margin by the title only. Changes to illustrations are indicated by miniature pointing hands. Changes to flow charts are indicated by a miniature hand pointing to the number of the step in which the change occurs.

Remove Pages Insert Pages

None A thru D i, ii i, ii 1-3, 1-4 1-3, 1-4 1-23 thru 1-26 1-23 thru 1-26 2-1, 2-2 2-1, 2-2 2-16.1, 2-16.2 2-16.1, 2-16.2 2-23, 2-24 2-23, 2-24 2-29 thru 2-38 2-29 thru 2-42 2-39 thru 2-42 2-43, 2-44

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TM 9-1425-450-12 C13

Remove Pages Insert Pages

2-57 thru 2-62 2-57 thru 2-62 2-95, 2-96 2-95, 2-96 2-113 thru 2-116 2-113 thru 2-116 2-119, 2-120 2-119, 2-120 2-127, 2-128 2-127, 2-128 2-133, 2-134 2-133, 2-134 2-144.1, 2-144.2 2-144.1, 2-144.2 2-144.5, 2-144.6 2-144.5, 2-144.6 2-153 thru 2-158 2-153 thru 2-158 2-163, 2-164 2-163, 2-164 2-169, 2-170 2-169, 2-170 2-175 thru 2-346 2-175/(2-176 blank) 2-347, 2-348 2-347, 2-348 2-407 thru 2-408.10 2-407 thru 2-408.13/(2-408.14 blank) none 2-409 thru 2-410.15/(2-410.16 blank) 2-411 thru 2-414 2-411 thru 2-414 2-459, 2-460 2-459, 2-460 3-3, 3-4 3-3/(3-4 blank) 3-11 thru 3-90 none 3-91, 3-92 3-91, 3-92 3-95, 3-96 3-95, 3-96 B-3, B-4 B-3, B-4 B-7 thru B-10 B-7 thru B-10 B-13, B-14 B-13, B-14 B-15 thru B-24 none D-5, D-6 D-5, D-6 D-7, D-8 none D-9, D-10 D-9, D-10 E-1 thru E-4 E-1 thru E-4

2. This transmittal sheet should be filed in the front of the publication for reference purposes.

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TM 9-1425-450-12 C13

0420201 Distribution: To be distributed in accordance with the initial distribution number (IDN) 320441, requirements for TM 9-1425-450-12.

By Order of the Secretary of the Army:

PETER J. SCHOOMAKER General, United States Army

Chief of Staff Official:

JOEL B. HUDSON Administrative Assistant to the

Secretary of the Army

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TM 9-1425-450-12C12

Change

No. 12

HEADQUARTERSDEPARTMENT OF THE ARMY

Washington, D.C., 8 December 1997

Operator and Organizational Maintenance Manual

FOR

TOW 2 WEAPON SYSTEM, GUIDED MISSILE SYSTEM M220A2

WARNING - This document contains technical data whose export is restricted by the ArmsExport Control Act (Title 22, U.S.C. Sec 2751 et seq.) or Executive Order 12470. Violators ofthese export laws are subject to severe criminal penalties.

DISTRIBUTION STATEMENT - Distribution authorized to Department of Defense and DODcontractors only to protect critical technical data on systems or hardware. This determinationwas made Oct 1986. Other requests shall be referred to Commander, U.S. Army Aviation andMissile Command, ATTN: AMSAM-WS-LM, Redstone Arsenal, AL 35898-5238.

DESTRUCTION NOTICE - Destroy by any method that will prevent disclosure of contents orreconstruction of the document.

TM 9-1425-450-12, 25 May 1983, is changed as follows:

1. The pages affected by this change, appearing in the following listing, are to be inserted in the manual.New or changed material is indicated by a vertical bar in the margin of the page. Where a completeparagraph, chapter, section, or appendix is changed or added, a vertical line is placed in the margin by thetitle only. Changes to illustrations are indicated by miniature pointing hands. Changes to flow charts areindicated by a miniature hand pointing to the number of the step in which the change occurs or a verticalline is placed in the margin by the change.

Remove Pages Insert Pages

i, ii i, ii1-9, 1-10 1-9, 1-102-21, 2-22 2-21, 2-222-27 thru 2-31 2-27 thru 2-312-42.1, 2-42.2 2-42.1, 2-42.22-95, 2-96 2-95, 2-962-97, 2-98 2-97, 2-982-113, 2-114 2-113, 2-1142-123 thru 2-126 2-123 thru 2-1262-157, 2-158 2-157, 2-1582-313 thru 2-316 2-313 thru 2-3162-401 thru 2-404 2-401 thru 2-404B-3 thru B-10 B-3 thru B-10B-13, B-14 B-13, B-14D-1, D-2 D-1, D-2E-3, E-4 E-3, E-4

2. This transmittal sheet should be filed in front of the publication for reference purposes.

Page 14: TM 9 1425 450 12 TOW 2 Weapon System

By Order of the Secretary of the Army:

DENNIS J. REIMERGeneral, United States Army

Chief of Staff

Administrative Assistant to theSecretary of the Army

04299

DISTRIBUTION:

To be distributed in accordance with Initial Distribution Number (IDN) 320441, requirements for TM 9-1425-450-12.

Page 15: TM 9 1425 450 12 TOW 2 Weapon System

TM 9-1425-450-12

C11

Change ) HEADQUARTERSDEPARTMENT OF THE ARMY

Washington, D.C., 18 November 1992No. 11 )

Operator and Organizational Maintenance Manual

FOR

TOW 2 WEAPON SYSTEM, GUIDED MISSILE SYSTEM M220A2

WARNING - This document contains technical data whose export is restricted by the Arms Export Control

Act (Title 22, U.S.C. Sec 27S1 et seq. ) or Executive Order 12470. Vlolatora of these export Iowa are

subject to severe crlmlnel penaltlee.

DISTRIBLJTION STATEMENT - Dlatrlbution authorized to Department of Defenae end DoD contractora only

to protect crltlcal technical data on ayatems or hardware, Th18 determination was made Nov 1986. Other

requeate shall be re?erred to Project Manager, TOW Systems, AlTN: SFAE-FS.TO, Redstone Amenal,

AL 3589H71O.

DESTRUCTION NOTICE - De$troy by any method that wIII prevent dlacloaure of contents or recormtruc.

tlono?thedooument.

TM 9-1425-450-12, 25 May 1983, is changed as follows:

1. The pages affected by this change, appearing in the following listing, are tobe inserted in the manual. New or changed text is indicated by a vertical bar inthe marginis changedChanges tocharts arethe change

of the page. Where a complete paragraph, chapter, section, or appendixor added, a vertical line is placed in the margin by the title only.illustrations are indicated by miniature pointing hands. Changes to flowindicated by a miniature hand pointing to the number of the step in whichoccurs.

Remove Pages Insert Pages

i, ii i, ii1-13, 1-14 1-13, 1-142-21, 2-22 2-21, 2-22None 2-22.1/(2-22.2 blank)2-25 thru 2-30 2-25 thru 2-302-41, 2-42 2-41, 2-422-123, 2-124 2-123, 2-1242-143, 2-144 2-143, 2-1442-315, 2-316 2-315, 2-3162-399, 2-400 2-399, 2-4002-411, 2-412 2-411, 2-4122-465, 2-466 2-465, 2-4662-469, 2-470 2-469, 2-4704-1, 4-2 4-1, 4-24-2.1, 4-2.2 4-2.1, 4-2.24-5, 4-6 4-5, 4-6B-7, B-8 B-7, B-8

2. This transmittal sheet should be filed in the front of the publication forreference purposes.

PIN: 053139-011

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TM 9-1425-450-12

By Order of the Secretary of the Army:

C11

GORDON R. SULLIVANGeneral, United States Army

Chief of StaffOffical:

MILTON H. HAMILTONAdministrative Assistant to the

Secretary of the Army03083

Distr ibut ion :

To be distributed in accordance with DA Form 12-32-E, Block 0441,requirements for TM 9-1425-450-12.

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TM 9-1425-450-12

Insert the latest changed pages. Destroy superseded pages.

LIST OF EFFECTIVE PAGES

NOTE: The portion of the text affected by the latest change is indicated by a vertical line in the outer margin of the page. Changes to illustrations are indicated by miniature pointing hands. A vertical line indicates added or completely revised chapters, sections, paragraphs, tables, etc., by the title.

Dates of issue for original and changed pages are:

Basic 0 25 May 1983 Change 07 25 May 1989

Change 01 02 April 1984 Change 08 22 November 1990

Change 02 01 November 1984 Change 09 10 December 1990

Change 03 10 January 1986 Change 10 2 December 1991

Change 04 25 February 1987 Change 11 18 November 1992

Change 05 24 November 1987 Change 12 08 December 1997

Change 06 29 April 1988 Change 13 14 September 2004

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 457, CONSISTING OF THE FOLLOWING:Page No. *Change Page No. *Change Page No. *Change No. No. No.

2-10 blank.......................... 8 1-12 ................................... 0 Cover............................... 13 2-11 ................................... 8 1-13 ................................... 0 a ........................................ 0 2-12 ................................... 7 1-14 ................................. 11 b ........................................ 0 2-13 ................................... 8 1-15 ................................... 0 c......................................... 0 2-14 ................................... 4 1-16 ................................... 0 d ........................................ 0 2-15 ................................... 2 1-17 ................................... 6 e ........................................ 0 2-16 ................................... 2 1-18 ................................... 1 f ......................................... 0 2-16.1 ................................ 1 1-19 ................................... 1 A ...................................... 13 2-16.2 .............................. 13 1-20 ................................... 0 B ...................................... 13 2-17 ................................... 3 1-21 ................................... 0 C...................................... 13 2-18 ................................... 3 1-22 ................................... 0 D...................................... 13 2-19 ................................... 0 1-23 ................................. 13 i........................................ 13 2-20 ................................... 0 1-24 ................................. 13 ii ....................................... 13 2-21 ................................. 12 1-25 ................................. 13 iii ........................................ 7 2-22 ................................. 11 1-26 ................................... 8 iv........................................ 0 2-22.1 .............................. 11 1-27 ................................... 0 v......................................... 0 2-22.2 blank..................... 11 1-28 ................................... 0 vi........................................ 0 2-23 ................................... 4 1-29 ................................... 0 1-1 ..................................... 0 2-24 ................................. 13 1-30 ................................... 0 1-2 ..................................... 4 2-25 ................................. 11 2-1 ................................... 13 1-3 ..................................... 7 2-26 ................................... 3 2-2 ................................... 13 1-4 ................................... 13 2-27 ................................. 12 2-3 ..................................... 0 1-5 ..................................... 6 2-28 ................................. 13 2-4 ..................................... 0 1-6 ..................................... 6 2-29 ................................. 12 2-5 ..................................... 0 1-7 ..................................... 0 2-30 ................................. 13 2-6 ..................................... 5 1-8 ..................................... 0 2-31 ................................ 13 2-7 ..................................... 0 1-9 ..................................... 0 2-32 - 2-41 deleted.......... 13 2-8 ..................................... 0 1-10 ................................. 12 2-9 ..................................... 8 1-11 ................................... 1

* Zero in this column indicates an original page. Change 13 A

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TM 9-1425-450-12

LIST OF EFFECTIVE PAGES (CONT) Page No. *Change No.

2-42 ................................. 11 2-42.1 ................................ 2 2-42.2 .............................. 12 2-42.3 ................................ 2 2-42.4 ................................ 5 2-43 ................................. 13 2-44 ................................... 5 2-45 ................................... 8 2-46 ................................... 0 2-47 ................................... 0 2-48 ................................... 0 2-49 ................................... 0 2-50 ................................... 1 2-51 ................................... 1 2-52 ................................... 0 2-53 ................................... 0 2-54 ................................... 0 2-55 ................................... 4 2-56 ................................... 4 2-57 ................................. 13 2-58 ................................. 13 2-59 ................................. 13 2-60 ................................. 13 2-61 ................................. 13 2-62 ................................. 13 2-63 ................................... 0 2-64 ................................... 0 2-65 ................................... 0 2-66 ................................... 0 2-67 ................................... 2 2-68 ................................... 0 2-69 ................................... 0 2-70 ................................... 0 2-71 ................................... 0 2-72 ................................... 0 2-73 ................................. 10 2-74 ................................... 0 2-75 ................................... 4 2-76 ................................... 8 2-77 - 2-80 deleted............ 8 2-81 ................................... 0 2-82 ................................... 8 2-83 ................................... 0 2-84 ................................... 4 2-85 ................................... 4 2-86 ................................... 0 2-87 ................................... 0 2-88 ................................... 4 2-89 ................................... 0

Page No. *Change No.

2-90 ................................... 0 2-91 ................................... 0 2-92 ................................... 8 2-92.1 ................................ 8 2-92.2 ................................ 8 2-93 ................................... 0 2-94 ................................... 8 2-95 ................................. 13 2-96 ................................. 12 2-97 ................................. 12 2-98 ................................... 0 2-99 ................................... 0 2-100 ................................. 0 2-101 ................................. 7 2-102 ................................. 8 2-103 ................................. 8 2-104 ................................. 8 2-105 ................................. 8 2-106 ................................. 8 2-107 ................................. 8 2-108 ................................. 8 2-109 ................................. 8 2-110 ................................. 8 2-111 ................................. 8 2-112 ................................. 8 2-113 ............................... 13 2-114 ................................. 0 2-115 ............................... 13 2-116 ................................. 8 2-117 ................................. 0 2-118 ................................. 0 2-119 ................................. 8 2-120 ............................... 13 2-121 ................................. 0 2-122 ................................. 0 2-123 ............................... 12 2-124 ................................. 0 2-125 ............................... 12 2-126 ................................. 0 2-127 ............................... 13 2-128 ............................... 13 2-129 ................................. 0 2-130 ................................. 8 2-131 ................................. 0 2-132 ................................. 0 2-133 ................................. 4 2-134 ............................... 13 2-135 ................................. 0 2-136 ................................. 0

Page No. *Change No.

2-137 ................................. 0 2-138 ................................. 0 2-139 ................................. 0 2-140 ................................. 0 2-141 ................................. 3 2-142 ................................. 3 2-143 ............................... 11 2-144 ................................. 3 2-144.1 ............................ 13 2-144.2 .............................. 4 2-144.3 .............................. 4 2-144.4 .............................. 3 2-144.5 .............................. 3 2-144.6 ............................ 13 2-145 ................................. 0 2-146 ................................. 0 2-147 ................................. 0 2-148 ................................. 0 2-149 ................................. 0 2-150 ................................. 0 2-151 ................................. 0 2-152 ................................. 0 2-153 ................................. 0 2-154 ............................... 13 2-155 ................................. 0 2-156 ............................... 13 2-157 ............................... 11 2-158 ............................... 13 2-159 ................................. 0 2-160 ................................. 8 2-161 ............................... 10 2-162 ................................. 0 2-163 ................................. 0 2-164 ................................. 0 2-165 ................................. 0 2-166 ................................. 0 2-167 ................................ 0 2-168 ................................. 0 2-169 ................................. 0 2-170 ............................... 13 2-171 ................................. 0 2-172 ................................. 0 2-173 ................................. 0 2-174 ................................. 0 2-175 ............................... 13 2-176 ............................... 13 2-177 – 2-345 deleted..... 13 2-347 ............................... 13

*Zero in this column indicates an original page. B Change 13

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LIST OF EFFECTIVE PAGES (CONT) Page No. *Change No.

2-348 ................................... 5 2-349 ................................... 2 2-350 ................................... 2 2-351 ................................... 2 2-353 ................................... 2 2-354 ................................... 2 2-355 ................................... 2 2-356 ................................... 5 2-357 ................................... 2 2-358 ................................... 2 2-359 ................................... 2 2-360 ................................... 2 2-361 ................................... 2 2-362 ................................... 2 2-363 ................................... 2 2-364 ................................... 2 2-365 ................................... 2 2-366 ................................... 2 2-367 ................................... 2 2-368 ................................... 8 2-369 ................................... 4 2-370 ................................... 4 2-371 ................................... 2 2-372 ................................... 8 2-373 ................................... 2 2-374 ................................... 2 2-375 ................................... 2 2-376 ................................... 4 2-377 ................................... 3 2-378 ................................... 2 2-379 ................................... 2 2-380 ................................... 2 2-381 ................................... 2 2-382 ................................... 2 2-383 ................................... 2 2-384 ................................. 10 2-385 ................................... 2 2-386 ................................... 2 2-387 ................................... 2 2-388 ................................... 2 2-389 ................................... 2 2-390 ................................... 2 2-391 ................................... 2 2-392 ................................... 2 2-393 ................................... 2 2-394 ................................... 2 2-395 ................................... 2 2-396 ................................... 3 2-396.1 ................................ 3

Page No. *Change No.

2-396.2 blank ...................... 3 2-397 ................................... 2 2-398 ................................... 2 2-399 ................................. 11 2-400 ................................... 2 2-401 ................................. 12 2-402 ................................... 2 2-403 ................................. 12 2-404 ................................... 2 2-405 ................................... 2 2-406 ................................... 2 2-407 ................................. 13 2-408 ................................. 13 2-408.1 .............................. 13 2-408.2 .............................. 13 2-408.3 .............................. 13 2-408.4 .............................. 13 2-408.5 .............................. 13 2-408.6 .............................. 13 2-408.7 .............................. 13 2-408.8 .............................. 13 2-408.9 .............................. 13 2-408.10 ............................ 13 2-408.11 ............................ 13 2-408.12 ............................ 13 2-408.13 ............................ 13 2-408.14 blank .................. 13 2-409 ................................. 13 2-410 ................................. 13 2-410.1 .............................. 13 2-410.2 .............................. 13 2-410.3 .............................. 13 2-410.4 .............................. 13 2-410.5 .............................. 13 2-401.6 .............................. 13 2-410.7 .............................. 13 2-410.8 .............................. 13 2-410.9 .............................. 13 2-410.10 ............................ 13 2-410.11 ............................ 13 2-410.12 ............................ 13 2-410.13 ............................ 13 2-410.14 ............................ 13 2-410.15 ............................ 13 2-410.16 blank .................. 13 2-411 ................................. 11 2-412 ................................. 13 2-413 ................................... 7 2-414 ................................. 13

Page No. *Change No.

2-415 ................................. 7 2-416 ................................. 7 2-417 ................................. 7 2-418 ................................. 7 2-419 ................................. 7 2-420 ................................. 7 2-421 ................................. 7 2-422 ................................. 7 2-423 ................................. 7 2-424 ................................. 7 2-425 ................................. 7 2-426 ................................. 7 2-427 ................................. 7 2-428 ................................. 7 2-429 ................................. 7 2-430 ................................. 7 2-431 ................................. 7 2-432 ................................. 7 2-433 ................................. 7 2-434 ................................. 5 2-435 ................................. 2 2-436 ................................. 5 2-437 ................................. 2 2-438 ................................. 2 2-439 ................................. 2 2-440 ................................. 2 2-441 ................................. 2 2-442 ................................. 2 2-443 ................................. 2 2-444 ................................. 2 2-445 ................................. 2 2-446 ................................. 2 2-447 ................................. 2 2-448 ................................. 2 2-449 ................................. 2 2-450 ................................. 2 2-451 ................................. 2 2-452 ................................. 2 2-453, 2-454 deleted......... 5 2-455 ................................. 5 2-456 ................................. 2 2-457 ................................. 2 2-458 ................................. 2 2-459 ............................... 13 2-460 ................................. 2 2-461 ................................. 2 2-462 ................................. 2 2-463 ................................. 2 2-464 ................................. 2

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Page No. *Change No.

2-465 ............................... 11 2-466 ............................... 11 2-467 ................................. 8 2-468 ................................. 8 2-469 ............................... 11 2-470 ............................... 11 2-471 ................................. 2 2-472 blank ....................... 2 3-1 ..................................... 0 3-2 ..................................... 0 3-3 ................................... 13 3-4 blank.......................... 13 3-5 ..................................... 8 3-6 ................................... 0 3-7 ..................................... 0 3-8 ..................................... 5 3-8.1 .................................. 5 3-8.2 blank ........................ 5 3-9 ..................................... 0 3-10 ................................... 5 3-10.1 ................................ 4 3-10.2 ................................ 4 3-10.3 ................................ 8 3-10.4 ................................ 8 3-10.5 ................................ 8 3-10.6 ................................ 8 3-11 – 3-90 deleted ......... 13 3-91 ................................. 13 3-92 ................................. 13 3-93 ................................... 3 3-94 ................................... 8 3-95 ................................... 8 3-96 ................................. 13 4-1 ..................................... 0 4-2 ................................... 11 4-2.1 ................................ 10 4-2.2 ................................ 11 4-3 ..................................... 0 4-4 ..................................... 2 4-5 ................................... 11 4-6 ................................... 11 4-7 ..................................... 5 4-8 ..................................... 5 4-9 ..................................... 0 4-10 ................................... 0 A-1..................................... 0 A-2 blank ........................... 0 B-1..................................... 0 B-2..................................... 0

Page No. *Change No.

B-3................................... 13 B-4..................................... 4 B-5..................................... 4 B-6................................... 12 B-7................................... 11 B-8................................... 13 B-9..................................... 4 B-10................................. 13 B-11................................... 4 B-12................................... 4 B-13................................. 13 B-14................................. 13 B-15 – B-24 deleted ........ 13 C-1..................................... 0 C-2..................................... 4 C-3..................................... 4 C-4..................................... 2 D-1..................................... 0 D-2................................... 12 D-3..................................... 8 D-4................................... 10 D-5................................... 13 D-6................................... 13 D-7 – D-8 deleted............ 13 D-9................................... 13 D-10................................. 13 E-1................................... 13 E-2................................... 13 E-3................................... 13 E-4................................... 10

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TECHNICAL MANUAL) HEADQUARTERS ) DEPARTMENT OF THE ARMY No. 9-1425-450-12 ) WASHINGTON, D.C. 25 May 1983

Operator and Organizational Maintenance Manual

for

TOW 2 WEAPON SYSTEM, GUIDED MISSILE SYSTEM M220A2

(TOW 2 HEAVY ANTITANK/ASSAULT WEAPON SYSTEM)

REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS You can improve this manual. If you find any mistakes or if you know of a way to improve these procedures, please let us know. Mail your letter, DA Form 2028 (Recommended Changes to Publications and Blank Forms) directly to: Commander, U.S. Army Aviation and Missile Command, ATTN: AMSAM-MMC-MA-NP, Redstone Arsenal, AL 35898-5000. A reply will be furnished to you. You may also provide DA Form 2028 information to AMCOM via e-mail, fax, or the World Wide Web. Our fax number is: DSN 788-6546 or Commercial 256-842-6546. Our e-mail address is [email protected]. Instructions for sending an electronic 2028 may be found at the back of this manual immediately preceding the hard copy 2028. For the World Wide Web use: https://amcom 2028.Redstone.army.mil. WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C. Sec. 2751 et. seq.) or the Export Administration Act of 1979, as amended, title 50, U.S.C. Sec. 2751, et. seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25. DISTRIBUTION STATEMENT – Distribution authorized to Department of Defense and DoD contractors only due to critical technology. This determination was made in October 1986. Other requests for this document shall be referred to Project Manager, Close Combat Weapons Systems, ATTN: SFAE-MSL-CWS-O, Redstone Arsenal, AL 35898-5750 DESTRUCTION NOTICE – Destroy by any method that will prevent disclosure of contents or reconstruction of the document.

OZONE DEPLETING CHEMICAL INFORMATION This document has been reviewed for the presence of Class I Ozone Depleting Chemicals by the Engineering, Environment, and Logistics Oversight Office. As of Base Document through Change 11, dated 25 May 1983, all references to Class I Ozone Depleting Chemicals have been removed from this document by substitution with chemicals that do not cause atmospheric ozone depletion.

TABLE OF CONTENTS

PAGE HOW TO USE THIS MANUAL iii

CHAPTER 1. INTRODUCTION 1-1

SECTION I. General Information 1-2

SECTION II. Equipment Description and Data 1-9

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TABLE OF CONTENTS (CONT)

SECTION III. Technical Principles of Operation 1-26

CHAPTER 2. OPERATING INSTRUCTIONS 2-1

SECTION I. Description and use of Controls and Indicators 2-2

SECTION II. Service Upon Receipt of Material 2-17

SECTION III. Preventive Maintenance Checks and Services (PCMS) 2-18

SECTION IV. Emplacement of Tripod Mounted TOW 2 System 2-57

SECTION V. Deleted 2-175

SECTION VI. Deleted 2-272

SECTION VII. Deployment of High Mobility Multipurpose Wheeled Vehicle (HMMWV) 2-347

SECTION VII. Operation Under Unusual Conditions 2-459

CHAPTER 3. MAINTENANCE INSTRUCTIONS 3-1

SECTION I. Repair Parts, Special Tools, and Test Equipment 3-2

SECTION II. Maintenance Procedures 3-3

CHAPTER 4. AMMUNITION (MISSILE) 4-1

APPENDIX A REFERENCES A-1

APPENDIX B MAINTENANCE ALLOCATION CHART B-1

APPENDIX D COMPONENTS OF END ITEM LIST D-1 APPENDIX E ADDITIONAL AUTHORIZATION LIST E-1

ii Change 13

APPENDIX C EXPENDABLE SUPPLIES AND MATERIALS LIST C-1

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HOW TO USE THIS MANUAL

NOTE

The examples used in this section are samples only and will notalways match the pages in this manual.

1. Suppose you want to know how toinstall the battery in the mis-sile guidance set (MGS).

2. Look at the cover, and you willsee the chapter titles listedtop to bottom. Find “MAINTEN-ANCE INSTRUCTIONS”.

3. You will see that “MAINTENANCEINSTRUCTIONS” is Chapter 3.

4. If you open the manual to page 3-1,you will find the beginning ofChapter 3.

5. Right under the chapter title youwill see a list of all the sectionsby title and page number.

6. Look down the list until you cometo Section II. MAINTENANCE PROCE-DURES . . . 3-3.

GO TO NEXT PAGE

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HOW TO USE THIS

7. Now that you have reached thesection you want you will seethe title of each paragraph, theparagraph number and the pagenumber.

8. Now look down the list until youcome to MISSILE GUIDANCE SETBATTERY ASSEMBLY INSTALLATIONand and read across. The infor-mation you want is located inparagraph 3-6 on page 3-7. Nowturn to page 3-7.

MANUAL (CONT)

9. Now that you are at the paragraphyou want you will find somethingelse that’s new. SOME PROCEDURESHAVE BOXES AROUND THEM. The boxedprocedures and the pictures gotogether, so you don’t have to lookfor a picture by number or look onother pages to find out what thebattery assembly looks like. Inthis TM, it’s right there. Thesmall box in the upper left corneris the step number.

10. When you find procedures that are not boxed, you don’t need to look for apicture. Either you’ve seen it before, and-now know where the control (orwhatever) is, or you just don’t need one to do the job.

11. You can find procedures in other sections the same way. First, find the sec-tion you think the procedures should be in, open the manual to that section,and find the page number of the procedure from the list at the beginning ofthe section.

12. You can also use the table of contents on page i in the front of this manual.

GO TO NEXT PAGEiv

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HOW TO USE THIS MANUAL (CONT)

13. Paragraph 2-33 contains the System Checkout procedureSystem. The procedure enables you to find faulty TOW

for the TOW 2 Weaponequipment. You then

remove and replace any faulty equipment in order to make the TOW 2 WeaponSystem work right.

14. The System Checkout procedure is written in flow chart style. Each set ofinstructions is written in a box and the boxes are connected by arrows. Byfollowing the arrows you can work your way through the procedure. Thefollowing chart tells you what the various boxes mean.

Beginning and ending ofprocedure.

Do instruction beforelooking for an indica-tion.

Look for a YES or NOindication. For a NOindication go to correc-tive action block.

Do steps following YESindication.

Go to next page andcontinue the procedure.

Do steps in correctiveaction block.

Go to next page

v

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C H A P T E R 1

I N T R O D U C T I O N

C H A P T E R O V E R V I E W

This chapter contains references to U.S. Army forms and manuals forreporting equipment problems, and suggesting improvements. Nomenclatureis described and a glossary is given of terms used in this manual. Thischapter also provides a description of the TOW 2 Weapon System and ageneral discussion of how the equipment is operated.

CHAPTER CONTENTS PAGE

Section I. GENERAL INFORMATION 1-2

Section II. EQUIPMENT DESCRIPTION 1-9

Section III. TECHNICAL PRINCIPLES OF OPERATION 1-26

1-1

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Section 1. G E N E R A L I N F O R M A T I O N

SECTION CONTENTS

SCOPE

MAINTENANCE FORMS AND RECORDS

REPORTING EQUIPMENT IMPROVEMENT RECOMMENDATIONS (EIRs)

ADMINISTRATIVE STORAGE

LIMITED STORAGE

DESTRUCTION OF ARMY MATERIEL TO PREVENT ENEMY USE

NOMENCLATURE CROSS-REFERENCE LIST

LIST OF ABBREVIATIONS

GLOSSARY

PARA

1-1

1-2

1-3

1-4

1-5

1-6

1-7

1-8

1-9

PAGE

1-2

1-2

1-2

1-3

1-3

1-3

1-4

1-5

1-7

1-1 . S C O P E

This manual contains information and guidance for the operator, crew, and usingorganization on the operation, set-up, and maintenance of the TOW 2 Weapon SystemGuided Missile System M220A2.

1-2 . M A I N T E N A N C E

Department of the Armythose written about in(TAMMS).

F O R M S A N D R E C O R D S

forms and procedures used for equipment maintenance will beDA PAM 738-750, The Army Maintenance Management System

1-3 . R E P O R T I N G E Q U I P M E N T I M P R O V E M E N T R E C O M M E N D A T I O N S ( E I R s )

If your TOW equipment needs improvement, let us know. Send us an EIR. You, theuser, are the only one who can tell us what you don’t like about your equipment.Let us know why you don’t like the design. Tell us why a procedure is hard toperform. Put it on an SF 368 (Quality Deficiency Report). Mail it to us at:

CommanderU.S. Army Missile CommandATTN : AMSMI-QA-CFRedstone Arsenal, AL 35898-5290

We’ll send you a reply.

1-2 Change 4

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1-4 . A D M I N I S T R A T I V E S T O R A G E

There are no special procedures for administrative storage. See para. 4-4for storage information.

1-5. L I M I T E D S T O R A G E

Storage facilities for the TOW 2 Weapon system should provide:

Maximum protection against physical damage, deterioration, and corrosion.

Ambient temperature within the range of -53.9 to +68.3°C (-65 to +155°F).

Level ground with maximum protection from exposure to elements.

Adequate drainage.

Before the TOW 2 Weapon System is placed in limited storage, you should:

Remove the battery assembly from the missile guidance set.

Mark each component with date it was placed into storage.

1-6 . D E S T R U C T I O N O F A R M Y M A T E R I E L T O P R E V E N T E N E M Y U S E

For information on destruction of Army materiel to prevent enemy use, seeTM 750-244-4-2.

Change 7 1-3

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1-7. NOMENCLATURE CROSS-REFERENCE LIST

This cross-reference list of official nomenclature to technical manual nomenclature lists the major items of the TOW 2 Weapon System.

TM NOMENCLATURE OFFICIAL NOMENCLATURE

TOW 2 Launcher Launcher, Tubular, Guided Missile M220A2

Missile Guidance Set (MGS) Missile Guidance Set AN/TSQ-136

Day Sight Tracker Sight, Optical, Guided Missile Launcher MX-9155/TSQ

Traversing Unit Traversing Unit, Guided Missile Launcher M83

Tripod Mount, Tripod, Guided Missile Launcher M159A1

Launch Tube Tube, Guided Missile Launcher M22

Battery Assembly Battery Assembly BB-287 (XO-2)/T

Power Conditioner Conditioner, Power

Shroud Bag Bag, Shroud Assembly

Strap Assembly TOW Strap Assembly

Deleted Deleted

Deleted Deleted

Deleted Deleted

Deleted Deleted

Deleted Deleted

Deleted Deleted

HMMWV Truck, Utility: TOW Carrier; M966

Battery Charger Charger, Battery, PP-4884A/T

Night Sight Night Vision Sight, AN/TAS-4A or AN/TAS-4C

Boresight Collimator Collimator, Boresight, SU-93A/TAS

Night Sight Vehicle Power Conditioner Conditioner, Power, Night Sight Vehicle

Night Sight Battery Power Conditioner Conditioner, Power, Night Sight Battery

1-4 Change 13

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1-7. NOMENCLATURE CROSS-REFERENCE LIST (CONT)

TM NOMENCLATURE OFFICIAL NOMENCLATURE

Battery Power Conditioner Cable

Power Cables

Boresight Collimator Power Cable

Equipment Cover

Battery (2 each)

Boresight Collimator Carrying

Case

Lens Cleaning Materials

Night Sight Field HandlingCase

Cargo/Loader’s Door

1-8. LIST OF ABBREVIATIONS

ACQ Acquisition

AGC

APC

ASP

AZ

BATT

BRT

BS

C

CB1

cm

CTRS

Cable Assembly 8Wl, Battery Pack

Cables, Power

Cable Assembly, Boresight Collimator

Cover, Equipment

Battery, Primary Lithium-Organic BA-5590/U

Case, Carrying, Collimator, Boresight

Materials, Cleaning, Lens

Case, Field Handling

Cargo Shell Door

Adjustable Gain Control

Armored Personnel Carrier

Ammunition Supply Point

Azimuth

Battery

Brightness

Boresight

Celsius

Circuit Breaker 1

Centimeter

Contrast

dc Direct Current

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1-8. LIST OF ABBREVIATIONS (CONT)

EOD Explosive Ordnance Disposal

EIR Equipment Improvement Recommendations

EL Elevation

F Fahrenheit

HMMWV High Mobility Multipurpose Wheeled Vehicle

IR Infrared

kg Kilogram

Kph Kilometers Per Hour

LOS Line of Sight

MAC Maintenance Allocation Chart

MGS Missile Guidance Set

MOIC Missile Ordnance Inhibit Circuit

NFOV Narrow Field-of-View

NVS Night Vision Sight

OSS Day Sight Tracker (formerly Optical Sight)

PA Post Amplifier (part of Night Sight)

PARA Paragraph

PMCS Preventive Maintenance Checks and Services

TM Technical Manual

TOW Tube-Launched, Optically-Tracked, Wire Command-Link

TVPC Power Conditioner (also called TOW Vehicle Power Conditioner)

WFOV Wide Field-of-View

1-6 Change 6

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1-9. GLOSSARY

A

ABSORBENT – Able to soak up or totake in

ACQUISITION (ACQ) – To find the target

ACTIVATED – Start, energize

AFT – Behind, rearward

ALLOCATION – To assign, distribute orgive

ARC (ARCING) – A visible discharge ofelectricity

AUTHORIZE – To allow or permit

AZIMUTH – Right/left direction usuallymeasured in degrees from North

B

BREECH – Part of launcher oppositebore

C

CIRCUIT – The path of an electriccurrent

COMPOSITION – The parts of a thing

CONFIGURATION – A certain (particular)arrangement of parts

CORROSION – Something eaten away asby rust

CROSS-REFERENCE – A note to anotherpart of book giving furtherinformation

D

DATA – Collection of facts

DEPLOYED – To place in battle forma-tion or appropriate positions

DESICCANT – A drying chemical

DETENT – A catch used to position andhold one mechanical part in relationto another

DETERIORATION – The processworse in quality or state

E

ELECTRONICS – A combinationand circuits that processimpulses

of growing

of wireselectrical

ELEVATION – Up/down direction measuredin degrees from horizon

EXCESSIVE – Too much

EXCURSION – Off-line from line of sight

EXPENDABLE – Throw-away materiel

F

FUNCTION – Operation

H

HAZARD – Danger, risk

HUMIDITY – Amount of moisture inthe air

I

INSULATION – A barrier against weather,electrical current or sound

INTEGRAL – Necessary

1-7

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1-9. GLOSSARY (CONT)

INTERVAL - Period of time betweenevents

L

LIMITED VISIBILITY - Darkness, smoke,fog

M

MANUAL - Handbook, guidebook

N

NOMENCLATURE - Official name of equipment

O

OVERLOAD - In excess, too much

P

POLARITY – Plus or minus terminal onbattery

R

RECHARGEABLE – Able to restore theactive materials

S

SEALANT – Agent used to stop leaks

SEQUENCE – Order of events

SOLVENT – Liquid substance used to breakup dirt, etc.

STOW – Put away, store

SURGE – Sudden rise in electricalcurrent

PRECAUTION - Steps taken to preventdamage or injury

1-8

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Section Il . EQUIPMENT DESCRIPTION

SECTION CONTENTS

SCOPE

PURPOSE OF TOW 2 WEAPON SYSTEM

CAPABILITIES AND FEATURES

LOCATION AND DESCRIPTION OF MAJOR COMPONENTS

EQUIPMENT DATA

DECONTAMINATING APPARATUS

FIRE EXTINGUISHER

PARA

1-10

1-11

1-12

1-13

1-14

1-15

1-16

PAGE

1-9

1-9

1-9

1-11

1-23

1-25

1-25

1-10 . S C O P E

This section gives a brief description of the components which make up the TOW 2Weapon System.

1-11 . PURPOSE OF TOW 2 WEAPON SYSTEM

The TOW 2 Weapon System is an easily moved, heavy antitank weapon designed to attackand defeat armored vehicles and other hard targets, such as field fortifications.

The TOW 2 Weapon System consists of a launcher and encased missile. The launcherconsists of a launch tube, traversing unit, missile guidance set, night sight, twobattery assemblies (one spare), day sight tracker, and a tripod. The night sight isused to aid in tracking during limited visibility.

1-12 . CAPABILITIES AND FEATURES

Major weapon system components:

a. Launcher

1. Launch tube

2. Traversing unit

3. Missile guidance set

4. Battery assemblies (2)

5. Day sight tracker

6. Tripod

1-9

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1-12. CAPABlLlTlES AND FEATURES (CONT)

7. Power conditioner

8. Night sight equipment set(a) Night sight

(b) Boresight collimator

(c) Night sight vehicle power conditioner

(d) Night sight battery power conditioner

b. TOW Missile

The TOW 2 Weapon System has the following capabilities and features:

l Operates in all weather conditions in which the gunner can see the target through the daysight tracker or the night sight.

l Operates during day and night.

l Operates in temperatures of -32o to +52oC (-25o to +125oF).

l Operates at altitudes up to 3,050 meters (10,000 feet).

l High first-round-hit chance against targets that stay still or move.

l Entire weapon system can be hand carried by the weapons crew.

l Easy to operate.

l Firing sites can be changed quickly to avoid being seen or to engagetargets not within range of a single firing position.

l Mounting kits allow mounting on several different vehicles.

l Easily installed or removed without the use of tools.

l Weapon system can be checked out by self-test without the use of test equipment.

l Failed components can be replaced at the operating sites by Direct Support.

l Minimum and maximum effective range of missile is 65 to 3750 meters.

1-10 Change 12

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1-13. LOCATION AND DESCRIPTION OF MAJOR COMPONENTS

Change 1 1-11

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1-13 . LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (CONT)

Launch Tube

Holds the nose end of the encased missile.

Provides mechanical guidance for the first part of the missile flight.

Protects the crew from the missile launch motor blast.

Allows the gunner to track a target 360° in azimuth. Azimuth lock permitsyou to lock the traversing unit in one position (straight forward).

Allows the gunner to track from +30° (above horizontal) to -20° (below hori-zontal) in elevation. Elevation lock has detents in +30° and -8° position.Elevation brake locks in intermediate positions.

Contains the trigger used to fire the missiles.

Bridge clamp contains the arming lever and electrical connector between thelauncher and the encased missile.

1-12

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1-13 . LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (CONT)

Missile Guidance Set

Contains electronic circuits required for missile control and launcherself-test purposes.

Controls on the front panel let the operator select the following modes ofoperation:

Tactical operation

System checkout.

1-13

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1-13 . LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (CONT)

Battery Assembly

Two nickel cadmium battery assemblies are issued with each TOW launcher.One to be installed in the missile guidance set and one spare.

Long-lasting because they can be recharged many times on the TOW batterycharger. To recharge battery assemblies, see TM 9-6130-470-12.

Easily removed from and installed in the missile guidance set.

Has enough energy for at least 50 missile firings or training exerciseswhen fully charged.

Can be stored at temperatures ranging from -50°C (-60°F) to+50°C (+122°F) without damage. Even though a battery may eventually loseall or part of its charge through self discharge, it can be returned toservice on the TOW battery chargers.

Charge retention (the ability of a stored battery to retain its energyonce it has been charged) is both time and temperature dependent. Tominimize this self discharge it is recommended that batteries be stored atlowest possible temperature.

Has acceptable life span of three to five years.

Battery Charge Retention Storage Schedule

Hours Storage periodSchedule Storage temperature per day days

1 25 ±2.8°C (77 ±5°F) 24 302 37.8 ±2.8°C (100 ±5°F) 20

51.6 ±2.8°C (125 ±5°F) 4 143 65.5 ±2.8°C (150 ±5°F) 24 3

The TOW battery must be recharged every 30 days or as defined in scheduleabove to maintain proper charge.

The TOW battery will not be adversely affected if stored on the groundor on metal, concrete, or wood shelves.

1-14 Change 11

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1-13. LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (CONT)

1-15

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1-13. LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (CONT)

1-16

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1-13 . LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (CONT)

Change 6 1-17

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1-18 Change 1

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1-13 . LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (CONT)

Change 1 1-19

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1-13 . LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (CONT)

1-20

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1-13 . LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (CONT)

1-21

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1-13 . LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (CONT)

1-22

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1-14. EQUIPMENT DATA

a. Transportation Data

The list below gives the dimensions and weight of the TOW 2 Weapon System parts packaged for shipping.

Item

Length in (cm)

Width in (cm)

Height in (cm)

Volume cu. ft (l)

Weight lb. (kg)

Launcher (complete) 75.0 (190.5)

40.5 (102.9)

34.0 (86.6)

60.0 (983.2)

550 (250)

Missile guidance set (including battery)

24.5 (62.2)

22.6 (57.3)

18.5 (46.9)

5.9 (167.1)

75.0 (34.0)

Battery assembly

22.4 (56.9)

12.0 (30.5)

15.1 (38.4)

2.3 (66.3)

26.0 (11.8)

Launch tube

45.5 (115.5)

12.5 (31.7)

12.5 (31.7)

4.1 (116.1)

31.0 (14.1)

Day sight tracker

32.6 (82.9)

23.3 (59.1)

22.8 (57.9)

10.0 (283.2)

72.0 (32.7)

Traversing unit

27.8 (70.7)

25.6 (64.9)

18.0 (45.7)

7.4 (209.6)

108.0 (48.9)

Tripod

47.8 (121.3)

15.5 (39.6)

14.8 (37.5)

6.3 (179.0)

66.0 (29.9)

Power Conditioner

23.5 (59.7)

13.1 (33.3)

17.1 (43.4)

3.0 (86.1)

28.0 (12.7)

Missile (in overpack)

57.3 (145.5)

11.5 (29.2)

11.5 (29.2)

4.4 (124.6)

93.0 (42.1)

Night sight with case

21.0 (53.3)

14.2 (36.0)

10.9 (27.8)

1.9 (53.8)

35.0 (15.9)

Boresight collimator with case 21.7

(55.2) 16.0

(40.5) 10.6

(26.8) 2.1

(60.0) 37.0

(16.8) Night sight vehicle power conditioner with cables 10.6

(26.8) 8.5

(21.6) 6.5

(16.5) 0.3

(9.6) 7.0

(3.2) Night sight battery power

conditioner (without batteries)

10.0 (25.3)

10.0 (25.3)

11.8 (29.9)

0.7 (19.3)

13.0 (5.9)

Lithium Battery (four)

9.5 (24.1)

6.5 (16.5)

6.0 (27.8)

0.2 (60))

35.0 (5.4)

Battery carrying case (without batteries)

9.5 (24.1)

9.8 (24.8)

7.5 (19.1)

0.4 (11.3)

5.0 (2.3)

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1-14. EQUIPMENT DATA

b. Mounting Data

This list below gives the weights and measurements of the TOW 2 Weapon System.

Item

Length in (cm)

Width in (cm)

Height in (cm)

Weight lb. (kg)

Launcher (complete with night sight)

80.0 (230.2)

64.0 (162.6)

56.0 (141.2)

246.0 (111.5)

Missile guidance set (including battery assembly)

16.0 (40.6)

17.4 (44.2)

11.3 (28.7)

58.5 (26.5)

Battery assembly

15.5 (39.4)

4.75 (12.1)

9.75 (24.8)

20.5 (9.3)

Launch tube

42.0 (106.7)

9.0 (22.9)

8.0 (20.3)

11.0 (5.0)

Encased missile (see Table 4-1)

Day sight tracker

20.8 (52.7)

12.8 (32.5)

13.8 (35.1)

31.0 (14.1)

Night sight (without case)

19.5 (49.5)

11.5 (29.2)

9.0 (22.9)

21.0 (9.5)

Boresight collimator (with case) 20.5 (52.1)

15.0 (38.1)

9.5 (24.1)

19.0 (8.6)

Night sight vehicle power conditioner with cables

8.5 (21.6)

6.3 (15.9)

3.1 (8.0)

5.5 (2.5)

Night sight battery power conditioner with batteries

9.4 (23.9)

9.1 (23.2)

10.8 (27.3)

15.5 (7.0)

Lithium Battery

4.5 (11.4)

1.5 (3.8)

5.5 (14.0)

2.5 max (1.1)

Battery carrying case with two batteries 9.0

(22.9) 9.4

(23.9) 7.0

(17.8) 8.5

(3.9)

Battery Charger

12.3 (31.2)

14.16 (36.0)

12.25 (31.1)

40 max (18.2)

Traversing Unit

13.0 (33.0)

19.8 (50.3)

20.6 (52.3)

58.0 (26.3)

Tripod (retracted-lying down)

42.5 (108.0)

13.5 (34.3)

13.5 (34.3)

22.0 (10.0)

Power conditioner

15.5 (39.4)

4.8 (12.1)

9.8 (24.8)

18.0 (8.2)

1-24 Change 13

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1-15. DECONTAMINATING APPARATUS

Refer to para. 2-348 for location of M13 decontamination kit on HMMWV.

Reference TM 3-3430-214-12 & P for details on how to use the kit.

1-16. FIRE EXTINGUISHER

The fire extinguisher is located near the night sight vehicle power conditioner on the HMMWV (para 2-76, step 31).

Change 13 1-25

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Section Ill. TECHNICAL PRINCIPLES OF OPERATION

SECTION CONTENTS PARA PAGE

SCOPE 1-17 1-26

FUNCTIONAL OPERATION OF TOW 2 WEAPON SYSTEM 1-18 1-26

1-17. SCOPE

This section gives a

1-18. FUNCTIONAL

brief description of how

OPERATION OF TOW 2

a. Selecting a Target

the TOW 2 Weapon System works.

WEAPON SYSTEM

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1-18 . FUNCTIONAL OPERATION OF TOW 2 WEAPON SYSTEM (CONT)

b. Firing

1-27

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1-18 . FUNCTIONAL OPERATION OF TOW 2 WEAPON SYSTEM (CONT)

c. Guiding Missile to Target

1-28

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1-18 . FUNCTIONAL OPERATION OF TOW 2 WEAPON SYSTEM (CONT)

c. Guiding Missile to Target (cont)

1-29

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1-18. FUNCTIONAL OPERATION OF TOW 2 WEAPON SYSTEM (CONT)

c. Guiding Missile to Target (cont)

1-30

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CHAPTER 2

OPERATING INSTRUCTIONS

CHAPTER OVERVIEW

This chapter tells the crew how to operate and maintain TOW 2 Weapon System equipment. A description of the TOW 2 Weapon System Controls and indicators is also given.

CHAPTER CONTENTS PAGE

Section I. DESCRIPTION AND USE OF CONTROLS AND INDICATORS 2-2

Section II. SERVICE UPON RECEIPT OF MATERIEL 2-17

Section III. PREVENTIVE MAINTENANCE CHECKS AND SERVICES (PMCS) 2-18

Section IV. EMPLACEMENT OF TRIPOD MOUNTED TOW 2 SYSTEM 2-57

Section V. DELETED 2-271

Section VI. DELETED 2-272

Section VII. DEPLOYMENT OF HIGH MOBILITY MULTIPURPOSE WHEELED VEHICLE (HMMWV)

2-347

Section VIII. OPERATION UNDER UNUSUAL CONDITIONS 2-459

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Section I. DESCRIPTION AND USE OF CONTROLS AND INDICATORS

SECTION CONTENTS PARA PAGE

SCOPE 2-1 2-2

MISSILE GUIDANCE SET PANEL CONTROLS AND INDICATORS 2-2 2-3

DAY SIGHT TRACKER CONTROLS AND INDICATORS 2-3 2-5

TRAVERSING UNIT CONTROLS AND INDICATORS 2-4 2-6

TRIPOD CONTROLS AND INIDCATORS 2-5 2-7

NIGHT SIGHT CONTROLS AND INDICATORS 2-6 2-9

BORESIGHT COLLIMATOR CONTROLS AND INDICATORS 2-7 2-14

NIGHT SIGHT VEHICLE POWER CONDITIONER CONTROLS AND INDICATORS

2-8 2-15

NIGHT SIGHT BATTERY POWER CONDITIONER CONTROLS AND INDICATORS

2-8.1 2-16

POWER CONDITIONER CONTROLS AND INDICATORS 2-8.2 2-16.1

DELETED 2-9 2-16.2

2-1. SCOPE

This section identifies the controls and indicators of the units that make up the TOW 2 Weapon System. Listed next to each control is a brief description of its purpose and use.

2-2 Change 13

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2 - 2 . MISSILE GUIDANCE SET PANEL CONTROLS AND INDICATORS

2-3

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2-2 . MISSILE GUIDANCE SET PANEL CONTROLS AND INDICATORS (CONT)

2-4

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2 - 3 . D A Y SIGHT TRACKER CONTROLS AND INDICATORS

2-5

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2-4 . TRAVERSING UNIT CONTROLS AND INDICATORS

2-6 Change 5

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2-5 . TRIPOD CONTROLS AND INDICATORS

2-7

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2-5 . TRIPOD CONTROLS AND INDICATORS (CONT)

2-8

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2 - 6 . NIGHT SIGHT CONTROLS AND INDICATORS

Change 8 2-9 / (2 -10 b lank)

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2 - 6 . NIGHT SIGHT CONTROLS AND INDICATORS (CONT)

Change 8 2-11

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2-6 . NIGHT SIGHT CONTROLS AND INDICATORS (CONT)

2-12 Change 7

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2 - 6 . N I G H T S I G H T C O N T R O L S A N D I N D I C A T O R S ( C O N T )

Change 8 2-13

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2 - 7 . B O R E S I G H T C O L L I M A T O R C O N T R O L S A N D I N D I C A T O R S

2-14 Change 4

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2-8 . NIGHT SIGHT VEHICLE POWER CONDITIONER CONTROLS ANDI N D I C A T O R S

Change 2 2-15

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2-8 .1 NIGHT SIGHT BATTERY POWER CONDITIONER CONTROLSAND INDICATORS

2-16 Change 2

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2 - 8 . 2 POWER CONDITIONER CONTROLS AND INDICATORS

Change 1 2-16.1

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2-9. DELETED

2-16.2 Change 13

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Section Il . SERVICE UPON RECEIPT OF MATERIEL

SECTION CONTENTS PARA PAGE

SCOPE 2-10 2-17

SERVICE UPON RECEIPT CHECKLIST 2-11 2-17

2 - 1 0 . S C O P E

This section covers the required service upon receipt to insure that the TOW 2Weapon System is complete and operational.

2 - 1 1 . SERVICE UPON RECEIPT CHECKLIST

The crew will perform the receiving inspection to determine whether the equipmentis complete and ready to use. When handling, inspecting, and maintaining theequipment, observe the following instructions:

a. Make an initial inventory when the equipment is received. Note any missingitems and report them promptly. Refer to Appendix D, Components of End Item Listfor the major components of the TOW 2 Weapon System.

b. Check national stock numbers, part numbers, and serial numbers to make surethat the correct items were received.

c. Check that all modification work orders published against the equipment havebeen incorporated.

d. Check all tags and stenciled information for correctness and completeness.

e. Perform a visual inspection of TOW 2 Weapon System components by doing thepreventive maintenance checks and services for your equipment. These proceduresare located in Section III of this chapter.

f. Perform necessary cleaning in accordance with the procedures given in paragraph2-16.

g. Report any deficiencies using applicable reports, records and forms. SeeDA PAM 738-750.

h. Do not. force levers, knobs, switches, or controls beyond their mechanicalstops.

i. Do not make any adjustments or repairs to TOW 2 Weapon System unless speci-Fically authorized by the maintenance allocation chart (MAC). If a componentcannot be adjusted or repaired in accordance with authorized procedures, refer theproblem to the supporting organization.

j. Use only those tools and equipment items authorized for performance of main-tenance as specified in the MAC.

k. Assemble TOW 2 Weapon System on tripod and perform system checkout procedure(paragraphs 2-27 through 2-33).

Change 3 2-17

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Sect ion I l l . PREVENTIVE MAINTENANCE CHECKS AND SERVICES (PMCS)

SECTION CONTENTS PARA PAGE

SCOPE 2-12 2-18

COLUMN ENTRIES USED IN PMCS 2-13 2-19

TOW 2 WEAPON SYSTEM PMCS 2-14 2-20

CLEANING 2-15 2-42.4

GENERAL CLEANING OF TOW 2 WEAPON SYSTEM 2-16 2-42.4

CLEANING RUBBER PARTS 2-17 2-45

CLEANING BATTERY ASSEMBLY 2-18 2-47

CLEANING CONNECTORS 2-19 2-48

CLEANING DAY SIGHT TRACKER LENS 2-20 2-49

CLEANING NIGHT SIGHT LENS 2-21 2-52

INSPECTION 2-22 2-55

PAINTING 2-23 2-55

2 - 1 2 . SCOPE

This section tells how to do the preventive maintenance checks and services (PMCS)required for the TOW 2 Weapon System. PMCS represent the minimum number of essen-tial checks. Before you begin the PMCS, keep in mind the following general infor-mation which is just as important as the specific checks.

a. Before operating any equipment, do all the before (B) PMCS. Be sure to keep inmind all CAUTIONS and WARNINGS.

b. While operating any equipment, do all the during (D) PMCS. Be sure to keep inmind all CAUTIONS and WARNINGS.

c. After operating any equipment, do all the after (A) PMCS.

d. Once every six months, while equipment is in service, do all semiannual (S)PMCS.

e. Once a year, while equipment is in service, do all annual (A) PMCS.

f. If your equipment fails to operate, report any deficiencies using the proper forms. See DA PAM 738-750.

2-18 Change 3

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2 - 1 3 . COLUMN ENTRIES USED IN PMCS

B -Before D- During A-After S - Semi-Annually A - Annually

Item to be checked

1 Connector J1

Check for damage or dirt

For readinessreporting, equip-

ment is not ready/available if:

Connectorcracked ordented andbe used.

badlycannot

1 Column 1, Item No. Column 1 numbers the checks and services to be

2

performed in chronological order. This column will also be used as asource of item numbers for the “TM Number” column on DA Form 2404,Equipment Inspection and Maintenance worksheet, in recording resultsof PMCS.

Column 2, Interval. Column 2 specifies the intervals at which the PMCSwill be performed. A dot (Ž) in any “Interval” column indicates whenyou are to perform that PMCS. The letters indicate the interval asfollows:

B - Before oprationD - During operationA - After operationS - Once every six months (semi-annually)A - Once a year (annually)

Column 3, Item to be checked. Column 3 identifies the part of theequipment to be checked and the procedures for performing the check.

Column 4, Equipment will be reported “Not Ready/Available” if. Column4 contains the criteria which will cause the equipment to be unable toperform its primary mission.

3

4

2-19

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2 - 1 4 . TOW 2 WEAPON SYSTEM PMCS

TABLE 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS AND SERVICES

B - Before D - During A - After S - Semi-Annually A - Annually

For readinessInterval reporting, equip-

Item ment is not ready/No. B D A S A Item to be checked available if:

Do not perform PMCS withencased missile loaded inlaunch tube. Missile can beaccidentally fired duringPMCS.

1. Tripod

Check operation of leg locks, and detent Leg locks arestop levers. inoperable.

Detent stopCheck for dirt, rust and loose, damaged levers do notor missing parts. Clean as necessary operate properly.(see para. 2-15). Coupling clamp

broken or missing.Level vialsbroken or nobubble.

2-20

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2-14 . TOW 2 WEAPON SYSTEM PMCS (CONT)

NOTE: The Elevation Depression Limiter Assembly listed below ispart of Mounting Kit located in Appendix E, (NSN 1450-01-099-2714).

Table 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS ANDSERVICES (CONT)

ItemNo

B - Before D - During A - After

Interval

B D A S A Item to be checked

2 . Traversing Unit

Check for damaged or missing parts.Make sure day sight tracker and launchtube can be moun ted . Check thataz imu th lock , e l e v a t i o n l o c k a n delevat ion brake work property. ForHMMWV operation, check that elevationand depression stops are pinned in upposition.

For readinessreporting, equip-ment is not ready/available if:

S - Semi-Annually A - Annually

Day sight tracker orlaunch tube cannotbe mounted.

Traversing unit willnot m a t e w i t htripod.

Elevation ordepression l imiterassembly notoperational (forHMMWV only).

Change 12 2-21

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2 - 1 4 . TOW 2 WEAPON SYSTEM PMCS (CONT)

TABLE 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS AND SERVICES (CONT)

B - Before D - During A - After S - Semi-Annually A - Annually

ItemNo.

2.(cont)

2-22

Interval

Change 11

Item to be checked

Traversing Unit (cont)

Check coil cable 2W1 and postamplifiercable for damage or loose connections.Check cable connectors and 2W1 adapterfor damage, broken pins, or foreignmaterial. Check saddle bolts are notloose or missing.

For readinessreporting, equip-

ment is not ready/available if:

Coil cable or post-amplifier cableconnector damaged.Saddle bolts looseor missing.

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2 - 1 4 . TOW 2 WEAPON SYSTEM PMCS (CONT)

TABLE 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS AND SERVICES (CONT)

13- Before D - During A - After S - Semi-Annually A - Annually

Change 11 2-22 .1 / (2 -22 .2 b lank)

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2 - 1 4 . TOW 2 WEAPON SYSTEM PMCS (CONT)

TABLE 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS AND SERVICES (CONT)

B - Before D - During A - After S - Semi - Anually A - Annually

ItemNo.

2.(Cont)

3.

Interval

Item to be checked

Traversing Unit (cont)

Check verification label to make suresemi-annual verification is not pastdue.

Clean as necessary (see paras. 2-15and 2-16.)

Notify direct support to perform semi-annual verification.

Launch Tube

Check launch tube for cracks, pits,tears, visible raised areas, exposedfabric, or exposed threads inside.Check index lugs for damage. Check fordirt and other foreign material. Cleanas required.

For readinessreporting, equip-ment is not ready/

available if:

Verification duedate past due.

Inside bore split,cracked, pitted,torn or gougedthrough one layerof fiberglass orhas visible raisedareas, exposedfabric or exposedthreads.

Index lugs damagedand will notengage traversingunit properly.

Change 4 2-23

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2-14. TOW 2 WEAPON SYSTEM PMCS (CONT)

TABLE 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS AND SERVICES (CONT)

B - Before D - During A - After S - Semi-Annually A - Annually

Interval

Item No.

B D A S A Item to be checked

For readiness reporting, equipment is not ready/available if:

4. Day Sight Tracker

Check for damaged or missing components.

Make sure that all controls operate properly (see para. 2-3).

Make sure that image can be seen through eyepiece. Clear image in sharp

focus cannot be seen.

Make sure that day sight tracker mates securely with traversing unit. Day sight should not rock at mounting plate if pressure is applied in any direction at front end of optical sight.

Day sight tracker will not mate with traversing unit.

2-24 Change 13

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para 2-15

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2 - 1 4 . TOW 2 WEAPON SYSTEM PMCS (CONT)

TABLE 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS AND SERVICES (CONT)

B - Before D - During A - After S - Semi-Annually A - Annually

C h a n g e 1 1 2-25

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CAUTION

para 2-6

para 2-15

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2 - 1 4 . TOW 2 WEAPON SYSTEM PMCS (CONT)

TABLE 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS AND SERVICES (CONT)

B - Before D - During A - After S - Semi-Annually A - Annually

2-26 Change 3

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2-14. TOW 2 WEAPON SYSTEM PMCS (CONT)

Table 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS ANDSERVICES (CONT)

B - Before D - During A - After S - Semi-Annually A - Annually

Interval

For readinessreporting, equip-

Item ment is not ready/No B D A S A Item to be checked available if:

5. o Night Sight (cont)cont.

Check battery power conditioner for Battery power con-dents, cracks or other damage that might ditioner not service-prevent proper operations. able.

Check fo r two ba t te r ies ins ta l led in Batteries notbattery power conditioner. installed.

Check for two spare batteries available. New batteries notavailable in original

l Notify direct support to perform night plastic wrap.sight verification.

RADlATlON HAZARD

The anti-reflective coating on night sighto n i n f r a r e d o p t i c s c o n t a i n s t h o r i u mfluoride which is slightly radioactive. Theonly potential hazard involves ingestion(swallowing or inhaling) of this coatingmaterial. Dispose of broken lenses, etc.,in accordance with AR 385-11.

5.1 l Inspect lens and eyepiece for cracks andscratches.

l Boresight Collimator

Check boresight collimator and case fordamaged or missing components.

Change 12 2-27

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Interval

A - Annually

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2-14. TOW 2 WEAPON SYSTEM PMCS (CONT)

Table 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS ANDSERVICES (CONT)

B - Before D - During A - After S - Semi-Annually

SERVICES (CONT)

For readinessreporting, equip-

Item ment is not ready/No B D A S A Item to be checked available if:

5.1 Boresight Collimator (cont)cont.

Inspect lenses and mirrors for cracks or O p t i c s a r e b a d l yscratches. scratched or

broken.

Check serviceability of knobs. Knobs Inoperable.

Check ver i f icat ion label to make suresemi-annual verification is not past due.

l Verification due date past due. Notify directsupport to performboresight collimatorverification.

6 . l Missile Guidance Set

C h e c k f o r d a m a g e d o r m i s s i n g Display damaged.components.

Check connectors for damage and bent Bent or broken pinsor broken pins. o r damaged

connectors.

Make sure tha t a l l con t ro ls opera teproperly (see para 2-2).

Check that battery can be installed. Battery can not beinstalled.

2-28 Change 12

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2-14. TOW 2 WEAPON SYSTEM PMCS (CONT)

Table 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS AND

ItemNo

6.cont.

lnterval

SERVICES (CONT)

B - Be fo re D - Dur ing A - After S - Semi-Annually A - Annually

B D A S A

l

Item to be checkedMissile Guidance Set (cont)

Check verification label to make suresemi-annual verification is not past due.

Clean as required (see para 2-15 and 2-16.

Notify direct support to perform semi-annual verification.

For readinessreporting, equipment is not ready/available if:

Verification duedate past due.

Change 12 2-29

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2-14. TOW 2 WEAPON SYSTEM PMCS (CONT)

TABLE 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS AND SERVICES (CONT)

B - Before D - During A - After S - Semi-Annually A - Annually

Interval

Item No.

B D A S A Item to be checked

For readiness reporting, equipment is not ready/available if:

7. Battery Assembly

NOTE

The following checks must be performed for both battery assemblies for tripod mounted system.

Check battery assembly for dents, cracks or other damage that might prevent proper operation.

Battery assembly not serviceable.

Make sure that at least 4 wing nuts operate properly. Fewer than 4 wing nuts are operable.

Check that battery assembly can be installed in missile guidance set.

Battery assembly cannot be installed in missile guidance set.

Clean as required (see paras. 2-15 and 2-18).

Check battery charge label. Charge date has passed (see para. 1-13, page 1-14).

2-30 Change 13

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TM 9-1425-450-12

2-14. TOW 2 WEAPON SYSTEM PMCS (CONT)

TABLE 2-1. TOW 2 SYSTEM PREVENTIVE MAINTENANCE CHECKS AND SERVICES (CONT)

B - Before D - During A - After S - Semi-Annually A - Annually

Interval

Item No.

B D A S A Item to be checked

For readiness reporting, equipment is not ready/available if:

8. TOW 2 Weapon System

Perform system checkout procedure (see para. 2-33). Fails system checkout procedure.

NOTE • Both batteries must pass system

checkout procedure.

• When the weapon system is in storage (not in use), the system checkout procedure must be performed monthly.

One or both batteries fail system checkout procedure.

General appearance - check for loose, damaged, or missing parts.

Fails if any condition is present.

Notify direct support to perform system verification.

Change 13 2-31 (2-32 thru 2-41 deleted)

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table 2-1para 2-14

para 2-15

TM 9-1425-450-12

2 - 1 4 . TOW 2 WEAPON SYSTEM PMCS (CONT)

TABLE 2-4. TOW 2 HMMWV PREVENTIVE MAINTENANCE CHECKS AND SERVICES

B - Before D - During A - After S - Semi-Annually A - Annually

2-42 C h a n g e 1 1

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paras. 2-15

TM 9-1425-450-12

2 - 1 4 . TOW 2 WEAPON SYSTEM PMCS (CONT)

TABLE 2-4. TOW 2 HMMWV PREVENTIVE MAINTENANCE CHECKS AND SERVICES (CONT)

B - Before D - During A- After S - semi-Annually A - Annually

Change 2 2-42.1

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TM 9-1425-450-12

2-14. TOW 2 WEAPON SYSTEM PMCS (CONT)

Table 2-4. TOW 2 HMMWV PREVENTATIVE MAINTENANCE CHECKS AND SERVICES(CONT)

B - Before D - During A - After S - Semi-Annually A - Annually

ItemNo B D A S A

5.cont

Interval

6

7

2-42.2 Change 12

Item to be checked

Power Cables (cont)

Check TVPC power cable under loader’sseat.

HMMWV

Perform vehicle PMCS (see TM 9-2320- Vehicle280-10). PMCS.

Radio and Mount

Perform radio PMCS (see TM 11-5820-401-10-1 for VCR 46 series, or Sincgarsseries (see TM 11-5820-890-10-1).

For readinessreporting, equipment is not ready/available if:

fails

R a d i o o r m o u n tfails PMCS.

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TM 9-1425-450-12

2 - 1 4 . TOW 2 WEAPON SYSTEM PMCS (CONT)

TABLE 2-4. TOW 2 HMMWV PREVENTIVE MAINTENANCE CHECKS AND SERVICES (CONT)

B - Before D - During A - After S - Semi-Annually A - Annually

For readinessInterval reporting, equip-

Item ment is not ready/No. B D A S A Item to be checked available if:

8 Power Conditioner

NOTE

If power conditioner is notserviceable, both TOW batteriesmust be available and they mustpass system self test.

Check for damaged or missing components.

Make sure that at least four wing nuts Fewer than twoare operable. wing nuts on each

end are operableand one batteryfails systemself test.

Make sure that power conditioner can be Power conditionerinstalled in missile guidance set. damaged and cannot

be installed inmissile guidanceset and one batteryfails system selftest.

Clean as required (see paras. 2-15and 2-16).

Change 2 2-42.3

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WARNING

TM 9-1425-450-12

2 - 1 5 . CLEANING

Cleaning of TOW 2 Weapon System is important for maintaining good operation. Ifthe TOW 2 Weapon System is not kept clean, damage may be hidden and not found duringan initial inspection. General cleaning shall be done by organizationalmaintenance personnel before touch-up painting.

2 - 1 6 . GENERAL CLEANING OF TOW 2 WEAPON SYSTEM(Sheet 1 o f 3 )

NOTE

Before doing procedure below, check Section III contents (page2-18) for a specific cleaning procedure for the item you arecleaning. If no specific procedure is listed, do procedurelisted below.

MATERIALS: Scrub brush (item 4, Appendix C)Alcohol (item 2, Appendix C)Wiping rags (item 24, Appendix C)Gloves (item 32, Appendix C)

TOOLS: Goggles

SOLVENT (ALCOHOL) WILL BURN AND CAN HARM EYES AND SKIN

Keep it away from open flame.

Use only in area where there is plenty of fresh air.

If personnel are burned, get medical help right away.

Try not to get solvent on your bare skin,

If solvent gets in your eyes, wash them with plenty ofwater and get medical help right away.

After using solvent, wash carefully so that there is nosolvent on your bare skin.

2-42.4 Change 5

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TM 9-1425-450-12

2-16. GENERAL CLEANING OF TOW 2 WEAPON SYSTEM (CONT) (SHEET 2 OF 3)

RUBBER PARTS OR SEALANTS

Do not get alcohol on rubber parts on sealant. Alcohol can cause rubber parts to crack and sealants to melt.

CLEANING GLASS SURFACES

Do not clean glass surfaces with rags or scrub brush. These materials can scratch glass surfaces and cause the system not to work right.

Do not use high-pressure equipment (water or air) to clean the TOW launcher. Damage to system could occur.

Change 13 2-43

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TM 9-1425-450-12

2 - 1 6 . GENERAL CLEANING OF TOW 2 WEAPON SYSTEM (CONT)(Sheet 3 o f 3 )

END OF TASK

2-44 Change 5

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CAUTION

TM 9-1425-450-12

2 - 1 7 . CLEANING RUBBER PARTS(Sheet 1 Of 2)

MATERIALS: Detergent (item 9, Appendix C)Wiping rags (item 24, Appendix C)Glycerol item 12, Appendix C)

RUBBER PARTS OR SEALANTS

Do not use solvent on rubber parts or sealant. Solventcan cause rubber parts to crack and sealants to melt.

Change 8 2-45

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TM 9-1425-450-12

2 - 1 7 . CLEANING RUBBER PARTS (CONT)S H e e t 2 o f 2 )

NOTE

If detergent is not available, plain water can be usedto clean rubber parts.

For cold weather operation (temperature below O°C or+32°F), add glycerol to cleaning water. Glycerol pre-vents water from freezing during use.

A. For grease, or if dry wiping rag cannot remove the dirt, mix detergentwith water.

B. Wet a clean wiping rag with detergent and water mixture.

C. Wipe rubber parts with wet wiping rag.

D. Wipe any excess detergent and water mixture from rubber parts using aclean wiping rag wet with water only.

E. Dry rubber parts using clean, dry wiping rag.

END OF TASK

2-46

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WARNING

TM 9-1425-450-12

2 - 1 8 . C L E A N I N G B A T T E R Y A S S E M B L Y

MATERIALS: Scrub brush (item 4, Appendix C)Wiping rag (item 24, Appendix C)Glycerol (item 12, Appendix C)

BATTERY CORROSION POWDER WILL BURN

Do not let battery corrosion powder get on skin orclothing. Battery corrosion powder will burn the skin anddestroy your clothes.If battery corrosion powder gets on skin or clothes, washright away.Destroy all wiping rags after use.

NOTE

For cold weather operation (temperature below 0°C or 32°F,add glycerol to cleaning water. Glycerol prevents waterfrom freezing.

END OF TASK

2-47

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WARNING

CAUTION

TM 9-1425-450-12

2 - 1 9 . CLEANING CONNECTORS

MATERIALS: Alcohol (item 2, Appendix C)Orangewood stick (item 16, Appendix C)Wiping rag (item 24, Appendix C)

ALCOHOL WILL BURN

Keep alcohol away from heat and open flame. Use only in area where there is plenty of fresh air. If personnel are burned, get medical help right away.

RUBBER PARTS OR SEALANTS

Do not get alcohol on rubber parts or sealant. Alcohol cancause rubber parts to crack and sealants to melt.

END OF TASK

2-48

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CAUTION

TM 9-1425-450-12

2 - 2 0 . CLEANING DAY SIGHT TRACKER LENS(Sheet 1 of 3)

MATERIALS : Alcohol (item 2, Appendix C)Camel hair brush (item 3, Appendix C)Lens paper (item 18, Appendix C)Rubber syringe (item 27, Appendix C)De-icer (item 7, Appendix C)Wiping rag (item 24, Appendix C)

Do not use this procedure to clean night sight lens. Refer to para 2-21 for special cleaning of night sight lens.

Do not touch lens surface with fingers.

NOTE

If moisture has frozenon lens surface, do step 1. If moisturehas not frozenon lens surface, start with step 2.

2-49

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CAUTION

TM 9-1425-450-12

2 - 2 0 . CLEANING DAY SIGHT TRACKER LENS (CONT)(Sheet 2 of 3)

2-50 Change 1

Page 107: TM 9 1425 450 12 TOW 2 Weapon System

CAUTION

WARNING

TM 9-1425-450-12

2 - 2 0 . CLEANING DAY SIGHT TRACKER LENS (CONT)(Sheet 3 of 3)

END OF TASK

Change 1 2-51

Page 108: TM 9 1425 450 12 TOW 2 Weapon System

CAUTION

TM 9-1425-450-12

2-21 . CLEANING NIGHT SIGHT LENS(Sheet 1 of 3)

MATERIALS: Cotton padLens cleang

Do notmateri a

(itemng so

17, Appendix C)ution (item 25, Appendix C)

clean niqht sight with anyths listed. Damage to night sight

NOTE

During cold weather, use warm water

ng other than thecould occur.

and lens cleaningsolution. Make sure these liquids are not hot; just warmenough not to freeze on night sight lens.

A. Rinse night sight lens by pouring clean drinking water over lens surface.

B. Wet cotton pad with lens cleaning solution.

GO TO NEXT PAGE

2-52

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CAUTION

TM 9-1425-450-12

2 - 2 1 . CLEANING NIGHT SIGHT LENS (CONT)(Sheet 2 of 3)

A .

B .

C .

D.

L i g h t l y d a b ( d o n o t r u b ) p a d w i t h l e n s c l e a n i n g s o l u t i o n o n l e n s s u r f a c e ,c o v e r i n g s u r f a c e c o m p l e t e l y .

D o n o t l e t l e n s c l e a n i n g s o l u t i o n d r y o n n i g h t s i g h t l e n s .D a m a g e t o n i g h t s i g h t l e n s c o u l d o c c u r .

W a i t b e t w e e n o n e t o t h r e e m i n u t e s f o r l e n s c l e a n i n g s o l u t i o n t o l o o s e nh e a v y d i r t .

R i n s e l e n s c l e a n i n g s o l u t i o n o f f o f n i g h t s i g h t l e n s b y p o u r i n gc l e a n d r i n k i n g w a t e r o v e r l e n s s u r f a c e .

R e p e a t s t e p s 1 B t h r o u g h 2 C u n t i l a l l d i r t i s c l e a n e d o f f o f n i g h t s i g h tl e n s .

GO TO NEXT PAGE

2-53

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CAUTION

TM 9-1425-450-12

2 - 2 1 . CLEANING NIGHT(Sheet 3 of 3)

When wiping

SIGHT LENS (CONT)

lens, wiping motion should be in one directiononly (left-to right). Wiping in more than one direction cancause damage to night sight.

NOTE

Throw away all dirty cotton pads. Do not re-use.

A. Apply lens cleaning solution to a small area of night sight lens.

B. Gently wipe (left to right) lens surface with clean cotton pad.

C. Rinse night sight lens with clean drinking water.

D. Dry night sight lens by wiping (left to right) with clean, dry, cottonpad.

END OF TASK

2-54

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WARNING

CAUTION

TM 9-1425-450-12

2 - 2 2 . I N S P E C T I O N

Detailed inspection procedures for the TOW 2 Weapon System are found in the preven-tive maintenance checks and services, paragraphs 2-12 thru 2-14. These checks andservices may have to be performed more often because of extensive use, adverseweather conditions, etc.

2 - 2 3 . P A I N T I N G( S h e e t 1 o f 2 )

Paint, primer, and thinner are toxic and flammable. Theymust be used with extreme care. Do not get them on skin.Wear eye protection and rubber gloves when using. Avoid pro-longed or repeated breathing of vapors. Use only in wellventilated area. Keep away from heat and open flames. Ifinjury occurs, get medical help right away.

Bearings, rubber, or other components which might be damagedby cleaning, masking or paint must be removed beforeproceeding.

Use masking tape to insure that no paint is applied to thefollowing: countersinks, counterbores, bolt holes, bearingsurfaces, attaching surfaces, preformed packing grooves, andthose areas treated with solid film lubricant.

a. Organizational maintenance personnel are authorized to spot paint the TOW 2Weapon System equipment. Spot painting detailed procedures are found in TM 43-0139.For spot painting, use polyurethane paint No. 383 for all green surfaces andNo. 37038 for all black front panels. Surfaces must be cleaned (paras 2-15 thru2-21) before any spot painting takes place. Organizational maintenance personnelare also authorized to remove the yellow markings from the tripod legs. To paintthe tripod legs do the following paragraph b.

Change 4 2 - 5 5

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TM 9-1425-450-12

2 - 2 3 . PAINTING (CONT)(Sheet 2 o f 2 )

b.

To paint the tripod legs, first mask off the area to be painted. Remove theyellow markings from the masked-off area by sanding it down. Clean the sandedarea, coat it with primer, and paint the area with green polyurethane paint.The detent stop markings and nomenclature need not be repainted.

2-56 Change 4

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TM 9-1425-450-12

Section IV. EMPLACEMENT OF TRIPOD MOUNTED TOW 2 SYSTEM

SECTION CONTENTS PARA PAGE SCOPE 2-24 2-57

CONNECTING AND DISCONNECTING CABLES 2-25 2-58

SELECTION OF SITE FOR TRIPOD MOUNTED TOW 2 WEAPON SYSTEM 2-26 2-60

SETUP OF TRIPOD 2-27 2-62

INSTALLATION OF TRAVERSING UNIT ON TRIPOD MOUNTED TOW 2 SYSTEM

2-28 2-66

INSTALLATION OF LAUNCH TUBE ON TRIPOD MOUNTED TOW 2 SYSTEM 2-29 2-68

INSTALLATION OF DAY SIGHT TRACKER ON TRIPOD MOUNTED TOW 2 SYSTEM

2-30 2-70

INSTALLATION OF NIGHT SIGHT ON TRIPOD MOUNTED TOW 2 SYSTEM 2-31 2-73

INSTALLATION OF MISSILE GUIDANCE SET WITH TRIPOD MOUNTED TOW 2 SYSTEM

2-32 2-81

SYSTEM CHECKOUT PROCEDURE 2-33 2-84

LOADING ENCASED MISSILE INTO LAUNCH TUBE FOR TRIPOD MOUNTED TOW 2 WEAPON SYSTEM

2-34 2-120

PREPARATION TO FIRE MISSILE 2-35 2-128

MISSILE FIRING PROCEDURE 2-36 2-135

MALFUNCTIONS 2-37 2-142

FAILURE TO FIRE - HANGFIRE PROCEDURES 2-38 2-142

FAILURE TO FIRE - MISFIRE PROCEDURES 2-39 2-144.2

DUD 2-40 2-145

IRREGULAR FLIGHT 2-41 2-146

ACTION AFTER FIRING WITH ADDITIONAL MISSILES TO BE FIRED 2-42 2-147

REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE 2-43 2-152

DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL 2-44 2-160

2-24. SCOPE

This section covers all the information needed by the TOW crew to set up, checkout, and fire the TOW missile from a ground emplacement. This section also tells how to set up and operate the night sight.

Change 13 2-57

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TM 9-1425-450-12

2-25. CONNECTING AND DISCONNECTING CABLES (Sheet 1 of 2)

The procedure in this paragraph can be used as a general rule of thumb for removing and installing connectors. If you are unfamiliar with the TOW 2 Weapon System connector, this procedure will aid you when you connect or disconnect cables. To connect cables, do steps 1 and 2 below. To disconnect cables, do steps 3 and 4.

NOTE Use of bayonet style connectors is explained in the applicable procedures.

Connector pins are fragile. Use noside to side pressure when installingconnectors, as this can causemisalinement and bent or broken pins.

A. Slide connector into receptacle.

B. Turn locking nut on connector in direction of arrow until tight.

C. Push down on connector with palm of hand.

D. Repeat steps B and C until connector is tightened completely.

GO TO NEXT PAGE

A. Line up keys of connector with keyways of receptacle. B. Make sure that all keys have a keyway to slide into.

2-58 Change 13

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TM 9-1425-450-12

2-25. CONNECTING AND DISCONNECTING CABLES (CONT) (SHEET 2 OF 2)

3

Turn locking nut in direction of arrow until threads are not attached.

4

A. Pull connector straight out of receptacle.

B. Replace receptacle cover (if applicable).

END OF TASK

Change 13 2-59

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TM 9-1425-450-12

2-26. SELECTION OF SITE FOR TRIPOD MOUNTED TOW 2 WEAPON SYSTEM (SHEET 1 OF 2)

1

If forward slope at launch site is greater than 30 degrees (30°), injury to personnel and damage to equipment may occur when missile is fired. If sideways slope is greater than 10 degrees (10°), adequate tracking may be impossible.

Avoid a position where the system is pointing toward the sun. The sun's reflection off the lens of any sight device may give away your position.

NOTE

Select a level location if at all possible.

A. Check that forward slope at possible launch site is not more than 30 degrees (30°).

B. Check that sideways slope is not more than 10 degrees (10°).

GO TO NEXT PAGE

2-60 Change 13

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TM 9-1425-450-12

2-26. SELECTION OF SITE FOR TRIPOD MOUNTED TOW 2 WEAPON SYSTEM (SHEET 2 OF 2)

2

If backblast area is not clear, injury to personnel and damage to equipment may occur when missile is fired.

Check that backblast area (area within 75 meters or 246 feet behind the launch tube) is clear of personnel, equipment, and flammable material.

3

Do not fire missile over or in the direction of electrical wires. If command-link wires contact a live high voltage power line, injury to personnel and damage to equipment may occur. Check site for things blocking field-of-view. Move site if field-of-view is not large enough.

END OF TASK

Change 13 2-61

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TM 9-1425-450-12

2-27. SETUP OF TRIPOD (SHEET 1 OF 4)

1

A. If necessary, remove tripod from HMMWV (see para. 2-82).

B. Lift three lock handles up all the way to release position.

GO TO NEXT PAGE

2-62 Change 13

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TM 9-1425-450-12

2 - 2 7 . SETUP OF TRIPOD (CONT)

A.

B.

C.

Press one detent stop lever down and release.

Pull one leg of tripod out until leg support reaches the bottom band on leg.

Repeat steps A and B for other two legs.

A. Position tripod with coupling clamp handle facing direction of fire.

B. Using the detent stop lever, adjust tripod legs until the bubble ineach level vial is between the two marks shown.

C. Lower the lock handle on each leg all the way to locked position.

GO TO NEXT PAGE

2-63

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TM 9-1425-450-12

2 - 2 7 . SETUP OF TRIPOD (CONT)( S h e e t 3 o f 4 )

NOTE

Do this step if the ground is soft.

If the ground is not soft go to step 5.

A. Using heel of shoe, force all three tripod anchor claws into ground.

B. If additional support is needed, drive stakes into ground through holes intripod anchor foot.

GO TO NEXT PAGE

2-64

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TM 9-1425-450-12

2 - 2 7 . S E T U P O F T R I P O D ( C O N T )

(Sheet 4 o f 4 )

Open coupling clamp by pulling coupling clamp handle out.

END OF TASK

2-65

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TM 9-1425-450-12

2 - 2 8 . INSTALLATION OF TRAVERSING UNIT ON TRIPOD MOUNTEDTOW 2 WEAPON SYSTEM(Sheet 1 of 2)

A. Set up tripod (see para 2-27).

B. Hold traversing unit over tripod.

C. Pass coil cable down through body of tripod.

GO TO NEXT PAGE

2 - 6 6

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TM 9-1425-450-12

2 - 2 8 . INSTALLATION OF TRAVERSING UNIT ON TRIPOD MOUNTEDTOW 2 WEAPON SYSTEM (CONT)(Sheet 2 o f 2 )

A. Carefully place traversing unit on tripod.

B. Push coupling clamp handle in to fasten traversing unit to tripod.

C. Place azimuth lock in the LOCK position.

D. Turn traversing unit from side to side until it locks in place.

E. Pull coupling clamp handle out.

F. Turn traversing unit so locating pin is in direction of fire.

G. Push coupling clamp handle in.

H. Make sure coupling clamp is fastened and correctly adjusted byattempting to turn traversing unit.

I. If elevation/depression limiters are installed on traversing unit,remove locking pins, move limiters to down position, and reinstalllocking pins.

END OF TASK

Change 2 2-67

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TM 9-1425-450-12

2 - 2 9 . INSTALLATION OF LAUNCH TUBE ON TRIPOD MOUNTEDTOW 2 WEAPON SYSTEM(Sheet 1 of 2)

A. Install traversing unit on tripod (see para 2-28).

B. Lift up launch tube latch.

C. Place two launch tube pins in launch tube brackets so that launch tube ispointed in direction of fire.

GO TO NEXT PAGE

2-68

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TM 9-1425-450-12

2 - 2 9 . INSTALLATION OF LAUNCH TUBE ON TRIPOD MOUNTEDTOW 2 WEAPON SYSTEM (CONT)(Sheet 2 of 2)

A. Line up locating pin with mating hole in launch tube.

B. Place launch tube latch in launch tube catch.

C. Press down on launch tube latch until it latches.

END OF TASK

2-69

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CAUTION

TM 9-1425-450-12

2 - 3 0 . INSTALLATION OF DAY SIGHT TRACKER ON TRIPOD MOUNTEDTOW 2 WEAPON SYSTEM(Sheet 1 of 3)

DAY SIGHT TRACKER HANDLING

Handle day sight tracker very carefully. Day sight trackeris very fragile and can be easily damaged.Make sure day sight tracker is well supported until it istightly attached to traversing unit.Do not carry or lift day sight tracker by the latch handle.

A. Install traversing unit on tripod (see para 2-28).

B. If necessary, remove day sight tracker from shroud bag.

C. Hold day sight tracker with tracker hook mount facing traversing unitboresight plate.

D. Press and hold latch in towards latch handle.

E. Push latch handle all the way down. Release latch.

GO TO NEXT PAGE

2-70

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TM 9-1425-450-12

2 - 3 0 . INSTALLATION OF DAY SIGHT TRACKER ON TRIPOD MOUNTEDTOW 2 WEAPON SYSTEM (CONT)(Sheet 2 o f 3 )

A.

B.

C.

D.

Join day sight tracker index plate groove with traversing unit bore-sight guide.

Hold day sight tracker flush with traversing unit boresight guide.

Pull latch handle all the way up until latch releases.

Make sure day sight tracker is securely mounted to traversing unitbefore letting go.

GO TO NEXT PAGE

2-71

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TM 9-1425-450-12

2 - 3 0 . INSTALLATION OF DAY SIGHT TRACKER ON TRIPOD MOUNTEDTOW 2 WEAPON SYSTEM (CONT)(Sheet 3 of 3)

A. Make sure that RETICLE LIGHT switch is set to OFF.

B. Check humidity indicator to be sure that 30 percent section is blue.If the 30 percent section is pink or white, notify support mainte-

nance to replace desiccant at next scheduled maintenance.

END OF TASK

2-72

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CAUTION

TM 9-1425-4!50-12

2 - 3 1 . I N S T A L L A T I O N O F N I G H T S I G H T O N T R I P O D M O U N T E DT O W 2 W E A P O N S Y S T E M(Sheet 1 o f 4 )

Change 10 2-73

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TM 9-1425-450-12

2 - 3 1 . INSTALLATION OF NIGHT SIGHT ON TRIPOD MOUNTEDTOW 2 WEAPON SYSTEM (CONT)(Sheet 2 o f 4 )

A. Check locating “Vee Ways” on night sight and day sight tracker forforeign material. Clean if necessary.

B. Line up keyed hole on night sight with cam post on day sighttracker.

GO TO NEXT PAGE

2-74

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CAUTION

TM 9-1425-450-12

2 - 3 1 . INSTALLATION OF NIGHT SIGHT ON TRIPOD MOUNTEDTOW 2 WEAPON SYSTEM (CONT)(Sheet 3 o f 8 )

A. Place night sight on day sight tracker with night sight lens facing forward.

B. Make sure night sight seats securely on day sight tracker.

C. Using your right hand, move latch handle toward front of night sight (indirection of arrow) to lock in place. Make sure night sight is securelymounted to day sight tracker before letting go.

D. On night sight, remove protective cap from postamplifier cable connector andstore in assigned place in night sight field handling case.

E. Remove postamplifier cable connector from cable retainer on traversing unit.

Keep postamplifier cable clear of bridge clamp.

F. Aline yellow mark on postamplifier cable connector with yellow mark onnight sight.

G. Push in on postamplifier cable connector and turn to right until post-amplifier cable connector stops.

GO TO NEXT PAGE

Change 4 2-75

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2-31. INSTALLATION OF NIGHT SIGHT ON TRIPOD MOUNTEDTOW 2 WEAPON SYSTEM (CONT)(Sheet 4 of 4)

A. Open battery power conditioner lid and connect output cable connector 8W1P2(8J1) to connector on battery power conditioner.

B. Connect battery power conditioner output cable connector 8W1P1 (1J3) tonight sight input power connector J1.

C. Set circuit breaker to ON.

A. Remove front lens cover from night sight by releasing two latches.

B. Set night sight field-of-view switch to NFOV.

END OF TASKAll data on pages 2-77 thru 2-80 deleted.

2-76 Change 8

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TM 9-1425-450-12

TOW 2 WEAPON SYSTEM(Sheet 1 of 3)

2-32. INSTALLATION OF MISSILE GUIDANCE SET WITH TRIPOD MOUNTED

A. Install traversing unit on tripod (see para 2-28).

B. Install launch tube (see para 2-29).

C. Install day sight tracker on traversing unit (see para 2-30).

D. Install night sight (see para 2-31).

E. Unlatch two latches at front of missile guidance set.

F. Open cover all the way and remove.

G. Stow cover in a safe place out of the way of personnel.

GO TO NEXT PAGE

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CAUTION

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2 - 3 2 . INSTALLATION OF MISSILE GUIDANCE SET WITH TRIPOD MOUNTEDTOW 2 WEAPON SYSTEM (CONT)(Sheet 2 o f 3 )

NOTE

If battery assemblyis not in missileguidance set,install batteryassembly (para 3-6).

Place missile guidance setclose to the rear of thetripod and clear of load-ing and firing operations.

Be sure there is no dirt in endof coil cable connector. Dirtcan cause connector to make badcontact with missile guidanceset, resulting in poor systemoperation.

Do not apply downward pressure oncoil cable connector. This cancause misalinement and bent pins.

A. On coil cable connector lineup yellow colored index linewith yellow colored mating linenext to connector J1 on missileguidance set.

B. Turn locking nut in directionof arrow until red mark on J1connector cannot be seen.

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TOW 2 WEAPON SYSTEM (CONT)(Sheet 3 o f 3 )

2 - 3 2 . INSTALLATION OF MISSILE GUIDANCE SET WITH TRIPOD MOUNTED

A. Place missile guidance set near base of tripod and forward of loadingand firing operations.

B. Place night sight battery power conditioner next to missile guidance set.

C. At the beginning of each operating day, do system checkout procedure(para 2-33).

END OF TASK

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WARNING

CAUTION

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2 - 3 3 . S Y S T E M C H E C K O U T P R O C E D U R E( S h e e t 1 o f 3 4 )

PERSONNEL: Two MOS 11H (Soldier A will perform all steps except those which callfor Soldier B)

Do not perform system checkout procedurewith encased missile loaded. Missile canbe accidentally fired during systemcheckout.

Before performing system checkout procedurethe TOW 2 launcher must be completely set-up.Failure to do this could result in damage tothe system.

Do system checkout procedure as quickly aspossible. If too much time is taken to dosystem checkout procedure, battery assemblymay not have enough power to fire missiles.

NOTE

A self test can be initiated by performingsteps 10 thru 15 of the system checkoutprocedure. If the day sight tracker bore-sight knobs are moved to obtain a steadygreen lamp indication on the azimuth/elevation cross. YOU must also perform thenight34).sight

sight boresight check (steps 22 thruThe self test and night sight bore-check must be performed if:

Moved over rough terrain10 degree F temperature changeSystem operated more than 4 hoursLocation change using extended travel modeOperating site changed (ground mode only).

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2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 2 o f 36 )

NOTE

Each time a unit is re-moved and replaced, returnto step 01 (start of test)unless told otherwise.

Whenever a problem isfound, if the first cor-rective action does notsolve the problem, do thesecond corrective actionand repeat the test. Ifproblem still exists, con-tinue on with any addi-tional corrective actionwhich may be listed.

If you are doing thisprocedure using vehiclepower, corrective actionsinvolving batteries willnot apply. Instead, checkpower conditioner andnight sight vehicle powerconditioner cable con-nections and make sureON/OFF switches are ON.If launcher is still nogo, replace power con-ditioner with battery(paras 3-7 and 3-6) or usebattery power conditionerinstead of night sightvehicle power conditioner,as applicabLe.

STEP 01

Set up TOW 2 launcher com-pletely and install nightsight (para 2-25 thru2-32).

Go to next page

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2 - 3 3 . S Y S T E M C H E C K O U T P R O C E D U R E ( C O N T )( S h e e t 3 o f 3 6 )

Continued from previous page

CHECKING TRIGGER

Do not have encasedmissile loaded whenchecking trigger.

If trigger is checkedwith missile loaded, themissile will fire.

Personal injury canoccur if missile isfired by mistake.

If personnel are injuredby missile firing bymistake, get medicalhelp right away.

Go to next page

2-86

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(para 3-63)

(para 3-63)

(para 3-63)

T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 3 3 . S Y S T E M C H E C K O U T P R O C E D U R E ( C O N T )( S h e e t 4 o f 3 6 )

2 - 8 7

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(para 2-15)

(para 3-63)

(para 3-63)

2-33.

T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 8 8 C h a n g e 4

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2-33.

(para 2-15)

(para 3-63)

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2 - 8 9

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2-33.

para 3-63

(para 3-63)

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2 - 9 0

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(para 3-63)

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2 - 3 3 . SYSTEM CHECKOUT--PROCEDURE (CONT)(Sheet 8 o f 36 )

2 - 9 1

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2-33.

(para 3-63)

(para 3-63)

T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 9 2 Change 8

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2-33.

(para 3-63)

(para 3-63)

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C h a n g e 8 2-92 .1

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para 3-63

para 3-63

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2 - 3 3 . S Y S T E M C H E C K O U T( S h e e t 9 . 2 o f 3 6 )

2-92.2 Change 8

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2-93

2-93

para 3-5 .

(para 3-63).

(para 3-63).

para 3-5 .

(para 3-63).

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2-33. SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 10 of 36)

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(para 3-63).

(para 3-63)

(para 3-63).

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2-33. SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 11 of 36)

2-94 Change 8

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2-33. SYSTEM CHECKOUT PROCEDURE (CONT) (SHEET 12 OF 36)

Continued from previous page

GO TO NEXT PAGE

Under combat conditions, if PA FAIL, OSS FAIL, orMGS FAIL occurs, the TOW 2 system can still befired in a degraded mode if the optical sight can beboresighted (steps 41 thru 43). However, this kind oflaunch increases the chances that control of themissile may be lost. [Exceptions: Do not fire TOW2B if PA FAIL occurs.]

Change 13 2-95

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2-33. SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 13 of 36)

2-96 Change 12

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2-33. SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 14 of 36)

Cont inued f rom prev ious page

Change 12 2-97

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2-33. SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 15 of 36)

2-98

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para 3-63

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2-33. SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 16 of 36)

2-99

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(para 3-63).

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2-33. SYSTEM CHECKOUT(Sheet 17 of 36)

PROCEDURE (CONT)

2-100

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para 3-63

T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)

(Sheet 18 o f 36 )

Change 7 2-101

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T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 19 o f 36 )

2-102 Change 8

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para 3-63

T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 20 o f 36 )

Change 8 2-103

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2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 21 of 36)

2 - 1 0 4

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2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 22 o f 36 )

Change 8 2-105

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para 3-63

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2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 23 o f 36 )

2 -106 C h a n g e 8

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2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 24 o f 36 )

Change 8 2 - 1 0 7

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para 3-63

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2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 25 o f 36 )

2 - 1 0 8 C h a n g e 8

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para 2-31

para 3-63

T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 26 o f 36 )

Continued from previous page

Change 8 2-109

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2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 27 of 36)

2 - 1 1 0 Change 8

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T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 28 o f 36 )

Change 8 2-111

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para 3-63

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2 - 3 3 . S Y S T E M C H E C K O U T P R O C E D U R E ( C O N T )

2 - 1 1 2 C h a n g e 8

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2-33. SYSTEM CHECKOUT PROCEDURE (CONT) (SHEET 30 OF 36)

Continued from previous page

STEP 34 NOTE: It is critical that the night sight be focused using the following procedures prior to any TOW missile firing.

a. Remove boresight collimator power cable from night sight connector J4. b. Remove boresight collimator power cable from connector 3J1, put dust covers on cable, and stow in night sight carrying case. c. Holding boresight collimator, release securing latches. d. Slide boresight collimator off of night sight. e. Place boresight collimator into boresight collimator case. f. Close and latch boresight collimator case. g. Stow boresight collimator case. h. Adjust the Night Sight diopter adjustment ring to get a clear focused cross hair. i. Set FOV to NFOV. j. Select a Night target between 300 to 1000 meters. k. Adjust BRT and CTRS full CCW. l. Adjust BRT CW until slight red haze occurs. m. Adjust CTRS CW until image is visible. n. Adjust the range focus knob to a Sharp Focus (adjust CTRS and BRT Controls as necessary).

NOTE: The night sight is now focused for a clear picture and good missile tracking at 300 meters or or greater. For targets less than 300 meters; refocus will be necessary. GO TO NEXT PAGE

Change 13 2-113

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para 3-63

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2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)

(Sheet 31 of 36)

2 - 1 1 4 Change 8

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2-33. SYSTEM CHECKOUT PROCEDURE (CONT) (SHEET 32 OF 36)

Continued from step 11

Under combat conditions with PA FAIL andOSS PASS, the TOW 2 system can still befired using only the day sight tracker forguidance. If limited visibility conditions causehandoff during flight, control of the missile maybe lost. EXCEPTION: Do not fire TOW 2B ifPA FAIL occurs.

NOTE

Change 13 2-115

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para 3-63

TM 9-1425-450-12

2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 33 o f 36 )

2-116 Change 8

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para 3-63

T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 34 o f 36 )

2-117

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2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 35 o f 36 )

2 - 1 1 8

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2 - 3 3 . SYSTEM CHECKOUT PROCEDURE (CONT)(Sheet 36 o f 36 )

Change 8 2-119

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2-34. LOADING ENCASED MISSILE INTO LAUNCH TUBE FOR TRIPOD MOUNTED TOW 2 WEAPON SYSTEM (SHEET 1 OF 8)

PERSONNEL: Two MOS 11H (Soldier A and Soldier B) 1

A. Perform system checkout procedure (para. 2-33).

B. (Soldier A) Stand on left side of TOW 2.

C. Ensure FOV for night sight is set to NFOV.

2

A. (Soldier A) On traversing unit, make sure azimuth lock is in position.

B. (Soldier A) Make sure elevation lock is in LOCKED position.

GO TO NEXT PAGE

2-120 Change 13

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T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 3 4 . LOADING ENCASED MISSILE INTO LAUNCH TUBE FOR TRIPODMOUNTED TOW 2 WEAPON SYSTEM (CONT)(Sheet 2 of 8)

2 -121

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2-34.

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2-122

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2-34. LOADING ENCASED MISSILE INTO LAUNCH TUBE FOR TRIPODMOUNTED TOW 2 WEAPON SYSTEM (CONT)(Sheet 4 of 8)

lf the missile case is punctured or damageddo not attempt to use the encased missile.If missile is damaged it should be be treatedas hazardous materiel and EOD personnelshould be notified for proper disposal.

Use care not to punch a hole in the encased missilediaphragm when forward handling ring is removed.

NOTE

Save forward handling ring and quick releaseclamp to be used again if missile is not fired.

(Soldier B) Pull up on quick release clamp at forwardhandling ring and remove both from encased missile.Ensure o-ring is removed from forward end of encasedmissile.

GO TO NEXT PAGE

Change 12 2-123

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2 - 3 4 . LOADING ENCASED MISSILE INTO LAUNCH TUBE FOR TRIPODMOUNTED TOW 2 WEAPON SYSTEM (CONT)(Sheet 5 o f 8 )

2 - 1 2 4

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2-34. LOADING ENCASED MISSILE INTO LAUNCH TUBE FOR TRIPODMOUNTED TOW 2 WEAPON SYSTEM (CONT)(Sheet 6 of 8)

7

A. (Soldier B) Turn inside portion of protective cover 2 complete turns counterclockwise.

B. (Soldier B) Turn protective cover counterclockwise and remove from electrical connector.Keep protective cover for future use.

C. (Soldier B) Verify rubber o-ring remains inside protective cover and is not affixed to missilelaunch tube on the electrical connector.

GO TO NEXT PAGE

Change 12 2-125

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2 - 3 4 . LOADING ENCASED MISSILEMOUNTED TOW 2 WEAPON(Sheet 7 of 8)

INTO LAUNCH TUBE FOR TRIPODSYSTEM (CONT)

2-126

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2-34. LOADING ENCASED MISSILE INTO LAUNCH TUBE FOR TRIPOD MOUNTED TOW 2 WEAPON SYSTEM (CONT)

(SHEET 8 OF 8)

9

A. (Soldier B) Lower back end of encased missile and make sure that it is placed so that electrical connector will join with bridge clamp.

B. (Soldier B) Lower bridge clamp.

Failure to completely close locking handle could result in a premature wire cut and loss of missile.

C. (Soldier B) While pushing down on bridge clamp, pull bridge clamp locking handle backward and down to lock encased missile in launch tube.

DO NOT raise arming lever until ready to fire at selected target.

END OF TASK

Change 13 2-127

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2-35. PREPARATION TO FIRE MISSILE (SHEET 1 OF 7)

1

A. Load encased missile (see para. 2-34).

B. Visually select the target without using the day sight tracker or night sight.

C. Put elevation lock in UNLOCKED position.

D. Put azimuth lock in UNLOCK position.

the elevation of the launch tube is greater• When than 20 degrees above the horizon, hazards to the gunner and equipment exist.

• Pressure waves from the back blast can injure the gunner and damage the equipment.

GO TO NEXT PAGE

2-128 Change 13

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T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 3 5 . PREPARATION TO FIRE MISSILE (CONT)(Sheet 2 o f 7 )

2 - 1 2 9

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2 - 3 5 . PREPARATION TO FIRE MISSILE (CONT)(Sheet 3 of 7)

2 - 1 3 0 Change 8

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TM 9-1425-450-12

2 - 3 5 . PREPARATION TO FIRE MISSILE (CONT)

(Sheet 4 of 7)

2-131

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2 - 3 5 . PREPARATION TO FIRE MISSILE (CONT)(Sheet 5 of 7)

2-132

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T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 3 5 . PREPARATION TO FIRE MISSILE (CONT)(Sheet 6 of 7)

C h a n g e 4 2-133

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2-35. PREPARATION TO FIRE MISSILE (CONT) (SHEET 7 OF 7)

7

A. On night sight, set FIELD-OF-VIEW selector to WFOV.

B. Select target and adjust RANGE FOCUS, CTRS, and BRT controls as necessary.

C. Place crosshairs on target. D. On night sight, set FIELD-OF-VIEW selector to NFOV.

E. Adjust RANGE FOCUS, CTRS, and BRT controls as necessary. Review para. 2-33, Step 34 k-m.

8

NOTE

The night sight provides for missile tracking during field obscurant (dust, smoke, fog, etc.), or electronic counter-measure conditions. To take advantage of this capability, both the night and day sights must be ON, regardless of which sight is used to acquire the target. Night sight must be in NFOV. DO NOT fire TOW 2B if PA FAIL occurred during self-test.

A. Select the day sight tracker or night sight, whichever gives you the better target image, depending upon battlefield visibility.

B. Turn control knobs to keep crosshairs on center of target.

C. Go to para. 2-36.

END OF TASK

2-134 Change 13

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T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2-36. MISSILE FIRING PROCEDURE(Sheet 1 of 7)

2-135

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2 - 3 6 . MISSILE FIRING PROCEDURE (CONT)(Sheet 2 of 7)

2-136

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2 - 3 6 . MISSILE FIRING PROCEDURE (CONT)(Sheet 3 of 7)

NOTE

T h e f i r i n g p r o c e d u r e i s t h e s a m e w h e n u s i n g t h e d a y s i g h tt racker o r n igh t s igh t .

A . P repare to f i re m iss i le (see para 2 -35) .

B . (So ld ie r A) L ine up the c rossha i rs on the cen te r o f the v i s ib le masso f t h e t a r g e t .

C . (So ld ie r A ) I f the re i s no obs t ruc t ion o r covered a rea a long the expec tedpath of the target and the target is moving 35 Kph or less, go ahead andf i r e , s t a r t i n g a t S t e p 2 .

D . (So ld ie r A ) I f an obs t ruc t ion o r covered a rea appears in your f i e ld o f v iew,d o n ’ t f i r e a t t h e t a r g e t . The missi le might hi t the obstruct ion and neverreach the ta rge t .

2-137

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2 - 3 6 . MISSILE FIRING(Sheet 4 of 7)

PROCEDURE (CONT)

NOTE

When arming lever is raised, encased missile is electrically connected to launcher.

(Soldier B) Raise arming lever.

GO TO NEXT PAGE

2-138

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2 - 3 6 . MISSILE FIRING PROCEDURE (CONT)(Sheet 5 of 7 )

If two unsuccessful firings occur in a row, the launcher shouldnot be fired again.maintenance personnel.

If the missile launch

It should first be checked by support

NOTE

motor does not fire within 1.5 secondsafter the firing trigger is pushed, warn weapon crew of a mis-fire and continue to track the target. Follow the proceduresfor HANGFIRE (see para 2-38).

(Soldier A) When ready to fire, raise trigger cover to expose trigger.

GO TO NEXT PAGE

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2 - 3 6 . MISSILE FIRING PROCEDURE (CONT)(Sheet 6 of 7)

Make sure crew is out of firing danger zones before pressingtrigger.All crew members stay in their firing positions until mis-sile hits target or explodes.Serious injury to personnel could result if crew members arein firing danger zones when missile is fired.

(Soldier A) Push triggerin to fire missile.

GO TO NEXT PAGE

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2 - 3 6 . MISSILE FIRING PROCEDURE (CONT)(Sheet 7 o f 7 )

.

NOTE

Track with smooth motions on the control knobs. Do not makejerky movements.Target may be hidden for a short time during tracking.Continue tracking at the same rate as before losing sight oftarget.When target reappears, it should be close to aiming point.Do not change from night sight to day sight tracker or viceversa after missile has fired.

A. (Soldier A) Turn control knobs to track the target, keeping crosshairs onthe center of the target.

B. (Soldier A) Stop tracking when missile hits the target or explodes.

C. If additional missiles are to be fired go to para 2-42.

D. If no additional missiles are to be fired go to para 2-43.

E. If missile was not fired, go to para 2-43.

F. If missile malfunctions, go to para 2-37. If HMMWV mounted, go to para2-79.1.

END OF TASK

Change 3 2-141

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2-37. MALFUNCTIONS

a. After the missile leaves the launch tube, a DUD or IRREGULAR FLIGHT can occur.

DUD. A dud is when the warhead fails to explode. The warheads of all dudsshould be noted and reported to EOD personnel for disposal. Refer to para 2-40for DUD procedures.

IRREGULAR FLIGHT. An irregular or uncontrolled flight of a missile may occurbecause of any of the following conditions:

Defective missilePoor operator trackingDefective launcher

Refer to para 2-41 for IRREGULAR FLIGHT procedures.

b. FAILURE TO LAUNCH. When the missile fails to leave the launch tube after thenormal 1.5 second delay after pressing the trigger, either a FAILURE TO LAUNCH -HANGFIRE or a FAILURE TO LAUNCH - MISFIRE condition exists.

FAILURE TO LAUNCH - HANGFIRE. After the trigger is pressed, usuallythe distinctive impulse of the squibs firing to activate the missile batteriesand gyro and the gyro spin noise can be heard. When the missile fails tolaunch and these prefire functions ARE heard, the condition is FAILURE TOLAUNCH - HANGFIRE. Refer to para 2-38 for FAILURE TO LAUNCH - HANGFIREprocedures,

FAILURE TO LAUNCH - MISFIRE. When the missile fails to launch and theseprefire functions are NOT heard, the condition is FAILURE TO LAUNCH -MISFIRE. Refer to para 2-39 for FAILURE TO LAUNCH - MISFIRE procedures.

2-38. FAILURE TO LAUNCH - HANGFIRE PROCEDURES(Sheet 1 of 4)

NOTE

For HMMWV hangfire procedures, refer to para 2-79.1.

The crew must exercise extreme care to avoid injury from a delayedmissile launch. A delayed launch usually occurs within one minute.However, it could occur as long as 30 minutes after pressing thetrigger.

Keep all personnel out of forward and aft danger zones (see para 2-34).

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2-38. FAILURE TO LAUNCH - HANGFIRE PROCEDURES (CONT)(Sheet 2 of 4)

Training/Testing Combat

A. Alert crew by stating HANGFIRE A. Alert crew by stating HANGFIREand continue to track target and continue to track targetfor one minute. for one minute.

A HANGFIRE missile must not be returned to theamunition supply point. Notify Explosive OrdnanceDisposal Detachment in accordance with unit standardoperating procedures.

B. If missile fails to launch after B. If missile fails to launch afterone minute, lower arming lever. one minute, lower arming lever.

C. Place elevation lock in LOCKED C. Place elevation lock in LOCKEDposition. position.

D. Place azimuth lock in LOCKED D. Place azimuth lock in LOCKEDposition. position.

E. Wait 30 minutes.

GO TO NEXT PAGE

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2-38. FAILURE TO LAUNCH - HANGFIRE PROCEDURES (CONT)(Sheet 3 of 4)

If the launcher is mounted on a vehicle, and the vehicleis not positioned with its front or rear in line withthe target, it must be repositioned such that eitherthe front or rear of the vehicle is in line with thetarget. The weapons station must be rotated duringvehicle repositioning movement such that the forwardend of the missile is pointing toward the target atall times.

Training/Testing Combat

A. Open bridge clamp. A. Open bridge clamp.

B. Remove missile from launch B. Remove missile from launch

tube. Keep missile pointed tube. Keep missile pointeddownrange at all times. downrange at all times.

GO TO NEXT PAGE

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2-38. FAILURE TO LAUNCH - HANGFIRE PROCEDURES (CONT) (SHEET 4 OF 4)

3

Training/Testing Combat

A. In vehicle modes only: Hand missile over side of vehicle to another crew member.

A. In vehicle modes only: Hand missile over side of vehicle to another crew member.

B. Keeping missile pointed down-range, carry it to dud pit. If there is no dud pit, place missile on ground at least 200 meters from launcher.

B. Keeping missile pointed down-range, carry it to dud pit. If there is no dud pit, place missile on ground at a safe distance from launcher.

C. Notify EOD personnel. C. Notify EOD personnel.

If the launcher is mounted on a vehicle, do not hand off amalfunctioned missile to the front or rear of the vehicle.A malfunctioned missile must be handed off from thelauncher to either the left or right side of the vehicle.Missile must remain pointed toward the target at alltimes.

END OF TASK

Change 13 2-144.1

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2-39. FAILURE TO LAUNCH - MISFIRE PROCEDURES(Sheet 1 of 5)

NOTE

For HMMWV misfire procedures, refer to para 2-79.2.

The crew must exercise extreme care to avoid injury from adelayed missile launch. A delayed launch usually occurswithin one minute. However, it could occur as long as30 minutes after pressing the trigger.

Keep all personnel out of forward and aft danger zones(see para 2-34).

Training/Testing Combat

A. Alert crew by stating MISFIRE. A. Alert crew by stating MISFIRE.

B. Continue to track target for 1 B. Continue to track target for 1minute and press trigger again. minute and press trigger again.

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2-39. FAILURE TO LAUNCH - MISFIRE PROCEDURES (CONT)(sheet 2 of 5)

Training/Testing Combat

A. Do missile guidance set self A. Do missile guidance set selftest for battery. If battery test for battery. If batteryfails, replace battery. fails, replace battery.(In vehicle mode, check power (In vehicle mode, check powerconditioner ON/OFF switch and conditioner ON/OFF switch andcable connections.) cable connections.)

B. On missile guidance set, make B. On missile guidance set, makesure coil cord connector is sure coil cord connector isproperly attached to connector properly attached to connectorJ1. Turn coil cord connector J1. Turn coil cord connectorlocknut clockwise until tight locknut clockwise until tightto make sure that coil cord to make sure that coil cordconnector is locked in place. connector is locked in place.

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2 -39 . FAILURE TO LAUNCH - MISFIRE PROCEDURES (CONT)(Sheet 3 of 5)

Training/Testing Combat

A. Insure bridge clamp locking A. Insure bridge clamp lockinghandle is properly seated. handle is properly seated.

B. Lower arming lever. B. Lower arming lever.

C. Check backblast area. C. Check backblast area.

D. Raise arming lever. D. Raise arming lever.

E. Press trigger. E. Press trigger.

F. If missile still fails to F. If missile still fails tolaunch, continue tracking launch, continue trackingtarget for one minute. target for one minute.

G. Lower arming lever. G. Close trigger cover.

H. Close trigger cover. H. Place elevation lock in LOCKED

I. Place elevation lock in LOCKEDposition.

position. I. Place azimuth lock in LOCKED

J. Place azimuth lock in LOCKEDposition.

position.

K. Wait 30 minutes.GO TO NEXT PAGE

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2-39. FAILURE TO LAUNCH - MISFIRE PROCEDURES(Sheet 4 of 5)

TM 9-1425-450-12

(CONT)

Training/Testing

A. Open bridge clamp.

B. Remove missile from launchtube. Keep missile pointeddownrange at all times.

A.

B.

Combat

Open bridge clamp.

Remove missile from launchtube. Keep missile pointeddownrange at all times.

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2-39. FAILURE TO LAUNCH - MISFIRE PROCEDURES (SHEET 5 OF 5)

3

Training/Testing Combat

A. In vehicle modes only: Hand missile over side of vehicle to another crew member.

A. In vehicle modes only: Hand missile over side of vehicle to another crew member.

B. Keeping missile pointed down-range, carry it to dud pit. If there is no dud pit, place missile on ground at least 200 meters from launcher.

B. Keeping missile pointed down-range, carry it to dud pit. If there is no dud pit, place missile on ground at a safe distance from launcher.

C. Notify EOD personnel. C. Notify EOD personnel.

END OF TASK

If the launcher is mounted on a vehicle, do not hand off amalfunctioned missile to the front or rear of the vehicle. A malfunctioned missile must be handed off from thelauncher to either the left or right side of the vehicle.Missile must remain pointed toward the target at alltimes.

2-144.6 Change 13

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2 - 4 0 . DUD

If the warhead fails to explode, then the missile is a dud.All duds must be thought of as armed and very dangerous.Report the location of all duds to Explosive Ordnance Dis-posal (EOD) personnel.

4

A. Remove empty missile case from launch tube (see para 2-43).

B. Tell EOD personnel the location of all duds.

END OF TASK

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2 - 4 1 . IRREGULAR FLIGHT

NOTE

An irregular or out-of-control missile can be caused by:

Bad missileBad launcherVery poor operator tracking.

Report all missile problems as required by AR 75-1 and AR 702-5.

END OF TASK

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2 - 4 2 . ACTION AFTER FIRING WITH ADDITIONAL MISSILESTO BE FIRED(Sheet 1 o f 5 )

PERSONNEL: Two MOS llH (Soldier A and Soldier B)

Do not press trigger with empty missile case in launch tube.Possible shorts can result, damaging the prefire, fire, andwirecutter circuits.

(Soldier A) After missile has ended flight, lower trigger cover overtrigger.

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2 - 4 2 . ACTION AFTER FIRING WITH ADDITIONAL MISSILESTO BE FIRED (CONT)(Sheet 2 of 5)

A. (Soldier A) On traversing unit, put azimuth lock in LOCK position.

B. (Soldier A) Turn traversing unit from side to side until it locksin place.

C. (Soldier A) Put elevation lock in LOCKED position.

D. (Soldier B) Tilt trunnion until launch tube is locked in down position.

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2 - 4 2 . ACTION AFTER FIRING WITH ADDITIONAL MISSILESTO BE FIRED (CONT)(Sheet 3 of 5)

NOTE

Do not lower arming lever to safe position before openingbridge clamp. Command - link wires will not be cut if arm-ing lever is lowered before bridge clamp is opened.

Opening the bridge clamp does the following:

Cuts command-link wires.Forces arming lever down to electrically disconnectlauncher from empty missile case.turns launcher off.

(Soldier B) Pull up on bridge clamp locking handle and open bridgeclamp.

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2 - 4 2 . ACTION AFTER FIRINGTO BE FIRED (CONT)(Sheet 4 of 5)

WITH ADDITIONAL MISSILES

A.

B.

(Soldier B) Remove empty missile case from launch tube.

(Soldier B) Dispose of empty missile case in accordancewith unit standard operating procedure.

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2 - 4 2 . ACTION AFTER FIRING WITH ADDITIONAL MISSILESTO BE FIRED (CONT)(Sheet 5 of 5)

Be careful when pulling command-link wires out of launch tube.The command-link wires are very small and strong and can causeinjury if handled wrong.

A. (Soldier B) Check launch tube to see if command-linkinside of tube. If they are, pull command-link wiresof launch tube.

B. (Soldier B) Load another encased missile.

wires are caughtout from front

END OF TASK

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2 - 4 3 . REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE(Sheet 1 of 8)

PERSONNEL: Two MOS llH (Soldier A and Soldier B)

Do not press trigger with empty missile case in launch tube.Possible shorts can result, damaging the prefire, fire, andwirecutter circuits.

(Soldier A) After missile has ended flight, lower trigger cover overtrigger.

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(Sheet 2 o f 8 )2 - 4 3 . REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT)

A. (Soldier A) On traversing unit, put azimuth lock in LOCK position.

B. (Soldier A) Turn traversing unit from side to side until it locksin place.

C. (Soldier A) Put elevation lock in LOCKED position.

D. (Soldier B) Tilt trunnion until launch tube is locked in down position.

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2-43. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT) (SHEET 3 OF 8)

If missile was not fired, lower arming lever before openingbridge clamp. This will prevent the command link wire frombeing cut under any situation.

3

(Soldier B) If missile was not fired, lower arming lever.

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(Sheet 4 o f 8 )2 - 4 3 . REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT)

NOTE

If missile was fired, do not lower arming lever to safeposition before opening bridge clamp. Command-linkwires will not be cut if arming lever is lowered beforebridge clamp is opened.

Opening the bridge clamp does the following:

Cuts command-link wires.Forces arming lever down to electrically disconnectlauncher from empty missile case.Turns launcher off.

(Soldier B) Pull upon bridge clampclamp.

locking handle and open bridge

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2-43. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT) (SHEET 5 OF 8)

5

A. (Soldier B) Remove encased missile or empty missile case from launch tube.

B. (Soldier B) If missile case is empty, dispose of it in accordance with unit standard operating procedure. Go to step 8.

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2-43. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT) (SHEET 6 OF 8)

6

On encased missile:

A. (Soldier B) Inspect umbilical electrical connector to determine if it is stuck in the depressed position. If this is stuck in the depressed position, notify EOD personnel. Do not transmit radio frequencies within 150 feet of ammunition.

B. (Soldier B) Position protective cover on electrical connector so that grooves on protective cover line up with notches on electrical connector. Turn protective cover clockwise to secure it in place.

C. (Soldier B) Turn inside portion of protective cover fully clockwise to lock.

Injury or death to personnel may occur if theumbilical plunger does not return to the upposition. (Plunger should be flush with the rim).

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2-43. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT) (SHEET 7 OF 8)

7

A. (Soldier B) Replace quick release clamp, preformed packing and forward handling ring on encased missile.

B. (Soldier B) Push down on quick release clamp to secure forward handling ring.

C. (Soldier B) If missile will not be fired within a short time, tag the missile with the date it was initially prepared for firing.

D. (Soldier B) Put encased missile in stowed position (see para. 2-75 for HMMWV).

END OF TASK

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2 - 4 3 . REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT)(Sheet 8 o f 8 )

NOTE

Do the following step only if empty missilecase was removed.

Be careful when pulling command-link wires out of launchtube.The command-link wires are very small and strong and cancause injury if handled wrong.

A. (Soldier B) Pull command-link wires out from front of launch tube.

B. (Soldier B) Check inside rear of launch tube for dirt. If dirty, cleanwith clean cloth.

END OF TASK

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2-44. DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL(Sheet 1 of 15)

PERSONNEL: Four MOS llH (Soldier A, Soldier B, Soldier C, and Soldier D)

A. Make sure that encased missile or empty missile case has been unloaded fromTOW 2 Weapon System (see para 2-43).

B. (Soldier A) Set ON/OFF/STBY switch to OFF.

C. (Soldier A) Set battery power conditioner circuit breaker to OFF.

D. (Soldier A) Disconnect battery power conditioner cable from night sightand battery power conditioner.

E. (Soldier A) Stow cable in battery power conditioner case lid.

F. (Soldier A) Close battery power conditioner lid and secure latch.

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2 - 4 4 . DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)(Sheet 2 o f 15 )

A.

B.

C.

D.

E.

F.

Do not handle or lift night sight by lens cover.A loose lens cover latch could result inequipment damage if night sight is dropped.

(Soldier A) Place front lens cover onnight sight and secure with two latches.

(Soldier A) Turn diopter adjustment ring to full clockwise position onnight sight.

(Soldier A) On night sight, turn postamplifier cable connector lock ringcounterclockwise.

(Soldier A) Pul 1 straight out on postamplifier cable connector to removefrom night sight.

(Soldier A) Insert postamplifier cable connector into cable retainer ontraversing unit.

(Soldier A) On night sight, install protective cap on postamplifier cableconnector.

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2 - 4 4 . DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)(Sheet 3 o f 15 )

A. (Soldier A) Support the night sight securely.

B. (Soldier A) Move latch handle all the way back to unlock position.

(Soldier A) Remove night sight from mounting on day sight tracker.

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2 - 4 4 . DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)(Sheet 4 o f 15 )

A. (Soldier B) Open two latches on night sight field handling case.

B. (Soldier B) Open night sight field handling case.

C. (Soldier A) Place night sight in night sight field handling case inupside-down position.

D. (Soldier A) Close and secure night sight field handling case.

(Soldier A) On day sight tracker, check optical surfaces forcleanliness. Clean optical surfaces if dirty (see para 2-20).

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2-44. DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT) (SHEET 10 OF 15)

7

(Soldier A) On day sight tracker, make sure that boresight elevation cover and boresight azimuth cover are closed firmly and are not broken. Turn eyepiece fully CCW.

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(Sheet 6 o f 15 )2 - 4 4 . DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)

Before operating the latch assembly make sure day sighttracker is well supported on traversing unit and will notfall .Do not carry or lift the day sight tracker by the latchhandle.

A. (Soldier A) Put arm underneath day sight tracker and hold day sight trackerfirmly.

B. (Soldier A) Pull and hold latch in toward latch handle.

C. (Soldier A) Push latch handle toward traversing unit. Release latch.

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2 - 4 4 . DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)(Sheet 7 o f 15 )

When the day sight tracker is set aside or stored make surethe latch handle is closed.

(Soldier A) Carefully lift day sight tracker off traversing unit and place inshroud bag.

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2 - 4 4 . DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)(Sheet 8 Of 15)

NOTE

Make sure coil cable connectordoes not touch the groundonce it is removed.If dirt becomes lodged inthe coil cable connector,it may be impossible toget a good connection thenext time the coil cableis connected to the missileguidance set.

A. (Soldier B) Pull missile guidance set out from under tripod.

B. (Soldier B) On missile guidance set, turn coil cable connector locking nutin direction of arrow until threads are no longer attached.

C. (Soldier B) Pull straight up on coil cable connector to remove it frommissile guidance set.

A. (Soldier B) Insert catch strikes on cover into bow handles at rear ofmissile guidance set.

B. (Soldier B) Close cover.

C. (Soldier B) Close latches.

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2 - 4 4 . DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)(Sheet 9 o f 15 )

(Soldier B) On traversing unit, pull up on rear of launch tube latch.

A. (Soldier B) Lift the launch tube pins out of the launch tube brackets toremove launch tube from traversing unit.

B. (Soldier B) Make sure inside of launch tube is clean.

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2 - 4 4 . DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)(Sheet 10 o f 15 )

(Soldier C) Pull out coupling clamp handle to release traversing unitfrom tripod.

A. (Soldier C) Lift traversing unit off tripod.

B. (Soldier B) Place coil cable in bottom of traversing unit by winding coilcable and pushing up at the same time.

C. (Soldier A) Close coupling clamp handle.

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2-44. DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT) (SHEET 11 OF 15)

16

(Soldier A) Release tripod legs by turning leg lock handles upward.

17

NOTE

Tripod legs close automatically when tripod is lifted off the ground.

(Soldier A) Grasp top of tripod and lift tripod off the ground.

18

A. Inspect, clean, and stow weapon system in vehicle if available.

B. If weapon system is to be carried by foot, do steps 19 through 26.

C. If weapon system is to be loaded into HMMWV, go to para. 2-74.

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2 - 4 4 . DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)(Sheet 12 o f 15 )

(Soldier A) Carry tripod and day sight tracker.

(Soldier B) Carry missile guidance set and launch tube.

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2-44. DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)(Sheet 13 o f 15 )

(Soldier C) Carry traversing unit.

(Soldier D) Carry encased missile.

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2 - 4 4 . DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)(Sheet 14 o f 15 )

(Any available crew member) Carry night sight in field handling case withstraps.

(Any available crew member) Carry boresight COll imator in field handlingcase with straps.

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2 - 1 7 3

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2 - 4 4 . DISASSEMBLY OF TRIPOD MOUNTED LAUNCHER FOR TRAVEL (CONT)(Sheet 15 of 15)

2 - 1 7 4

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Section V. DELETED

All data on pages 2-177 through 2-346 deleted.

Change 13 2-175/(2-176 blank)

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Section VII. DEPLOYMENT OF HIGH MOBILITY MULTIPURPOSE WHEELED

VEHICLE (HMMWV)

SECTION CONTENTS PARA PAGE

SCOPE 2-73 2-347

INSTALLATION OF TOW 2 LAUNCHER SYSTEM ON HMMWV 2-74 2-348

LOADING ENCASED MISSILES ONTO HMMWV 2-75 2-358

PREPARATION FOR OPERATION OF TOW 2 SYSTEM IN HMMWV 2-76 2-368

SELECTION OF SITE FOR HMMWV MOUNTED TOW 2 WEAPON SYSTEM

2-77 2-393

FIRING ANGLE LIMITATIONS ON HMMWV 2-78 2-395

LOADING ENCASED MISSILE INTO LAUNCH TUBE ON HMMWV 2-79 2-396.1

PREPARATION TO FIRE MISSILE 2-79.01 2-408

MISSILE FIRING PROCEDURE 2-79.02 2-408.7

FAILURE TO LAUNCH - HANGFIRE PROCEDURES 2-79.1 2-409

FAILURE TO LAUNCH - MISFIRE PROCEDURES 2-79.2 2-408.5

DELETED 2-80 2-408.10

PREPARATION OF HMMWV FOR TRAVEL 2-81 2-411

REMOVAL OF LAUNCHER SYSTEM FROM HMMWV 2-82 2-434

REMOVAL OF ENCASED MISSILES FROM HMMWV 2-83 2-444

ADJUSTMENT OF GUNNER'S PLATFORM 2-84 2-452

OPERATION OF WEAPONS RING 2-85 2-456

2-73. SCOPE

This section tells the crew how to set up and operate the TOW 2 Weapon System on the HMMWV. The procedures for loading and removing encased missiles on the HMMWV are also covered. System checkout, preparation to fire, and firing procedures are the same as those for tripod mounted launcher deployment.

Change 13 2-347

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2 - 7 4 . INSTALLATION OF TOW 2 LAUNCHER SYSTEM OF HMMWV(Sheet 1 o f 10 )

2-348 Change 5

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WARNING

TM 9-1425-450-12

2 - 7 4 . INSTALLATION OF TOW 2 LAUNCHER SYSTEM OF HMMWV (CONT)(Sheet 2 o f 10 )

Never open one end of cargo/loader’s doorwithout first insuring that opposite endis securely closed. Not doing so willcause both ends to open at same timecausing injury to personnel, damage toequipment, or mission abort.

From rear of vehicle, raise cargo/loader’s door and lower tailgateall the way down (TM 9-2320-280-10).

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2 - 7 4 . INSTALLATION OF TOW 2 LAUNCHER SYSTEM OF HMMWV (CONT)(Sheet 3 o f 10 )

A. Install two MGS battery assemblies in battery racks and securewith wing nuts.

B. Install power conditioner in missile guidance set (see para 3-8).

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(Sheet 4 o f 10 )2 - 7 4 . INSTALLATION OF TOW 2 LAUNCHER SYSTEM OF HMMWV (CONT)

A.

B.

C.

Install traversing unit on traversing unit adapter and secure withcoupling clamp.

Install elevation/depression limiter assembly to traversing unit andsecure with screw.

Turn traversing unit so bridge clamp locking handle is facing cargo door.

Change 2 2-351

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2 - 7 4 . INSTALLATION OF TOW 2 LAUNCHER SYSTEM OF HMMWV (CONT)(Sheet 5 o f 10 )

A. Install boresight collimator and secure with two straps,

B. Install night sight and secure with two straps.

Make sure day sight tracker is inside shroud bag, then install andsecure with two straps.

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2 - 7 4 . INSTALLATION OF TOW 2 LAUNCHER SYSTEM OF HMMWV (CONT)(Sheet 6 o f 10 )

A. Install spare battery pack and secure with strap.

B. Install night sight battery power conditioner and secure with strap.

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2-74 . INSTALLATION OF TOW 2 LAUNCHER(Sheet 7 o f 10 )

A.

B.

C.

D.

Install

Install

Close

Close

SYSTEM OF HMMWV (CONT)

launch tube on cargo/loader’s door and secure with strap.

tripod and secure with coupling clamp and one strap.

and secure tailgate.

cargo/loader’s door.

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WARNING

TM 9-1425-450-12

2 - 7 4 . INSTALLATION OF TOW 2 LAUNCHER SYSTEM OF HMMWV (CONT)(Sheet 8 o f 10 )

Never open one end of cargo/loader’s doorwithout first insuring that opposite endis securely closed. Not doing so willcause both ends to open at same timecausing injury to personnel, damage toequipment, or mission abort.

Using forward latch, unlatch and raise cargo/loader’s door(TM 9-2320-280-10).

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2 - 7 4 . INSTALLATION OF TOW 2 LAUNCHER(Sheet 9 o f 10 )

SYSTEM OF HMMWV (CONT)

A. Install M13 decontamination kit and secure with strap.

B. Close cargo/loader’s door.

Release two fasteners behind back cushion of gunner’s seatand remove gunner’s seat back rest.

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2 - 7 4 . INSTALLATION OF TOW 2 LAUNCHER

TM 9-1425-450-12

S Y S T E M O F HMMWV (CONT)(Sheet 10 o f 10 )

Slide water can (on edge) into place and secure with strap.

A. Reinstall gunner’s seat back rest and secure with two fasteners.

B. Load encased missiles in missile rack (see para 2-75).

END OF TASKChange 2 2-357

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WARNING

TM 9-1425-450-12

2 - 7 5 . LOADING ENCASED MISSILES ONTO HMMWV(Sheet 1 o f 10 )

PERSONNEL: Two MOS 11H

Never open one end of cargo/loader’s doorwithout first insuring that opposite endis securely closed. Not doing so willcause both ends to open at same timecausing injury to personnel, damage toequipment, or mission abort.

A. From rear of vehicle, raise cargo/loader’s door and lower tailgateall the way down (TM 9-2320-280-10).

B. Unlatch coupling clamp and strap securing tripod and remove tripod fromvehicle.

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2 - 7 5 . LOADING ENCASED MISSILES ONTO HMMWV (CONT)(Sheet 2 o f 10 )

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2 - 7 5 . LOADING ENCASED MISSILES ONTO HMMWV (CONT)(Sheet 3 o f 10)

Unlatch two latches (TM 9-2320-280-10) securing 3rd tier of missile rackand allow 3rd tier to rise.

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2 - 7 5 . LOADING ENCASED MISSILES ONTO HMMWV (CONT)(Sheet 4 o f 10 )

A. Fold down 3rd tier support brace.

B. Unlatch two latches securing 2nd tier of missile rack and allow2nd tier to rise.

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WARNING

TM 9-1425-450-12

2 - 7 5 . LOADING ENCASED MISSILES ONTO HMMWV (CONT)(Sheet 5 o f 10 )

Two soldiers are required to installa missile in missile rack.

Do not drop encased missile. Handling rings or launch con-tainer may be bent or damaged.

Do not break diaphragm on end of encased missile. If watergets into launch container, missile can be damaged.

Do not dispose of bad missiles. If encased missile isdamaged or handling rings badly bent, return encased missileto ammunition unit for inspection.

NOTE

Perform this step for all missiles as theyare loaded.

Check diaphragm for breaks.

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CAUTION

TM 9-1425-450-12

2 - 7 5 . LOADING ENCASED MISSILES ONTO HMMWV (CONT)(Sheet 6 o f 10 )

All missiles must be loaded in the rack nose endforward, with retaining band of rear couplingclamp seated in rear resting pad groove. Missilesmust be rotated so coupling clamps are free ofresting pads and electrical connectors are neartop of missile. Improper loading of missilesmay cause damage to missile rack, resulting inmission abort.

A. Load Missile 6, then missile 5, in missile rack.

B. Lower 2nd tier and secure with two latches on support brace.

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2 - 7 5 . LOADING ENCASED MISSILES ONTO HMMWV (CONT)(Sheet 7 o f 10 )

A. Load missile 4 in missile rack.

B. Raise 3rd tier support brace.

C. Load missile 3 in missile rack.

D. Lower 3rd tier and secure with two latches.

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2 - 7 5 . LOADING ENCASED MISSILES ONTO HMMWV (CONT)(Sheet 8 o f 10 )

A. Load missile 2 in missile rack and secure with two straps.

B. Load missile 1 in missile rack and secure with two straps.

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2 - 7 5 . LOADING ENCASED MISSILES ONTO HMMWV (CONT)(Sheet 9 o f 10 )

Place day sight tracker in stowage bracket and secure with two straps.

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2 - 7 5 . LOADING ENCASED MISSILES ONTO HMMWV (CONT)(Sheet 10 o f 10 )

A. Load tripod behind missile rack and secure with coupling clamp and strap.

B. Close and secure tailgate.

C. Close cargo/loader’s door.

END OF TASK

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2 - 7 6 . P R E P A R A T I O N F O R O P E R A T I O N O F T o w 2 L A U N C H E RS Y S T E M I N H M M W V ( S h e e t 1 o f 2 5 )

PERSONNEL: Four MOS 11H (Driver, Squad Leader, Gunner, Loader) TOOL: 3/16 inch socket head screw key

A. (Gunner) Unlatch rear retaining strap securing missile guidance setto gunner’s platform.

B. (Driver) Unlatch forward retaining strap securing missile guidanceset to gunner’s platform.

C. (Gunner) Release two latches to remove missile guidance set cover andhand cover to squad leader.

D. (Squad Leader) Stow missile guidance set cover in squad leader’sfootwell.

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para 3-8

TM 9-1425-450-12

2 - 7 6 . P R E P A R A T I O N F O R O P E R A T I O N O F T O W 2 L A U N C H E R S Y S T E MI N H M M W V ( S h e e t 2 o f 2 5 )

A.

B.

(Gunner) Release three latches securing hatch cover to hatch.

(Gunner) Grab hatch cover handle, open hatch, and enter weapon station.

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C h a n g e 4 2-369

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2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (CONT) (Sheet 3 o f 25)

A. (Gunner) Secure hatch cover to weapons station with two securing handles.

B. (Gunner) Rotate weapon station so gunner’s back rest is toward rear ofvehicle (see para 2-85).

C. (Gunner) Lift missile guidance set from gunner’s platform to weaponstation missile guidance set bracket, with power conditioner away fromgunner’s hatch, and secure with four retaining latches.

D. (Gunner) Make sure gunner’s platform is set to correct height toaccommodate you (see para 2-84).

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2 - 7 6 . PREPARATION FORIN HMMWV (CONT)

OPERATION OF TOW 2 LAUNCHER(Sheet 4 o f 25 )

S Y S T E M

(Gunner) Release latch securing launcher mountfrom launcher mount, and secure cover open with

cover, open cover awaylatch.

(Loader) Release lower coupling clampstowage base.

securing traversing unit adapter to

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2-76.

TM 9-1425-450-12

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2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (CONT) (Sheet 6 of 25)

A. (Gunner) Place azimuth lock in LOCK position.

B. (Gunner) Turn traversing unit from side to side until it locks in place.

C. (Gunner) Pull top coupling clamp handle out.

D. (Gunner) Turn traversing unit so azimuth lock points toward rear ofvehicle.

E. (Gunner) Push coupling clamp handle in.

F. (Gunner) Make sure coupling clamp is correctly adjusted and fastened byattempting to turn the traversing unit.

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2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (CONT) (Sheet 7 of 25)

A. (Gunner) Make sure that elevation lock on traversing unit is in LOCKEDposition.

B. (Gunner) Turn control knobs forward until trunnion clicks and locks inplace.

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2-76. PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (CONT) (Sheet 8 of 25)

Never open one end of cargo/loader’s doorwithout first insuring that opposite endis securely closed. Not doing so willcause both ends to open at same timecausing injury to personnel, damage toequipment, or mission abort.

(Loader) Release cargo/loader’s door using forward latch and raisecargo/loader’s door (TM 9-2320-280-10).

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2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEM)( IN HMMWV (CONT) (Sheet 9 o f 25 )

(Gunner) Working from inside vehicle, reach up and pull coil cablefrom traversing unit and extend coil cable.

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2 - 7 6 . PREPARATION FORIN HMMWV (CONT)

TM 9-1425-450-12

OPERATION OF TOW 2 LAUNCHER SYSTEM(Sheet 10 o f 25 )

Be sure there is no dirt or foreignmatter in end of coil cable connec-tor attached to traversing unit.Dirt can cause connector not to makegood contact with missile guidanceset.

Poor contact can result in poor sys-tem operation.

Do not apply downward pressureon coil cable connector. Thiscan cause misalinement andbent pins.

A. (Gunner) On coil cable con-nector, line up yellowcolored index line withyellow colored mating linenext to connector J1 onmissile guidance set.

B. (Gunner) Turn locking nut indirection of arrow until redmark on J1 connector cannotbe seen.

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2 - 7 6 . PREPARATION FOR S Y S T E M

IN HMMWV (CONT)

OPERATION OF TOW 2 LAUNCHER(Sheet 11 o f 25 )

(Loader) Unlatch strap securing launch tube to cargo/hand launch tube to gunner.

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loader’s door and

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2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (cONT) (sheet 12 o f 25 )

A. (Gunner) Make sure opening in launch tube is up.

B. (Gunner) Lift up launch tube latch.

C. (Gunner) Put launch tube on traversing unit by sliding index pins intobrackets in traversing unit.

A. (Gunner) Line up locating pin on traversing unit with mating hole inlaunch tube.

B. (Gunner) Place launch tube latch in launch tube catch.

C. (Gunner) Press down on launch tube latch until it latches.

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2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (CONT) (Sheet 13 of 25)

A. (Loader) Unlatch two straps securing day sight tracker to stowagebracket.

Handle day sight tracker very carefully. Itcan be easily damaged.

Do not carry or lift the day sight tracker bythe latch handle. Always lift and carry itat mounting holes.

B. (Loader) Remove day sight tracker from shroud bag.

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2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (CONT) (Sheet 14 of 25)

A. (Loader) While squeezing latch, push latch handle all the wayclown . Release latch.

B. (Loader) Hand day sight tracker to gunner,

C. (Gunner) Hold day sight tracker with tracker hook mount in 1 ine withtraversing unit boresight plate.

A. (Gunner) Tilt top of daysight tracker slightlytoward traversing unit.

B. (Gunner) Guide trackerhook mount of day sighttracker over tip oftraversing unitboresight plate.

Change 2 2-381

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2 - 7 6 . PREPARATION FORIN HMMWV (CONT)

OPERATION OF TOW 2 LAUNCHER SYSTEM(Sheet 15 o f 25 )

A. (Gunner) Join day sight tracker index plate groove with traversing unitboresight guide.

B. (Gunner) Pull latch handle all the way up until it locks in place.

C. (Gunner) Make sure day sight tracker is securely mounted to traversingunit before letting go.

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2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (CONT) (Sheet 16 o f 25)

A. (Gunner) On day sight tracker, make sure that RETICLE LIGHT switch isset to OFF.

B. (Gunner) Check humidity indicator to be sure that 30 percent section isblue. If 30 percent section is pink or white, notify support maintenance.

(Gunner) Make sure lens assembly on day sight tracker is clean.

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2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (CONT) (Sheet 17 of 25)

A. (Loader) Unlatch two straps and remove night sight field handling case.

B. (Loader) Open night sight field handling case and remove night sightfrom case.

C. (Loader) Remove postamplifier cable connector cap from night sight andstow in night sight field handling case.

D. (Loader) Hand night sight to gunner and set night sight fieldhandling case back on shelf.

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2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHERIN HMMWV (CONT) (Sheet 18 of 25)

TM 9-1425-450-12

S Y S T E M

A. (Gunner) Place coarse azimuth knob in position No. 1 (forward position).

B. (Gunner) Move latch handle toward rear of night sight (in directionarrow) to unlock position.

of

A. (Gunner)for forei

B. (Gunner)tracker.

Check locating “Vee Ways” on night sight and day sight trackergn material. Clean if necessary with wiping-rag.

Line up keyed hole on night sight with cam post on day sight

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2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (CONT) (Sheet 19 of 25)

A. (Gunner) Place night sight on day sight tracker with night sight lensfacing forward.

B. (Gunner) Make sure night sight seats securely on day sight tracker.

C. (Gunner) Using your right hand, move latch handle toward front of nightsight (in direction of arrow) to lock in place. Make sure night sightis securely mounted to day sight tracker before letting go.

D. (Gunner) Remove postamplifier cable connector from cable retainer ontraversing unit.

Keep postamplifier cable clear of bridge clamp.

E. (Gunner) Aline yellow mark on postamplifier cable connector with yellowmark on night sight.

F. (Gunner) Push in on postamplifier cable connector and turn clockwiseuntil postamplifier cable connector stops.

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2-76 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (CONT) (Sheet 20 of 25)

(Squad Leader) Remove TVPC power cable from under

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loader’s seat.

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2 - 7 6 . PREPARATION FORIN HMMWV (CONT)

OPERATION OF TOW 2 LAUNCHER SYSTEM(Sheet 21 o f 25 )

A. (Squad Leader) Connect connector P2 of TVPC power cable topower conditioner cable.

B. (Squad Leader) Uncoil power conditioner cable from cable bracketand hand up to gunner.

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OPERATION OF TOW 2 LAUNCHER SYSTEM(Sheet 22 o f 25 )

2 - 7 6 . P R E P A R A T I O N F O RIN HMMWV (CONT)

A. (Gunner) Line up TVPC power cable connector P1 with connector J1 onpower conditioner.

B. (Gunner) Push down on TVPC power cable connector P1 and turn lockingnut clockwise.

(Squad Leader) Uncoil night sight power cable 2W2 from cablehand connector up to gunner.

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bracket and

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2-76 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEMIN HMMWV (CONT) (Sheet 23 o f 25)

(Squad Leader) On night sight vehicle power conditioner, make sureON/OFF switch is set to OFF.

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IN HMMWV (CONT) (Sheet 24 o f 25)2 - 7 6 . PREPARATION FOR OPERATION OF TOW 2 LAUNCHER SYSTEM

A. (Gunner) On night sight, make sure ON/OFF/STBY switch is set to OFF.

B. (Gunner) Remove protective caps from night sight. power cable and nightsight connector J1.

C. (Gunner) Connect night sight power cable 2W2 to night sight input powerconnector J1.

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Change 2 2-391

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2 - 7 6 . PREPARATION FORIN HMMWV (CONT)

OPERATION OF TOW 2 LAUNCHER SYSTEM(Sheet 25 o f 25 )

(Squad Leader) Make sure both cables are connected to night sight vehiclepower conditioner and set ON/OFF switch to ON.

At the beginning of each operating day, do system checkout procedure(para 2-33).

END OF TASK

2 - 3 9 2 Change 2

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2 - 7 7 . SELECTION OF SITE FOR HMMWV MOUNTED TOW 2 WEAPON SYSTEM(Sheet 1 of 2)

If up/down slope at launch site is greater than 30 degrees(300), injury to personnel and damage to equipment mayoccur when missile is fired.

Install TOW 2 launcher in HMMWV (see para 2-76).

If back blast area is not clear, injuryto personnel and damage to equipmentmay occur when missile is fired.

(Squad Leader) Check that back blastarea (area within 75 meters or 246feet behind launch vehicle) is clearof personnel, equipment, andflammable material.

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2 - 7 7 . SELECTION OF SITE FOR HMMWV MOUNTED TOW 2 WEAPON SYSTEM(Sheet 2 of 2)

Do not fire missile over or in thedirection of electrical wires. Ifcommand-link wires contact a livehigh voltage power line, injury topersonnel and damage to equipmentmay occur.

A. (Gunner) Check site for things blocking field of view.

B. (Driver) Move site if field of view is not large enough.

A.

B.

NOTE

Do not fire missile if sideslope is greater than 10degrees. Missile guidancewill not be accurate.

(Gunner) Check level gage tomake sure side slope is nogreater than 10 degrees.

(Driver) If side slope exceeds10 degrees, rotate vehicle orselect new launch site.

END OF TASK

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2 - 7 8 . F IRING ANGLE LIMITATIONS OF HMMWV(Sheet 1 o f 2 )

TM 9-1425-450-12

Injury to the gunner and damage to the equipment can occur ifthe TOW 2 system is fired at angles greater than 20 degrees orless than -20 degrees for all firing positions except over thecargo/loader’s door. If firing over the cargo/loader’s door,firing angles should not exceed +20 degrees or -13 degrees.

Pressure waves and flying debris can cause injury to personneland equipment damage.

There are restrictions to the elevation angle in which a missile may be firedfrom a HMMWV launcher. The restricted firing angles are those greater than20 degrees or less than -20 degrees for all firing positions except over the cargo/loader’s door. If firing over the cargo/loader’s door, firing angles should notexceed +20 degrees or -13 degrees. The HMMWV may be struck by the missile orseverely damaged by the back blast if the launcher is pointed in a restrictedposition while being fired. In addition, personnel may be injured.

An elevation and depression limiter assembly is provided with the HMMWV as a safetydevice. When the elevation and depression stops are in the “up” position and pinned,firing angle limitation will be +20 degrees and -10 degrees.

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2-78. FIRING ANGLE LIMITATIONS OF HMMWV (CONT)(Sheet 2 of 2)

If the elevation and depression stops are disengaged, the following three examplesshow how the firing angle is limited by the danger of the missile or back blaststriking the HMMWV.

A. If the launcher is pointed directly forward then the gunner must not allow theelevation of the launcher to exceed +20 degrees or -20 degrees.

B. If the launcher is pointed over the right front tire then the gunner must notallow the elevation of the launcher to exceed +20 degrees or -20 degrees.

c. If the launcher is pointed directly over the cargo/loader’s door then thegunner must not allow the elevation of the launcher to exceed +20 degrees or-13 degrees.

2-396 Change 3

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2 - 7 9 . LOADING ENCASED MISSILE INTO LAUNCH TUBE ON HMMWV(Sheet 1 o f 12 )

PERSONNEL: Two MOS 11H (Gunner and Loader)

NOTE

At the beginning of each work day,do System Checkout procedure(para 2-33).

Prepare TOW 2 launcher system foroperation (see para 2-76).

A. (Gunner) On traversing unit put azimuth lock in LOCK position.

B. (Gunner) Put elevation lock in LOCKED position.

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Change 3 2-396.1/(2-396.2 blank)

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2 - 7 9 . LOADING ENCASED MISSILE INTO LAUNCH TUBE ON HMMWV (CONT)(Sheet 2 of 12)

A. (Gunner) Turn traversingunit from side to side untilit locks in place.

13. (Gunner) Turn control knobsforward until trunnion locksin place.

(Gunner) Push locking handleforward, then up and openbridge clamp.

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2 - 7 9 . LOADING ENCASED MISSILE INTO LAUNCH TUBE ON HMMWV (CONT)(Sheet 3 o f 12 )

Never open one end of cargo/loader’s door withoutfirst insuring that opposite end is securelyclosed. Not doing so will cause both ends to openat same time causing injury to personnel, damageto equipment, or mission abort.

(Loader) Using forward latch, unlatch and raise cargo/loader’s door(TM 9-2320-280-10).

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2 - 7 9 . LOADING ENCASED MISSILE INTO LAUNCH TUBE ON HMMWV (CONT)(Sheet 4 o f 12 )

If the missile case is punctured or damaged in sucha way that the missile inside may be damaged, themissile should be treated as hazardous material andEOD personnel notified.

Do not drop encased missile. Handling rings or launch con-tainer may be bent or damaged.

Do not break diaphragm on end of encased missile. If watergets into launch container, missile can be damaged.

Do not dispose of bad missiles. If encased missile isdamaged or handling rings badly bent, return encased missileto ammunition unit for inspection.

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2 - 7 9 . LOADING ENCASED MISSILE INTO LAUNCH TUBE ON HMMWV (CONT)(Sheet 5 o f 12 )

NOTE

Missiles must be unloaded in numerical order.

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2-79. LOADING ENCASED MISSILE INTO LAUNCH TUBE ON HMMWV (CONT)(Sheet 6 OF 12)

8

lf the missile case is punctured or damageddo not attempt to use the encased missile.If missile is damaged it should be treatedas hazardous material and EOD personnelshould be notified for proper disposal.

Use care not to punch a hole in the encased missilediaphragm when forward handling ring is removed.

NOTE

Save forward handling ring and quick releasedamp to be used again if missile is not fired.

(Loader) Pull up on quick release clamp at forwardhandling ring and remove both from encased missile.Ensure o-ring is removed from forward end of encasedmissile.

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2 - 7 9 . LOADING ENCASED MISSILE INTO LAUNCH TUBE ON HMMWV (CONT)(Sheet 7 o f 12 )

Make sure that all personnel are clear of firing danger zonebefore going ahead with missile loading procedure.

NOTE

If missile diaphragms get damaged while the loading operationis being done, missile may still be fired.

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2-79. LOADING ENCASED MISSILE INTO LAUNCH TUBE ON HMMWV (CONT)(Sheet 8 of 12)

9

A. (Loader) Turn inside portion of protective cover two complete turns counterclockwise.

B. (Loader) Turn protective cover counterclockwise and remove from electrical connector. Verifyrubber o-ring remains inside protective cover and is not affixed to missile launch tube on the electricalconnector. Keep protective cover for future use.

C. (Loader) Turn encased missile so that electrical connector is on top (facing up).

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2 - 7 9 . LOADING ENCASED MISSILE INTO LAUNCH TUBE ON HMMWV (CONT)(Sheet 9 o f 12 )

A. (Loader) Remove next available missile from missile rack. If necessary,refer to para 2-83 (steps 4 thru 6) for detailed instructions.

B. (Loader) Hand encased missile up to gunner, making sure electricalconnector is on top side.

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2 - 7 9 . LOADING ENCASED(Sheet 10 o f 12 )

TM 9-1425-450-12

MISSILE INTO LAUNCH TUBE ON HMMWV (CONT)

A.

B.

(Gunner) Raise rear end of encased missile and slide encased missileforward and down into launch tube until lugs are firmly in place.

(Gunner) Lower back end of encased missile, making sure that it isplaced so that electrical connector will join with bridge clamp.

A. (Gunner) Lower bridge clamp.

B. (Gunner) Push down on top of bridge clamp and pull bridge clamp lockinghandle downward and backward to lock encased missile in launch tube.

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Chnage 2 2 - 4 0 5

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2-79 . LOADING ENCASED MISSILE INTO LAUNCH TUBE ON HMMWV (CONT)(Sheet 11 o f 12 )

Cargo/loader’s door must be closed and securelylatched at both ends before firing a missile.Firing missile with door not secure will causeinjury to personnel, damage to equipment, ormission abort.

A. (Loader) Close cargo/loader’s door.

B. (Gunner) Make sure cargo/loader’s door is securely latched at forward end.

c. (Squad Leader) Make sure cargo/loader’s door is securely latched at rear.

e n d .

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2-79. LOADING ENCASED MSSILE INTO LAUNCH TUBE ON HMMWV (CONT)

(SHEET 12 OF 12)

14

Do paras. 2-79.01 and 2-79.02.

se arming lever until ready to fire at seleDO NOT rai cted target.

Change 13 2-407

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2-79.01. PREPARATION TO FIRE MISSILE

(SHEET 1 OF 7)

1

A. Load encased missile (see para. 2-34).

B. Visually select the target without using the day sight tracker or night sight.

C. Put elevation lock in UNLOCKED position.

D. Put azimuth lock in UNLOCKED position.

n the elevation of the launch tube is greater• Whe than 20 degrees above the horizon, hazards to the gunner and equipment exist.

• Pressure waves from the back blast can injure the gunner and damage the equipment.

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2-79.01. PREPARATION TO FIRE MISSILE

(SHEET 2 OF 7)

• Remove glasses before looking through day sight tracker or night sight.

• Do not look at sun or bright lights through day sighttracker.

• Serious eye damage can occur if too much light isseen through day sight tracker.

• If eye damage occurs from looking through day sight tracker, cover eyes and get medical help right away.

2

A. Look through day sight tracker or night sight.

B. Turn control knobs to point the day sight tracker and night sight in the general direction of the selected target.

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2-79.01. PREPARATION TO FIRE MISSILE (SHEET 3 OF 7)

3

A. Adjust focus control on day sight tracker until crosshairs are in focus.

B. When needed to see crosshairs clearly, set RETICLE LIGHT switch to ON.

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2-79.01. PREPARATION TO FIRE MISSILE

(SHEET 4 OF 7)

4

Turn control knobs until crosshairs are positioned on target.

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2-79.01. PREPARATION TO FIRE MISSILE

(SHEET 5 OF 7)

5

Set ON/OFF/STBY switch to ON and allow approximately 3 to 5 minutes for cool down.

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2-79.01. PREPARATION TO FIRE MISSILE (CONT) (SHEET 6 OF 7)

6

A. On night sight, look through eyepiece.

B. Turn DIOPTER ADJUSTMENT RING to focus reticule.

C. Check that battery monitor light and Not Ready light are off.

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2-79.01. PREPARATION TO FIRE MISSILE (CONT) (SHEET 7 OF 7)

7

A. On night sight, set FIELD-OF-VIEW selector to WFOV.

B. Select target and adjust RANGE FOCUS, CTRS, and BRT controls as necessary.

C. Place crosshairs on target.

D. On night sight, set FIELD-OF-VIEW selector to NFOV.

E. Adjust RANGE FOCUS, CTRS, and BRT controls as necessary. Review para. 2-33, Step 34 k-m.

8

NOTE

The night sight provides for missile tracking during field obscurant (dust, smoke, fog, etc.), or electronic counter-measure conditions. To take advantage of this capability, both the night and day sights must be ON, regardless of which sight is used to acquire the target. Night sight must be in NFOV. DO NOT fire TOW 2B if PA FAIL occurred during self-test.

A. Select the day sight tracker or night sight, whichever gives you the better target image, depending upon battlefield visibility.

B. Turn control knobs to keep crosshairs on center of target. C. Go to para. 2-36.

END OF TASK

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2-79.02. MISSILE FIRING PROCEDURE (SHEET 1 OF 7)

PERSONNEL: Two MOS 11H (Soldier A and Soldier B)

• Wear ear plugs (V-51R or equal) when firing TOW missile.Ear damage can occur if missile is fired.

• If ear damage occurs after missile is fired, get medical helpright away.

Make sure that the bridge clamp locking handle is fully downand locked before firing a missile. The command-link wires may be cut at firing if the locking handle is not fully locked.

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2-79.02. MISSILE FIRING PROCEDURE (CONT) (SHEET 2 OF 7)

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Do not fire missile over or in the direction of electrical wires. If command-link wires contact a live high voltage power line, injury to personnel and damage to equipment may occur.

NOTE A moving target may be able to find a covered positionprotecting it from your missile. You must be able tojudge if your missile will successfully hit the target afterlaunch. If there is not obstruction or covered area alongthe expected path of the target and the target is moving35 Kph or less, you can successfully launch and destroythe target. The day sight tracker can help you to makethis determination.

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2-79.02. MISSILE FIRING PROCEDURE (CONT) (SHEET 3 OF 7)

NOTE

The firing procedure is the same when using the daysight tracker or night sight.

1

A. Prepare to fire missile (see para. 2-35).

B. (Soldier A) Line up the crosshairs on the center of the visible mass of the target.

C. (Soldier A) If there is no obstruction or covered area along the expected path of the target and the target is moving 35 Kph or less, go ahead and fire, starting at Step 2.

D. (Soldier A) If an obstruction or covered area appears in your field of view, don't fire at the target. The missile might hit the obstruction and never reach the target.

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2-79.02. MISSILE FIRING PROCEDURE (CONT) (SHEET 4 OF 7)

2

(Soldier B) Raise arming lever.

NOTE

When arming lever is raised, encased missile iselectrically connected to launcher.

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2-79.02. PREPARATION TO FIRE MISSILE (SHEET 5 OF 7)

If two unsuccessful firings occur in a row, the launchershould not be fired again. It should first be checked bysupport maintenance personnel.

NOTE

If the missile launch motor does not fire within 1.5seconds after the firing trigger is pushed, warn weaponcrew of a misfire and continue to track the target.Follow the procedures for HANGFIRE (see para. 2-38).

3

(Soldier A) When ready to fire, raise trigger cover to expose trigger.

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2-79.02. MISSILE FIRING PROCEDURE (CONT) (SHEET 6 OF 7)

4

(Soldier A) Push trigger in to fire missile.

• Make sure that the crew is out of firing danger zonesbefore pressing trigger.

• All crew members stay in their firing positions untilmissile hits target or explodes.

• Serious injury to personnel could result if crewmembers are in firing danger zones when missile isfired.

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2-79.02. MISSILE FIRING PROCEDURE (CONT) (SHEET 7 OF 7)

5

A. (Soldier A) Turn control knobs to track the target, keeping crosshairs on the center of the target.

B. (Soldier A) Stop tracking when missile hits the target or explodes.

C. If additional missiles are to be fired, go to para. 2-42.

D. If no additional missiles are to be fired, go to para. 2-43.

E. If missile was not fired, go to para. 2-43.

F. If missile malfunctions, go to para. 2-37. If HMMWV mounted, go to para. 2-79.1.

NOTE • Track with smooth motions on the control knobs. Do not make jerky

movements. • Target may be hidden for a short time during tracking. • Continue tracking at the same rate as before losing sight of target. • When target reappears, it should be close to aiming point. • Do not change from night sight to day sight tracker or vice versa after

missile has fired.

END OF TASK

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2-79.1. FAILURE TO LAUNCH - HANGFIRE PROCEDURES (Sheet 1 of 4)

• The crew must exercise extreme care to avoid injury from a delayedmissile launch. A delayed launch usually occurs within one minute.However, it could occur as long as 30 minutes after pressing thetrigger.

• Do not open the cargo/loader’s door during failure to launchprocedures. Should the missile fire with the cargo/loader’s door open,severe injury to personnel or damage to equipment will result.

NOTE

• Keep all personnel out of firing danger zones (see para. 2-79).

Refer to para 2-37 for a description of missile malfunctions.

The following depicts a 2- and 3-man crew for the HMMWV.

FRONT OF HMMWV

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2-79.1. FAILURE TO LAUNCH – HANGFIRE PROCEDURES (CONT) (Sheet 2 of 4)

A. (Gunner) Alert crew by starting HANGFIRE and continue to track

target for one minute.

B. (Gunner) If missile fails to launch after one minute, close trigger cover and lower arming lever. C. (Gunner) Place elevation lock into LOCKED position. D. (Gunner) Place azimuth lock into

LOCKED position.

Training/Testing Combat

A. (Gunner) Alert crew by stating HANGFIRE and continue to track target for one minute.

B. (Gunner) If missile fails to launch after one minute, close trigger cover and lower arming lever. C. (Gunner) Place elevation lock into LOCKED position/ D. (Gunner) Place azimuth lock into LOCKED position.

Training/Testing

A. Crew dismount vehicle, close doors. B. Call EOD. C. Wait 30 minutes.

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2-79.1. FAILURE TO LAUNCH - HANGFIRE PROCEDURES (CONT) (Sheet 3 of 4)

A. (Gunner) Remount vehicle and A. (Gunner) Open bridge clamp. B. (Gunner) Remove missile from launch tube. Keep missile pointed downrange at all times.

open bridge clamp. B. (Gunner) Remove missile from launch tube. Keep missile pointed downrange at all times.

If the vehicle is not positioned with its front or rear in line with thetarget, it must be repositioned such that either the front or rear of the vehicle is in line with the target. The weapons station must berotated during vehicle repositioning movement such that the forwardend of the missile is pointing toward the target at all times.

Training/Testing Combat

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2-79.1. FAILURE TO LAUNCH - HANGFIRE PROCEDURES (CONT) (Sheet 4 of 4)

Do not hand off a malfunctioned missile to the front or rear of the vehicle. A malfunctioned missile must be handed off from the launcher to either the left or right of the vehicle.

Training/Testing Combat

A. (Gunner) Hand missile over side of vehicle to loader. B. (Loader) Keeping missile pointed downrange, carry it to dud pit. If there is no dud pit, place missile on ground at least 200 meters from the launcher. Mark missile location.

A. (Gunner) Hand missile over side of vehicle to loader.

B. (Loader) Keeping missile pointed down range, place missile on ground at a safe distance from the launcher.

END OF TASK

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2-79. 2. FAILURE TO LAUNCH - MISFIRE PROCEDURES (Sheet 1 of 5)

• The crew must exercise extreme care to avoid injury from a delayedmissile launch. A delayed launch usually occurs within one minute.However, it could occur as long as 30 minutes after pressing thetrigger.

• Keep all personnel out of firing danger zones (see para. 2-79.)

• Do not open the cargo/loader’s door during failure to launchprocedures. Should the missile fire with the cargo/loader’s dooropen, severe injury to personnel or damage to equipment will result.

Combat Training/Testing

A. (Gunner) Alert crew by stating MISFIRE and continue to track target for 1 minute.

B. (Gunner) Press trigger again. C. (Gunner) If missile still fails to launch, close

trigger cover and lower arming lever. D. (Gunner) Lock azimuth and elevation locks.

A. (Gunner) Alert crew by stating MISFIRE andcontinue to track target for 1 minute.

B. (Gunner) Press trigger again. C. (Gunner) If missile still fails to launch, close

trigger cover and lower arming lever. D. (Gunner) Lock azimuth and elevation locks.

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2-79.2. FAILURE TO LAUNCH - MISFIRE PROCEDURES (CONT) (Sheet 2 of 5)

Training/Testing Combat

A. (Gunner) On missile guidance set, run battery self test by pressing and holding TEST/OPERATE switch. If no go, check power conditioner ON/OFF switch and TVPC power cable connector PI. If still no go, replace power conditioner with battery and repeat battery self test.

A. (Gunner) On missile guidance set, run battery self test by pressing and holding TEST/

OPERATE switch. If no go, check power conditioner ON/OFF switch and TVPC power cable connector P1. If still no go, replace power conditioner with battery and repeat battery self-test.

B. (Gunner) On missile guidance set, make sure coil cord connector is properly attached to connector J1. Turn coil cord connector clockwise until tight to make sure coil cord connector is locked in place.

B. (Gunner) On missile guidance set, make sure coil cord connector is properly at- tached to connector J1. Turn coil cord connector clockwise until tight to make sure coil cord connector is locked into place.

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2-79.2. FAILURE TO LAUNCH - MISFIRE PROCEDURES (CONT) (Sheet 3 of 5)

Combat Training/Testing

A. (Gunner) Ensure bridge clamp locking handle is properly seated.

B. (Gunner) Unlock azimuth and elevation locks.

C. (Gunner) Raise arming lever. Check for proper mating of electrical connector. Raise trigger cover.

D. (Gunner) Press trigger.

E. (Gunner) If missile still fails to launch, continue tracking target for one minute.

F. (Gunner) Close trigger cover.

G. (Gunner) Lower arming lever.

H. (Gunner) Lock azimuth and elevation locks.

A. (Gunner) Ensure bridge clamp locking handle is properly seated.

B. (Gunner) Unlock azimuth and elevation lock.

C. (Gunner) Raise arming lever Check for proper mating of electrical connector. Raise trigger cover.

D. (Gunner) Press trigger.

E. (Gunner) If missile still fails to launch, continue tracking target for one minute.

F. (Gunner) Close trigger cover.

G. (Gunner) Lower arming lever.

H. (Gunner) Lock azimuth and elevation locks.

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2-79.2. FAILURE TO LAUNCH - MISFIRE PROCEDURES (CONT) (Sheet 4 of 5)

Training/Testing

A. Crew dismount vehicle, close doors.

B. Call EOD.

C. Wait 30 minutes.

If the vehicle is not positioned with its front or rear in line with the target, it mustbe repositioned such that either the front or rear of the vehicle is in line with the target. The weapons station must be rotated during vehicle repositioningmovement such that the forward end of the missile is pointing toward the target at all times.

Training/Testing Combat

A. (Gunner) Remount vehicle and open bridge clamp.

B. (Gunner) Remove missile from launch tube. Keep missile pointed downrange at all times.

A. (Gunner) Open bridge clamp.

B. (Gunner) Remove missile from launch tube. Keep missile pointed downrange at all times.

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2-79.2. FAILURE TO LAUNCH – MISFIRE PROCEDURES (CONT) (SHEET 5 OF 5)

6

NOTE

Training/Testing Combat

A. (Gunner) Hand missile over side of vehicle to loader.

A. (Gunner) Hand missile over side of vehicle to loader.

B. (Loader) Keeping missile pointed downrange, carry it to dud pit. If there is no dud pit, place missile on ground at least 200 meters from launcher. Mark missile location.

B. (Loader) Keeping missile pointed downrange, place missile on ground at a safe distance from launcher.

END OF TASK

THIS PAGE INTENTIONALLY LEFT

Do not hand off a malfunctioned missile to the front or rear of thevehicle. A malfunctioned missile must be handed off from thelauncher to either the left or right of the vehicle.

If the missile is handed off to the driver’s side, the driver must perform duties of the loader.

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2-80. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (SHEET 1 OF 8)

PERSONNEL: Two MOS 11H (Soldier A and Soldier B)

1

(Soldier A) After missile has ended flight, lower trigger cover over trigger.

Do not press trigger with empty missile case in launchtube. Possible shorts can result, damaging the prefire,fire, and wirecutter circuits.

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2-80. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT) (SHEET 2 OF 8)

2

A. (Soldier A) On traversing unit, put azimuth lock in LOCK position.

B. (Soldier B) Turn traversing unit from side to side until it locks in place.

C. (Soldier A) Put elevation lock in LOCKED position.

D. (Soldier B) Tilt trunnion until launch tube is locked in down position.

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2-80. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT) (SHEET 3 OF 8)

If missile was not fired, lower arming lever before openingbridge clamp. This will prevent the command link wire frombeing cut under any situation.

3

(Soldier B) If missile was not fired, lower arming lever.

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2-80. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT) (SHEET 4 OF 8)

4

NOTE Opening the bridge clamp does the following:

(Soldier B) Pull up on bridge clamp locking handle and open bridge clamp.

If missile was fired, do not lower arming lever to safe positionbefore opening bridge clamp. Command-link wires will not becut if arming lever is lowered before bridge clamp is opened.

• Cuts command-link wires. • Forces arming lever down to electronically disconnect

launcher from empty missile case. • Turns launcher off.

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2-80. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT) (SHEET 5 OF 8)

4

A. (Soldier B) Remove encased missile or empty missile case from launch tube. B. (Soldier B) If missile case is empty, dispose of it in accordance with unit standard

operating procedure. Go to step 8.

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2-80. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT) (SHEET 6 OF 8)

6

On encased missile: A. (Soldier B) Inspect umbilical electrical connector to determine if it is stuck in the depressed

position. If this is stuck in the depressed position, notify EOD personnel. Do not transmit radio frequencies within 150 feet of ammunition.

B. (Soldier B) Position protective cover on electrical connector so that grooves on protective cover line up with notches on electrical connector. Turn protective cover clockwise to secure it in place.

C. (Soldier B) Turn inside portion of protective cover fully clockwise to lock.

Injury or death to personnel may occur if theumbilical plunger does not return to the upposition. (Plunger should be flush with therim).

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2-80. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT) (SHEET 7 OF 8)

7

A. (Soldier B) Replace quick release clamp, preformed packing and forward handling ring on encased missile.

B. (Soldier B) Push down on quick release clamp to secure forward handling ring. C. (Soldier B) If missile will not be fired within a short time, tag the missile with the date it was initially

prepared for firing. D. (Soldier B) Put encased missile in stowed position (see para. 2-75 for HMMWV).

TASK COMPLETED

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2-80. REMOVAL OF ENCASED MISSILE OR EMPTY MISSILE CASE (CONT) (SHEET 8 OF 8)

NOTE

8

A. (Soldier B) Pull command-link wires out from front of launch tube. B. (Soldier B) Check inside rear of launch tube for dirt. If dirty, clean

with clean, dry cloth.

END OF TASK

• Be careful when pulling command-link wires out of launch tube.

• The command-link wires are very small and strong and can cause injury if handled improperly.

Do the following step only if empty missilewas removed.

Change 13 2-410.15/(2-410.16 Blank)

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL(Sheet 1 o f 23 )

PERSONNEL: Four MOS 11H (Driver, Squad Leader, Gunner, Loader)

EQUIPMENT CONDITION: TOW 2 Launcher System Prepared for Operation (para 2-76)

Failure to dismount TOW weapon system during travelcan cause damage to Missile Guidance Set connectors,Traversing Unit connectors, Traversing Unit brackets,and Manportable Thermal Night Sight brackets.

Never open one end of cargo/loader’s doorwithout first insuring that opposite endis securely closed. Not doing so willcause both ends to open at same timecausing injury to personnel, damage toequipment, or mission abort.

(Loader) Using forward latch, open cargo/loader’s door (TM 9-2320-280-10).

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2-81 PREPARATION OF HMMWV FOR TRAVEL (SHEET 2 OF 23)

2

NOTE

If no encased missile or empty missile case is in launch tube, go to step 3.

A. Perform para. 2-80 to remove encased missile or empty missile case from launch tube.

B. Go to step 4.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 3 o f 23 )

TM 9-1425-450-12

A. (Gunner) Set azimuth lock to LOCK position.

B. (Gunner) Set elevation lock to LOCKED position.

C. (Gunner) Turn control knobs forward until trunnion locks in place.

D. (Gunner) Turn traversing unit from side to side until it locks in place.

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2-81. PREPARATION OF HMMWV FOR TRAVEL (CONT) (SHEET 4 OF 23)

4

A. (Gunner) On night sight, set ON/OFF/STBY switch to OFF.

B. (Gunner) Put front lens cover on night sight and secure latches.

C. (Gunner) Turn diopter adjustment ring to full clockwise position.

Do not handle or lift night sight by lens cover.A loose lens cover latch could result inequipment damage if night sight is dropped.

5

(Gunner) On day sight tracker, make sure RETICLE LIGHT switch is set to OFF. Turn eyepiece fully CCW.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 5 o f 23 )

(Squad Leader) On night sight vehicle power conditioner, set powerswitch to OFF.

A.

B.

C.

(Gunner) Remove night sightpower cable from night sightinput power connector J1.

(Gunner) Install protectivecaps on night sight power

night sightJ1.

Hand night sightdown to squad

cable andconnector

(Gunner)power cableleader.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 6 o f 23 )

(Squad leader) Coil night sight power cable 2W2 onto cable bracket.

(Gunner) Disconnect coil cable from missile guidance set.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 7 o f 23 )

(Gunner) Working from inside vehicle, stow coil cable in bottom oftraversing unit by winding cord and pushing up at the same time.

A. (Gunner) Set power conditioner ON/OFF switch to OFF.

B. (Gunner) Disconnect TVPC power cable connector from powerconditioner.

C. (Gunner) Hand TVPC power cable down to squad leader.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 8 o f 23 )

A. (Squad Leader) Coil power conditioner cable onto cable bracket.

B. (Squad Leader) Disconnect TVPC power cable from power conditionercable.

(Squad Leader) Stow TVPC power cable under loader’s seat.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 9 o f 23 )

A.

B.

C.

D.

(Gunner) On night sight, turn postamplifier cable connectorcounterclockwise.

(Gunner) Pu11 straight out on postamplifier cable connector to removefrom night sight.

(Gunner) Install postamplifier cable connector into cable retainer ontraversing unit.

(Gunner) Hold night sight securely and move latch handle toward backof night sight to unlock position.

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2-81. PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 10 o f 23 )

(Gunner) Remove night sight from mounting on day sight tracker.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 11 o f 23 )

A. (Loader) Remove night sight field handling case from behindloader’s seat.

B. (Loader) Open two latches and open cover on night sight field handlingcase.

C. (Gunner) Hand night sight to loader.

D. (Loader) Install protective cap on night sight connector.

E. (Loader) Place night sight inupside-down position.

F. (Loader) Close cover on nightlatches.

G. (Loader) Stow night sight fieland secure with two straps.

night sight field handling case in

sight field handling case and close two

d handling case behind loader’s seat

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 12 o f 23 )

(Gunner) On day sight tracker, make sure boresight azimuth cover andboresight elevation cover are secure.

(Gunner) Make sure azimuth lock and elevation lock are locked ontraversing unit.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 13 o f 23 )

A.

B.

(Gunner) Hold day sight tracker firmly.

(Gunner) While squeezing latch, push latch handle toward traversingunit. Release latch.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 14 o f 23 )

Handle day sight tracker very carefully. It can be easilydamaged.

Do not carry or lift the day sight tracker by the latchhandle. Always lift and carry it at mounting holes.

A. (Gunner) Lift day sight tracker from traversing unit.

B. (Gunner) Hand day sight tracker down to loader.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 15 o f 23 )

A. (Loader) Place day

B. (Loader) Place daywith two straps.

sight tracker

sight tracker

in shroud bag.

in stowage bracket and secure

(Gunner) On traversinglaunch tube.

unit, pull up on launch tube latch to release

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2-81. PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 16 o f 23 )

A. (Gunner) Raise front of launch tube and lift launch tube pins out oflaunch tube brackets in traversing unit.

B. (Gunner) Remove launch tube and hand it down to loader.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 17 o f 23 )

A. (Loader) Stow launch tube on cargo/loader’s door and secure withstrap.

B. (Loader) Close cargo/loader’s door.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 18 o f 23 )

(Gunner) Release coupling clamp at bottom end of traversing unitadapter.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 19 o f 23 )

(Gunner) Lift traversing unit and traversing unit adapter offlauncher mount.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 20 o f 23 )

(Gunner) Place traversing unit and adapter on stowage base and securewith coupling clamp.

(Gunner) Close launcher mount cover and secure with latch.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 21 o f 23 )

A. (Gunner) Set gunner’s platform to full down position (see para 2-84).

B. (Gunner) Unlatch two securing handles securing hatch cover.

C. (Gunner) Unlatch four straps securing missile guidance set.

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2 - 8 1 . P R E P A R A T I O N O F H M M W V F O R T R A V E L ( C O W(Sheet 22 o f 23 )

(Gunner) Place missile guidanceset on gunner’s platform facingfront of vehicle.

(Gunner) Grab hatch cover handle, close hatch, and secure with threelatches.

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2 - 8 1 . PREPARATION OF HMMWV FOR TRAVEL (CONT)(Sheet 23 o f 23 )

A. (Gunner) Lay missile guidance set flat on gunner’s platform.

B. (Squad Leader) Hand missile guidance set cover to gunner.

C. (Gunner) Install missile guidance set cover and secure with twolatches.

D. (Driver) Secure missile guidance set forward retaining strap.

E. (Gunner) Secure missile guidance set rear retaining strap.

F. (Squad Leader) Check to make sure all equipment is stowed and securedto vehicle.

END OF TASK

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2 - 8 2 . REMOVAL OF LAUNCHER SYSTEM FROM HMMWV(Sheet 1 o f 10 )

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2 - 8 2 . REMOVAL OF LAUNCHER SYSTEM FROM HMMWV (CONT)(Sheet 2 o f 10 )

Never open one end of cargo/loader’sdoor without first insuring thatopposite end is securely closed.Not doing so will cause both ends toopen at same time causing injury topersonnel, damage to equipment, ormission abort.

Using forward latch, unlatch and raise cargo/loader’s door(TM 9-2320-280-10).

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2 - 8 2 . REMOVAL OF LAUNCHER SYSTEM FROM HMMWV (CONT)(Sheet 3 o f 10 )

A. Unlatch strap and remove M13 decontamination kit,

B. Close cargo/loader’s door.

Release two fasteners behind back cushion of gunner’s seat and remove gunner’sseat back rest.

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2 - 8 2 . REMOVAL OF LAUNCHER SYSTEM FROM HMMWV (CONT)(Sheet 4 o f 10 )

Unlatch strap and remove water can.

Reinstall gunner’s seat back rest and secure with two fasteners.

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2 - 8 2 . REMOVAL OF LAUNCHER SYSTEM FROM HMMWV (CONT)(Sheet 5 o f 10 )

Never open one end of cargo/loader’s doorwithout first insuring that opposite endis securely closed. Not doing so willcause both ends to open at same timecausing injury to personnel, damage toequipment, or mission abort.

A. From rear of vehicle, raise cargo/loader’s door and lower tailgate allthe way down (TM 9-2320-280-10).

B. Unlatch coupling clamp and strap and remove tripod from vehicle.

C. Unlatch strap and remove launch tube from cargo/loader’s door.

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2 - 8 2 . REMOVAL OF LAUNCHER SYSTEM FROM HMMWV (CONT)(Sheet 6 o f 10 )

A. Unlatch strap and remove spare battery pack.

B. Unlatch strap and remove night sight battery power conditioner.

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2-82 . REMOVAL OF LAUNCHER SYSTEM FROM HMMWV (CONT)(Sheet 7 o f 10 )

Unlatch two straps and remove day sight tracker.

Unlatch two straps and remove night sight.

Unlatch two straps and remove boresight collimator.

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2 - 8 2 . REMOVAL OF LAUNCHER SYSTEM FROM HMMWV (CONT)(Sheet 8 of 10)

Unlatch coupling cltraversing unit.

Unlatch two straps and remove missile guidance set.

amp between traversing unit and adapter and remove

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2 - 8 2 . REMOVAL OF LAUNCHER SYSTEM FROM HMMWV (CONT)(Sheet 9 o f 10 )

A. Unlock two MGS battery assemblies by loosening wing nuts.

B. Remove MGS battery assemblies from battery racks.

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2 - 8 2 . REMOVAL OF LAUNCHER SYSTEM FROM HMMWV (CONT)(Sheet 10 o f 10 )

A. Close and secure tailgate.

B. Close cargo/loader’s door.

C. Remove encased missiles from missile rack (see para 2-83).

END OF TASK

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2 - 8 3 . REMOVAL OF ENCASED MISSILES FROM HMMWV(Sheet 1 of 8)

PERSONNEL: Two MOS 11H

Never open one end of cargo/loader’s doorwithout first insuring that opposite endis securely closed. Not doing so willcause both ends to open at same timecausing injury to personnel, damage toequipment, or mission abort.

A. From rear of vehicle, raise cargo/loader’s door and lower tailgate allthe way down (TM 9-2320-280-10).

B. Unlatch coupling clamp and strap and remove tripod from vehicle.

C. Unlatch strap and remove launch tube from cargo/loader’s door.

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2 - 8 3 . REMOVAL OF ENCASED MISSILES FROM HMMWV (CONT)(Sheet 2 o f 8 )

Unlatch two straps and remove day sight tracker.

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2 - 8 3 . REMOVAL OF ENCASED MISSILES FROM HMMWV (CONT)(Sheet 3 of 8)

Two soldiers are required to remove a missile from missile rack.

• Do not drop encased missile. Handling rings or launch containermay be bent or damaged.

• Do not break diaphragm on end of encased missile. If watergets into launch container, missile can be damaged.

• Do not dispose of bad missiles. If encased missile is damagedor handling rings badly bent, return encased missile to ammuni-tion unit for inspection.

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T M 9 - 1 4 2 5 - 4 5 0 - 1 2

2 - 8 3 . REMOVAL OF ENCASED MISSILES FROM HMMWV (CONT)(Sheet 4 o f 8 )

A. Unlatch two straps and remove missile 1.

B. Unlatch two straps and remove missile 2.

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2 - 8 3 . REMOVAL OF ENCASED MISSILES FROM HMMWV (CONT)(Sheet 5 of 8)

A. Unlatch two latches securing 3rd tier of missile rack and allow3rd tier to rise.

B. Remove missile 3.

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2-83. REMOVAL OF ENCASED MISSILES FROM HMMWV (CONT)(Sheet 6 o f 8 )

A. Fold down 3rd tier support brace.

B. Remove missile 4.

C. Unlatch two latches securing 2nd tier of missile rack and allow2nd tier to rise.

D. Remove missile 5.

E. Remove missile 6.

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2 - 8 3 . REMOVAL OF ENCASED MISSILES FROM HMMWV (CONT)(Sheet 7 of 8)

A. Close and latch missile rack.

B. Install day sight tracker and secure with two straps.

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2 - 4 5 0 Change 2

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2 - 8 3 . REMOVAL OF ENCASED MISSILES FROM HMMWV (CONT)(Sheet 8 o f 8 )

A. Load tripod behind missile rack and secure with coupling clamp and strap.

B. Close and secure tailgate.

C. Close cargo/loader’s door.

END OF TASK

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2-84 . ADJUSTMENT OF GUNNER’S PLATFORM(Sheet 1 o f 2 )

A. To raise gunner’s platform from stowage position, remove two lockpinsfrom stowage locations, grab gunner’s platform at center hole, liftgunner’s platform to either raised position, and secure with twolockpins at sides of gunner’s platform.

B. To adjust gunner’s platform to other raised position, grab and supportgunner’s platform at center hole, remove two lockpins, lift or lowergunner’s platform to other raised position, and reinstall two lockpins.

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2 - 8 4 . ADJUSTMENT OF( S h e e t 2 o f 2 )

TM 9-1425-450-12

GUNNER’S PLATFORM (CONT)

TO return gunner’s platform to stowage position, grab and support gunner’splatform at center hole, remove two lockpins, lower gunner’s platform, andinstall two lockpins in stowage locations.

END OF TASK

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2 - 8 5 . OPERATION OF WEAPONS RING(Sheet 1 o f 3 )

Do not turn weapons ring more than ±300 degrees from straightahead when power cables are attached to launcher. Tracking maybe restricted or equipment damaged.

A. To unlock weapons ring, move brake handle to up position.

B. Rotate weapons ring by gripping brake handle and stationary handle.

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2 - 8 5 . OPERATION OF WEAPONS RING (CONT)(Sheet 2 o f 3 )

To lock weapons ring, move brake handle to down position. If necessary,rotate weapons ring slightly to engage lock.

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2-85 . OPERATION OF WEAPONS RING (CONT)(Sheet 3 of 3)

The gunners sling serves as a seat rest or frontal restrainer for a gunnerpositioned in the weapon station. It is adjustable as needed.

END OF TASK

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Section VIII. OPERATION UNDER UNUSUAL CONDITIONS

SECTION CONTENTS PARA PAGE SCOPE 2-86 2-459 COLD WEATHER 2-87 2-460 HOT WEATHER 2-88 2-461 HIGH HUMIDITY 2-89 2-462 AIR PRESSURE 2-90 2-464 HIGH WINDS 2-91 2-464 SALT WATER 2-92 2-464 OVER WATER 2-93 2-465 SMOKE AND AREA FIRES 2-94 2-471

2-86. SCOPE

The operational procedures covered in this chapter will be used when operating the TOW 2 Weapon System under unusual conditions.

The problems you will have in operating the TOW 2 Weapon System under unusual conditions are as follows:

a. Finding and tracking the right target.

b. Keeping the equipment operational.

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para 2-21

para 2-15

TM 9-1425-450-12

2-87. COLD WEATHER

When the TOW 2 Weapon System is set up, perform the procedures below to keep itoperational .

NOTE

The TOW 2 Weapon System will notoperate properly below -31.7°C(-25°F).

Check for ice and snow on thelens surfaces of the day sighttracker and night sight.

A. Avoid breathing on daysight tracker optics.

B. Check all mechanicaldevices such as switches,clamps, and levers for iceor snow.

END OF TASK

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2 - 8 8 . HOT WEATHER

NOTE

The TOW 2 Weapon System will not operate properly above+140° Fahrenheit.

Avoid exposing the encased missiles and TOW 2 Weapon System components to prolongeddirect sunlight in hot weather. Particular weapon system components that needprotection from the heat of direct sunlight are:

• Night Sight• Day Sight Tracker• Missile Guidance Set• Traversing Unit

If no suitable shelter is available to protect encased missiles andweapon system components, use any available materials (tarpaulins, cloth,leafy branches, etc.) to provide shade.

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2 - 8 9 . HIGH HUMIDITY(Sheet 1 of 2)

MATERIALS: Ml antifogging kit (item 15, Appendix C)

The TOW 2 Weapon System will operate regardless of the humidity. Moisture can beprevented from settling on the lenses by frequent use of the Ml antifogging kit.

Do not use M1 antifogging kit onfront lens of night sight. Thiswill degrade the infrared image.See lens cleaning instructions,paragraph 2-21.

NOTE

A.

B.

C.

D.

• The M1 antifogging kit cannot preventfrost.

the formation of

• The following steps show how to use the M1 antifogging kit.

Pull cloth out of M1 antifogging kit bottle.

Apply clean water to eyepiece and lens surface.

After water gets on the surface of lens, wipe the lens firmly in acircular motion with cloth.

NOTE

If the cloth becomes wet allow it to dry without beingsqueezed.

Store cloth in bottle when not in use.

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2 - 8 9 . HIGH HUMIDITY (CONT)(Sheet 2 o f 2 )

A. Avoid exposing the TOW 2 Weapon System and encased missile to rain,snow, or hail when not engaged in operations.

NOTE

Unnecessary exposure to severe weather can increasethe amount of maintenance needed by the TOW system.

B. If no suitable shelter is available to protect the TOW 2 Weapon Systemfrom poor weather, then a tarpaulin or other material should be usedto cover the weapon system and encased missiles.

If the weapon system and encased missiles have been exposed to wet weather, dothe following procedures:

A. Remove all moisture from optical surfaces and those surfaces which are tobe protected by covers, caps, etc. Perform cleaning procedures for opticalsurfaces (see para 2-20 and 2-21).

B. The encased missile and weapon system should be dried if time and condi-tions permit.

C. Avoid getting water into electrical connectors or on exposed electricalpins.

END OF TASK

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2 - 9 0 . AIR PRESSURE

The air is “thinner” at higher altitudes. The missile will require more timeto correct for a steer error at high altitude than for the same steer error ata low altitude. Since missile steering is done automatically by the weapon sys-tem, the gunner only has to track the target through the day sight tracker. TheTOW 2 Weapon System will operate properly up to an altitude of 10,000 feet.

2 - 9 1 . HIGH WINDS

NOTE

• Firing missile into a high cross wind can causeslight tracking problems.

• Generally, however, the TOW 2 Weapon system willautomatically adjust for the effects of cross windson the TOW missile.

A. The launcher should be shielded from high winds if possible to avoidtracking problems.

B. Try to select targets either up or down wind from the launcher.

2 - 9 2 . SALT WATER

NOTE

Salt water in contact with night sight could corrodeand damage the lens. Do the following procedure toclean the night sight.

A. Clean lens carefully with fresh water.

B. Use a clean cotton pad and dab lightly over lens in order to remove tracesof water and dry the lens.

C. Use clean cloth and wipe out traces of water on other parts.

D. Leave the assembly exposed to air for an hour to dry off the eyepiececushion assembly.

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2 - 9 3 . OVER WATER(Sheet 1 o f 6 )

The TOW 2 Weapon System’s range is limited when fired over water. If the guidewires get too close to the water, the signal sent will be shorted.

The various types of TOW missiles may be fired over water to a maximum range asshown below and limited range as shown on the next page.

TOW missileBTM-71A-2A,meters wide

BGM-71A, BGM-71A-2, BGM-71A-2A, BTM-71A, BTM-71A-2,or BTM-71A-2B can be fired over water 3610 feet or 1100with a maximum range shown.

TOW missile BGM-71A-1, BGM-71A-3, BGM-71A-3A, BGM-71C, BGM-71C-1,BG14-71C-1A, BGM-71C-2B, BGM-71C-4B, BGM-71D, BGM-71D-1B, BGM-71D-3B,BGM-71E, BG14-71E-1B, BGM-71E-3B, BGM-71F, BTM-71A-1, BTM-71A-1B,BTM-71A-3, BTM-71A-3A, BTM-71A-3B, BTM-71D-1B, or BTM-71E-2B can befired over water 2626 feet or 800 meters wide-with a maximum rangeshown.

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2 - 9 3 . OVER WATER (CONT)(Sheet 2 o f 6 )

TOW missile BGM-71A, BGM-71A-2, BGM-71A-2A, BTM-71-2,BTM-71A-2A, or BTM-71A-2B can be fired over water 4593 feet or 1400meter wide with a limited range shown.

TOW missile BGM-71A-1, BGM-71A-3, BGM-71A-3A, BGM-71C, BGM-71C-1,BGM-71C-1A, BGM-71C-2B, BGM-71C-4B, BGM-71D, BGM-71D-1B, BGM-71D-3BBGM-71E, BGM-71E-1B, BGM-71E-3B, BGM-71F, BTM-71A-1, BTM-71A-1B,BTM-71A-3, BTM-71A-3A, BTM-71A-3B, or BTM-71E-2B can befired over water 3610 feet or 1100 meters wide with a limited rangeshown.

NOTE

If the TOW 2 launcher or target is raised above thesurface of water, the missile firing range isincreased.

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2 - 9 3 . OVER WATER (CONT)(Sheet 3 of 6)

The missile firing range for the given heights above water is determined by usingthe following four graphs. To use the graphs, first determine the height abovewater of the TOW 2 launcher. Put a mark at the height on the left-hand columnof the graph. Then determine the height above water of the target. Put a markat that height on the right-hand column of the graph. Connect the two markswith a straight line. Find where the line crosses the center column. Thereading at that point on the center column tells the maximum range the missilecan travel without getting too close to the water.

NOTE

If you are measuring in feet, use the graph in step 5or step 8. If you are measuring in meters, use thegraph in step 6 or step 7.

Use to find range of TOW missile BGM-71A, BGM-71A-2, BGM-71A-2A, BTM-71A,BTM-71A-2, BTM-71A-2A or BTM-71A-2B in feet. For example, line (a) on the graphshows the missile can hit the target across an 8000-foot strip of water whenlauncher is 12 feet above water and target is 36 feet above water. Line (b)shows that when the launcher is 75 feet above water and the target is 3 feetabove water, the missile can hit the target across a 9840-foot strip of water.

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2 - 9 3 . OVER WATER (CONT)(Sheet 4 o f 6 )

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2 - 9 3 . OVER WATER (CONT)( S h e e t 5 o f 6 )

Use to find range of TOW missile BGM-71A-1, BGM-71A-3, BGM-71A-3A,BGM-71C, BGM-71C-1, BGM-71C-lA, BGM-71C-2B, BGM-71C-4B, BGM-71D,BGM-71D-lB, BGM-71D-3B, BGM-71E, BGM-71E-1B, BGM-71E-3B, BGM-71F,BTM-71A-1, BTM-71A-1B, BTM-71A-3, BTM-71A-3A, BTM-71A-3B, BTM-71D-1B,or BTM-71E-2B in meters. For example, line (a) on the graph showsthe missile can hit the target across a 3750-meter strip of water ifthe launcher is 41 meters above water level and target is 1 meterabove water level. Line (b) shows that if the launcher is 6 metersabove water and the target is 18 meters above water, the missile canhit the target across a 2625-meter strip of water.

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2 - 9 3 . OVER WATER (CONT)(Sheet 6 o f 6 )

Use to find range of TOW missile BGM-71A-1, BGM-71A-3, BGM-71A-3A,BGM-71C, BGM-71C-1, BGM-71C-1A, BGM-71C-2B, BGM-71C-4B, BGM-71D,BGM-71D-1B, BGM-71D-3B, BGM-71E, BGM-71E-1B, BGM-71E-3B, BGM-71F,BTM-71A-1, BTM-71A-1B, BTM-71A-3, BTM-71A-3A, BTM-71A-3B, BTM-71D-1B,or BTM-71E-2B in feet. For example, line (a) on the graph showsthe missile can hit the target across a 12,300-foot strip of water ifthe launcher is 134 feet above water level and target is 5 feetabove water level. Line (b) shows that if the launcher is 20 feetabove water and the target is 50 feet above water, the missile canhit the target across a 7925-foot strip of water.

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2 - 9 4 . SMOKE AND AREA FIRES

A. Smoke can obscure the gunner’s line-of-sight and hide the target whenusing the day sight tracker. The gunner should use the night sightwhen visibility is limited.

B. A fire can burn through the command-link wire causing you to losecontrol of the missile. Avoid firing through fire and over fires ifthere is the possibility that the wires will contact the fire beforemissile impact.

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CHAPTER 3

MAINTENANCE INSTRUCTIONS

CHAPTER OVERVIEW

This chapter tells the operator how to keep the TOW 2 Weapon System inworking condition.

CHAPTER CONTENTS PAGE

Section I. REPAIR PARTS, SPECIAL TOOLS AND TEST EQUIPMENT 3-2

Section II. MAINTENANCE PROCEDURES 3-3

3-1

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Section I. REPAIR PARTS, SPECIAL TOOLS, AND TEST EQUIPMENT

SECTION CONTENTS PARA PAGE

SCOPE

SPECIAL TOOLS AND

SPARES AND REPAIR

3-1 3-2

TEST EQUIPMENT 3-2 3-2

PARTS 3-3 3-2

3-1 . SCOPE

This section tells the operator what repair parts, special tools, and test equipmentare necessary to maintain the

3-2 . SPECIAL TOOLS AND

No special tools or equipment

3-3 . SPARES AND REPAIR

Spares and repair parts aretools list covering organizational maintenance for the TOW 2 Weapon System(TM 9-1425-450-24P).

TOW 2 Weapon System.

TEST EQUIPMENT

is needed to maintain the TOW 2 Weapon System.

PARTS

listed and illustrated in the repair parts and special

3-2

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Section II. MAINTENANCE PROCEDURES

SECTION CONTENTS PARA PAGE

SCOPE 3-4 3-5

MISSILE GUIDANCE SET BATTERY ASSEMBLY REMOVAL 3-5 3-6

MISSILE GUIDANCE SET BATTERY ASSEMBLY INSTALLATION 3-6 3-7

MISSILE GUIDANCE SET POWER CONDITIONER REMOVAL 3-7 3-8

MISSILE GUIDANCE SET POWER CONDITIONER INSTALLATION 3-8 3-9

REMOVAL OF WINGED STUDS FROM BATTERY ASSEMBLY 3-8.1 3-10.1

REPLACEMENT OF WINGED STUDS ON BATTERY ASSEMBLY 3-8.2 3-10.3

REMOVAL OF WINGED STUDS FROM POWER CONDITIONER 3-8.3 3-10.4

REPLACEMENT OF WINGED STUDS ON POWER CONDITIONER 3-8.4 3-10.6

DELETED 3-9 thru 3-60.2

REMOVAL OF BATTERY POWER CONDITIONER BATTERIES 3-61 3-91

INSTALLATION OF BATTERY POWER CONDITIONER BATTERIES

3-62 3-91

REMOVAL OF EYEGUARD CUSHION 3-62.1 3-94

INSTALLATION OF EEGUARD CUSHION 3-62.2 3-95

REMOVAL/REPLACEMENT PROCEDURES INDEX 3-63 3-96

Change 13 3-3/(3-4 Blank)

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Section I l . MAINTENANCE PROCEDURES (CONT)

SECTION CONTENTS (CONT)

INSTALLATION OF STRAP ASSEMBLIES ON MISSILE CARRIER

REMOVAL OF SPARE BATTERY RACK FROM MISSILE CARRIER

INSTALLATION OF SPARE BATTERY RACK IN MISSILE CARRIER

STOWAGE OF REAR SEAT IN MISSILE CARRIER

PREPARING REAR SEAT FOR USE IN MISSILE CARRIER

REMOVAL OF MISSILE STORAGE RACK TIE-DOWN STRAPS FROMJEEP LAUNCHER

INSTALLATION OF MISSILE STORAGE RACK TIE-DOWN STRAPS ONJEEP LAUNCHER

REMOVAL OF M236 MOUNTING KIT FROM MISSILE CARRIER

INSTALLATION OF M236 MOUNTING KIT IN MISSILE CARRIER

REMOVAL OF NIGHT SIGHT VEHICLE POWER CONDITIONER FROMHMMWV

INSTALLATION OF NIGHT SIGHT VEHICLE POWER CONDITIONERIN HMMWV

REMOVAL OF BATTERY POWER CONDITIONER BATTERIES

INSTALLATION OF BATTERY POWER CONDITIONER BATTERIES

REMOVAL OF EYEGUARD CUSHION

INSTALLATION OF EYEGUARD CUSHION

REMOVAL/REPLACEMENT PROCEDURES INDEX

PARA

3-52

3-53

3-54

3-55

3-56

3-57

3-58

3-59

3-60

3-60.1

3-60.2

3-61

3-62

3-62.1

3-62.2

3-63

PAGE

3-82

3-83

3-84

3-86

3-87

3-88

3-89

3-90

3-90

3-90.1

3-90.3

3-90.6

3-92

3-94

3-95

3-96

3 - 4 . S C O P E

This section contains the removal and replacement procedures needed by the operatorto keep the TOW 2 Weapon System in operation.

Change 8 3-5

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3-5 . MISSILE GUIDANCE SET BATTERY ASSEMBLY REMOVAL

END OF TASK

3-6

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3 - 6 . MISSILE GUIDANCE SET BATTERY ASSEMBLY INSTALLATION

A.

B.

C.

D.

Remove protective cap from connector P10 and install on storage connector.

Line up connector P10 on battery assembly with connector J10 on missileguidance set.

Fit battery assembly tab into missile guidance set groove.

Push straight down/forward on battery assembly until connector P10 isjoined to connector J10.

A.

B.

While pushing down/forward on-battery assembly, turn six wing nuts indirection of arrow to tighten.

Keep pushing down/forward on battery assembly until at least two wing nutsare tight.

C.

END OF TASK

When all six wing nuts are tight, the battery assembly will be locked tothe missile guidance set.

3-7

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3 - 7 . M I S S I L E G U I D A N C E S E T P O W E R C O N D I T I O N E R R E M O V A L( S h e e t 1 o f 2 )

Injury to personnel or damage to equipment canoccur if power conditioner ON/OFF switch is notset to OFF.

A. Set power conditioner ON/OFF switch to OFF.

B. Turn power conditioner cable connector in direction of arrow and removecable connector.

C. On power conditioner, turn six wing nuts in direction of arrow to loosen.

GO TO NEXT PAGE

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3 - 7 . M I S S I L E G U I D A N C E S E T P O W E R C O N D I T I O N E R( S h e e t 2 o f 2 )

R E M O V A L ( C O N T )

A. Pull strai

B. Lift/pull

ght up/out on handle of power conditioner.

power conditioner until it is free of missile guidance set.

END OF TASK

Change 5 3-8.1/(3-8.2 blank)

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3 - 8 . MISSILE GUIDANCE SET POWER CONDITIONER INSTALLATION(Sheet 1 o f 2 )

A. Line up connector J2 on power conditioner with connector J10 on missileguidance set.

B. Fit power conditioner tab into missile guidance set groove.

C. Push straight down/forward on power conditioner until connector J2 isjoined to connector J10.

A. While pushing down/forward on power conditioner, turn six wing nuts indirection of arrow to tighten.

B. Keep pushing down/forward on power conditioner until at least two wingnuts are tight.

C. When all six wing nuts are tight, the power conditioner will be locked tothe missile guidance set.

GO TO NEXT PAGE

3-9

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3 - 8 . MISSILE GUIDANCE SET POWER CONDITIONER INSTALLATION (CONT)(Sheet 2 o f 2 )

Injury to personnel or damage to equipment canoccur if power condition ON/OFF switch is notset to OFF.

A. Make sure power conditioner ON/OFF switch is set to OFF.

B. Fit power conditioner cable connector onto connector J1 on power conditioner.

C. Turn locking nut on power conditioner cable connector in direction of arrowuntil tight.

D. Set power conditioner ON/OFF switch to ON.

END OF TASK

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T M 9 - 1 4 2 5 - 4 5 0 - 1 2

3 - 8 . 1 . R E M O V A L O F W I N G E D S T U D S F R O M B A T T E R Y A S S E M B L Y(Sheet 1 o f 2 )

TOOLS: Retaining ring pliers

The electrolyte in the batteries containspotassium hydroxide, a caustic chemicalagent.

Should a battery be damaged:handle with extreme care.Prevent any part of the body(especially the face) fromcoming in contact with theelectrolyte.

Should electrolyte come in contact withthe body:

use boric acid solution andcleanse contact area immediately.Rinse contact area with plenty ofwater.

If any part of the battery assembly isleaking, it is defective. Replacebattery assembly.

Change 4 3-10.1

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3-8 .1 . REMOVAL OF WINGED STUDS FROM BATTERY ASSEMBLY (CONT)( S h e e t 2 o f 2 )

Do not expand retaining ring anymore than necessary.

A. Remove retaining ring (1) from winged stud (2)

B. Remove winged stud (2) from battery assembly (3).

END OF TASK

3-10.2 Change 4

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3 - 8 . 2 . R E P L A C E M E N T O F W I N G E D S T U D S O N B A T T E R Y A S S E M B L Y

TOOLS: Retaining ring pliers

A. Put shaft (1) of winged stud (2) through hole (3) in battery assembly (4).

Do not expand retaining ring anymore than necessary.

B. Install retaining ring (5) on shaft (l), with retaining ring flat side down.

END OF TASK

Change 8 3-10.3

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3-8.3. REMOVAL OF WINGED STUDS FROM POWER CONDITIONER

(SHEET 1 OF 2)

TOOLS: Retaining ring pliers

Make sure power conditioner power switch is set toOFF, and discharge the power conditioner beforedisassembly.

Serious burns to personnel and damage to TVPC mayoccur if power conditioner is not discharged beforedisassembly.

Discharge the power conditioner by raisingTEST/OPERATE switch to TEST and hold. Wait untilthe PASS/FAIL indicators go out.

3-10.4 Change 8

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3-8.3. REMOVAL OF WINGED STUDS FROM POWER

(SHEET 2 OF 2)

CONDITIONER (CONT)

Do not expand retaining ring anymore than necessary.

A. Remove retaining ring (1) from winged stud (2).

B. Remove winged stud (2) from power conditioner (3).

END OF TASK

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3-8.4. REPLACEMENT OF WINGED STUDS ON POWER CONDITIONER

TOOLS: Retaining ring pliers

A. Put shaft (1) of winged stud (2) through hole (3) in power conditioner (4).

Do not expand retaining ring anymore than necessary.

B. Install retaining ring (5) on shaft (1), with retaining ring flat side down.

END OF TASK

3-10.6 Change 8

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3-61. REMOVAL OF BATTERY POWER CONDITIONER BATTERIES (SHEET 1 OF 2)

Change 13 3-91

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3-61. REMOVAL OF BATTERY POWER CONDITIONER BATTERIES (SHEET 2 OF 2)

A. Slide six latches (1) to unlatched position and remove battery cover (2) and gasket (3).

B. Remove two batteries (4).

END OF TASK

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3 - 6 2 . INSTALLATION OF BATTERY POWER CONDITIONER BATTERIES (CONT)(Sheet 2 o f 2 )

A. Insert terminals of each battery (1) into mating connector (2) andpress down on battery (1).

B. Install gasket (3) and battery cover (4) and latch six latches (5).

C. Close battery case lid (6) and secure latch (7).

END OF TASK

Change 2 3-93

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3-62.1. REMOVAL OF EYEGUARD CUSHION

TOOLS: Eyepiece protective cover - 10192460-81411 or (81411A)

MATERIALS: Lens paper (item 18, App C)

Always use eyepiece protective cover in thisprocedure. Damage to eyepiece lens may resultif it is not used. Make sure that eyepieceprotective cover and eyepiece lens (1) areclean before installing eyepiece protectivecover.

A. Clean eyepiece lens (1).

B. Wipe eyepiece protective cover clean.

C. Install eyepiece protective cover over eyepiece lens (l).

D. Turn eyeguard cushion (2) counterclockwise and remove itfrom eyepiece assembly (3).

END OF TASK

3-94 Change 8

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3-62.2. INSTALLATION OF EYEGUARD CUSHION

TOOLS: Eyepiece protective cover - 10192460-81411 or (81411A)Orangewood stick

MATERIALS: Lens paper (item 18, App C)

TM 9-1425-450-12

Always use eyepiece protective cover in thisprocedure. Damage to eyepiece lens may resultif it is not used. Make sure that eyepiece pro-tective cover and eyepiece lens (1) are cleanbefore installing eyepiece protective cover.

A. Clean eyepiece lens (1).

B. Wipe eyepiece protective cover clean,

C. Place eyeguard cushion (2) on eyeguard mounting plate (3) and turnclockwise until tight.

D. Using clean orangewood stick, remove eyepiece protective cover fromeyepiece lens (1).

END OF TASK

Change 8 3-95

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3-63. REMOVAL/REPLACEMENT PROCEDURES INDEX

Tripod Mounted

TOW 2 System

HMMWV Mounted

TOW 2 System Item

Remove (para)

Replace (para)

Remove (para)

Replace (para)

Battery Assembly 3-5 3-6 3-5 3-6

Missile Guidance Set 2-44 2-32 2-82 2-76

Traversing Unit 2-44 2-28 2-82 2-76

Day Sight Tracker 2-44 2-30 2-82 2-76

Battery Power Conditioner Batteries

3-61 3-62 3-61 3-62

Night Sight 2-44 2-31 2-82 2-76

Launch Tube 2-44 2-29 2-82 2-76

Power Conditioner N/A N/A 3-7 3-8

3-96 Change 13

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CHAPTER 4

AMMUNITION (MISSILE)

CHAPTER OVERVIEW

This chapter contains a description of the TOW missiles. It includesinstructions for storing and shipping the TOW missiles, and for inspectingthe missiles when they are first received.

CHAPTER CONTENTS PARA PAGE

TOW MISSILE 4-1 4-2

HAZARD CLASSIFICATION 4-2 4-3

EXPLOSIVE CONTENTS 4-3 4-3

HANDLING AND STORAGE 4-4 4-3

INSPECTION UPON RECEIPT OF TOW MISSILE 4-5 4-7

4-1

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4 - 1 . TOW MISSILE

The TOW missile used with the TOW 2 Weapon System is encased in a launch con-tainer which is put into the TOW 2 launcher when ready for use. The TOWmissile comes in 18 attack types (BGM series) containing a high-explosivewarhead, and 11 practice types (BTM series) having an inactive warhead.Missile size and weight data is summarized in table 4-1. The various typesof TOW missiles are identified in table 4-1.1.

Table 4-1. TOW Encased Missile Size and Weight Data

Nomenclature

Length

Diameter

Volume

Weight

Explosive Weight(Approx.)

Warhead

Launch Motor

Flight Motor

Guided Missile, SurfaceAttack, BGM Series

50.6 in

8.6 in

1.7 cu ft

54.2 lb61.3 lb2

64.1 lb3

63.9 lb4

5.3 lbl

4.5 lb2

6.9 lb3

7.0 lb4

5.4 lb

1.2 lb

(128.4 cm)

(21.9 cm)

(48.1 L)

(24.6 kg)(27.9 kg)(29.1 kg)(29.0 kg)

(2.4 kg)(2.0 kg)(3.1 kg)(3.2 kg)

(0.55 kg)

5.6 lb.

7.0 lb.2,3,4 (2.5 kg)

(3.2 kg)

Guided Missile, Practice(Inert Warhead, Live Motor)

BTM Series

50.6

8.6 in

1.7 cu ft

54.2 lb2

61.3 lb64.1 lb3

None

1.2 lb

5.6 lb2,3

(128.4 cm)

(21.9 cm)

(48.1 L)

(24.6 kg)(27.9 kg)(29.1 kg)

(0.55 kg)

(2.5 kg)(3.2 kg)

1BGM-71C, BGM-71C-1, BGM-71C-1A, BGM-71C-2B, and BGM 71C-4B2BGM-71D, BGM-71D-1B. and BGM-71D-3B3BGM-71E, BGM-71E-1B; BGM-71E-3B, and BTM-71E-2B4BGM-71F

4-2 Change 11

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4 - 1 . TOW MISSILE (CONT)

Table 4-1.1. TOW Missile Identification

Missile PartType Description Number

BGM-71A Guided missile, surface attack: normal range 10189999

BGM-71A-1 Guided missile, surface attack: extended range 11500160

BGM-71A-2 Guided missile, surface attack: missile ord- 13100906nance inhibit circuit (MOIC)

BGM-71A-2A Guided missile, surface attack: MOIC, coated 13296259launch motor

BGM-71A-3 Guided missile, surface attack: extended 13100902range, MOIC

BGM-71A-3A Guided missile, surface attack: extended 13296261range, MOIC, coated launch motor

BGFI-71C Guided missile, surface attack: improved TOW 13060893

BGM-71C-1 Guided missile, surface attack: improved TOW, 13100900MOIC

BGM-71C-1A Guided missile, surface attack: improved TOW, 13296263MOIC, coated launch motor

BGM-71C-2B Guided missile, surface attack: improved TOW, 13296476coated launch motor

BGM-71C-4B Guided missile, surface attack: improved TOW, 13296321digital electronics unit, coatedlaunch motor

BGM-71D Guided missile, surface attack: TOW 2 13194422

BGM-71D-1B Guided missile, surface attack: TOW 2, 13296474coated launch motor

BGM-71D-3B Guided missile, surface attack: TOW 2, 13296322digital electronics unit, coatedlaunch motor

GO TO NEXT PAGE

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4-1. TOW MISSILE (CONT)

(Table 4-1.1, continued)

Missile PartType Description Number

BGM-71E Guided missile, surface attack: TOW 2A 13218444

BGM-71E-1B Guided missile, surface attack: TOW 2A, 13296473coated launch motor

BGM-71E-3B Guided missile, surface attack: TOW 2A 13296323digital electronics unit, coatedlaunch motor

BGM-71F Guided missile, surface attack: TOW 2B 13296442

BTM-71A Guided missile, practice: normal range 10190149

BTM-71A-1 Guided missile, practice: extended range 11500162

BTM-71A-1B Guided missile, practice: extended range 13296489coated launch motor

BTM-71A-2 Guided missile, practice: MOIC 13100908

BTM-71A-2A Guided missile, practice: MOIC, cobalt-free 13296260launch motor

BTM-71A-2B Guided missile, practice: MOIC, coated 13296486launch motor

BTM-71A-3 Guided missile, practice: extended range 13100904MOIC

BTM-71A-3A Guided missile, practice: extended range, 13296262MOIC, coated launch motor

BTM-71A-3B Guided missile, practice: extended range, 13296324digital electronics unit, coated launchmotor

BTM-71D-lB Guided missile, practice: TOW 2, coated 13296497launch motor

BTM-71E-2B Guided missile, practice: TOW 2A, digital 13367100electronics unit, coated launch motor

4-2.2 Change 11

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4 - 2 . HAZARD CLASSIFICATION

TOW missile is listed in quantity distance class 1.1 and storage compatibilitygroup E for live and C for practice.

4 - 3 . EXPLOSIVE CONTENTS

Warhead is CLASS A EXPLOSIVE.

4 - 4 . HANDLING AND STORAGE

NOTE

Refer to TM 9-1300-206 for general information about handlingand storage. See following precautions about handling andstorage of TOW encased missile.

a. Handling

(1) Do not try to remove missile from launch container.

(2) Do not handle encased missile roughly or drop it. Damage mayoccur to motor propellant grain or other components and causea failure at launch or in flight.

4-3

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4 - 4 . HANDLING AND STORAGE (CONT)

b. Storage

(1) Follow good storage practice. Protect encased missiles from sun, rain, andmoisture. Use at least six inches of dunnage under the wooden overpacks. Putwaterproof cover over and around stack of missiles. Shelter should be big enoughto have good air circulation. Shelter and encased missiles should be easy to getat so missiles will stay in good condition and be ready for immediate use.

(2) All encased missiles in storage area must be stored with nose ends pointingin the same direction. Direction of storage should permit the least danger topersonnel or equipment in case of explosionor fire.

(3) Storage area should provide the most protection from damage, corrosion, orwearing away. Storage temperature must be between -53.9 and +68.3°C (-65 to155°F). The storage area should:

(a) Be on level ground and have the most protection from the weather.

(b) Have good drainage.

(c) Be arranged so that inspection of missiles can be doneas required.

(d) Meet quantity-distance requirements. Refer to TM 9-1300-206 for generalinformation on storage of ammunition. Missiles are encased and stored in woodenoverpacks. Inspection must be done on encased missiles before they are stored.Storage data is included in table 4-2.

4-4 Change 2

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4 - 4 . HANDLING AND STORAGE (CONT)

Table 4-2. TOW Encased Missile Color Coding, Shipment, and Storage Data

Guided Missile, Practice,Guided Missile, Surface (Inert Warhead, Live Motors)

Nomenclature Attack, BGM Series BTM Series

National stock number 1410-00-087-1521 (BGM-71A) 1410-00-087-1527 (BTM-71A)(NSN) 1410-01-007-2507 (F3GM-71A-1) 1410-01-007-2508 (BTM-71A-1)

1410-01-139-1512 (BGM-71A-2) 1410-01-309-8302 (BTM-71A-1B)1410-01-257-6493 (BGM-71A-2A) 1410-01-137-9976 (BTM-71A-2)1410-01-181-6032 (BGM-71A-3) 1410-01-257-6494 (BTM-71A-2A)1410-01-257-7584 (BGM-71A-3A) 1410-01-309-8301 (BTM-71A-2B)1410-01-106-8514 (BGM-71C) 1410-01-180-6791 (BTM-71A-3)1410-01-180-6790 (BGM-71C-1) 1410-01-257-7585 (BTM-71A-3A)1410-01-257-7583 (BGM-71C-1A) 1410-01-313-5364 (BTM-71A-3B)1410-01-309-8303 (BGM-71C-2B) 141O-O1-3O3-5172 (BTM-71D-1B)1410-01-313-5365 (BGM-71C-4B) 1410-01-343-8924 (BTM-71E-2B)1410-01-135-2092 (BGM-71D)1410-01-301-0815 (BGM-71D-1B)1410-01-313-5366 (BGM-71D-3B)1410-01-229-9948 (BGM-71E)1410-01-300-0254 (BGM 71E-1B)1410-01-313-5367 (BGM-71E-3B)1410-01-322-5333 (BGM-71F)

Basic color of encased Olive drab Olive drabmissile

Color of data markings White or yellow Whiteon encased missile

Color code marking Four 2-inch brown squares Four 2-inch brown squareson encased missile 90° apart, or 2-inch 900 apart, or 2-inchback end brown stripes brown stripes

Color code marking Four 2-inch yellow Four 2-inch blue squareson encased missile squares 900 apart, or 900 apart, or 2-inch bluewarhead end 2-inch yellow stripes stripes

Basic color of wooden Olive drab or unpainted Olive drab or unpaintedoverpack container

Color code marking on Six black 3-inch squares, Six blue 3-inch squares,wooden overpack placed diagonally opposite placed diagonally opposite

on top, in upper left hand on top, in upper left handcorner on sides, and in corner on sides, and inupper right hand corner upper right hand corneron ends on ends

Color of data marking White or black White or blackon wooden overpack

DOT marking on wooden ROCKET AMMUNITION WITH ROCKET AMMUNITION WITHoverpack EXPLOSIVE PROJECTILE INERT LOADED PROJECTILE

GO TO NEXT PAGE

Change 11 4-5

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4 - 4 . HANDLING AND STORAGE (CONT)

(Table 4-2, continued)

Nomenclature

DOT hazardclassification

Quantity-distanceclassification

Storage compatibilitygroup

Storage temperaturelimit

4-6

Guided Missile, SurfaceAttack, BGM Series

CLASS A EXPLOSIVE

1.1

E

-53.9 to +68.3°C(-65 to +155°F)

Guided Missile, Practice,Inert Warhead, Live Motors)

BTM Series

CLASS A EXPLOSIVE

1.1

C

-53.9 to +68.3°C

(-65 to +155°F)

c. Overpack data

TOW encased missile is normally shipped and stored in a wooden overpack to pro-tect it from shocks, being shaken, and being dropped. The overpack contains theencased missile and padding around the missile. The launch container is part ofthe encased missile and provides protection for it. Take care in handling andmoving the encased missile.

Change 11

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4 - 5 . INSPECTION UPON RECEIPT OF TOW MISSILE

APPLICABLE CONFIGURATION: All missiles

NOTE

After receipt inspection, surveillance inspection of theencased missile is required every 12 months. When annualinspection becomes due, notify supporting organization soinspection can be done.

A. Inspect outside of wooden overpack to make sure that it is not damaged inany way.

B. Encased missile in the wooden overpack may be in a plastic bag. If it isin a bag, a humidity indicator is located in the bag and can be seen throughthe window in the back end of the wooden overpack. If the humidity indica-tor is blue, go to next page. If the humidity indicator is pink, remove theplastic bag and throw it away, and take the encased missile back to theappropriate ammunition supply point (ASP) as soon as possible.

C. If encased missile is not in a plastic bag, the humidity indicator on theback end of the encased missile will be visible through the window in therear of the wooden overpack. If the humidity indicator is blue, go to nextpage. If the humidity indicator is pink, take the encased missile back tothe appropriate ammunition supply point (ASP) as soon as possible.

GO TO NEXT PAGE

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4 - 5 . INSPECTION UPON RECEIPT OF TOW MISSILE (CONT)

A. Check markings on wooden overpack to be sure that ammunition is identifiedright. See table 4-2 for identification data.

B. Check shipping papers to make sure that the ammunition received is whatis on the shipping papers.

GO TO NEXT PAGE

4-8 Change 5

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4 - 5 . INSPECTION UPON RECEIPT OF TOW MISSILE (CONT)

Check launch container for proper markings, identification, and colorcoding. See table 4-2.

GO TO NEXT PAGE

4-9

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4 - 5 . INSPECTION UPON RECEIPT OF TOW MISSILE (CONT)

Do not break diaphragm on end of encased missile. If moisturegets into launch container, missile can be damaged.

ENCASED MISSILE

A. If encased missile is in a plastic bag, open bag and remove missile.Throw bag away.

B. Position protective cover on electrical connector so that grooves onprotective cover line up with notches on electrical connector. Turnprotective cover clockwise to secure it in place.

C. Turn inside portion of protective cover fully clockwise.

D. Check forward and rear handling rings on encased missile to make surethey are not damaged.

END OF TASK

4-10

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APPENDIX A

REFERENCES

This appendix contains a list of manuals that are necessary to properly maintain theequipment covered in this manual. For publications applicable to the TOW 2 WeaponSystem, see TM 9-1425-450-L.

A-1/(A-2 blank)

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APPENDIX B

MAINTENANCE ALLOCATION CHART

B-1. GENERAL

This appendix contains the maintenance allocation chart which shows the lowest levelof maintenance authorized to do certain maintenance operations.

B-2. MAINTENANCE FUNCTIONS

The maintenance functions will be limited to and defined as follows:

a. Inspect. To determine the serviceability of an item by comparing itsphysical, mechanical, and/or electrical characteristics with establishedstandards through examination (e.g., by sight, sound, or feel).

b. Test. To verify serviceability by measuring the mechanical, pneumatic,hydraulic, or electrical characteristics of an item. and comparing thosecharacteristics with prescribed standards.

c. Service. Operations required periodically to keep an item in properoperating condition, i.e., to clean (includes decontaminate, whenrequired), to preserve, to drain, to paint, or to replenish fuel,lubricants, chemical fluids, or gases.

d. Adjust. To maintain or regulate, within prescribed limits, by bringinginto proper or exact position, or by setting the operating characteristicsto specified parameters.

e. Aline. To adjust specified variable elements of an item to bring aboutoptimum or desired performance.

f. Calibrate. To determine and cause corrections to be made or to be adjustedon instruments or test, measuring, and diagnostic equipments used inprecision measurement. Consists of comparisons of two instruments, one ofwhich is a certified standard of known accuracy, to detect and adjust anydiscrepancy in the accuracy of the instrument being compared.

g. Remove/Install. To remove and install the same item when required toperform service or other maintenance functions. Install may be the act ofemplacing, seating, or fixing into position a spare, repair part, or module(component or assembly) in a manner to allow the proper functioning of anequipment or system.

h. Replace. To remove an unserviceable item and install a “serviceablecounterpart in its place. “Replace” is authorized by the MAC and is shownas the 3rd position code of the SMR code.

i. Repair. The application of maintenance services, including faultlocation/troubleshooting, removal/installation, and disassembly/assemblyprocedures, and maintenance actions to identify troubles and restoreserviceability to an item by correcting specific damage, fault,malfunction, or failure in a part, subassembly, module (component orassembly), end item, or system.

B-1

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j. Overhaul. That maintenance effort (service/action) prescribed to restorean item to a completely serviceable/operational condition as required bymaintenance standards in appropriate technical publications (i.e., DMWR).Overhaul is normally the highest degree of maintenance performed by theArmy. Overhaul does not normally return an item to like new condition.

k. Rebuild. Consists of those services/actions necessary for the restorationof unserviceable equipment to a like new condition in accordance withoriginal manufacturing standards. Rebuild is the highest degree ofmateriel maintenance applied to Army equipment. The rebuild operationincludes the act of returning to zero those age measurements (hours/miles,etc.) considered in classifying Army equipment/components.

B-3. COLUMN ENTRIES

An explanation of columns used in the maintenance allocation chart will be limitedto those shown. Entries for these columns are explained below:

a. Column 1. Group Number. Column 1 lists group numbers, the purpose ofwhich is to identify components, assemblies, subassemblies, and moduleswith the next higher assembly.

b. Column 2. Component/Assembly. Column 2 contains the noun names ofcomponents, assemblies, subassemblies, and modules for which maintenance isauthorized.

c. Column 3. Maintenance Functions. Column 3 lists the functions to beperformed on the item listed in Column 2.

Column 4.d. Maintenance Category. Column 4 specifies, by the listing of a“work time” figure in the appropriate subcolumn(s), the lowest level ofmaintenance authorized to perform the function listed in Column 3. Thisfigure represents the active time required to perform that maintenancefunction at the indicated category of maintenance. If the number orcomplexity of the tasks within the listed maintenance function vary atdifferent maintenance categories, appropriate “work time” figures will beshown for each category. The number of man-hours specified by the “worktime” figure represents the average time required to restore an item(assembly, subassembly, component, module, end item or system) to aserviceable condition under typical field operating conditions. This timeincludes preparation time, troubleshooting time, and qualityassurance/quality control time in addition to the time required to performthe specific tasks identified for the maintenance functions authorized inthe maintenance allocation chart.

e. Column 5. Tools and Equipment. Column 5 specifies by code, those commontool sets (not individual tools) and special tools, test, and supportequipment required to perform the designated function. These are identi-fied in the Tool and Test Equipment Requirements table following the MAC.

f. Column 6. Remarks. Column 6 contains an alphabetic code which leads toremarks which are pertinent to the item opposite the particular code.Remarks are located “in the Remarks table following the MAC:

B-2

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MAINTENANCE ALLOCATION CHART FOR LAUNCHER, TUBULAR, GM M220A2, M220A3, M220A4

(1) (2) (3) (4) (5) (6) Group Number

Component/Assembly

Maintenance Function

Maintenance Category*

Tools and Equip- ment

Re- marks

C O F H D 0010 Launcher, Tubular

GM M220A2 Inspect Test

.02

.30

.58

3, 4, 5, 7, 8, 12 12

A.1

Aline Install Repair

.04

.15

.20

1.52

3, 4, 5, 7, 8, 12

Test (180 day verification)

2.00 3, 4, 5, 7, 8, 12

1000 Missile Guidance Set, AN/TSQ-136

Test Replace Repair 180 day veri- fication

.02

.60 1.72 2.00

7

1, 3, 4, 5, 7

3, 4, 5, 7, 8, 12

1040 Housing Assy Replace .26

Transformer Replace .70 1

Connector, Battery, P1

Replace Repair

.84 .84

1

1060 Carrier Board Assy, MGS

Replace 1.32 1

1080 Carrier Board Assy, PCU

Replace 1.4 1 A

1100 Error Detector (AZ)

Replace .28 1

1100 Error Detector (EL)

Replace .28 1

1120 Cmd Sig Generator Replace .28 1

1140 Programmer Replace .28 1

1160 Guidance I/O Replace .28 1

*C – Operator/Crew F – Direct Support D – Depot O - Organizational H – General Support

Change 13 B-3

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TM 9-1425-450-12

MAINTENANCE ALLOCATION CHART FOR LAUNCHER,

(1)

GroupNumber

1180

1200

1200

1220

1240

1260

1280

1300

1320

1340

1360

1380

(2)

Component/Assembly

VTT PMM

Guidance MPM

VTT MPM

Guidance PMM

VTT I/O

Timing/Control

Video Processor

BITE Assy

PCU BITE

PCU CurrentRegulator

PCU Motor Drive

PCU LinearRegulators

TUBULAR, GM M220A2

(3)

MaintenanceFunction

Replace

Replace

Replace

Replace

Replace

Replace

Replace

Replace

Replace

Replace

Replace

Replace

Maintenance Category*

C O

0 - OrganizationalF - Direct Support

(4)

*C - Operator/Crew H - General SupportD - Depot

F

.28

.28

.28

.28

.28

.28

.28

.28

.50

.50

.50

.50

H

(5)

Tool Sand

Equip-ment

1

1

1

1

1

1

1

1

1

1

1

1

(6)

Re-marks

B-4 Change 4

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TM 9-1425-450-12

(1)

MAINTENANCE ALLOCATION CHART FOR LAUNCHER,TUBULAR, GM M220A2

(2)

Component/Assembly

1400

1420

1440

1460

1480

PCU +15V Switcher

Pcu +5V supply

PCU Relay/Squib

Fuse

Front Panel Assy

Display IntensityPot.

Switch (TEST/OPERATE)

Interface Assy

Lamps, Display

(3)

MaintenanceFunction

Replace

Replace

Replace

Replace

ReplaceRepair

Replace

Replace

Replace

Replace

(4)

Maintenance Category*

C O

*C - Operator/Crew H - General SupportO - OrganizationalF - Direct Support

D - Depot

F

.50

.50

.50

.20

.48

.04

.66

.66

1.38

.12

H D

(5)

Toolsand

Equip-ment

1

1

1

1

1,7

1

1

1

1

(6)

Re-marks

Change 4 B-5

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TM 9-1425-450-12

MAINTENANCE ALLOCATION CHART FOR LAUNCHERTUBULAR, GM M220A2

(1)

GroupNumber

2000

(4)

3000

4000

2

2

2

B-6 Change 12

(2)

Component/Assembly

MGS Battery

Tube, GM LauncherM22

Sight, OpticalMX9155/TSQ

Eyeguard

Cover, Housing

Valve, Pneumatic

Dessicant Container

Indicator, Humidity

Housing, Front

Window, Optical 2 ea

*C - Operator/Crew F - Direct Support D - Depot O - Organizational H - General Support

(3)

MaintenanceFunction

InspectTest

ServiceReplaceRepair

InspectReplaceRepair

InspectTestServiceReplaceRepair

180 dayannual ver.

InspectReplace

Replace

Replace

Replace

Replace

Replace

Replace

.10

.40

1.00

1.00

1.00

1.00

1.00

1.50

1.50

C O F H D

.05

.03

.50

.02

.02

.10

.12

.19

.62

.321.003.00.327.00

2.00

1.34

( 5 )Tools

andEquipment

3,5,6,1413

1,3,5,6,13,14

11

221,2,20

1,2,22,233,4,5,7,8,12

1

1

1

1

1

1

1,2

(6)

Re-marks

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TM 9-1425-450-12

MAINTENANCE ALLOCATION CHART FOR LAUNCHER.

(1)

GroupNumber

4020

4040

4060

4080

4100

4160

4180

(2)

Component/Assembly

Switch Assy,Reticle

Cover, BoresightKnobs 2 ea

Knobs, Boresight2 ea

Lens Assy, 13X

Latch Assembly

Handle Assembly

Eyepiece, Tracker

Tracker Assy

Motor, Tracker

Resolver Assy

Terminal BoardAssy TB2

Preamplifier

Modulator Assy

Sensor Assy

Cable Harness Assy

Prism Subassy,Boresight Diode

TUBULAR, GM M220A2

(3) (4)

MaintenanceFunction

Replace

Replace

Replace

Replace

Repair

Repair

ReplaceRepair

ReplaceRepair

Replace

ReplaceClean

Replace

Replace

Replace

Replace

Replace

Replace

Maintenance Category*

C

*C - Operator/Crew H - General SupportO - Organizational D - DepotF - Direct Support

O F

1.50

.50

.50

1.50

1.32

.98

1.001.50

2.001.64

2.00

2.00.20

2.00

1.50

1.50

1.50

1.50

2.00

H D

(5) (6)

Tool Sand

Equip-ment

1

1

1

1,2

1,2

1,2

11

11,2

1

11

1

1

1

1

1

1

Change 11

Re-mark:

1

B-7

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TM 9-1425-450-12

MAINTENANCE ALLOCATION CHART FOR LAUNCHER, TUBULAR, GM M220A2

(1) (2) (3) (4) (5) (6) Maintenance Category * Tools

Group Number

Component/Assembly

Maintenance Function

C

O

F

H

D

and Equip- ment

Re- marks

Reticle Light Assy Replace 3.00 1

5000 Traversing Unit, M83

Inspect Test

.60 .58

2,3,5, 10

180 Day Replace Repair

.03

2.00 5.18

3,4,5, 7,8,12 1,2,3, 4,5,25

Handle Assy, Locking Elevation

Repair 1.00 1.50

1, 2

Chain Assy

Adjust Replace

1.00 1.50

1, 2 1

Equilibrator

Adjust Replace Repair

1.00 2.00 2.00

1,2, 1,2 1,2

Interface Harness Assy (2A2W1)

Replace Repair

1.50 3.22

1 1,18,

19

Umbilical Cable Assy (2W1)

Replace Repair

.10 .20

24 1,18,

19

Post Amp Cable Assy (2W1)

Replace Repair

.16 .36

1 1,18,

19

5020 Clamp, Bridge

Inspect Test Adjust Replace Repair

.10

.40 .50

1.00 4.00

2 1,2 1,2 1 1

5060 Cable Assy, (2W2)

Inspect Test Replace Repair

.20 .40

2.00 2.00

1 1,3,5

11 1

*C – Operator/Crew F – Direct Support D – Depot O - Organizational H – General Support

B-8 Change 13

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TM 9-1425-450-12

MAINTENANCE ALLOCATION CHART FOR LAUNCHER,TUBULAR, GM M220A2

(1) (2) (3) (4) (5) (6)

GroupNumber Component/Assembly

Damper, Azimuth

Generator,Tachometer

Damper, Elevation

Generator,Tachometer

Trunnion Assy

Cable Assy, J1(10225693)

Cable Assy(10189491)

Wiring Harness

Tripod Assembly,Launcher M159A1

Coupling Clamp

ToolsMaintenance Category* and

Maintenance Equip- Re-Function c 0 F H D ment marks

Replace .50 1

Replace 1.00 1,2

Replace 2.00 1

Replace 1.00 1,2Repair 2.00

Repl ace 4.00 1,2Repair 5.20 1

Inspect .40Test .60 3,5,10Repair 2.00 1,18,19

Replace 3.00Repair 3.00 1,18,19

Inspect .40 3,5,10Test .60 3,5,10Replace 2.00Repair 2.60 1,3,5,

10,18,19

Inspect .04

Replace .1Repair 1.0 1

Inspect .1Adjust .2Replace .5Repair .5

*C - Operator/Crew H - General SupportO - Organizational D - DepotF - Direct Support

Change 4 B-9

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MAINTENANCE ALLOCATION CHART FOR LAUNCHER, TUBULAR, GM M220A2

(1) (2) (3) (4) (5) (6) Maintenance Category *

Group Number

Component/Assembly

Maintenance Function

C

O

F

H

D

Tools and Equip- ment

Re- marks

Claw, Anchor Tripod Replace Repair

.5 .5

Foot, Anchor Tripod Replace Repair

.5 .5

Locking Mechanism, Tripod Leg

Replace Repair

.5 .5

Leg, Tripod Replace Repair

.5 .5

Body, Tripod Replace 1.5

7000 Sight, Night Vision, Infrared, AN/TAS-4A or AN/TAS-4C

Inspect Test

.04 .48

4,5,9,

11

B

Aline Replace Repair

.02

2.0

1.78

11

1,4,5, 9,11

180 day Annual Ver

.10

2.00

3,4,5, 7,8,12

Boresight Collimator 180 day Annual Ver

1.0

Conditioner, Power, Night Sight Battery

Replace

.10 C

Batteries (2) Replace .10 C

Cable, Battery Power Conditioner

Replace

.10 C

Power Cable, Boresight Collimator

Replace D

*C – Operator/Crew F – Direct Support D – Depot O - Organizational H – General Support

B-10 Change 13

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TM 9-1425-450-12

(1)

GroupNumber

9600

MAINTENANCE ALLOCATION CHART FOR LAUNCHER,TUBULAR, GM M220A2

Component/Assembly

Conditioner,Power

(3)

MaintenanceFunction

InspectTest

ReplaceRepair

(4)

Maintenance Category*

C

.02

.03

0

*C - Operator/crew H - General SupportO - OrganizationalF - Direct support

D - Depot

F

.502.00

5.50

H D

(5)

Toolsand

Equip-ment

1,3,4,5,16

1,3,4,5,16,17

(6)

Re-marks

Change 4 B-11

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TM 9-1425-450-12

MAINTENANCE ALLOCATION CHART FOR LAUNCHER,TUBULAR, GM M220A2 (CONT)

TOOL AND TEST EQUIPMENT REQUIREMENTS

Tool orTest

EquipmentReference Maintenance National/NATO Tool

Code Category Nomenclature Stock Number Number

1 F Tool Kit, GM Maintenance: 5180-00-179-3574 5180-92-Wire-Guided Missile System CL-A52Repairer MOS 27E

2 F Supplementary Equipment, 4935-00-134-7730 10681618GM System Test Station;TOW

3 F Digital Multimeter, 6625-00-500-6640 N/ATektronix DM-501

4 F Oscilloscope, Tektronix 6625-01-023-7092 N/ASC-502

5 F Power Mainframe, TM-503 6625-00-373-7528 N/A

6 F Digital Multimeter, 6625-00-210-7584 N/AFluke 8000A

7 F Test Set, Missile Guidance 4935-01-147-5999 13099749Set, AN/TSM-152

8 F Test Set, Electrical 4935-01-119-3460 13195336Circuit, AN/TSM-158

9 F Test Set, Amplifier, 5855-01-144-4837 13099878AN/TAM-5

10 F Test Set, Electrical 6625-01-120-0027 13195112Cable, AN/TSM-149

11 F Test Set, Night Vision 5855-01-154-3871 SM-C-Sight AN/TAM-3A 806808

12 F Collimator, Boresight 5855-01-109-6433 N/A

13 O-F Battery Charger, 6130-01-018-9786 11500154PP 4884A/T

B-12 Change 4

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TM 9-1425-450-12

MAINTENANCE ALLOCATION CHART FOR LAUNCHER, TUBULAR, GM M220A2, M220A3, M220A4 (CONT)

TOOL AND TEST EQUIPMENT REQUIREMENTS

Tool or Test Equipment Reference Code

Maintenance Category

Nomenclature

National/NATO Stock Number

Tool Number

14 F Cable, Power Monitor 4935-01-128-4773 N/A

15 F Monitor, Battery Charger N/A 13060888

16 F Test Adapter, Power Conditioner

4935-01-112-3068 13060899

17 F Module Extractor 5120-01-126-4482 N/A

18 F Extraction Tool, No. 20 N/A CET-20-5

19 F Insertion Tool, No. 20 N/A CET-20-5

20 F Purge and Fill Kit T1045171 4920-01-016-5454

21 O Tool Kit, General Mechanic 5181-00-177-7033 N/A

22 F IFTE N/A

23 F TOW/DRAGON TPS N/A

24 F Special Tool, for removing 2W1 cable

N/A 13012628

25 F Autocollimator 6650-01-129-4968 N/A

or

Boresight Alinement Tube 4933-01-435-3166 13569468

and Special Socket Wrench 5120-01-435-3163 13569467

26 F Boresight Collimator Test Set

Change 13 B-13

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TM 9-1425-450-12

MAINTENANCE ALLOCATION CHART FOR LAUNCHER, TUBULAR, GM M220A2 (CONT)

REMARKS

Reference Code Remarks

A Replace PCU carrier Assembly at field level by installing or replacing transformer or battery connector. All other repairs at depot level.

For complete MAC, refer to TM 9-5855-450-24.

C For complete MAC, refer to TM 9-5855-884-24.

D For complete MAC, refer to TM 9-5855-885-24.

B

B-14 Change 13 Pages B-15 thru B-24 deleted

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A P P E N D I X C

E X P E N D A B L E S U P P L I E S A N D M A T E R I A L S L I S T

Sect ion I . I N T R O D U C T I O N

C - 1 . S C O P E

This appendix lists expendable supplies and materials you will need to operate andmaintain the TOW 2 Weapon System. These items are authorized to you by CTA 50-970,Expendable Items (Except Medical, Class V, Repair Parts, and Heraldic Items).

C - 2 . E X P L A N A T I O N O F C O L U M N S

a. Column 1 - Item Number. This number is assigned to the entry in the listingand is referenced in the narrative instructions to identify the material (e.g.,“Use desiccant item 8, Appendix C“).

b. Column 2 - Level. This column identifies the lowest level of maintenance thatrequires the listed item.

C - Operator/Crew

O - Organizational Maintenance

c. Column 3 - National Stock Number. This is the National stock number assigned tothe item; use it to request or order the item.

d. Column 4 - Description. Indicates the Federal item name and, if required, adescription to identify the item. The last line for each item indicates the partnumber followed by the Federal Supply Code for Manufacturer (FSCM) in parentheses,if applicable.

e. Column 5 - Unit of Measure (U/M). Indicates the measure used in performingthe actual maintenance function. This measure is expressed by a two-characteralphabetical abbreviation (e.g., ea, in., pr). If the unit of measure differsfrom the unit of issue, requisition the lowest unit of issue that will satisfyyour requirements.

C-1

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TM 9-1425-450-12

Sect ion I I . E X P E N D A B L E S U P P L I E S A N D M A T E R I A L S L I S T

Some materials in this section are toxic and/or flammable. Seefootnotes at the end of this listing.

(1) (2) (3) (4) (5)

NationalItem Stock

Number Level Number Description U/M

1 8040-00-843-3466 Adhesive, Fed Spec MMM-A-121GL Bond,Vulcanized Syn Rubber to Metal

2 C1,26810-00-201-0906 Alcohol, Denatured (81348) PT

0B760GRADE 3

3 0 8020-00-245-4509 Brush, Camel Hair EA

4 0 7920-00-282-2470 Brush, Scrub EA

5 0 8305-00-267-3015 Cloth, Cheesecloth, White,Unshrunk, 36 W, 0.87 to 1.03Oz. per Sq. Yd.CCCC440TY2CLASS 2 - 361NWIDE

6 8030-00-837-6557 Compound, Corrosion PreventiveMIL-C-16173, Grade 3

7 0 6850-00-835-0484 Deicing-Defrosting 0DO0190 (81346) OZ

8 0 6850-00-264-6568 Desiccant, Bag

9 0 7930-00-282-9699 Detergent GL

10 0 8010-01-160-6741 1,2 Paint, Polyurethane, MIL-C-46168,

Type Optional, Green 383 QT

11 01,28010-01-141-2419 Paint, Polyurethane, MIL-C-46168, QT

Type 1, Black 37038

12 C 6810-00-264-6637 Glycerol, Technical OG491 (81348) PT

1Toxic2Flammable

C-2 Change 4

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TM 9-1425-450-12

(1) (2) (3) (4) (5)

NationalItem Stock

Number Level Number Description U/M

13 9150-00-985-7246 Grease LB

15 C 6850-00-127-7193 M1 Antifogging Kit 95-16-1 EA

16 5120-00-293-2081 Orangewood Stick BX

17 0 8320-00-299-8625 Pad, Cotton LB

18 C 6640-00-597-6745 Paper, Lens (05347 )UUP313TYPE1OR2 (81348)UUP313CTYPE2 (81348)NNNP40

19 Plastisol, MIL-P-20689, Type 1

20 0 8010-01-193-0519 Primer, MIL-P-53022A QT

21 8080-00-835-2114 Primer, Fed Spec TT-P-1757, ColorYellow

23 8030-00-145-0300 Putty, MIL-P-8116B, Zinc Chromate

24 0 7920-00-205-1711 Rag, Wiping Cotton, Bleached or LBUnbleached, for General PurposeUse, SPEC DOD-R-30,50 lb BE MS16746-131 (96906)DDDR30CLASS2 (81348)

25 C 7930-00-880-4454 Solution, Lens Cleaning GL

26 6810-00-281-2785 1’2 Solvent, Cleaning, MethylethylKetone, Fed Spec TT-M-261

1Toxic2Flammable

Change 4 C-3

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TM 9-1425-450-12

(1)

ItemNumber

27

28

29

30

31

32

(2)

Level

O

0

0

0

(3)

NationalStockNumber

6520-00-501-8000

7510-00-266-6710

6810-00-579 -84311,2

8040-00-843-0802

8040-00-851-0211

8415-00-266-8673,8415-00-266-8675,8415-00-266-8677,8415-00-266-8679

(4)

Description

Syringe, Rubber

Tape, pressure sensitive adhesivecrepe paper backing, opaque,masking, 2 W MS16698-73

Toluene Technical, TT-T-548

Sealant, RTV, Clear

Sealant, RTV, Black

Gloves, Rubber, Acid andAlkali Resistant

(96906)

(81238)

(5)

U/M

EA

RO

PR

1Toxic2Flammable

C-4 Change 2

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TM 9-1425-450-12

APPENDIX D

COMPONENTS OF END ITEM LIST

D-1 . S C O P E

This appendix lists components of end item and basic issue items for the TOW 2Weapon System to help you inventory items required for safe and efficient operation.

D-2 . GENERAL

The Components of End Item and Basic Issue Items lists are divided into the follow-ing sections;

a. Section I. Components of End Item. This listing is for informational purposesonly, and is not authority to requisition replacements. These items are partof the end item, but are removed and separately packaged for transportation orshipment. As part of the end item, these items must be with the end itemwhenever it is issued or transferred between property accounts. Illustrationsare furnished to assist you in identifying the items.

b. Section II. Basic Issue Items. These are the minimum, essential itemsrequired to place the TOW 2 Weapon System in operation, to operate it, and toperform emergency repairs. Although shipped separately packaged, BII must bewith the TOW 2 Weapon System during operation and whenever it is transferredbetween property accounts. The illustrations will assist you with hard-to-identify items. This manual is your authority to request/requisition replace-ment BII, based on TOE/MTOE authorization of the end item.

D-3 . EXPLANATION OF COLUMNS

The following provides an explanation of columns found in the tabular listings:

a. Column (1) - Illustration Number (Illus Number). This column indicates thenumber of the illustration in which the item is shown.

b. Column (2) - National Stock Number. Indicates the National stock numberassigned to the item and will be used for requisitioning purposes.

c. Column (3) - Description. Indicates the Federal item name and, if required,a minimum description to identify and locate the item. The last line foreach item indicates the FSCM (in parentheses) followed by the part number.

d. Column (4) - Unit of Measure (U/M). Indicates the measure used in perform-ing the actual operation/maintenance function. This measure is expressed bya two-character alphabetical abbreviation (e.g., ea, in, pr).

e. Column (5) - Quantity required (Qty rqr). Indicates the quantity of theitem authorized to be used with/on the equipment.

D-1

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TM 9-1425-450-12

Section I. COMPONENTS OF END ITEM

NOTE

This appendix list is for inventory of your system only. If a parts list is needed, consultTM 9-1425-450-24P.

(1) (2) (3) (4) (5)lllus National Stock Description Q T YNumber Number FSCM and Part Number U/M rqr

D-1 LAUNCHER, TUBULAR, EA 1GUIDED MISSILE,M220A2, M220A3, M220A4(cons is t ing o f i tems l i s tedbelow) (18876)

1440-01-104-9834 131953251440-01-269-5849 13281240-03071440-01-298-9788 13195325-02061440-01-328-8286 13195325-03071440-01-287-0103 13195325-04081440-01-411-8942 13281240-0408

D-1

D-1

D-1

D-1

D-1

Battery Assembly, BB-287 EA 26140-00-454-8261 (X0-2)/T (18876) 10189465

Missile Guidance S e t , E A 1AN/TSQ-136 (18876)

1430-01-143-9408 130998901430-01-299-2287 13099890-02061430-01-328-8267 13099890-03071430-01-411-1684 13099890-0408

Mount, Tripod, Guided Missile EA 1Launcher M159A1 (18876)

1440-00-456-1731 10224837

Shroud Bag (18876) EA 11440-00-078-1641 10679791

Sight, Optical, Guided Missile EA 1Launcher, MX-9155/TSQ(18876)

1440-01-198-5891 132183141440-01-215-6014 132183291440-01-271-7428 13281200

D-2 Change 12

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TM 9-1425-450-12

COMPONENTS OF END ITEM (CONT)

*Cable is part of Traversing Unit

Figure D-1. Launcher, Tubular, Guided Missile, M220A2

Change 8 D-3

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TM 9-1425-450-12

S e c t i o n I . C O M P O N E N T S O F E N D I T E M ( C O N T )

Illus National Stock Description QtyNumber Number FSCM and Part Number U/M rqr

D-1 Strap Assembly (18876) EA 51440-00-478-0334 10679923

D-1 Traversing Unit, Guided Missile EA 1Launcher, M83 (18876)

1440-01-115-3405 13194972

D-1 Tube, Guided Missile Launcher, EA 1M22 (18876)

1440-00-196-0038 11486778

S e c t i o n I I . B A S I C I S S U E I T E M S

(1) (2) (3) (4) (5)Illus National Stock Description QtyNumber Number FSCM and Part Number U/M rqr

There are No Basic Issue Items Authorized

D-4 Change 10

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TM 9-1425-450-12

BASIC ISSUE ITEMS

(1) Illus

Number

(2) National Stock

Number

(3) Description

FSCM and Part Number

(4)

U/M

(5) Qty rqr

5850-01-076-1337 Field Handling Case, Boresight Collimator (80063) SM-D-806491-1 or SM-D-807945

EA 1

D-3 5855-01-077-4518 Equipment Cover (80063) SM-D-804553-1

EA 1

D-3 5855-01-143-3181 Vehicle Power Conditioner (80063) SM-C-969172 or (18876) 13251616

EA 1

D-3 6135-01-143-4470 or 5855-01-248-5725

Vehicle Power Conditioner (80063) SM-C-969172 or (18876) 13251616

EA 1

D-3 5855-01-213-3258 Field Handling Case, Battery (80063) SM-D-969617-1

EA 1

- None OPERATOR AND ORGANIZATIONAL MAINTENANCE MANUAL FOR TOW 2 WEAPON SYSTEM, M220A2 (18876)

EA 1

TM 9-1425-450-12

D-3

Change 13 D-5

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BASIC ISSUE ITEMS (CONT)

Figure D-3. Equipment Set, Night Vision Sight, AN/UAS-12A or AN/UAS-12C

D-6 Pages D-7 thru D-8 deleted Change 13

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BASIC ISSUE ITEMS (CONT)

Figure D-4. TOW Carrier Truck (HMMWV)

Figure D-5. DELETED

Change 13 D-9

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TM 9-1425-450-12

Figure D-6. DELETED

D-10 Change 13

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TM 9-1425-450-12

APPENDIX E

ADDITIONAL AUTHORIZATION LIST

Section 1. INTRODUCTION

E-1. SCOPE

This appendix lists additional items you are authorized for the support of the TOW 2 Weapon System.

E-2. GENERAL

This list identifies items that do not have to accompany the TOW 2 Weapon System and that do not have to be turned in with it. These items are all authorized to you by CTA, MTOE, TDA, or JTA.

E-3. EXPLANATION OF LISTING

Section II. ADDITIONAL AUTHORIZATION LIST

National stock numbers, descriptions, and quantities are provided to help you identify and request the additional items you require to support this equipment.

Illus

Number

National Stock

Number

Description

FSCM and Part Number

U/M

Qty rqr

- 6130-01-018-9786 Battery Charger, PP-4884A/T (18876) 11500154

EA 1

GO TO NEXT PAGE

Change 13 E-1

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TM 9-1425-450-12

Section II. ADDITIONAL AUTHORIZATION LIST (CONT)

Illus Number

National Stock Number

Description FSCM and Part Number

U/M Qty rqr

E-1 DELETED

E-2

13220196 or 5855-01-152-8781 5855-01-245-8689

*EQUIPMENT SET, NIGHT VISION SIGHT AN/UAS-12A (consisting of items listed below)

13251667

EA 1

E-2 AN/TAS-4A (18876)

5855-01-143-3183 5855-01-250-2343

Night Vision Sight (NVS) Set,

13220197 or 13251668

EA 1

E-2 5855-01-109-6433 5855-01-248-5724

Boresight Collimator, SU-93A/TAS (80063) SM-C-775002 or (18876) 13251666

EA 1

E-2

5850-01-076-1337 5850-01-227-5482

Field Handling Case, Boresight Collimator (80063) SM-D-806491-1 or SM-D-807945

EA 1

E-2 5855-01-077-4518

Equipment Cover (80063) SM-D-804553-1

EA 1

E-2 5855-01-143-3181 5855-01-250-4155 6130-01-224-7162

Vehicle Power Conditioner (80063) SM-C-969712 or (18876) 13251616 or (18876) 13221206

EA 1

E-2 6135-01-143-4470 5855-01-248-5725

Battery Power Conditioner (80063) SM-D-969172 or (18876) 13251627

EA 1

E-2 5855-01-213-3258

Field Handling Case, Battery (80063) SM-D-969617-1

EA 1

E-2

5855-01-212-4997 5855-01-281-9700

*EQUIPMENT SET, NIGHT VISION SIGHT AN/UAS-12A (consisting of items listed below) 13265071 or 13294193

EA 1

*Additional Authorized Items include either AN/UAS-12A or AN/UAS-12C.

GO TO NEXT PAGE

E-2 Change 13

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TM 9-1425-450-12

Section II. ADDITIONAL AUTHORIZATION LIST (CONT)

Illus Number

National Stock Number

Description FSCM and Part Number

U/M Qty rqr

E-2

5855-01-281-9699 5855-01-300-8215

13265072 13294194

5855-01-218-6992

5855-01-316-9644 5855-01-328-6204

NIGHT VISION SIGHT (NVS) Set, AN/TAS-4C (18876)

13265254 13265281 13285289

None

EA 1

OPERATOR AND ORGANIZATIONAL MAINTENANCE MANUAL FOR TOW 2 WEAPON SYSTEM, M220A2 (18876) TM 9-1425-450-12

FIGURE E-1. DELETED

Change 13 E-3

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TM 9-1425-450-12

ADDITIONAL AUTHORIZATION LIST (CONT)

Figure E-2. Equipment Set, Night Vision Sight, AN/UAS-12A or AN/UAS-12C

E-4 Change 10 t7U.S. GOVERNMENT PRINTING OFFICE: 1994- S33-072/00038

Page 461: TM 9 1425 450 12 TOW 2 Weapon System

By Order of the Secretary of the Army:

Official:

E. C. MEYERGeneral, United States Army

Chief of Staff

ROBERT M. JOYCEMajor General, United States Army

The Adjutant General

Distribution:

To be distributed in accordance with DA Form 12-32, Section II, OrganizationalMaintenance requirements for TOW Weapon System.

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These are the instructions for sending an electronic 2028The following format must be used if submitting an electronic 2028. The subject line must beexactly the same and all fields must be included; however only the following fields aremandatory: 1, 3, 4, 5, 6, 7, 8, 9, 10, 13, 15, 16, 17, and 27.

From: “Whomever” <[email protected]>To: [email protected]

Subject: DA Form 20281. From: Joe Smith2. Unit: home3. Address: 4300 Park4. City: Hometown5. St: MO6. Zip: 777777. Date Sent: 19--OCT--938. Pub no: 55--2840--229--239. Pub Title: TM10. Publication Date: 04--JUL--8511. Change Number: 712. Submitter Rank: MSG13. Submitter FName: Joe14. Submitter MName: T15. Submitter LName: Smith16. Submitter Phone: 123--123--123417. Problem: 118. Page: 219. Paragraph: 320. Line: 421. NSN: 522. Reference: 623. Figure: 724. Table: 825. Item: 926. Total: 12327. Text:This is the text for the problem below line 27.

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RECOMMENDED CHANGES TO PUBLICATIONS AND

BLANK FORMSFor use of this form, see AR 25--30; the proponent agency is ODISC4.

Use Part II (reverse) for Repair Parts and Spe-cial Tool Lists (RPSTL) and Supply Catalogs/Supply Manuals (SC/SM)

DATE

8/30/02

TO: (Forward to proponent of publication or form)(Include ZIP Code)

Commander, U.S. Army Aviation and Missile Command

ATTN: AMSAM--MMC--MA--NP

R eds t one A r s enal, AL 35898

FROM: (Activity and location)(Include ZIP Code)

MSG, Jane Q. Doe

1234 Any Street

Nowhere Town, AL 34565

PART 1 -- ALL PUBLICATIONS (EXCEPT RPSTL AND SC/SM) AND BLANK FORMS

PUBLICATION/FORM NUMBER

TM 9--1005--433--24DATE

16 Sep 2002TITLE Organizational, Direct Support, And GeneralSupport Maintenance Manual for Machine Gun, .50Caliber M3P and M3P Machine Gun Electrical Test SetUsed On Avenger Air Defense Weapon System

ITEM

NO.

PAGE

NO.

PARA--

GRAPH

LINE

NO. *

FIGURE

NO.

TABLE

NO.RECOMMENDED CHANGES AND REASON

1 WP0005

PG 3

2 Test or Corrective Action column should identify a different WP number.

* Reference to line numbers within the paragraph or subparagraph.

TYPED NAME, GRADE OR TITLE

MSG, Jane Q. Doe, SFC

TELEPHONE EXCHANGE/AUTOVON, PLUS EXTEN-SION

788--1234

SIGNATURE

DA FORM 2028, FEB 74 REPLACES DA FORM 2028, 1 DEC 68, WHICH WILL BE USED. USAPA V3.01

Page 466: TM 9 1425 450 12 TOW 2 Weapon System

TO: (Forward direct to addressee listed in publication)

Commander, U.S. Army Aviation and Missile Command

ATTN: AMSAM--MMC--MA--NP

R eds t one A r s enal, AL 35898

FROM: (Activity and location) (Include ZIP Code)

MSG, Jane Q. Doe

1234 Any Street

Nowhere Town, AL 34565

DATE

8/30/02

PART II -- REPAIR PARTS AND SPECIAL TOOL LISTS AND SUPPLY CATALOGS/SUPPLY MANUALS

PUBLICATION NUMBER DATE TITLE

PAGE

NO.

COLM

NO.

LINE

NO.

NATIONAL STOCK

NUMBER

REFERENCE

NO.

FIGURE

NO.

ITEM

NO.

TOTAL NO.OF MAJOR

ITEMSSUPPORTED

RECOMMENDED ACTION

PART III -- REMARKS (Any general remarks or recommendations, or suggestions for improvement of publications and

blank forms. Additional blank sheets may be used if more space is needed.)

TYPED NAME, GRADE OR TITLE

MSG, Jane Q. Doe, SFC

TELEPHONE EXCHANGE/AUTOVON,PLUS EXTENSION

788--1234

SIGNATURE

USAPA V3.01

Page 467: TM 9 1425 450 12 TOW 2 Weapon System

RECOMMENDED CHANGES TO PUBLICATIONS AND

BLANK FORMSFor use of this form, see AR 25--30; the proponent agency is ODISC4.

Use Part II (reverse) for Repair Parts and Spe-cial Tool Lists (RPSTL) and Supply Catalogs/Supply Manuals (SC/SM)

DATE

TO: (Forward to proponent of publication or form)(Include ZIP Code) FROM: (Activity and location)(Include ZIP Code)

PART 1 -- ALL PUBLICATIONS (EXCEPT RPSTL AND SC/SM) AND BLANK FORMS

PUBLICATION/FORM NUMBER DATE T I T LE

ITEM

NO.

PAGE

NO.

PARA--

GRAPH

LINE

NO. *

FIGURE

NO.

TABLE

NO.RECOMMENDED CHANGES AND REASON

* Reference to line numbers within the paragraph or subparagraph.

TYPED NAME, GRADE OR TITLE TELEPHONE EXCHANGE/AUTOVON, PLUS EXTEN-SION

SIGNATURE

DA FORM 2028, FEB 74 REPLACES DA FORM 2028, 1 DEC 68, WHICH WILL BE USED. USAPA V3.01

Commander, U.S. Army Aviation and Missile CommandATTN: AMSAM-MMC-MA-NPRedstone Arsenal, AL 35898

Page 468: TM 9 1425 450 12 TOW 2 Weapon System

TO: (Forward direct to addressee listed in publication) FROM: (Activity and location) (Include ZIP Code) DATE

PART II -- REPAIR PARTS AND SPECIAL TOOL LISTS AND SUPPLY CATALOGS/SUPPLY MANUALS

PUBLICATION NUMBER DATE TITLE

PAGE

NO.

COLM

NO.

LINE

NO.

NATIONAL STOCK

NUMBER

REFERENCE

NO.

FIGURE

NO.

ITEM

NO.

TOTAL NO.OF MAJOR

ITEMSSUPPORTED

RECOMMENDED ACTION

PART III -- REMARKS (Any general remarks or recommendations, or suggestions for improvement of publications and

blank forms. Additional blank sheets may be used if more space is needed.)

TYPED NAME, GRADE OR TITLE TELEPHONE EXCHANGE/AUTOVON,PLUS EXTENSION

SIGNATURE

USAPA V3.01

Commander, U.S. Army Aviation and Missile CommandATTN: AMSAM-MMC-MA-NPRedstone Arsenal, AL 35898

Page 469: TM 9 1425 450 12 TOW 2 Weapon System

The Metric System and Equivalents

Linear Measure Liquid Measure

1 centiliter = 10 milliters = .34 fl. ounce1 centimeter = 10 millimeters = .39 inch 1 deciliter = 10 centiliters = 3.38 fl. ounces1 decimeter = 10 centimeters = 3.94 inches 1 liter = 10 deciliters = 33.81 fl. ounces1 meter = 10 decimeters = 39.37 inches 1 dekaliter = 10 liters = 2.64 gallons1 dekameter = 10 meters = 32.8 feet 1 hectoliter = 10 dekaliters = 26.42 gallons1 hectometer = 10 dekameters = 328.08 feet 1 kiloliter = 10 hectoliters = 264.18 gallons1 kilometer = 10 hectometers = 3,280.8 feet

Square MeasureWeights

1 sq. centimeter = 100 sq. millimeters = .155 sq. inch1 centigram = 10 milligrams = .15 grain 1 sq. decimeter = 100 sq. centimeters = 15.5 sq. inches1 decigram = 10 centigrams = 1.54 grains 1 sq. meter (centare) = 100 sq. decimeters = 10.76 sq. feet1 gram = 10 decigram = .035 ounce 1 sq. dekameter (are) = 100 sq. meters = 1,076.4 sq. feet1 decagram = 10 grams = .35 ounce 1 sq. hectometer (hectare) = 100 sq. dekameters = 2.47 acres1 hectogram = 10 decagrams = 3.52 ounces 1 sq. kilometer = 100 sq. hectometers = .386 sq. mile1 kilogram = 10 hectograms = 2.2 pounds1 quintal = 100 kilograms = 220.46 pounds Cubic Measure1 metric ton = 10 quintals = 1.1 short tons

1 cu. centimeter = 1000 cu. millimeters = .06 cu. inch1 cu. decimeter = 1000 cu. centimeters = 61.02 cu. inches1 cu. meter = 1000 cu. decimeters = 35.31 cu. feet

Approximate Conversion Factors

To change To Multiply by To change To Multiply by

inches centimeters 2.540 ounce-inches Newton-meters .007062feet meters .305 centimeters inches .394yards meters .914 meters feet 3.280miles kilometers 1.609 meters yards 1.094square inches square centimeters 6.451 kilometers miles .621square feet square meters .093 square centimeters square inches .155square yards square meters .836 square meters square feet 10.764square miles square kilometers 2.590 square meters square yards 1.196acres square hectometers .405 square kilometers square miles .386cubic feet cubic meters .028 square hectometers acres 2.471cubic yards cubic meters .765 cubic meters cubic feet 35.315fluid ounces milliliters 29,573 cubic meters cubic yards 1.308pints liters .473 milliliters fluid ounces .034quarts liters .946 liters pints 2.113gallons liters 3.785 liters quarts 1.057ounces grams 28.349 liters gallons .264pounds kilograms .454 grams ounces .035short tons metric tons .907 kilograms pounds 2.205pound-feet Newton-meters 1.356 metric tons short tons 1.102pound-inches Newton-meters .11296

Temperature (Exact)

°F Fahrenheit 5/9 (after Celsius °Ctemperature subtracting 32) temperature

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PIN: 053139-000