welcome to technical order 00-105e-9, 1 february 2006 ... segment 18.pdf · mishap response...
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THIS IS SEGMENT 18 COVERING CHAPTER 18 TO THE DC-10.
TECHNICAL ORDER 00-105E-9 TECHNICAL CONTENT MANAGER
WRITTEN CORRESPONDENCE:
HQ AFCESA/CEXFATTN: Fire and Emergency Services Egress Manager139 Barnes Drive Suite 1Tyndall AFB, Florida 32403-5319
E-MAIL: [email protected]
INTERNET: HQ AFCESA Fire and Emergency Services PUBLIC WEB PAGE: http://www.afcesa.af.mil/CEX/cexf/index.asp Safety Supplements: http://www.afcesa.af.mil/CEX/cexf/_firemgt.asp
PHONE: (850) 283-6150DSN 523-6150
FAX: (850) 283-6383DSN 523-6383
For technical order improvements, correcting procedures, and other inquiries,please use the above media most convenient.
This page is provided to notifiy the user of any informational changes made to Technical Order 00-105E-9 in this Segment and the currentRevision. Informational changes will be referenced in the Adobe Reader’s Bookmark tool as a designator symbol illustrated as a <[C]> forquick reference to the right of the affected aircraft. The user shall insure the most current information contained in this TO is used for hisoperation. Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies. If the user printsout pages his unit requires, the user shall print the affected page(s), remove and destroy the existing page(s), and insert the newly printedpage(s) in the binder provided for that purpose. A Master of this TO shall be retained in the unit’s library for reference, future printingrequirements and inspections.
CHAPTER AIRCRAFT PAGE EXPLANATION OF CHANGE
SEGMENT 18 INFORMATION CHANGE NOTICE
None.
TO 00-105E-9
Chapter 18 Cover
NOTE
Chapter 18 contains emergency rescue andmishap response information for the following aircraft:
DC-3DC-6DC-7DC-8DC-9
DC-10MD-11MD-80MD-90
L-1011-1L-1011-500
707717720727737747757767777
T.O. 00-105E-9
18-1. INTRODUCTION AND USE.
18-2. This section contains emergency rescue andmishap response information illustrations in alpha-numerical order relative to type and model of aircraft.This arrangement of illustrations is maintained fromChapter 4 throughout the remainder of the publica-tion.
18-3. GENERAL ARRANGEMENT.
18-4. Aircraft type designation has been positionedin the upper right corner of the horizontal illustrationfor rapid identification. Additional aids to rapid orien-tation are:
a. Recent technological advances in avia-tion have caused concern for the modern firefighter.Aircraft hazards, cabin configurations, airframe ma-terials, and any other information that would be help-ful in fighting fires, the locating and rescue of per-sonnel will be added as the information becomes avail-able.
b. Suggested special tools/equipment arelisted in the upper left corner, on the Aircraft/Entrypage of each listed aircraft.
c. Procedural steps covering emergency/normal entrances, cut-ins, engine/APU shutdown,safetying ejection/escape systems, and aircrew ex-traction are outlined on the left side of each page withcoordinated illustrations on the right.
d. Illustrations located on right side of pagesare coordinated with text by numerals and small let-ters depicting both paragraph and subparagraph onthe page.
e. Each illustration is consistently coloredand/or pattern keyed to highlight essential emergencyrescue information.
f. Details are pulled directly from the illustra-tion to highlight an area, thus eliminating unneces-sary searching for desired information.
CHAPTER 18
COMMERCIAL/CIVIL RESERVE AIRFLEET(CRAF)
AEROSPACE EMERGENCY RESCUEAND MISHAP RESPONSE INFORMATION
18-1
18-5. CIVIL RESERVE AIR FLEET (CRAF)
Major US carriers represented in CRAF are man-aged by AMC, Scott AFB, IL in the Civil Air Director-ate for Operations. Short and long range aircraft areused based on a particular task. Nearly 20 milliontons capacity can be moved on any given day. 536aircraft are currently committed.
Commercial aircraft used as US strategic airlifters havepromised, under the CRAF program, to make up morethan 90 percent of the Air Force’s long-range passen-ger-carrying capability and 30 percent of its cargo-hauling capability. As of 1995, commitments for the747 aircraft designated by the USAF as the C-19, arefor 136 passenger and 110 cargo equivalents. Thesefigures are based on current European-based sce-narios. This affects long-range international routes.
The 747 “classic” or -100/200 model can be convertedfrom a passenger to a freighter configuration in a mat-ter of hours. The main entrance is main deck cargocapability where the side cargo door is modified forthis conversion when needed. Passenger seats areremoved or reduced in number and the main deck isconverted to accept pallets.
Aeromedical evacuation aircraft or flying hospitalconfigurations are also part of CRAF. Air Forcekits converting aircraft into flying medical facilitiesfit only Boeing 767s. See the 767 segment for thisinformation. 44 aircraft are needed to fulfill require-ments. 19 are committed.
There are three stages in a call-up emergency:
Stage I: Can be set in motion by the head of the USTransportation Command. The use of a few aircraftfrom any one carrier resulting in a minimal impact onnormal civilian business.
Stage II: Activated only at the Secretary of Defenselevel. Impact is necessarily more serious. Airlinesshould be able to maintain normal operations.
Stage III: Must be authorized by an emergency dec-laration from the US President or Congress. Wouldlikely cause a serious impact on US civilian transpor-tation schedules.
FAA Part 139.315 - Index Categories Based on Aircraft Length ICAO Annex 14 - RFFS Categories Based on Aircraft Length & Fuselage Width (aircraft overall length; maximum fuselage width)
Index A - < 90' Category 1 - < 9m (29.5'); 2m (6.6') Category 6 - 28m (91.9') - < 39m (128.0'); 5m (16.4")Index B - 90' - <126' Category 2 - 9m (29.5') - <12m (39.4'); 2m (6.6') Category 7 - 39m (128.0') -<49m (160.8'); 5m (16.4")Index C - 126' - <159' Category 3 - 12m (39.4') - <18m (59.1'); 3m (9.8') Category 8 - 49m (160.8') - <61m (200.1'); 7m (23.0')Index D - 159' - <200' Category 4 - 18m (59.1') - <24m (78.7'); 4m (13.1') Category 9 - 61m (200.1') - <76m (249.3'); 7m (23.0')Index E - 200' or greater Category 5 - 24m (78.7') - <28m (91.9'); 4m (13.1') Category 10 - 76m (249.3') - <90m (295.3'); 8m (26.3')
FAA ARFF (Aircraft Rescue & Fire Fighting) Index ICAO RFFS (Rescue Fire Fighting Service) Category*Aircraft A B C D E Aircraft 6 7 8 9 10707 (all) X 707 (all) X717-200 X 717-200 X720 X 720 X727-100 X 727-100 X727-200 X 727-200 X737-100 X 737-100 X737-200 X 737-200 X737-300 X 737-300 X737-400 X 737-400 X737-500 X 737-500 X737-600 X 737-600 X737-700 X 737-700 X737-800 X 737-800 X737-900 X 737-900 XBBJ X BBJ XBBJ2 X BBJ2 X747SP X 747SP X747-100,200,300 X 747-100,200,300 X 747-400, 400ER X 747-400, 400ER X 757-200 X 757-200 X757-300 X 757-300 X767-200 X 767-200 X767-300 X 767-300 X767-400 X 767-400 X 777-200, 200LR X 777-200, 200LR X 777-300, 300ER X 777-300, 300ER X DC-8-43,55 X DC-8-43,55 XDC-8-61,71 X DC-8-61,71 XDC-8-62,72 X DC-8-62,72 XDC-8-63,73 X DC-8-63,73 XDC-9-15 X DC-9-15 XDC-9-21 X DC-9-21 XDC-9-32 X DC-9-32 XDC-9-41 X DC-9-41 XDC-9-51 X DC-9-51 XDC-10-10 X DC-10-10 XDC-10-30,40 X DC-10-30,40 XMD-11 X MD-11 X MD-81,82,83,88 X MD-81,82,83,88 XMD-87 X MD-87 XMD-90-30 X MD-90-30 X
* No Boeing Commercial Jet Aircraft In Categories 1 - 5 or 10
Boeing Commercial Aircraft - Rescue & Fire Fighting Categories (FAA & ICAO)
10/11/02Airport Technology
Boeing Commercial Airplanes
DC-3
DC
-3.
T.O. 00-105E
-9
AIRCRAFT PAINT SCHEME
1
DC-3
C-47
DC-3
DC
-3.
T.O. 00-105E
-9
AIRCRAFT DIMENSIONS
2
HEIGHT 16’ 11”(5.18 M)
LENGTH63’ 9” (19.43 M)
WING SPAN95’ 6 “ (29.20 M)
DC-3
DC
-3.
T.O. 00-105E
-9
3
FLAMMABLE MATERIALS AND ENTRY/EXIT LOCATIONS
HYDRAULIC FLUID TANK
FUELTANKS804 GAL(3043 L)
EMERGENCY EXITS
CARGO DOOR
MAIN CABIN ENTRANCE DOOR
ENGINEOIL TANK
ENGINE OIL TANK
BATTERIES
PILOT’S ENTRY DOOR
OXYGEN BOTTLE
DEICER FLUIDTANK
OVERHEAD EMERGENCY EXIT
A 2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL EMERGENCYEXITS AND FORCED ACCESS AREAS
DC-3
DC
-3.
T.O. 00-105E
-9
4
SPECIAL TOOLS/EQUIPMENTPower Rescue SawFire Drill II
AIRCRAFT ENTRY
1. EMERGENCY ENTRY - DC-3/C-47
a. Pull emergency exit external handle, located on emergency exit aft of wing, each side of fuselage, to unlock and pull emergency exit hatch outward.
b. Rotate overhead crew escape hatch handle, located forward top center of fuselage, clockwise then pull hatch up and aft.
2. NORMAL ENTRY
a. Rotate main cabin entry handle, located on main cabin entry door, clockwise, then open door outward.
b. Pull pilot’s cargo door handle, located on fuselage forward right side on pilot’s cargo door, down. Open door outward.
3. CUT-IN
a. Cut-in areas are located at normal and emergency entrance points and at crew windows, left and right side of flightdeck.
NOTE: Crew size: 2 to 3. Passengers: 27 to 28.
FIRE CONTROLBOX (AC-47D)
400 GAL
400 GAL
204
204
200
200
385 385
PORTABLEOXYGENBOTTLES
BATTERIES
FLARE LAUNCHER
AMMUNITION
GUN POSITIONS (AC-47D)
OXYGEN CYLINDERS
1bOVERHEAD CREWEMERGENCY EXIT3aCUT-IN
1aEMERGENCY EXITS3aCUT-IN
2aMAIN CABINENTRY DOOR
3aCUT-IN
2bCREW ENTRY DOOR3aCUT-IN
3aFLIGHTDECKWINDOWSCUT-IN
DC-3
DC
-3.
T.O. 00-105E
-9
5
ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE EMERGENCY SHUTDOWN
a. Pull firewall shutoff valve handle, located on engine fire extinguisher control panel, to the OUT position.
b. Turn master ignition switch, located on center overhead panel, to OFF position.
c. Turn battery switch, located on overhead switch panel, to OFF position.
2. ENGINE NORMAL SHUTDOWN
a. Retard throttle control levers, located between pilot’s and co-pilot’s seats, to full CLOSE position.
b. Place mixture control levers, located between pilot’s and co-pilot’s seats, to the aft CUT-OFF position.
c. Turn master ignition switch, located on center overhead switch panel, to OFF position.
d. Turn battery switch, located on overhead switch panel, to OFF position.
3. AIRCREW EXTRACTION
a. Unlatch lap belt and remove shoulder harness from crewmember(s).
NOTE: If seat tracks are not damaged during crash landing, use adjustable seat control to retract seats to aft position in removing crewmember(s).
2aTHROTTLECONTROLLEVERS
2bMIXTURECONTROLLEVERS
1b, 2cMASTERIGNITIONSWITCHES
ENGINE FIRE EXTINGUISHER CONTROL PANEL
1c, 2dBATTERY SWITCH
1aFIREWALL SHUTOFFVALVE HANDLES
DC-6
DC
-6.
T.O. 00-105E
-9
AIRCRAFT PAINT SCHEME
1
DC-6
USAF: C-118 USN: R6D “LIFTMASTER”VC-118 “The Independence” AND VIP
DC-6 FIREBOMBER
DC-6 FIREBOMBER“Still in service.”
DC-6
DC
-6.
T.O. 00-105E
-9
AIRCRAFT DIMENSIONS
2
WINGSPAN 117' 6" (35.8 M)
HEIGHT 28' 8" (8.7 M)
LENGTH 105' 7" (32.1 M)
DC-6
DC
-6.
T.O. 00-105E
-9
3
FLAMMABLE MATERIALS AND ENTRY/EXIT LOCATIONSA 2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL EMERGENCYEXITS AND FORCED ACCESS AREAS
HYDRAULIC FLUID TANK
FUEL TANK2,702 GAL(10,228 L)
FORCEDACCESSAREAS
CARGO DOOR (DC-6A ONLY)
MAIN CABIN ENTRANCE DOOR
ENGINEOIL TANKS
ENGINE OIL TANK
BATTERIESCARGO DOOR(DC-6A ONLY)
OXYGEN BOTTLE
DEICERFLUIDTANK
PILOT’S ENTRANCE DOOR AUXILIARY OIL TANKS
FUEL TANK2,702 GAL(10,228 L)
FORCEDACCESSAREAS
DC-6
DC
-6.
T.O. 00-105E
-9
4
SPECIAL TOOLS/EQUIPMENTPower Rescue SawFire Drill II
AIRCRAFT ENTRY - DC-6/C-118
1. NORMAL ENTRY
a. Rotate external control handle, located on main cabin entry door aft left side of fuselage, UP to open door.
b. Rotate external control handle, located on crew entry door forward right side of fuselage, UP to open door.
2. EMERGENCY ENTRY
a. Pull handle on emergency exits, located over each wing, OUT and pull exit hatch outward.
3. CUT-IN
a. Cut-in areas (marked in red) are located at normal and emergency entries and at cargo compartment windows and doors.
FUEL TANKS
MAIN CABINENTRY DOOR
3aCUT-IN
2aEMERGENCYEXITS
CREWENTRYDOOR
BATTERIES
OXYGEN BOTTLES(C-118 ONLY)
695
526
719
695
526
719762
762
1bCREW ENTRYEXTERNALCONTROLHANDLE
1aPASSENGER ENTRYEXTERNAL CONTROL HANDLE
CARGO DOOR (C-118 ONLY)
AFT CARGODOOR (C-118 ONLY)
DC-6
DC
-6.
T.O. 00-105E
-9
5
ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN
a. Retard throttle control levers, located on control pedestal, to the CLOSED position.
b. Place mixture control levers, located on the control pedestal, to the CLOSED position.
c. Place ignition switches, located on forward overhead panel, to the OFF position.
d. Place master battery/generator switches cutoff bar, located on forward overhead panel, to the OFF position.
NOTE: If engines fail to shutdown, pull engine emer- gency T-handles, located on the main fire control panel, to the FULL-OUT position.
3. AIRCREW EXTRACTION
a. Unlatch lap belt and remove shoulder harness from crewmember(s).
NOTE: If seat tracks are not damaged during crash landing, use adjustable seat control to retract seats to aft position in removing crewmember(s).
1dMASTER BATTERY/GENERATORSWITCHES CUTOFF BAR
FORWARD OVERHEAD PANEL
1cIGNITIONSWITCHES
ENGINE EMERGENCY T-HANDLES
1aTHROTTLES
CONTROL PEDESTAL
1bMIXTURECONTROLLEVERS
DC-7
DC
-7.
T.O. 00-105E
-9
AIRCRAFT PAINT SCHEME
1
DC-7
C-74 GLOBEMASTER I
DC-7
DC
-7.
T.O. 00-105E
-9
2
AIRCRAFT DIMENSIONS
WINGSPAN 117' 6" (35.8 M)
HEIGHT 28' 7" (8.7 M)
LENGTH 108' 11" (33.2 M)
C-74
DC-7
DC
-7.
T.O. 00-105E
-9
3
FLAMMABLE MATERIALS AND ENTRY/EXIT LOCATIONSDC-7/DC-7B SERIES
FUEL TANK 2,756 GAL (10,433 L)
ENGINE OIL TANKS
ENGINE OIL TANKS
BATTERIES
FIRE ACCESS
PORTABLEOXYGENBOTTLES
FIRE EXTINGUISHER BOTTLES
PORTABLE OXYGEN BOTTLES
FLARES
FUEL TANK 2,756 GAL (10,433 L)
AUXILIARY ENGINE OIL TANK ON SOME ACFT
DC-7
DC
-7.
T.O. 00-105E
-9
4
FLAMMABLE MATERIALS AND ENTRY/EXIT LOCATIONS-ContinuedDC-7C SERIES
FUEL TANK 3,800 GAL (14,385 L)
ENGINE OIL TANKS
ENGINE OIL TANKS
BATTERIES
FIRE ACCESS
PORTABLEOXYGENBOTTLES
FIRE EXTINGUISHER BOTTLES AUXILIARY ENGINE OIL TANK ON SOME ACFT
FLARES
FUEL TANK 3,800 GAL (14,385 L)
DC-7
DC
-7.
T.O. 00-105E
-9
5
MAIN CABIN DOOR
1aMAIN CABIN DOOR
2a EMERGENCYEXIT DOOR
TYPICAL ESCAPE HATCHES
1aCREW AND CARGO DOOR
CHOP OUT AREAS
CHOP OUT AREAS
TYPICAL FIRE ACCESS
SPECIAL TOOLS/EQUIPMENTPower Rescue SawFire Drill II
AIRCRAFT ENTRY - DC-7 SERIES
1. NORMAL ENTRY- CREW AND MAIN DOORS
a. Rotate handle counterclockwise.
b. Pull door outward.
2. EMERGENCY EXIT DOORS
a. Pull handle out.
b Push door inward.
3. ESCAPE HATCHES
a. Pull handle out.
b. Rotate handle counterclockwise.
c. Pull hatch out.
4. CHOP OUT/CUT-IN AREAS
a. Cut-in areas (marked in red) are located at normal and emergency entries and at cargo compartment windows and doors.
1aCREW, MAIN ANDCARGO DOOR HANDLE
2aEMERGENCY EXIT DOOREXTERNAL HANDLE
4aCHOP OUT/CUT-IN
AIRCRAFT CROSS SECTION
3aESCAPE HATCHEXTERNAL HANDLE
DC-7
DC
-7.
T.O. 00-105E
-9
FLAMMABLE MATERIALS AND ENTRY/EXIT LOCATIONS-ContinuedDC-7C CARGO6
FUEL TANK 3,800 GAL (14,385 L)
ENGINE OIL TANKS
ENGINE OIL TANKS
BATTERIES
FIRE ACCESS
PORTABLEOXYGENBOTTLES
FIRE EXTINGUISHER BOTTLES AUXILIARY ENGINE OIL TANK ON SOME ACFT
FLARES
FUEL TANK 3,800 GAL (14,385 L)
DC-7
DC
-7.
T.O. 00-105E
-9
7
SPECIAL TOOLS/EQUIPMENTPower Rescue SawFire Drill II
AIRCRAFT ENTRY - DC-7C CARGO
1. NORMAL ENTRY- CREW AND MAIN DOORS
a. Rotate handle counterclockwise.
b. Pull door outward.
2. EMERGENCY EXIT DOORS
a. Pull handle out.
b Push door inward.
3. ESCAPE HATCHES
a. Pull handle out.
b. Rotate handle counterclockwise.
c. Pull hatch out.
4. CHOP OUT/CUT-IN AREAS
a. Cut-in areas (marked in red) are located at normal and emergency entries and at cargo compartment windows and doors.
1aCREW, MAIN ANDCARGO DOOR HANDLE
2aEMERGENCY EXIT DOOREXTERNAL HANDLE
4aCHOP OUT/CUT-IN
AIRCRAFT CROSS SECTION
3aESCAPE HATCHEXTERNAL HANDLE
1aMAINCABINDOOR
2aEMERGENCYEXIT DOOR
TYPICALESCAPEHATCHES
1aCREW ANDCARGO DOOR
CHOP OUTAREAS
CHOP OUTAREAS
TYPICAL FIRE ACCESS
FWDCARGO DOOR
AFTCARGO DOOR
FLARES
FIREEXTINGUISHER BOTTLES
SIDEWINDOW(2 EACH)
OXYGEN BOTTLE(2 EACH)
DC-7
DC
-7.
T.O. 00-105E
-9
ENGINE SHUTDOWN ANDAIRCREW EXTRACTION
7
1. ENGINE SHUTDOWN
a. Retard throttle control levers, located on control pedestal, to the CLOSED position.
b. Place mixture control levers, located on the control pedestal, to the CLOSED position.
c. Place ignition switches, located on forward overhead panel, to the OFF position.
d. Place master battery/generator switches cutoff bar, located on forward overhead panel, to the OFF position.
NOTE: If engines fail to shutdown, pull engine emer- gency T-handles, located on the main fire control panel, to the FULL-OUT position.
3. AIRCREW EXTRACTION
a. Unlatch lap belt and remove shoulder harness from crewmember(s).
NOTE: If seat tracks are not damaged during crash landing, use adjustable seat control to retract seats to aft position in removing crewmember(s).
1dMASTER BATTERY/GENERATORSWITCHES CUTOFF BAR
FORWARD OVERHEAD PANEL
1cIGNITIONSWITCHES
ENGINE EMERGENCY T-HANDLES
1aTHROTTLES
CONTROL PEDESTAL
1bMIXTURECONTROLLEVERS
DC
-8. DC-8T.O
. 00-105E-9
AIRCRAFT PAINT SCHEME
1
DC
-8. DC-8T.O
. 00-105E-9
AIRCRAFT DIMENSIONS
2
150.7’(45.93 M)
12.25’ (3.73 M)
13.55’ (4.13 M)
15.9’ (4.85 M)
57.5’ (17.53 M)
146.25’ (44.58 M) 47.5’
(14.48 M)
20.8’ (6.34 M) 142.4’
(43.40 M)
SCALE
5 10 15 M
0 10 20 30 40 50 FT
NOTE:HEIGHT VARIANCE
DC-8-4343’ 5.2” (13.24 M) MAXIMUM42’ 1.7” (12.84 M) MINIMUM
DC-8-43
SEE NOTE
DC
-8. DC-8T.O
. 00-105E-9
DC-8-55, 55F
AIRCRAFT DIMENSIONS-Continued
3
150.7’(45.93 M)
12.25’ (3.73 M)
13.55’ (4.13 M)
15.9’ (4.85 M)
57.5’ (17.53 M)
146.25’ (44.58 M) 47.5’
(14.48 M)
20.8’ (6.34 M) 142.4’
(43.40 M)
SCALE
5 10 15 M
0 10 20 30 40 50 FT
SEE NOTE
NOTE:HEIGHT VARIANCE
DC-8-55:43’ 6.7” (13.28 M) MAXIMUM42’ 1.7” (12.85 M) MINIMUM
DC-8-55F:43’ 8.9” (13.33 M) MAXIMUM42’ 1.3” (12.84 M) MINIMUM
DC
-8. DC-8T.O
. 00-105E-9
DC-8-62, -62F, -72, -72F
AIRCRAFT DIMENSIONS-Continued
4
157.5’(48.01 M)
12.25’ (3.73 M)
13.55’ (4.13 M)
15.9’ (4.85 M)
60.8’ (18.53 M) 152.9’
(46.60 M) 47.5’ (14.48 M)
20.8’ (6.34 M) 148.4’
(45.23 M)
SCALE
5 10 15 M
0 10 20 30 40 50 FT
SEE NOTE
NOTE:HEIGHT VARIANCE
DC-8-62, -72:43’ 3.0” (13.18 M) MAXIMUM42’ 3.6” (12.89 M) MINIMUM
DC-8-62F, -72F:43’ 3.8” (13.20 M) MAXIMUM42’ 3.0” (12.88 M) MINIMUM
DC
-8. DC-8T.O
. 00-105E-9
NOTE:HEIGHT VARIANCE
DC-8-61, -7143’ 2.7” (13.17 M) MAXIMUM41’ 11.7” (12.79 M) MINIMUM
DC-8-61F, -71F:43’ 2.3” (13.16 M) MAXIMUM42’ 1.0” (12.82 M) MINIMUM
DC-8-63, -73:43’ 0” (13.11 M) MAXIMUM42’ 1.4” (12.84 M) MINIMUM
DC-8-63F, -73F:43’ 1.5” (13.14 M) MAXIMUM42’ 1.4” (12.84 M) MINIMUM
DC-8-61, -61F, -63, 63F, -73, -73F
5
AIRCRAFT DIMENSIONS-Continued
187.4’(57.12 M)
12.25’ (3.73 M)
13.55’ (4.13 M)
15.9’ (4.85 M)
77.50’ (23.62 M) 182.9’
(55.75 M) 47.5’ (14.48 M)
20.8’ (6.34 M) 142.4’
(43.40 M)
SCALE
5 10 15 M
0 10 20 30 40 50 FT
SEE NOTE
DC
-8. DC-8T.O
. 00-105E-9
BATTERY(LOCATED IN RTWHEEL WELL)
CREWOXYGENSYSTEMBOTTLE
PASSENGEROXYGEN CYLINDERS
FUEL TANK8,950 GALS(33,879 L)
HYDRAULIC SUMPLOCATED IN LTWHEEL WELL
FUEL TANK8,950 GALS(33,879 L)
HYDRAULICACCUMULATORSLOCATED IN RTWHEEL WELL
FUEL TANK5,800 GALS(21,955 L)
HYDRAULIC ACCUMULATORSLOCATED IN NOSE WHEEL WELL
ENGINE OIL TANKS
HYDRAULICACCUMULATORLOCATED IN LTWING ROOT
HYDRAULIC ACCUMULATORSLOCATED IN LT WHEEL WELL
HYDRAULIC FLUID TANKSLOCATED IN LT WING ROOT
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II
AIRCRAFT ENTRY-DC-8
1. NORMAL/EMERGENCY ENTRY
a. PASSENGER AND SERVICE DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
b. EMERGENCY EXIT - To open door, hold handle, push release plate (handle on some aircraft only). Doors are hinged at bottom edge.
When doors are opened from outside, slide chutes automatically deploy. An opening door could injure rescue personnel
2. CUT-IN
a. Cut along window line as a last resort.
WARNING
AIRCRAFT CROSS SECTION
2aCUT-IN AREAS
1aPASSENGER AND SERVICE DOORS
1bEMERGENCY EXIT
6
DC
-8. DC-8T.O
. 00-105E-9
EMERGENCY RESCUE ACCESS
BREAK GLASS FOR ACCESS TOHANDLE AND SLIDE WINDOW AFT
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.
AFT PASSENGERENTRY DOOR
TYPICAL EMERGENCY EXITS
AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 9 FTWHEELS EXTENDED: 13 FT
CUT-IN/CHOP OUT AREAS
AFT SERVICEENTRY DOOR
FWD PASSENGERENTRY DOOR
FWD SERVICEENTRY DOOR
ACCESS TO ACCESSORYCOMPARTMENT
7
NOTE:1. Observe markings on all doors for operability. Donot attempt to open doors which are banded ormarked inoperable.
2. Do not stand in front of passenger service oremergency exit doors when opening. Escape slidewill inflate automatically when door is opened anddrop over lowered door.
DC
-8. DC-8T.O
. 00-105E-9
8
1. ENGINE SHUTDOWN - ALL MODELS
a. Retard fuel control levers, located on center console, to full aft OFF position.
b. Retard throttles, located on center console, to IDLE START position.
c. Place battery switch, located on upper left corner of flight engineer’s panel, to OFF position.
NOTE: If engines fail to shutdown, pull emergency fire T-handles, located on center overhead panel.
This type aircraft is not equipped with an APU.
2. AIRCREW EXTRACTION
a. Unlatch lap belt and remove shoulder harness form crewmember(s).
b. Passenger seats are equipped with lap belts only.
NOTE: If seat tracks are not damaged during crash landing, use adjustable seat control to retract seats to aft position.
AGENTDISCHARGEHANDLES
EMERGENCYFIRET-HANDLES(4 EACH)
FUEL, AIRHYDRAULICOFFPOSITION
AGENTSELECTPOSITION
1cBATTERY SWITCH
1bTHROTTLES
1aFUELCONTROLLEVERS
FLIGHT DECK LOOKING FORWARD
FLIGHT ENGINEER PANEL
ENGINE SHUTDOWN ANDAIRCREW EXTRACTION
DC
-8. DC-8T.O
. 00-105E-9
9
BATTERY(LOCATED IN RTWHEEL WELL)
CREWOXYGENSYSTEMBOTTLE
PASSENGEROXYGEN CYLINDERS
FUEL TANK8,800 GALS(33,312 L)
HYDRAULIC SUMPLOCATED IN LTWHEEL WELL
FUEL TANK8,800 GALS(33,312 L)
HYDRAULICACCUMULATORSLOCATED IN RTWHEEL WELL
FUEL TANK5,800 GALS(21,955 L)
HYDRAULIC ACCUMULATORSLOCATED IN NOSE WHEEL WELL
ENGINE OIL TANKS
HYDRAULICACCUMULATORLOCATED IN LTWING ROOT
HYDRAULIC ACCUMULATORSLOCATED IN LT WHEEL WELL
HYDRAULIC FLUID TANKSLOCATED IN LT WING ROOT
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II
AIRCRAFT ENTRY-DC-8F
1. NORMAL/EMERGENCY ENTRY
a. PASSENGER AND SERVICE DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
b. EMERGENCY EXIT - To open door, hold handle, push release plate (handle on some aircraft only). Doors are hinged at bottom edge.
When doors are opened from outside, slide chutes automatically deploy. An opening door could injure rescue personnel
2. CUT-IN
a. Cut along window line as a last resort.
WARNING
AIRCRAFT CROSS SECTION
2aCUT-IN AREAS
1aPASSENGER AND SERVICE DOORS
1bEMERGENCY EXIT
DC
-8. DC-8T.O
. 00-105E-9
EMERGENCY RESCUE ACCESS
BREAK GLASS FOR ACCESS TOHANDLE AND SLIDE WINDOW AFT
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.
AFT PASSENGERENTRY DOOR
TYPICAL EMERGENCY EXITS
AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 9 FTWHEELS EXTENDED: 13 FT
CUT-IN/CHOP OUT AREAS
AFT SERVICEENTRY DOOR
FWD PASSENGERENTRY DOOR
FWD SERVICEENTRY DOOR
ACCESS TO ACCESSORYCOMPARTMENT
10
REMOVAL OF DOOR IS RESTRICTEDON SOME AIRCRAFT FWD CARGO
COMPARTMENT DOORS
CARGO LOADINGDOOR
AFT CARGOCOMPARTMENT DOORS
NOTE:1. Observe markings on all doors for operability. Donot attempt to open doors which are banded ormarked inoperable.
2. Do not stand in front of passenger service oremergency exit doors when opening. Escape slidewill inflate automatically when door is opened anddrop over lowered door.
DC
-8. DC-8T.O
. 00-105E-9
11
BATTERY(LOCATED IN RTWHEEL WELL)
OXYGENBOTTLES
PASSENGEROXYGEN CYLINDERS
FUEL TANK8,950 GALS(33,879 L)
HYDRAULIC SUMPLOCATED IN LTWHEEL WELL
FUEL TANK8,950 GALS(33,879 L)
HYDRAULICACCUMULATORSLOCATED IN RTWHEEL WELL
FUEL TANK6,400 GALS(24,227 L)
HYDRAULIC ACCUMULATORSLOCATED IN NOSE WHEEL WELL
ENGINE OIL TANKS
HYDRAULICACCUMULATORLOCATED IN LTWING ROOT
HYDRAULIC ACCUMULATORSLOCATED IN LT WHEEL WELL
HYDRAULIC FLUID TANKS LOCATEDIN LT WING ROOT
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II
AIRCRAFT ENTRY-DC-8-61
1. NORMAL/EMERGENCY ENTRY
a. PASSENGER AND SERVICE DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
b. EMERGENCY EXIT - To open door, hold handle, push release plate (handle on some aircraft only). Doors are hinged at bottom edge.
c. EMERGENCY EXIT DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
When doors are opened from outside, slide chutes automatically deploy. An opening door could injure rescue personnel
2. CUT-IN
a. Cut along window line as a last resort.
WARNING
AIRCRAFT CROSS SECTION
2aCUT-IN AREAS
1aPASSENGER AND SERVICE DOORS
1bEMERGENCY EXIT
1cEMERGENCY EXIT DOORS
DC
-8. DC-8T.O
. 00-105E-9
EMERGENCY RESCUE ACCESS
BREAK GLASS FOR ACCESS TOHANDLE AND SLIDE WINDOW AFT
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.
AFT PASSENGERENTRY DOOR
TYPICAL EMERGENCY EXITS
AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 9 FTWHEELS EXTENDED: 13 FT
CUT-IN/CHOP OUT AREAS
AFT SERVICEENTRY DOOR
FWD PASSENGERENTRY DOOR
FWD SERVICEENTRY DOOR
ACCESS TO ACCESSORYCOMPARTMENT
12
GALLEY SERVICE DOOR
FWD CARGOCOMPARTMENT DOORS
AFT CARGOCOMPARTMENT DOORS
OVERWING EMERGENCY EXITS
CUT-IN/CHOP OUTAREAS
TYPICAL EMERGENCY EXIT DOORS
NOTE:1. Observe markings on all doors for operability. Donot attempt to open doors which are banded ormarked inoperable.
2. Do not stand in front of passenger service oremergency exit doors when opening. Escape slidewill inflate automatically when door is opened anddrop over lowered door.
DC
-8. DC-8T.O
. 00-105E-9
13
BATTERY(LOCATED IN RTWHEEL WELL)
CREWOXYGENSYSTEMBOTTLE
PASSENGEROXYGEN CYLINDERS
FUEL TANK8,950 GALS(33,879 L)
TYPICALHYDRAULICPUMP
FUEL TANK8,950 GALS(33,879 L)
HYDRAULICACCUMULATORSLOCATED IN RTWHEEL WELL
FUEL TANK6,400 GALS(24,227 L)
HYDRAULIC ACCUMULATORSLOCATED IN NOSE WHEEL WELL
ENGINE OIL TANKS
HYDRAULIC SUMPS
HYDRAULIC SUMP LOCATEDIN LT WHEEL WELL
HYDRAULIC ACCUMULATORLOCATED IN LT WING ROOT
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II
AIRCRAFT ENTRY-DC-8-62
1. NORMAL/EMERGENCY ENTRY
a. PASSENGER AND SERVICE DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
b. EMERGENCY EXIT - To open door, hold handle, push release plate (handle on some aircraft only). Doors are hinged at bottom edge.
When doors are opened from outside, slide chutes automatically deploy. An opening door could injure rescue personnel
2. CUT-IN
a. Cut along window line as a last resort.
WARNING
AIRCRAFT CROSS SECTION
2aCUT-IN AREAS
1aPASSENGER AND SERVICE DOORS
1bEMERGENCY EXIT
SURGE DAMPERLOCATED IN LTWING ROOT
MAIN HYDRAULIC RESERVOIRLOCATED IN LT WING ROOT
DC
-8. DC-8T.O
. 00-105E-9
EMERGENCY RESCUE ACCESS
BREAK GLASS FOR ACCESS TOHANDLE AND SLIDE WINDOW AFT
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.
AFT PASSENGERENTRY DOOR
TYPICAL EMERGENCY EXITS
AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 9 FTWHEELS EXTENDED: 13 FT
CUT-IN/CHOP OUT AREAS
AFT SERVICEENTRY DOOR
FWD PASSENGERENTRY DOOR
FWD SERVICEENTRY DOOR
ACCESS TO ACCESSORYCOMPARTMENT
14 NOTE:1. Observe markings on all doors for operability. Donot attempt to open doors which are banded ormarked inoperable.
2. Do not stand in front of passenger service oremergency exit doors when opening. Escape slidewill inflate automatically when door is opened anddrop over lowered door.
DC
-8. DC-8T.O
. 00-105E-9
15
BATTERY(LOCATED IN RTWHEEL WELL)
OXYGENBOTTLES
PASSENGEROXYGEN CYLINDERS
FUEL TANK8,950 GALS(33,879 L)
HYDRAULICPUMP
FUEL TANK8,950 GALS(33,879 L)
HYDRAULICACCUMULATORSLOCATED IN RTWHEEL WELL
FUEL TANK6,400 GALS(24,227 L)
HYDRAULIC ACCUMULATORSLOCATED IN NOSE WHEEL WELL
ENGINE OIL TANKS
HYDRAULICSUMPS
HYDRAULIC ACCUMULATORSLOCATED IN LT WHEEL WELL
HYDRAULIC FLUID TANKS LOCATEDIN LT WING ROOT
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II
AIRCRAFT ENTRY-DC-8-63
1. NORMAL/EMERGENCY ENTRY
a. PASSENGER AND SERVICE DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
b. EMERGENCY EXIT - To open door, hold handle, push release plate (handle on some aircraft only). Doors are hinged at bottom edge.
c. EMERGENCY EXIT DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
d. FORWARD UPPER CARGO DOOR EXTERNAL CONTROL PANEL - To open door, push lockpin handle down and hold. Insert wrench in hex end of door handle shaft and rotate counterclockwise to unlatch. Attach sling to door and hoist door open.
2. CUT-IN
a. Cut along window line as a last resort.
WARNING
AIRCRAFT CROSS SECTION
2aCUT-IN AREAS
1aPASSENGER AND SERVICE DOORS
1bEMERGENCY EXIT
1cEMERGENCY EXIT DOORS
When doors are opened from outside, slide chutes automatically deploy. An opening door could injure rescue personnel.
1dFWD UPPER CARGODOOR EXTERNALCONTROL PANEL
SURGE DAMPERLOCATED IN LT WING ROOT
SURGE DAMPER
HYDRAULIC SUMP LOCATEDIN LT WHEEL WELL
DC
-8. DC-8T.O
. 00-105E-9
16
EMERGENCY RESCUE ACCESS
CLEARVIEW WINDOWEXTERIOR ACCESS
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.
AFT PASSENGERENTRY DOOR
EMERGENCY EXIT DOORS ON SOME AIRCRAFT
AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 9 FTWHEELS EXTENDED: 13 FT
CUT-IN/CHOP OUT AREAS
AFT SERVICEENTRY DOOR
FWD PASSENGER ENTRY DOOR
FWD SERVICEENTRY DOOR
ACCESS TO ACCESSORY COMPARTMENT
GALLEY SERVICE DOOR
FWD CARGOCOMPARTMENT DOORS
AFT CARGOCOMPARTMENT DOORS
OVERWING EMERGENCY EXITS
TYPICAL EMERGENCY EXIT DOORS
CUT-IN/CHOP OUT AREAS
EXTERIOR CONTROLPANEL
FWD UPPER CARGO DOOR
NOTE:1. Observe markings on all doors for operability. Donot attempt to open doors which are banded ormarked inoperable.
2. Do not stand in front of passenger service oremergency exit doors when opening. Escape slidewill inflate automatically when door is opened anddrop over lowered door.
DC
-8. DC-8T.O
. 00-105E-9
17
BATTERYOXYGENBOTTLES
PASSENGEROXYGEN CYLINDERS
FUEL TANK8,950 GALS(33,879 L)
SPOILER RESERVOIRLOCATED IN RTWHEEL WELL
FUEL TANK8,950 GALS(33,879 L)
HYDRAULICACCUMULATORSLOCATED IN RTWHEEL WELL
FUEL TANK6,400 GALS(24,227 L)
HYDRAULIC ACCUMULATORSLOCATED IN NOSE WHEEL WELL
ENGINE OIL TANKS
OPTIONALAPU
HYDRAULIC ACCUMULATORLOCATED IN LT WHEEL WELL
HYDRAULIC RESERVOIR LOCATEDIN LT WING ROOT
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II
AIRCRAFT ENTRY-DC-8-71
1. NORMAL/EMERGENCY ENTRY
a. PASSENGER AND SERVICE DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
b. EMERGENCY EXIT - To open door, hold handle, push release plate (handle on some aircraft only). Doors are hinged at bottom edge.
c. EMERGENCY EXIT DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
d. FORWARD UPPER CARGO DOOR EXTERNAL CONTROL PANEL - To open door, push lockpin handle down and hold. Insert wrench in hex end of door handle shaft and rotate counterclockwise to unlatch. Attach sling to door and hoist door open.
2. CUT-IN
a. Cut along window line as a last resort.
WARNING
AIRCRAFT CROSS SECTION
2aCUT-IN AREAS
1aPASSENGER AND SERVICE DOORS
1bEMERGENCY EXIT
1cEMERGENCY EXIT DOORS
When doors are opened from outside, slide chutes automatically deploy. An opening door could injure rescue personnel.
1dFWD UPPER CARGODOOR EXTERNALCONTROL PANEL
AUXILIARYHYDRAULICPUMP
HYDRAULICACCUMULATOR
HYDRAULIC RUDDER RESERVOIRLOCATED IN LT WHEEL WELL
DC
-8. DC-8T.O
. 00-105E-9
18
EMERGENCY RESCUE ACCESS
CLEARVIEW WINDOWEXTERIOR ACCESS
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.
AFT PASSENGERENTRY DOOR
EMERGENCY EXIT DOORS ON SOME AIRCRAFT
AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 9 FTWHEELS EXTENDED: 13 FT
CUT-IN/CHOP OUT AREAS
AFT SERVICEENTRY DOOR
FWD PASSENGER ENTRY DOOR
FWD SERVICEENTRY DOOR
ACCESS TO ACCESSORY COMPARTMENT
GALLEY SERVICE DOOR
FWD CARGOCOMPARTMENT DOORS
AFT CARGOCOMPARTMENT DOORS
OVERWING EMERGENCY EXITS
TYPICAL EMERGENCY EXIT DOORS
CUT-IN/CHOP OUT AREAS
EXTERIOR CONTROLPANEL
FWD UPPER CARGO DOOR
NOTE:1. Observe markings on all doors for operability. Donot attempt to open doors which are banded ormarked inoperable.
2. Do not stand in front of passenger service oremergency exit doors when opening. Escape slidewill inflate automatically when door is opened anddrop over lowered door.
DC
-8. DC-8T.O
. 00-105E-9
19
BATTERYOXYGENBOTTLES
PASSENGEROXYGEN CYLINDERS
FUEL TANK8,950 GALS(33,879 L)
TYPICALHYDRAULICPUMP
FUEL TANK8,950 GALS(33,879 L)
HYDRAULICACCUMULATORSLOCATED IN RTWHEEL WELL
FUEL TANK6,400 GALS(24,227 L)
HYDRAULIC ACCUMULATORSLOCATED IN NOSE WHEEL WELL
ENGINE OIL TANKSOPTIONAL APU
HYDRAULIC ACCUMULATORLOCATED IN LT WHEEL WELL
MAIN HYDRAULIC RESERVOIRLOCATED IN LT WING ROOT
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II
AIRCRAFT ENTRY-DC-8-72
1. NORMAL/EMERGENCY ENTRY
a. PASSENGER AND SERVICE DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
b. EMERGENCY EXIT - To open door, hold handle, push release plate (handle on some aircraft only). Doors are hinged at bottom edge.
c. EMERGENCY EXIT DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
d. FORWARD UPPER CARGO DOOR EXTERNAL CONTROL PANEL - To open door, push lockpin handle down and hold. Insert wrench in hex end of door handle shaft and rotate counterclockwise to unlatch. Attach sling to door and hoist door open.
2. CUT-IN
a. Cut along window line as a last resort.
WARNING
AIRCRAFT CROSS SECTION
2aCUT-IN AREAS
1aPASSENGER AND SERVICE DOORS
1bEMERGENCY EXIT
1cEMERGENCY EXIT DOORS
When doors are opened from outside, slide chutes automatically deploy. An opening door could injure rescue personnel.
1dFWD UPPER CARGODOOR EXTERNALCONTROL PANEL
HYDRAULICRESERVOIR
HYDRAULICACCUMULATOR
HYDRAULIC RUDDER RESERVOIRLOCATED IN LT WHEEL WELL
DC
-8. DC-8T.O
. 00-105E-9
20
EMERGENCY RESCUE ACCESS
CLEARVIEW WINDOWEXTERIOR ACCESS
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.
AFT PASSENGERENTRY DOOR
EMERGENCY EXIT DOORS ON SOME AIRCRAFT
AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 9 FTWHEELS EXTENDED: 13 FT
CUT-IN/CHOP OUT AREAS
AFT SERVICEENTRY DOOR
FWD PASSENGER ENTRY DOOR
FWD SERVICEENTRY DOOR
ACCESS TO ACCESSORY COMPARTMENT
AFT CARGOCOMPARTMENT DOORS
OVERWING EMERGENCY EXITS
EXTERIOR CONTROLPANEL
FWD UPPER CARGO DOOR
CUT-IN/CHOP OUT AREAS
NOTE:1. Observe markings on all doors for operability. Donot attempt to open doors which are banded ormarked inoperable.
2. Do not stand in front of passenger service oremergency exit doors when opening. Escape slidewill inflate automatically when door is opened anddrop over lowered door.
DC
-8. DC-8T.O
. 00-105E-9
21
BATTERYOXYGENBOTTLES
PASSENGEROXYGEN CYLINDERS
FUEL TANK8,950 GALS(33,879 L)
SPOILER RESERVOIRLOCATED IN RTWHEEL WELL
FUEL TANK8,950 GALS(33,879 L)
HYDRAULICACCUMULATORSLOCATED IN RTWHEEL WELL
FUEL TANK6,400 GALS(24,227 L)
HYDRAULIC ACCUMULATORSLOCATED IN NOSE WHEEL WELL
ENGINE OIL TANKSOPTIONAL APU
HYDRAULIC ACCUMULATORLOCATED IN LT WHEEL WELL
MAIN HYDRAULIC RESERVOIRLOCATED IN LT WING ROOT
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II
AIRCRAFT ENTRY-DC-8-73
1. NORMAL/EMERGENCY ENTRY
a. PASSENGER AND SERVICE DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
b. EMERGENCY EXIT - To open door, hold handle, push release plate (handle on some aircraft only). Doors are hinged at bottom edge.
c. EMERGENCY EXIT DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.
d. FORWARD UPPER CARGO DOOR EXTERNAL CONTROL PANEL - To open door, push lockpin handle down and hold. Insert wrench in hex end of door handle shaft and rotate counterclockwise to unlatch. Attach sling to door and hoist door open.
2. CUT-IN
a. Cut along window line as a last resort.
WARNING
AIRCRAFT CROSS SECTION
2aCUT-IN AREAS
1aPASSENGER AND SERVICE DOORS
1bEMERGENCY EXIT
1cEMERGENCY EXIT DOORS
When doors are opened from outside, slide chutes automatically deploy. An opening door could injure rescue personnel.
1dFWD UPPER CARGODOOR EXTERNALCONTROL PANEL
AUXILIARYHYDRAULICPUMP
HYDRAULICACCUMULATOR
HYDRAULIC RUDDER RESERVOIRLOCATED IN LT WHEEL WELL
TYPICAL HYDRAULICPUMP IN 4 PLACES
DC
-8. DC-8T.O
. 00-105E-9
22
EMERGENCY RESCUE ACCESS
CLEARVIEW WINDOWEXTERIOR ACCESS
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.
AFT PASSENGERENTRY DOOR
EMERGENCY EXIT DOORS ON SOME AIRCRAFT
AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 9 FTWHEELS EXTENDED: 13 FT
CUT-IN/CHOP OUT AREAS
AFT SERVICEENTRY DOOR
FWD PASSENGER ENTRY DOOR
FWD SERVICEENTRY DOOR
ACCESS TO ACCESSORY COMPARTMENT
GALLEY SERVICE DOORON SOME AIRCRAFT
FWD CARGOCOMPARTMENT DOORS
AFT CARGOCOMPARTMENT DOORS
OVERWING EMERGENCY EXITS
TYPICAL EMERGENCY EXIT DOORS
CUT-IN/CHOP OUT AREAS
EXTERIOR CONTROLPANEL
FWD UPPER CARGO DOOR
NOTE:1. Observe markings on all doors for operability. Donot attempt to open doors which are banded ormarked inoperable.
2. Do not stand in front of passenger service oremergency exit doors when opening. Escape slidewill inflate automatically when door is opened anddrop over lowered door.
DC
-8. DC-8T.O
. 00-105E-9
CABIN CONFIGURATION
23 DC-8-43
177 PASSENGERS 6 ABREAST SEATING129 SEATS ON 31” (78.7 CM) PITCH 24 SEATS ON 34” (86.4 CM) PITCH 12 SEATS ON 36” (91.4 CM) PITCH 6 SEATS ON 33” (91.4 CM) PITCH 6 SEATS ON 37” (94.0 CM) PITCH
GALLEYS
CREWSTORAGE
ATTENDANT’SDOUBLE SEAT
LAVATORIES
LAVATORIES
WINDSCREENMAIN ENTRY DOOR (B)34.5X72” (87.6X182.9 CM)
EMERGENCY EXIT TYPE III20X38” (50.86X96.5 CM)
EMERGENCY EXIT TYPE III20X38” (50.86X96.5 CM)
AFT SERVICE DOOR (C)33.5X64” (85.1X162.6 CM)
AFT ENTRY DOOR (D)34.5X72” (87.6X182.9 CM)
GALLEY
SERVICE DOOR (A)33.5X64” (85.1X162.6 CM)
DC-8-55
189 PASSENGERS 6 ABREAST SEATING 66 SEATS ON 31” (78.7 CM) PITCH 66 SEATS ON 32” (81.3 CM) PITCH 39 SEATS ON 29” (99.1 CM) PITCH 18 SEATS ON 40” (101.6 CM) PITCH 6 SEATS ON 37” (94.0 CM) PITCH
GALLEY
ATTENDANT’SDOUBLE SEAT
LAVATORY
LAVATORIES
MAIN ENTRY DOOR (B)34.5X72” (87.6X182.9 CM)
EMERGENCY EXIT TYPE III20X38” (50.86X96.5 CM)
EMERGENCY EXIT TYPE III20X38” (50.86X96.5 CM)
AFT SERVICE DOOR (C)33.5X64” (85.1X162.6 CM)
AFT ENTRY DOOR (D)34.5X72” (87.6X182.9 CM)
GALLEYS
SERVICE DOOR (A)33.5X64” (85.1X162.6 CM)
GALLEY
DC
-8. DC-8T.O
. 00-105E-9
CABIN CONFIGURATION-Continued
24 DC-8-62, -72
189 PASSENGERS 6 ABREAST SEATING189 SEATS ON 34” (86.4 CM) PITCH
GALLEY
CREWSTORAGE
ATTENDANT’SDOUBLE SEAT
LAVATORIES
LAVATORIES
WINDSCREEN
MAIN ENTRY DOOR (B)34.5X72” (87.6X182.9 CM)
EMERGENCY EXIT TYPE III20X38” (50.86X96.5 CM)
EMERGENCY EXIT TYPE III20X38” (50.86X96.5 CM)
AFT SERVICE DOOR (C)34X64” (86.4X162.6 CM)
AFT ENTRY DOOR (D)34.5X72” (87.6X182.9 CM)
GALLEYS
SERVICE DOOR (A)33.5X64” (85.1X162.6 CM)
DC-8-61, -63, -71, -73
259 PASSENGERS 6 ABREAST SEATING177 SEATS ON 32” (81.3 CM) PITCH 24 SEATS ON 38” (96.5 CM) PITCH 58 SEATS ON 31” (78.7 CM) PITCH
1 AND 2GALLEY
ATTENDANT’S DOUBLE SEAT
LAVATORIES
LAVATORY
MAIN ENTRY DOOR (B)34.5X72” (87.6X182.9 CM)
EMERGENCY EXIT TYPE III20X38” (50.86X96.5 CM)
EMERGENCY EXIT TYPE III20X38” (50.86X96.5 CM)
AFT SERVICE DOOR (C)34X64” (86.4X162.6 CM)
AFT ENTRY DOOR (D)34.5X72” (87.6X182.9 CM)
SERVICE DOOR (A) 33.5X64” (85.1X162.6 CM)
3 AND 4GALLEY
ATTENDANT’SDOUBLE SEAT
ATTENDANTSEAT
EMERGENCY EXIT TYPE I 24X56” (61X142.2 CM)
EMERGENCY EXIT TYPE I24X56” (61X142.2 CM)
ATTENDANT’SDOUBLE SEAT
EMERGENCY EXIT TYPE I24X56” (61X142.2 CM)
ATTENDANT’SDOUBLE SEAT
EMERGENCY EXIT TYPE I24X56” (61X142.2 CM)
DC
-8. DC-8T.O
. 00-105E-9
CARGO CONFIGURATION
25 DC-8-55F
PALLETS 1 THROUGH 12 5543.2 CU ‘ (154. CU M)PALLET 13 460 CU’ (13.03 CU M)LOWER DECK CARGO 1390 CU’ (39.4 CU M)TOTAL CARGO 7293.2 CU’ (206.63 CU M)
BARRIER NET
CREW GALLEY
LAVATORY
FWD ENTRY DOOR34.5X72” (87.6X182.9 CM)
SERVICE DOOR34X64” (86.4X162.6 CM)
AFT ENTRY DOOR (D)34.5X72” (87.6X182.9 CM)
1 2 3 4 5 6 7 8 9 10 11 12 13
CARGO DOOR85X140” (215.9.6X355.6 CM)
CARGO PALLET (13 PLACES) 88X125” (224X318 CM)
SERVICE DOOR33.5X64” (85.1X162.6 CM)
DC-8-62F, -72F
PALLETS 1 THROUGH 13 5896.8 CU ‘ (154. CU M)PALLET 14 460 CU’ (13.03 CU M)LOWER DECK CARGO 1615 CU’ (45.74 CU M)TOTAL CARGO 7971.8 CU’ (225.77 CU M)
BARRIER NET
CREWGALLEY
LAVATORY
FWD ENTRY DOOR34.5X72” (87.6X182.9 CM)
SERVICE DOOR34X64” (86.4X162.6 CM)
AFT ENTRY DOOR (D)34.5X72” (87.6X182.9 CM)
1 2 3 4 5 6 7 8 9 10 11 12 13 14
CARGO DOOR85X140” (215.9.6X355.6 CM)
CARGO PALLET (14 PLACES)88X125” (224X318 CM)
SERVICE DOOR33.5X64” (85.1X162.6 CM)
DC-8-61F, -63F, -71F, -73F
PALLETS 1 THROUGH 17 7711.2 CU ‘ (218.4 CU M)PALLET 18 460 CU’ (13.03 CU M)LOWER DECK CARGO 2500 CU’ (70.8 CU M)TOTAL CARGO 10671.2 CU’ (302.23 CU M)
CREW GALLEY
LAVATORY
FWD ENTRY DOOR34.5X72” (87.6X182.9 CM)
SERVICE DOOR34X64” (86.4X162.6 CM)
AFT ENTRY DOOR34.5X72” (87.6X182.9 CM)
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18
MAIN CARGO DOOR85X140” (215.9.6X355.6 CM)
CARGO PALLET (18 PLACES) 88X125” (224X318 CM)
SERVICE DOOR33.5X64” (85.1X162.6 CM)
BARRIER NET
DC
-9. DC-9T.O
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AIRCRAFT PAINT SCHEME
1
DC
-9. DC-9T.O
. 00-105E-9
AIRCRAFT DIMENSIONS
2
104’ 4.8”(31.82 M)
SCALE
5 10M
0 10 20 30 40’
8’ 10.5”(2.70 M)
11’ 0”(3.35 M)DOOR (A)
DOOR (B)
SEENOTE
11’ 10.0”(3.61 M)
43’ 8.4”(13.32 M)
92’ 1.2”(28.07 M) 36’ 10.8”
(11.25 M) 7’ 7.2”(2.32 M)
16’ 4.8”(5.00 M)
89’ 4.8”(27.25 M)
DC-9-15
NOTE: DC-9-15 MAX - 27’ 7.0” (8.4 M) - MIN - 27’ 5.0” (8.4 M) DC-9-21 MAX - 27’ 5.0” (8.4 M) - MIN - 27’ 5.0” (8.4 M)
104’ 4.8”(31.82 M)
SCALE
5 10M
0 10 20 30 40’
8’ 10.5”(2.70 M)
11’ 0”(3.35 M)DOOR (A)
DOOR (B)
SEENOTE
11’ 10.0”(3.61 M)
43’ 8.4”(13.32 M)
92’ 1.2”(28.07 M)
36’ 10.8”(11.25 M)
7’ 7.2”(2.32 M)
16’ 4.8”(5.00 M)
DC-9-21
93’ 3.6”(28.44 M)
DC
-9. DC-9T.O
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AIRCRAFT DIMENSIONS-Continued
3
DC-9-32
119’ 3.6”(36.36 M)
SCALE
5 10M
0 10 20 30 40’
8’ 10.5”(2.70 M)
11’ 0”(3.35 M)DOOR (A)
DOOR (B)
11’ 10.0”(3.61 M)
53’ 2.4”(16.22 M) 107’ 0”
(32.61 M)
36’ 10.8”(11.25 M)
7’ 7.2”(2.32 M)
16’ 4.8”(5.00 M)
93’ 3.6”(27.25 M)
NOTE: DC-9-32 MAX - 27’ 9.0” (8.5 M) - MIN - 27’ 6.0” (8.4 M) DC-9-41 MAX - 28’ 5.0” (8.7 M) - MIN - 27’ 0” (8.5 M)
SEENOTE
DC-9-41
125’ 7.2”(38.28 M)
SCALE
5 10M
0 10 20 30 40’
8’ 10.5”(2.70 M)
11’ 0”(3.35 M)DOOR (A)
DOOR (B)
11’ 10.0”(3.61 M)
56’ 1.2”(17.10 M)
113’ 3.6”(34.53 M)
36’ 10.8”(11.25 M)
7’ 7.2”(2.32 M)
16’ 4.8”(5.00 M)
93’ 3.6”(27.25 M)
SEENOTE
DC
-9. DC-9T.O
. 00-105E-9
AIRCRAFT DIMENSIONS-Continued
4
DC-9-41
133’ 7”(40.72 M)
SCALE
5 10M
0 10 20 30 40’
8’ 10.5”(2.70 M)
11’ 0”(3.35 M)DOOR (A)
DOOR (B)
11’ 10.0”(3.61 M)
60’ 11”(18.57 M) 121’ 3”
(36.96 M)
36’ 10.8”(11.25 M)
7’ 7.2”(2.32 M)
16’ 0”(4.88 M) 93’ 4.2”
(28.45 M)
SEENOTE
DC-9-51
SEENOTE
NOTE: DC-9-51 MAX - 28’ 9.0” (8.8 M) - MIN - 28’ 3.0” (8.6 M)
DC
-9. DC-9T.O
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5
AIRCRAFT SKIN PENETRATION POINTS
FUSELAGE (BOTH SIDES)PENETRATE APPROXIMATELY 4 INCHESBELOW CABIN WINDOWS. AVOIDPENETRATING EMERGENCY EXITS.
ENGINE NACELLES (BOTH SIDES)PENETRATE MID-SECTION OF ENGINEBELOW ENGINE CENTER LINE
DC
-9. DC-9T.O
. 00-105E-9
6
ENGINE DANGER AREAS
DIS
TA
NC
E F
RO
M A
IRC
RA
FT
C L40
20
0
20
40
10
5
5
10
10
5
5
10
40
20
0
20
40
25 FT ENGINE INTAKE DANGER AREA
FEET METERS 100 200 300 400 500 600 700
30 60 90 120 150 180 210
IDLE POWER
AXIL DISTANCE BEHIND AIRCRAFT
TAKEOFFPOWER
Jet Intake and Blast Distances
@ 35 MPH
@ 45 MPH
@ 60 MPH
@ 75 MPH
@ 100 MPH
@ 150 MPH
@ 200 MPH
ENGINE BLAST DANGER AREAS
FEET
METERS
DC
-9. DC-9T.O
. 00-105E-9
7
AIRCRAFT DANGER AREAS
WARNING
Use extreme caution when opening access areas where fire is evident.
1. APU ACCESS DOORS
a. Insert screwdriver or similar tool into slot of camlock fasteners.
b. Turn fasteners to the left to open.
c. Pull down access doors.
2. ENGINE NACELLE LOWER COWL DOOR
a. Release four (4) latches on upper cowl door.
b. Push in safety latch release while holding door up with one hand.
c. Lower door to full open position.
1cAPU GROUNDCONTROL PANELACCESS DOOR
1a, 1bCAMLOCK SLOTHEAD LATCH
1cAPU ACCESS DOOR
2aUPPER COWL DOOR LATCH
2bSAFETY LATCH RELEASE
2cLOWER COWL DOOR
2aCOWL LATCHES(TYPICAL 4 PLACES)
APU ACCESS DOORS AND ENGINE NACELLELOWER COWL DOOR
DC
-9. DC-9T.O
. 00-105E-9
AIRCRAFT FLAMMABLE MATERIAL LOCATIONS
OPTIONAL AUXILIARY FUEL TANK
OPTIONAL AUXILIARY FUEL TANK
FUEL VENT BOX
FUEL VENT BOX
FUEL OVERFLOWSTAND PIPE
FUEL OVERFLOWSTAND PIPE
1386 GALS(5247 LITRES)
1386 GALS(5247 LITRES)
907 GALS(3433 LITRES)
HYDRAULIC ACCUMULATORS
HYDRAULIC ACCUMULATORS
FIRE EXTINGUISHER AGENT CONTAINERS
APU GROUND CONTROLPANEL ON FUSELAGE
PORTABLE OXYGEN BOTTLE
CREW OXYGENSYSTEM BOTTLES
RAIN REPELLENTCONTAINERS
PORTABLE OXYGENSYSTEM BOTTLE
CREW OXYGENSYSTEM BOTTLES
BATTERIES QUICKDISCONNECTSBATTERIES
ENGINE OIL TANKS
APU EXHAUST DUCTON RT SIDE ONLY
HYDRAULIC FLUIDRESERVOIR 1 PLACE INEACH WHEEL WELL
1
1
2
2
780/1000 GALS(2953/3785 LITRES)
580/780/1000/1250 GALS(2196/2953/3785/4732 LITRES)
8
DC
-9. DC-9T.O
. 00-105E-9
9
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw12 Foot LadderFire Drill II
AIRCRAFT ENTRY
1. NORMAL ENTRY
CAUTION
When doors are opened from outside, slide chutes automatically deploy.
a. Pull handle, located on left forward entry door, out, rotate counterclockwise and pull door outward.
b. Pull stairway handle, located forward left bottom side of fuselage, outward, press the open button to extend stairway.
c. Pull handle, located on right forward service door, out, rotate clockwise and pull door outward.
2. EMERGENCY ENTRY
Caution must be exercised when releasing tail cone. Keep personnel clear. Tail cone free falls when released from aircraft.
a. Push in jettisonable tail cone T-handle door, located on left fuselage forward of tail cone, pull T-handle to jettison tail cone. Jettison door is approximately 8.5 feet high.
b. Open rear stairway control panel, located on aft left exterior fuselage, push control handle to forward OPEN position to release stairway.
CAUTION
Stairway free falls to down position.
c. Push overwing exit door handle release, two doors are located over each wing, pull handle to unlatch door, push in and lift up forcibly.
WARNING
2cEMERGENCY OVERWING EXIT(BOTH SIDES)
2aTAIL CONEJETTISONHANDLE
2bCONTROL HANDLE
AFT ENTRANCE STAIRWAYCONTROL PANEL
OPEN BUTTON
1bFORWARDPASSENGERSTAIRWAYHANDLE
1cFORWARD SERVICEENTRANCE DOORHANDLE
1aPASSENGERDOORHANDLE
DC
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10
AIRCRAFT EMERGENCY EXITSAFT PASSENGER DOOR STAIRWAY INTERIORAND EXTERIOR CONTROLS
NOTE:· For manual stairway operation, hold interior or exterior control handle in open position. Stairway will free fall open.
· Interior control handle is removed on some aircraftmaking the stairway inoperable from the inside.
PASSENGER AFT ENTRANCESTAIRWAY EXTERIOR CONTROL PANEL
EMERGENCY EXIT
ON SOME AIRCRAFT
STAIR OPERATING HANDLE INSIDE
CONTROL HANDLE
OPEN DOOR FORACCESS STAIR CONTROL
PASSENGER AFT ENTRANCESTAIRWAY INTERIOR CONTROL PANEL
OPEN CLOSE
DC
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11
AIRCRAFT EMERGENCY EXITS-ContinuedPRESSURE BULKHEAD EMERGENCY EXIT, TAILCONE JETTISON,AND MAIN CARGO DOOR OPERATION
MAIN CARGO DOOR (IF APPLICABLE)
NOTE: Use only when all other exits are blocked and time permits.
MANUAL LATCH CONTROLS
a. If installed, turn vent door handle to the UNLOCKED position.b. Turn lockpin handle to UNLOCK and hold.c. Insert pipe in latch fitting and move to UNLOCK.d. Release spring loaded lockpin handle.
HOIST BAR
PLACE CABLE LOOP OR HOOKTHROUGH HERE TO MANUALLY HOIST DOOR OPEN
LATCHACTUATINGSOCKET
LOCKPIN HANDLE(Spring loaded to thelocked position.)
PIPE
VENT DOOR(SOME AIRCRAFT)
INSERT PIPE HERE TOMANUALLY UNLOCK ORLOCK DOOR
CARGO AIRCRAFT ONLY
AFT PRESSUREBULKHEAD
HANDLE IN TAIL SECTIONON PRESSURE BULKHEADDOOR (PULL TO UNLOCK PUSH DOOR IN)
HANDLE ON PRESSURE BULKHEAD DOOR (LIFT TO UNLOCK PULL DOOR IN)
ON SOMEAIRCRAFT
VIEWINGWINDOW
OPEN
INTERIOR VIEW
DC
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12
AIRCRAFT EMERGENCY EXITS1. CLEARVIEW WINDOW FOR CARGO AIRCRAFT ONLY
a. Push in both access doors.
b. Push window handle aft, then down.
c. Push window aft.
2. LOWER CARGO COMPARTMENT DOORS
a. Push circular section of door handle inward to raise thehandle.
b. Rotate door handle counterclockwise to unlatch door.
c. Push door upward into cargo compartment.
3. ELECTRICAL/ELECTRONIC COMPARTMENT DOOR
a. Push right side of handle inward and pull left side of handledown to unlatch door.
b. Push door inward and to the left to open.
EXTERIOR ACCESS(KNOCKOUT PANELS)
CARGOAIRCRAFTONLY
1b
1c
1a
CLEARVIEW WINDOW
2a
2b
(TYPICAL BOTH DOORS)
LOWER CARGOCOMPARTMENT DOORS
ELECTRICAL/ELECTRONICSCOMPARTMENT DOOR
PUSH PULL3a
DC
-9. DC-9T.O
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EMERGENCY RESCUE ACCESS
13
CLEARVIEW WINDOW - EXTERIORACCESS KNOCKOUT PANEL ONCARGO AIRCRAFT
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.
AFT PASSENGER ENTRY DOOR
PRESSURE BULKHEAD EMERGENCY EXIT
AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 4 FTWHEELS EXTENDED: 8 FT
PASSSENGER AFT ENTRANCESTAIRWAY INTERIOR CONTROLPANEL ON SOME AIRCRAFT
APU COMPARTMENT ACCESS DOOR
FWD PASSENGER ENTRY DOOR
FWD SERVICE ENTRY DOOR
TAIL CONE ACCESS DOOR
MAIN CARGO DOORAND EXTERNAL CONTROL PANELON CARGO AIRCRAFT ONLY
ENGINE NACELLE LOWER COWL DOOR
OVERWING EMERGENCY EXITS
CLEARVIEW WINDOW -CHILL PANE WITH CO2 ANDBREAK WITH HEAVY FIRE AXEFOR ACCESS TO HANDLE;SLIDE WINDOW AFT
CUT-IN/CHOP OUT AREAS
JETTISONABLE TAIL CONE
AFT LOWER CARGO DOOR
TAIL CONE JETTISON LATCH
FWD LOWER CARGO DOOR
DC
-9. DC-9T.O
. 00-105E-9
14
ENGINE/APU SHUTDOWN ANDAIRCREW EXTRACTION
1. ENGINE/APU SHUTDOWN
a. Place fuel control levers, located on pilot’s center console,to aft and OFF position.
b. Retard throttles, located on pilot’s center console, to IDLECUTOFF position.
c. Place battery switch, located on center over-head panel, toOFF position.
NOTE: If engines fail to shutdown, pull emergency fire T-handles out, located on pilot’s center forward panel.
d. Place APU master switch, located on center overheadpanel, to OFF position.
e. On the APU ground control panel, located to left of APUaccess doors on the tailcone, open door by pushing twolatches. Place APU master switch to the APU shutoff (up)position. If “Fire” light is illuminated ...place discharge fireswitch (up) position to release fire agent 1. Wait 10seconds to use fire agent 2, if applicable.
2. AIRCREW EXTRACTION
a. Unlatch lap belt and remove shoulder harness fromcrewmember.
b. If seat tracks are not damaged during crash landing, useadjustable seat controls to retract seat to aft position.Pilot’s controls are on right side of seat while co-pilot’s areon the left.
c. Flight crew cabin seats are equipped with lap belts andshoulder harnesses.
d. Passenger seats are only equipped with lap belts.
CENTER OVERHEAD PANELPILOT’S STATION (TYPICAL)
1dAPUMASTERSWITCH
1cBATTERY SWITCH
1bTHROTTLES
LOW AGENT INDICATING LIGHTS
LEFTENGINE
RIGHTENGINE
EMERGENCY FIRE T-HANDLES CENTER OVERHEAD PANEL
1aFUEL CONTROL LEVERS
FIREWARNINGHORN
DOOR
APU GROUNDCONTROLSAND FIREEXTINGUISHERS
LATCHES
1eAPUSHUTOFF
1eFIREAGENT DISCHARGE SWITCHES
APU GROUND CONTROL PANEL
DC
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CABIN CONFIGURATION
15 DC-9-15,-21
90 PASSENGERS 5 ABREAST SEATING50 SEATS ON 32” (81.3 CM) PITCH40 SEATS ON 31” (78.7 CM) PITCH
NOTE: Maximum of 90 passengers, 5-abreast seating available.
DC-9-32
115 PASSENGERS 5 ABREAST SEATING 55 SEATS ON 33” (83.8 CM) PITCH 10 SEATS ON 36” (91.4 CM) PITCH 50 SEATS ON 31” (78.7 CM) PITCH
NOTE: Maximum of 127 passengers, 5-abreast seating available.
GALLEY
ATTENDANT’SDOUBLE SEAT
LAVATORY
CREWSTORAGE
MAIN ENTRY DOOR (B)34.5X72” (87.6X182.9 CM)
EMERGENCY EXIT TYPE III 20X36” (51X91 CM)
SERVICE DOOR (A)27X48” (69X122 CM)
SCALE
0 2 4 6 METERS
0 10 20 FEET
LAVATORY
EMERGENCY EXIT TYPE III 20X36” (51X91 CM)
ATTENDANT’SDOUBLE SEAT
SCALE
0 2 4 6 METERS
0 10 20 FEET
GALLEY
ATTENDANT’SDOUBLE SEAT
LAVATORY
CREWSTORAGE
MAIN ENTRY DOOR (B)34.5X72” (87.6X182.9 CM)
EMERGENCY EXIT TYPE III 20X36” (51X91 CM)
SERVICE DOOR (A)27X48” (69X122 CM)
LAVATORY
EMERGENCY EXIT TYPE III 20X36” (51X91 CM)
ATTENDANT’SDOUBLE SEAT
DC
-9. DC-9T.O
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CABIN CONFIGURATION-Continued
16 DC-9-41
125 PASSENGERS 5 ABREAST SEATING66 SEATS ON 34” (86.4 CM) PITCH 5 SEATS ON 33” (83.8 CM) PITCH30 SEATS ON 32” (81.3 CM) PITCH25 SEATS ON 31” (78.7 CM) PITCH
NOTE: Maximum of 128 passengers, 5-abreast seating available.
DC-9-51
135 PASSENGERS 5 ABREAST SEATING 5 SEATS ON 35” (88.9 CM) PITCH 5 SEATS ON 34” (86.4 CM) PITCH 66 SEATS ON 33” (83.8 CM) PITCH 60 SEATS ON 32” (81.3 CM) PITCH
NOTE: Maximum of 397 passengers, 5-abreast seating available.
GALLEY
ATTENDANT’SDOUBLE SEAT
LAVATORY
CREWSTORAGE
MAIN ENTRY DOOR (B)34X72” (86X183 CM) EMERGENCY EXIT TYPE III
20X36” (51X91 CM)
SERVICE DOOR (A)27X48” (69X122 CM)
SCALE
0 2 4 6 METERS
0 10 20 FEET
LAVATORY
EMERGENCY EXIT TYPE III 20X36” (51X91 CM)
ATTENDANT’SDOUBLE SEAT
SCALE
0 2 4 6 METERS
0 10 20 FEET
GALLEY
ATTENDANT’SDOUBLE SEAT
LAVATORY
CREWSTORAGE
MAIN ENTRY DOOR (B)34X72” (86X183 CM)
EMERGENCY EXIT TYPE III 20X36” (51X91 CM)
SERVICE DOOR (A)27X48” (69X122 CM)
LAVATORY
EMERGENCY EXIT TYPE III 20X36” (51X91 CM)
ATTENDANT’SDOUBLE SEAT
DC
-9. DC-9T.O
. 00-105E-9
CARGO CONFIGURATION
17 DC-9-15F
DC-9-32F
LAVATORY
FWD ENTRY DOOR (B)34X72” (86.4X182.9 CM)TYPE 2
SERVICE DOOR (A)27X48” (68.6X121.9 CM)
SCALE
0 2 4 6 METERS
0 10 20 FEET
LAVATORY
SCALE
0 2 4 6 METERS
0 10 20 FEET
GALLEY
CARGO PALLET1 PLACE167 FT (4.7 M )
FWD CARGOBARRIER NET
CARGO DOOR (C)81X136” (205.7X345.4 CM)
CARGO PALLETS6 PLACES360 FT(10.2 M )
SERVICE DOOR (A)27X48” (69X122 CM)TYPE I LAVATORY
33
LAVATORYFWD ENTRY DOOR (B)34X72” (86.2X182.9 CM)TYPE I
CARGO VOLUMES
PALLET SIZE #1 THRU 6 88X108” (224X274 CM)
PALLETS 1 THRU 6 2161 FT (61.2 M )LOWER DECK CARGO 600 FT (17.0 M )TOTAL CARGO 2761 FT (78.2 M )
3 33 33 3
FWD CARGOBARRIER NET
1 2 3 4 5 6
CARGO VOLUMES
PALLET SIZES #1 and 10 54X88” (137X224 CM) #2 THRU 9 88X108” (224X274 CM)
PALLET 1 174 FT (4.9 M )PALLETS 2 THRU 9 2959 FT (83.8 M )PALLET 10 167 FT (4.7 M )LOWER DECK CARGO 895 FT (25.3 M )TOTAL CARGO 4195 FT (118.8 M )
3
3
3
3
3
3 3
1 2 3 4 5 6 7 8 9 10CARGO PALLETS1 PLACE174 FT(4.9 M )
33
33
CARGO PALLETS8 PLACES370 FT(10.5 M )
CARGO DOOR (C)81X136” (205.7X345.4 CM)
DC-10T.O
. 00-105E-9
DC
-10.
AIRCRAFT PAINT SCHEME
1
DC-10T.O
. 00-105E-9
DC
-10.
AIRCRAFT DIMENSIONS
DC-10 SERIES 10 (LOWER GALLEY) DC-10 SERIES 10 AND 10CF (UPPER GALLEY)
182’ 3.1”(55.55 M)
70”X66”(177.8CM X 167.6CM)
19’ 9”(6.02 M)
26’ 10”(8.18 M)
27’ 10.5”(8.50 M)
19’ 9”(6.02 M)
72’ 5”(22.07 M)
170’ 6”(51.97 M)
SEENOTE
155’ 4”(47.35 M)
71’ 2”(21.69 M)
35’ 0”(10.67 M)
SCALE
0 2 4 6 M
0 10 20 FT
NOTE: Height, depending on load varies from 57’ 4” (17.48M) to 58’ 5” (17.81M).
182’ 3.1”(55.55 M)
104”X66”(164.2CM X 167.6CM)
19’ 9”(6.02 M)
26’ 10”(8.18 M)
27’ 10.5”(8.50 M)
19’ 9”(6.02 M)
170’ 6”(51.97 M)
SEENOTE
155’ 4”(47.35 M)
71’ 2”(21.69 M)
35’ 0”(10.67 M)
SCALE
72’ 5”(22.07 M)
0 2 4 6 M
0 10 20 FT
CARGO DOOR 10CF ONLY
2
DC-10T.O
. 00-105E-9
DC
-10.
AIRCRAFT DIMENSIONS-Continued
3
DC-10 SERIES 30 AND 30CF (LOWER GALLEY)
181’ 7.2”(55.35 M)
19’ 9”(6.02 M)
26’ 10”(8.18 M)
27’ 10.5”(8.50 M)
19’ 9”(6.02 M)
170’ 6”(51.97 M)
SEENOTE
165’ 4”(50.39 M)
71’ 2”(21.69 M)
35’ 0”(10.67 M)
SCALE
72’ 5”(22.07 M)
0 2 4 6 M
0 10 20 FT
CARGO DOOR 30CF ONLY
DC-10 SERIES 30 AND 30CF (UPPER GALLEY)
181’ 7.2”(56.35 M)
19’ 9”(6.02 M)
26’ 10”(8.18 M)
27’ 10.5”(8.50 M)
19’ 9”(6.02 M)
170’ 6”(51.97 M)
SEENOTE
165’ 4”(50.39 M)
71’ 2”(21.69 M)
35’ 0”(10.67 M)
SCALE
72’ 5”(22.07 M)
0 2 4 6 M
0 10 20 FT
CARGO DOOR 30CF ONLY
NOTE: Height, depending on load varies from 57’ 2” (17.42M) to 58’ 7” (17.86M).
70”X66”(177.8CM X 167.6CM)
104”X66”(164.2CM X 167.6CM)
DC-10T.O
. 00-105E-9
DC
-10.
AIRCRAFT DIMENSIONS-Continued
DC-10 SERIES 40 AND 40CF (LOWER GALLEY)
182’ 2.6”(55.54 M)
19’ 9”(6.02 M)
26’ 10”(8.18 M)
27’ 10.5”(8.50 M)
19’ 9”(6.02 M)
170’ 6”(51.97 M)
SEENOTE
165’ 4”(50.39 M)
71’ 2”(21.69 M)
35’ 0”(10.67 M)
SCALE
72’ 5”(22.07 M)
0 2 4 6 M
0 10 20 FT
CARGO DOOR 40CF ONLY
DC-10 SERIES 40 AND 40CF (UPPER GALLEY)
182’ 3.1”(55.55 M)
104”X66”(164.2CM X 167.6CM)
19’ 9”(6.02 M)
26’ 10”(8.18 M)
27’ 10.5”(8.50 M)
19’ 9”(6.02 M)
170’ 6”(51.97 M)
SEENOTE
165’ 4”(50.39 M)
71’ 2”(21.69 M)
35’ 0”(10.67 M)
SCALE
72’ 5”(22.07 M)
0 2 4 6 M
0 10 20 FT
CARGO DOOR 40CF ONLY
NOTE: Height, depending on load varies from 57’ 2” (17.42M) to 58’ 7” (17.86M).
70”X66”(177.8CM X 167.6CM)
4
DC-10T.O
. 00-105E-9
DC
-10.5 JET INTAKE AND BLAST DISTANCES
NOTE: Crosswinds will have considerable effect on contours.
5 FEET
35 MPH EXHAUST CURVE (TAKEOFF POWER)
35 MPH EXHAUST CURVE (IDLE POWER)
215 FEET
1,500 FEET
A
B
A 20 FOOT RADIUS
B 30 FOOT RADIUS
VIEW LOOKING UP FROM BOTTOM OF AIRCRAFT
ENGINE DANGER AREAS
INTAKE DANGER AREA
IDLE DANGER AREA
TAKE OFF EXHAUST DANGER AREA
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-10.6
AIRCRAFT EVACUATION ROUTESAND CLEARVIEW WINDOW ENTRY1. CLEARVIEW WINDOW ENTRY To gain access into flight compartment:
a. Chill clearview window pane with CO2.
b. Break window pane with heavy fire ax or suitable device.
c. Depress lock lever and push lever aft.
d. Push crank handle outboard and turn clockwise to move window aft.
AFT
1cLOCK LEVER 1a, 1b
CLEARVIEW WINDOW
RAMPWITHSLIDE
ESCAPEROPES
1dCRANK HANDLE
DOUBLE TRACK EVACUATION SLIDES (BOTH SIDES)
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-10.7
ENGINE NACELLE DOORS ANDFAN COWL ACCESS DOORS1. ENGINE NACELLE DOORS To open fan reverser:
a. Open fan and core cowl doors.
b. Open blowout and lower latch access panel doors on bottom of reverser.
c. Release forward mounting ring latches on each side of reverser.
d. Press trigger on door tension latch handle to release handle.
e. Pull handle to fully unlatched position.
f. Disengage latch hook from u-bolt.
g. Insert speed handle or nut runner into flex- shaft socket and crank reverser half open.
2. TO OPEN FAN AND CORE COWL DOORS
a. Press trigger on door tension latch handle to release handle.
b. Pull handle to fully unlatched position.
c. Disengage latch hook from u-bolt.
d. Raise door to open position and engage hold-open rods with engine fittings.
FAN REVERSER
1a, 2dFAN COWL DOORS (2)
1bACCESS DOORS
1e, 2bLATCH HANDLE
1d, 2aTRIGGER
1f, 2cLATCH HOOK
1cRING LATCHES(3 PLACES EACHDOOR)
COMPARTMENTCOOLING AIR EXIT
ENGINE OIL TANKSERVICING DOOR CSD SERVICING
DOOR
PRESSURE RELIEF DOOR GENERATORCOOLINGAIR EXIT
GEARBOXBREATHEROUTLET
COMPARTMENTCOOLING AIRINLET COMPARTMENT
COOLING AIR EXIT
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-10.
AIRCRAFT ACCESS DOORS
8 1. CENTER ACCESSORY COMPARTMENT DOOR
a. Pull down external handle and rotate in direction indicated by placarding on door.b. Stow handle and slide door to right side of fuselage.
2. APU ACCESS DOOR
a. Press trigger to release handle.b. Support door after unlatching.c. Door opens down.
3. APU GROUND CONTROL PANEL COMPARTMENT DOOR
a. Press three (3) triggers on door to release three handles.b. Door opens down.
1aEXTERNALHANDLE
CENTER ACCESSORYCOMPARTMENTACCESS DOOR
APU COMPARTMENTACCESS DOOR
2aHANDLE
2aTRIGGER
3aTRIGGER
3aHANDLE(TYPICAL)
ON ACFT WITHLOWER GALLEYONLY
APUCONTROLPANEL
FIREWARNINGHORN
APU CONTROL PANELCOMPARTMENT DOOR
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-10.9
FUEL VENT BOX (TYPICAL BOTH WINGS)OVERBOARD OUTLET (TYPICAL BOTH WINGS)
FUEL TANK #3 6000 GAL. (APPROX.)PRESSURE REFUELING/DEFUELING ADAPTORS(INSIDE ACCESS DOOR, TYPICAL BOTH WINGS)
ENGINE #3 FUEL FIRE SHUTOFF VALVEENGINE #3 HYDRAULIC FIRE SHUTOFF VALVEPORTABLE OXYGEN BOTTLES (CTR PARTITION)
FIRE EXT AGENT CONTAINERS (800 PSI, ENG #3)ENGINE #3
FUEL TANK #2 (CONTINUES OPPOSITE WING 9700 GAL. APPROX.)
AUXILIARY FUEL TANK (14,600 GAL. APPROX.)CUT-IN AREA (TYPICAL ENGINES #1 & #3)
ENGINE OIL TANK (TYPICAL ENGINES #1 & #3)PORTABLE OXYGEN BOTTLE (FWD PARTITION- TYPICAL 6 ATTENDANT’S STATIONS)WATER FIRE EXT (RT ATTENDANT’S STATION)
DRY CHEMICAL FIRE EXT (LT ATTENDANT’S STATION)
DRY CHEMICAL FIRE EXT
PASSENGER DOOR PNUEMATIC BOTTLE (1500 PSI, TYPICAL ALL PASSENGER DOORS)
PORTABLE OXYGEN BOTTLES (FWD)
EMERGENCY LIGHTING BATTERY POWER SUPPLY
RAIN REPELLENT CONTAINER (90 PSI)
CLEARVIEW WINDOW (BOTH WINDOWS TYPICAL-CHOP IN AREA)
EMERGENCY LIGHTS CONTROL SWITCH(OVERHEAD SWITCH PANEL)
ENGINE FIRE CONTROL HANDLES
CREW PORTABLE OXYGEN BOTTLE (CREW COATROOM PARTITION)
AVIONICS COMPARTMENT LOWER DOORINERTIAL NAVIGATION SYSTEM BATTERIES (IF INSTALLED) CREW FIXED OXYGEN
BOTTLE (1850 PSI)OXYGENOVERFLOWVENT
ENGINE #1LOWER CARGO FIRE EXT CONTAINER INSTALLATION
EMERGENCY LIGHTING BATTERY POWER SUPPLYPASSENGER DOOR (42 X 76 INCHES, TYPICAL 6 PLACES)
FORWARD CARGO DOORUPPER CARGO DOOR (CONVERTIBLE FREIGHTER AIRCRAFT ONLY)
EMERGENCY LIGHTS CONTROL SWITCH (FWD LT ATTENDANT STATION)PASSENGER DOOR (32 X 76 INCHES, OPPOSITE DOOR TYPICAL)ESCAPE SLIDE PNEUMATIC BOTTLE (3000 PSI-INSIDE ESCAPE SLIDE-TYPICALALL PASSENGER DOORS)AVIONICS COMPARTMENT AFT DOOR
CARBON DIOXIDE AND WATER FIRE EXTINGUISHERS (FLIGHT COMPARTMENT ONCOATROOM PARTITION) FUEL TANK #1 (6000 GAL. APPROX.)
FUEL DUMP OUTLET (TYPICAL OPPOSITE WING)PORTABLE OXYGEN BOTTLES (4 1/4 OR 11 CU FT- AFT PARTITION)
EMERGENCYLIGHTING BATTERYPOWER SUPPLY
APU FUEL FIRE SHUTOFF VALVE
EMERGENCY LIGHTING BATTERYPOWER SUPPLY
CENTER CARGO DOOR
ENGINE #2ENGINE OIL TANKENGINE #2 HYDRAULICFIRE SHUTOFF VALVEFIRE EXT AGENT CONTAINERS (800 PSI-AFTACC COMP, FOR ENGINE #2 & APU AREA)HYDRAULIC FLUID RESERVOIR (AFTACCESSORY COMPARTMENTAFT ACCESSORY COMPARTMENT
APU EXHAUST DUCT (RT SIDE ONLY)APU COMPARTMENT DOORAPU FUEL FIRE SHUTOFF VALVEPRESSURE BULKHEAD (AFT END OFPASSENGER COMPARTMENT)HORIZONTAL STABILIZER JACK SCREWS &MOTORS ACCESS DDORWATER FIRE EXT (RT SIDE AFT DIVIDERPARTITION)AFT CARGO DOOR
CUT-IN AREA (SKIN 0.071 INCH, LONGERONS0.050 TO 0.063 INCH - TYPICAL 8 AREAS)
HYD ACCUMULATORS (1000 PSI, WHEELWELL, TYPICAL BOTH WHEELS)HYD FLUID RESERVOIR (WHEEL WELL,OPPOSITE SIDE TYPICAL)
FIRESEALS (TYPICAL ALL ENGINES)
APU GRD CONTROL PANEL (AFT OF WHEELWELL, LT SIDE)ENGINE #2 FWD FUEL SHUTOFF VALVEAPU FUEL FIRE SHUTOFF VALVEENGINE #1 FUEL FIRE SHUTOFF VALVE
WATER FIRE EXT (RT ATTENDANT STATION)DRY CHEMICAL FIRE EXT (LT ATT. STATION)ENGINE #1 HYDRAULIC FIRE SHUTOFFVALVE
CENTER ACCESSORY COMPARTMENT DOORMAIN BATTERIES (CTR ACC COMP.)
FIRE EXT AGENT CONTAINERS ( 800 PSIFOR ENGINE #1)
ENGINE #1 OIL TANK
AIRCRAFT FLAMMABLE MATERIAL LOCATIONS
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-10.10
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot Ladder¼ Inch Drive ToolFire Drill IIAIRCRAFT ENTRY
When emergency mode is used to open any passenger door, door will automatically move to full open position.
1. OPERATION OF ALL 8 DOORS WITH NON PUSH BUTTON TYPE: NORMAL MODE-ELECTRICALa. Pull door control handle out of recess.b. Move handle to open position and hold.c. When door is fully open, return handle to neutral detent.
IF DOOR DOES NOT OPEN:2. EMERGENCY MODE-PNUEMATIC (ALL 8 DOORS)a. Hold door control handle at open position.b. Depress and hold emergency opening button, or if emer- gency override lever is installed, rotate from safe to emer- gency and hold.c. Move door control handle to emergency position (see dotted PULL handle).
IF DOOR STILL DOES NOT OPEN:d. Push door inward as far as possible and hold. For forward doors, push in area of window.e. Use any available means to pry door upward.
Door with slide attached is very heavy. Required lifting force may exceed 400 pounds.
3. AUXILIARY MODE USING 1/4-INCH DRIVE FITTING (Applicable for forward left fuselage door only.)a. Hold door control handle at open position.b. Insert 1/4-inch drive tool in manual drive fitting and turn counterclockwise until door is open.
Torque applied in excess of 100 inch pounds or 500 RMPs may result in damage.
c. Return door control handle to neutral detent and push inward to stow.
WARNING
WARNING
CAUTION
CLOSE OPEN
FWD MID OVERWING AFT
LEFT FWD DOOR ONLY (SOME AIRCRAFT)
EMERGENCY OPENING BUTTON
AUXILIARY HANDLE
DOOR CONTROL HANDLE
MANUAL DRIVE(LEFT FWD DOORONLY SOME ACFT)
NEUTRALDETENT
POSITIVE STOP AT OPENPOSITION DURINGNORMAL OPERATION
POSITIVE STOP ATCLOSE POSITION
EMERGENCY
OPEN
CLOSE
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DC
-10.11
AIRCRAFT ENTRY-ContinuedWARNING
When emergency mode is used to open any passenger door, door will automatically move to full open position.
4. OPERATION OF ALL 8 DOORS WITH PUSH BUTTON TYPE: NORMAL MODE-ELECTRICALa. Pull door control handle out of recess to disarm escape slide.b. Move door control switch to open and hold.c. When door is fully open, release switch.
IF DOOR DOES NOT OPEN:5. EMERGENCY MODE-PNUEMATIC (ALL 8 DOORS)a. Pull door control handle out of fuselage.b. Rotate emergency override lever from safe position to emergency position and hold.c. Rotate door control handle to emergency position (see dotted PULL handle).
IF DOOR STILL DOES NOT OPEN:d. Push door inward as far as possible and hold. For forward doors, push in area of window.e. Use any available means to pry door upward.
Door with slide attached is very heavy. Required lifting force may exceed 400 pounds.
6. AUXILIARY MODE USING 1/4-INCH DRIVE FITTING (Applicable for forward left fuselage door only.)a. Pull handle out, rotate to free fall position and hold.b. Insert 1/4-inch drive into socket and rotate as indi- cated until door is open.
Torque applied in excess of 100 inch pounds or 500 RMPs may result in damage.
c. Release door control handle to neutral position.
CAUTION
WARNING
CLOSE OPEN
MID OVERWING AFTFWD
LEFT FWD DOOR ONLYPASSENGER DOORS (8)
EMERGENCYOVERRIDELEVER
EMERGENCY
SAFE
AUXILIARY HANDLE
DOORCONTROLSWITCH
FREE FALL
EMERGENCY
DOOR OPEN
CLOSED
NOTE: When moved to emergency position and held, allows door control handle to be moved to emergency for emer- gency opening of the door when electrical power is not available.
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DC
-10.12 7. FLIGHT COMPARTMENT ENTRY THROUGH THE AVIONICS COMPARTMENT
a. To open the avionics compartment lower access door, pull down and turn external handle counterclockwise.
b. Stow handle and slide door forward.
c. To open avionics compartment aft access door, turn handle up (clockwise) and push door.
d. To open avionics compartment emergency access door, push to open into flight compartment.
e. Use aft access door from passenger compartment to access flight compartment. Rotate handle up to unlock aft access door.
AIRCRAFT ENTRY-Continued
7cAFT ACCESSDOOR HANDLE
7bLOWERACCESSEXTERNALHANDLE
7aLOWERACCESS DOOR
FLIGHT COMPARTMENT
7eAFT ACCESSDOOR
7dEMERGENCYACCESS DOOR7d
AVIONICSCOMPARTMENT
7eAFT ACCESSDOOR HANDLE
VIEW LOOKING FORWARD
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DC
-10.13
AIRCRAFT ENTRY-Continued8. EXTERNAL CARGO DOOR OPERATION WITH POWER AVAILABLE
a. Press trigger to release handle.b. Pull handle out and up.c. Place door power switch on.d. Place door switch to open.
To prevent door from springing open, manually crank door actuator to the fully closed position prior to manually unlatching.
9. EXTERNAL CARGO DOOR OPERATION WITH MANUAL MODE-NO POWER
a. Press trigger to release handle.b. Pull handle out and up.c. Insert drive tool in latch manual drive fitting and turn drive tool toward unlock position until latches are open.d. Insert drive tool in door manual drive fitting and turn clockwise until door is open.
WARNING
CARGO DOOR
9dDOORSWITCH
9cPOWERSWITCH
LATCHVIEWINGPORT
VENT DOOR
9bDOOR HANDLE
9aTRIGGER
9c3/8 INCH LATCHMANUAL DRIVEFITTING RECEPTACLE
9d3/8 INCH LATCHMANUAL DRIVEFITTING RECEPTACLE
MANUAL OPERATION
LOCK PIN ENGAGEDSYSTEM SAFE
LOCK PINNOT ENGAGEDSYSTEM UNSAFE
CAUTION
BE SURE LOCKPINS ENGAGED
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DC
-10.14
AIRCRAFT ENTRY-Continued10. UPPER CARGO DOOR INTERNAL OPERATION CONVERTIBLE FREIGHTER AIRCRAFT ONLY
NOTE: If installed, pip pin must be removed from locktube to allow unlocking of lockpin handle.
a. To open manually, rotate vent door handle to unlock position.
b. Pull lockpin handle up to unlock position and hold.
c. Insert pipe or hydraulic hand pump handle in latch actuating socket and push down to unlatched position.
d. Release lockpin handle and remove pipe or hand pump handle from latch actuating socket.
e. Place cable loop or hook through latch actuating socket to manually hoist door open.
UNLOCK AND HOLD OPEN WHILE UNLOCKING LATCH MECHANISM
10b, 10dLOCK PINHANDLE
10eLATCHACTUATINGSOCKET
10cLATCH AND HYDRAULICHAND PUMP HANDLE(INSTALLED)
VIEWINGPORT
10aVENTDOOR
UNLOCK
LOCK
PUSH
LATCHED
UNLATCHED
LOCK PIN ENGAGEDSYSTEM SAFE
LOCK PIN NOTENGAGEDSYSTEM UNSAFE
CARGO DOOR VENT
OPEN PRIOR TO OPENING CARGO DOOR
CLOSE AND LOCK PRIOR TO FLIGHT
IF CARGO DOOR WILL NOT OPEN:
ROTATE DOOR CONTROL HANDLE TO “CLOSE” AND RELEASE
OPEN VENT DOOR
CARGO DOOR VENTUNLOCKED LOCKED
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-10.
EMERGENCY RESCUE ACCESS
15
CLEARVIEW WINDOW -CUTIN/CHOP OUT
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.
HORIZONTAL STABILIZER JACKSCREWS AND MOTORS ACCESSDOOR
AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 4 FTWHEELS EXTENDED: 8 FT
FWD PASSENGER ENTRY DOOR
FWD SERVICE ENTRY DOOR
APU COMPARTMENT DOOR
UPPER CARGO DOOR ON CONVERTIBLE FREIGHTER AIRCRAFT ONLY
CENTER CARGO DOOR
PASSENGER ANDSERVICE DOORS
CUT-IN/CHOP OUT AREAS
AFT ACCESSORYCOMPARTMENT DOOR
PRESSURE BULKHEAD
FWD CARGO DOOR
CUT-IN/CHOP OUT AREAS
AFT CARGO DOOR
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-10.16
ENGINE/APU SHUTDOWN AND AIRCREW EXTRACTION1. ENGINE SHUTDOWN
a. Retard throttles, located on pilot’s console, full aft position.
b. Place fuel control levers, located on pilot’s center console, aft and down to full detent.
c. Place APU fire control switch, located on flight engineer’s left panel to OFF position.
d. Place battery switch, located on flight engineer’s upper left panel, to OFF position.
e. If engines fail to shutdown: Lift “ENG/FIRE” handle guards, push emergency fire T-handles, located on pilot’s overhead panel, down and forward.
f. In case of engine fire: While holding forward pressure on handle, turn handle clockwise and hold. After 10 seconds, turn handle counterclockwise.
2. APU SHUTDOWN
a. Place the APU master switch, located on flight engineer’s upper forward panel or exterior panel down to the OFF position.
b. In case of APU light illumination: Place APU off and agent arm switch to agent arm UP position. Place CYL 1 to DISCHARGE up position. After 10 seconds place CYL 2 to DISCHARGE up position.
3. AIRCREW EXTRACTION
a. Rotate quick release knob on lap belt and remove shoulder harness.
b. Pull seat manual release handle to adjust seat to a recline position in removing crewmembers.
c. Passenger seats are equipped with lap belts only.
1eEMERGENCYT-HANDLES
CENTER OVERHEAD SWITCH PANEL
1aTHROTTLES
1bFUEL CONTROL LEVERS
1dBATTERY SWITCH
1cAPUSWITCH
APU EXTERIOR PANEL
APU FIRE
1cAPU FIRECONTROL SWITCH
UPPERFORWARD PANEL
FLIGHTENGINEERPOSITION
PILOT/COPILOT POSITION (FACING FORWARD)
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-10.
CABIN CONFIGURATION
17
GALLEY
LAVATORY
LAVATORY
ATTENDANT SEAT
ENTRY DOOR 4R42X76” (107X193 CM)
CLOSET
LAVATORY
LAVATORY
ATTENDANT SEAT
ATTENDANT SEAT
CLOSET
ATTENDANT SEAT ATTENDANT SEAT
CLOSET
ATTENDANT SEAT
ATTENDANT SEAT
ATTENDANT SEAT
GALLEY
ENTRY DOOR 3R42X76” (107X193 CM)
ENTRY DOOR 3L42X76” (107X193 CM)
ENTRY DOOR 2R42X76” (107X193 CM)
ENTRY DOOR 1R32X76” (81X193 CM)
ENTRY DOOR 1L32X76” (81X193 CM) ENTRY DOOR 2L
42X76” (107X193 CM)ENTRY DOOR 4L42X76” (107X193 CM)
DC-10 SERIES 10, 30, 30CF, 40 AND 40CFMIXED CLASS (LOWER GALLEY)
270 PASSENGERS222 8-ABREAST SEATING AT 34” (86 CM) PITCH 48 6-ABREAST SEATING AT 38” (97 CM) PITCH
NOTE: All entry doors are emergency exits.
SCALE
0 2 4 6 METERS
0 10 20 FEET
DC-10 SERIES 10, 30, 30CF, 40 AND 40CFALL ECONOMYCLASS
399 PASSENGERSALL ECONOMY 10-ABREAST SEATING AT 34”, 32”, 31”, 30”, AND 29” PITCH
NOTE: All entry doors are emergency exits.
SCALE
0 2 4 6 METERS
0 10 20 FEET
LAVATORY
LAVATORY
LAVATORY
LAVATORY
ATTENDANT SEAT
ATTENDANT SEAT
ENTRYDOOR 1R 32X76”(81X193 CM)
ENTRY DOOR 1L 32X76” (81X193 CM)
ATTENDANT SEAT
ATTENDANT SEAT
CLOSETCLOSET
ATTENDANT SEAT
ATTENDANT SEAT
GALLEYGALLEY
ATTENDANT SEAT
ENTRY DOOR 2R 42X76” (107X193 CM)
ENTRY DOOR 3R 42X76” (107X193 CM)
ATTENDANT SEAT
ENTRY DOOR 2L42X76” (107X193 CM)
ENTRY DOOR 3L42X76” (107X193 CM)
ENTRY DOOR 4L42X76” (107X193 CM)
ENTRY DOOR 4R 42X76” (107X193 CM)
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DC
-10.
CABIN CONFIGURATION-Continued
18
LAVATORY
LAVATORYATTENDANT SEAT
CLOSET
LAVATORY
LAVATORY
ATTENDANT SEAT
ATTENDANT SEAT
ATTENDANT SEAT
CLOSET
ATTENDANT SEAT
ENTRY DOOR 3L42X76” (107X193 CM)
ENTRY DOOR 2L42X76” (107X193 CM)
ENTRY DOOR 4L 42X76” (107X193 CM)
DC-10 SERIES 10, 30, 30CF, 40 AND 40CFMIXED CLASS (UPPER GALLEY)
277 PASSENGERS255 9-ABREAST SEATING AT 34” (86 CM) PITCH 22 6-ABREAST SEATING AT 34” (86 CM) PITCH
NOTE: All entry doors are emergency exits.
SCALE
0 2 4 6 METERS
0 10 20 FEET
DC-10 SERIES 10, 30, 30CF, 40 AND 40CFMIXED CLASS (MAIN DECK BAGGAGE)
215 PASSENGERS199 9-ABREAST SEATING AT 34” (86 CM) PITCH 22 6-ABREAST SEATING AT 42” (107 CM)
NOTE: All entry doors are emergency exits.
SCALE
0 2 4 6 METERS
0 10 20 FEET
LAVATORY
LAVATORIES
LAVATORY
LAVATORY
ATTENDANT SEAT
ATTENDANT SEAT
ENTRYDOOR 1R 32X76”(81X193 CM)
ENTRY DOOR 1L 32X76” (81X193 CM)
ATTENDANT SEAT
ATTENDANT SEAT
CLOSET
CLOSET
ATTENDANT SEAT
ATTENDANT SEAT
MAIN DECK BAGGAGE
ENTRY DOOR 2R 42X76” (107X193 CM)
ENTRY DOOR 3R342X76” (107X193 CM)
ATTENDANT SEAT
ENTRY DOOR 2L42X76” (107X193 CM)
ENTRY DOOR 3L42X76” (107X193 CM)
ENTRY DOOR 4L42X76” (107X193 CM)
ENTRY DOOR 4R 42X76” (107X193 CM)
ATTENDANT SEAT
LAVATORY
ENTRY DOOR 3R 42X76” (107X193 CM) ENTRY
DOOR 4R 42X76” (107X193 CM)
LAVATORY
ENTRY DOOR 2R 42X76” (107X193 CM) ENTRY
DOOR 1R 32X76”(81X193 CM)
ATTENDANT SEAT
ENTRY DOOR 1L 32X76” (81X193 CM)
LAVATORY
LAVATORY
LAVATORY
ATTENDANT SEAT
LAVATORY
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-10.
CARGO CONFIGURATION
19
DC-10 SERIES 10CF, 30CF, AND 40CFMAIN CABIN CARGO
9 g BARRIER NET
MAIN CARGO COMPARTMENT LENGTH=120 FT 11 INFLAT FLOOR AREA= 2200 SQ FTBULK VOLUME* = 16,760 CU FT
1R 2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 13R 14R 15R
* BULK VOLUME IS WATER VOLUME OF CABINBETWEEN STATIONS NOTED.
STA 495 STA 1946
DC-10 SERIES 10CF, 30CF, AND 40CFMAIN CABIN CARGO (88X108” PALLETS)
1L 2L 3L 4L 5L 6L 7L 8L 9L 10L 11L 12L 13L 14L 15L
MAIN CABIN CARGO VOLUME 30 - 88”X108” PALLETS12,248 CU FT (346.81 CU M)
DC-10 SERIES 10CF, 30CF, AND 40CFMAIN CABIN CARGO (88X125” PALLETS)
MAIN CABIN CARGO VOLUME 22 - 88”X125” PALLETS10,874 CU FT (307.95 CU M)
1R 2R 3R 4R 5R 6R 7R 8R 9R 10R 11R
1L 2L 3L 4L 5L 6L 7L 8L 9L 10L 11L
DC-10 SERIES TYPICAL CARGO SECTION
FULL OPEN=165
PARTIAL OPEN=165
0
0
CEILING AND HEIGHT 88” AT 2NDAND 3RD PASSENGER DOORS
84” FWD AND AFT DROP CEILINGS
CONSTANT SECTION 118.5” RADIUS
GROUNDLINE
102” OPENING
95” BASIC CEILING HEIGHT
66”
193.6 - 188.2”
FULL OPEN
42.4” FOR 70X66” DOOR17.6” FOR 104X66” DOOR
115.7 - 105.0” 125.5”164”
18’ 2”
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-10.20
CARGO CONFIGURATION-ContinuedDC-10 SERIES 10, 30, 30CF, 40 AND 40CFSTANDARD CENTER CARGO COMPARTMENT (LOWER GALLEY)
DC-10 SERIES 30, 30CF, 40 AND 40CFEXTENDED CENTER CARGO COMPARTMENT (UPPER GALLEY)
DC-10 SERIES 10, 10CF, 30, 30CF, 40 AND 40CFSTANDARD CENTER CARGO COMPARTMENT (UPPER GALLEY)
DC-10 SERIES 10, 10CF, 30, 30CF, 40 AND 40CF - CONTAINERS/PALLETSSTANDARD CENTER CARGO COMPARTMENT (UPPER GALLEY)
66X70”CARGO DOORRT SIDE ONLY(6 CONTAINERS)
66X70”CARGO DOORRT SIDE ONLY(8 CONTAINERS)
BULK CARGODOOR LTSIDE ONLY
NOTE: Aircraft may also have extended center compartment. 14 LD3 containers used.
BULKCARGO
66X70” OR 66X104”CARGO DOORRT SIDE ONLY(16 CONTAINERS)
66X70”CARGO DOORRT SIDE ONLY(10 CONTAINERS)
66X70” OR 66X104”CARGO DOORRT SIDE ONLY(16 CONTAINERS)
66X70”CARGO DOORRT SIDE ONLY(8 CONTAINERS)
BULK CARGODOOR LTSIDE ONLY
66X104”CARGO DOORRT SIDE ONLY(5 PALLETS)
66X70”CARGO DOORRT SIDE ONLY(8 CONTAINERS)
BULK CARGODOOR LTSIDE ONLY
NOTE: 5 Pallets and 8 LD3 containers used.
NOTE: 24 LD3 containers used.
NOTE: 26 LD3 containers used.