I2104

Starting Position: Overhead KNSE WORKSHEET Altitude: 12,000’ Heading: 360° SIMULATOR IN-FLIGHT COCKPIT SETUP Speed: 200 KIAS Discuss

a. IMC emergencies NATOPS statement on sound judgement IMC verses VMC considerations Example: Generator light in IMC verses VMC (land as soon as practical versus

possible)

b. Avionics Failures (Dual IAC Failure) NATOPS Procedure

c. BFI Differences between PFD and BFI displays BFI DISPLAY

T-6B Basic Instruments I2100 Block

STUDENT GRADE SHEET DATE __________________ INSTRUCTOR __________________________ MEDIA: UDT VT- ________ BRIEF TIME: ________ NAME: ____________________________________ EVENT:__________

# MANEUVER MIF I2101 I2102 12103 I2104 1 GENERAL KNOWLEDGE / PROCEDURES 3+ X X X X 2 EMERGENCY PROCEDURES 3+ X X X X 3 HEADWORK / SITUATIONAL AWARENESS 2+ X X X X 4 BASIC AIRWORK 3+ X X X X 5 IN-FLIGHT CHECKS / FUEL MANAGEMENT 2+ X X X X 7 TASK MANAGEMENT 2+ X X X X 8 COMMUNICATION 2 9 MISSION PLANNING / BRIEFING /

DEBRIEFING 2

10 GROUND OPERATIONS 2 11 TAKEOFF 2 12 DEPARTURE 2 40 S-1 PATTERN 3+ X X X 41 STEEP TURNS 3+ X X X X 42 IFR UNUSUAL ATTITUDES 3+ X X 43 TIMED TURNS 3+ X X X X 47 GCA PATTERN 3+ X X X 48 APPROACH PATTERN 3+ X X 50 ENROUTE PROCEDURES 2 51 ENROUTE DESCENT 2+ X X X SPECIAL SYLLABUS REQUIREMENTS 1 X

SSR: I2103 Proceed direct to Home Field using any available NAVAID DISCUSS ITEMS: I2101: Departures, steep turns, timed turns, enroute descent, and scan patterns. I2102: IMC emergencies, GCA pattern, and S-1 pattern. I2103: Approach maneuver and IFR unusual attitudes. I2104: IMC emergencies, avionics failures and BFI. DEPART ______________ ARRIVE ______________ SIDE # ______________ SIM TIME ___________

JPPT 1542.166B Rev 03/30/2017

SIMULATOR IN-FLIGHT COCKPIT SETUP BATT/GEN/AUX BATT………………………………………..On Avionics Master ….…………………………………………….On Probes Anti-Ice………………………………………………….On Bleed Air Inflow…………………………………………….Norm O2………………………………………………………………Normal Altimeter……………………………………………………….29.92 TCAS………………………………………………………………….On TAD……………………………………………………………………On Gear/Flaps.………………………………………….…………….Up Friction Lock…………………………………………….Adjusted PCL………………………………………………..…Set (for 200 KIAS) Seat and Rudder Pedals ………………………....Adjusted Seat Safety Pin…………………….Removed and Stowed

SIMULATOR GROUND PROCEDURES CHECKLIST Initial cockpit set up: Adjust seat height and rudder pedals; Batt, Gen, Aux Batt on; Avionics master on; Bleed air inflow Norm; O2 normal; TAD on; TCAS on BEFORE TAXI 17. UFCP AND MFD’S

b. UHF………….……….………… Copy ATIS and Obtain Clearance c. VHF COM………………………………………………. Set as Required d. VOR…………………………………………………….... Set as Required e. Transponder………………..……………………..….. SET, STANDBY f. FMS………………………………………..…………….. Set as Required g. Alt, G, Speed, Fuel flags….……...…………….. Set as Required

19. ALTIMETERS……..……____SET AND CHECKED TWICE (BOTH) Call for TAXI BEFORE TAKEOFF 3. FLAPS……………………………….….………………………………. TAKEOFF 4. TRIM……………………………….…………..…………….SET for TAKEOFF 11. SEAT SAFETY PIN……….….. REMOVED AND STOWED (BOTH) 12. ISS MODE SELECTOR…….……………….…. BOTH, ROGER BOTH Call for TAKEOFF LINEUP CHECKLIST 1. EXTERIOR LIGHTS ……...…….………..……………………..…………. ON 2. TRANSPONDER ……………………….…..………………………ALTITUDE 3. PROBES ANTI-ICE SWITCH ……….…………..……….………..…… ON 4. NOSE WHEEL STEERING ………………….……..……….………….. OFF 5. EICAS DISPLAY …………….…………….…………… CHECKED (BOTH) Flight Manual Date: 01 December 2017

AIR FORCE TO 1T-6B-1NAVY (NAVAIR) A1-T6BAA-NFM-100

ii

SCOPEThis manual contains the necessary information for safe andefficient operation of the aircraft. These instructions providea general knowledge of the aircraft, its characteristics, andspecific normal and emergency procedures. Instructions inthis manual are prepared to be understandable by the leastexperienced crewmember that can be expected to operate theaircraft.

SOUND JUDGEMENT

This manual provides the best possible operating instructionsunder most circumstances, but it is not a substitute for soundjudgement. Multiple emergencies, adverse weather, terrain,etc. may require modification of the procedures.

PERMISSIBLE OPERATIONS

The flight manual takes a positive approach and normallystates only what can be done. Unusual operations or configu-rations are prohibited unless specifically covered herein.Clearance from the using command must be obtained beforeany questionable operation, which is not specifically permit-ted in this manual, is attempted.

HOW TO BE ASSURED OF HAVING LATEST DATA

Refer to https://www.toindex-s.wpafb.af.mil/the Data Man-agement section for a listing of all current flight manuals,safety supplements, operational supplements, and checklists.Also, check the flight manual cover page, the title block ofeach safety and operational supplement, and all status pagesattached to formal safety and operational supplements. Clearup all discrepancies before flight.

ARRANGEMENT

The manual is divided into eight fairly independent sectionsto simplify reading it straight through or using it as a refer-ence manual.

SAFETY SUPPLEMENTS

Information involving safety will be promptly forwarded in asafety supplement. Urgent information is published ininterim safety supplements and transmitted by defense mes-sage system (DMS). Formal supplements are mailed. Thesupplement title block and status page (published with for-mal supplements only) should be checked to determine thesupplement’s effect on the manual and other outstandingsupplements.

OPERATIONAL SUPPLEMENTS

Information involving changes to operating procedures willbe forwarded by operational supplements. The procedure forhandling operational supplements is the same as for safetysupplements.

CHECKLISTS

The flight manual contains itemized procedures with neces-sary amplifications. The checklist contains itemized proce-dures without the amplification. Primary line items in theflight manual and checklist are identical. If a formal safety oroperational supplement affects the checklist, the affectedchecklist page will be attached to the supplement. Thechecklist page should be cut out and inserted in case the sup-plement is rescinded and the page is needed.

BFI Major differences from normal PFD:

-No Turn Needle (will need to use the 10 and 20% rule to compute AOB as needed for rates of turn)

-Side Slip indicator upside down. The BFI has it on the top of the ROLL POINTER so it moves with the roll pointer. On the PFD it is located on the bottom of the zero bank angle position of the ROLL ATTITUDE SCALE and remains stationary during turns.

-Altimeter is graduated in 20 ft increments vice 10.

-Miniature aircraft display is different.

-Only partial Heading indication visible (direction of large turns not as obvious).

-VSI has no pointer…digital readout with ^ /v indications for climb and descent.

Change 1 3-27

AIR FORCE TO 1T-6B-1NAVY NAVAIR A1-T6BAA-NFM-100

instrument, fire detection system (FIRE 1 only), IRU, andVHF radio (tuning provided by the standby VHF controlhead).

Systems that will be inoperative include:

• OBOGS

• ICS

• All electronic displays

• PMU

• Starter

• Fire detection system (FIRE 2)

• Landing gear indicators

• Normal flap operation and indicators

• Probes anti-ice

• Interior and exterior lighting, except backup flightinstrument

• ECS/pressurization

• UHF communications/navigation and GPS

1. Descent below 10,000 ft MSL - Initiate (as required)

OBOGS will be inoperative once the mainbattery is depleted or with battery failure.

NOTECockpit will depressurize when power to thebattery bus is lost.

2. AUX BAT switch - ON

NOTEBackup flight instrument and VHF tuning(standby VHF control head) will be poweredfor approximately 30 minutes by the auxil-iary battery. Plan to extend the landing gearusing the emergency extension system.Emergency flaps will not be functional if themain battery has failed. With normal flapextension and a loss of power to the batterybus, flaps will retract. Landing gear and flapposition indicators will not be powered. Thetaxi and landing lights will not be functional.

3. Land as soon as possible

AVIONICS FAILURES

NOTE• During all electronic display failures, the

pilot should confirm indications in both cock-pits (if occupied), reference alternate datasources or the backup instruments as applica-ble, and check applicable circuit breakers.

• In the following procedures, the term “reset”is used to describe the action of resetting acircuit breaker that is already open. The pilotshould assess the severity of the emergencyand equipment lost prior to resetting or open-ing any circuit breaker.

Integrated Avionics Computer (IAC) Failure (Single /Dual) (Loss of MFD Displays/Erratic Displays/Integrated Avionics System Synchronization Errors)

Dual IAC failure will result in the loss of HUD, UFCP andMFD displays in both cockpits.

Loss of a single IAC may not cause an IAC1 FAIL/IAC2FAIL message to be displayed, but may cause loss of MFDdisplays in one or both cockpits, erratic MFD displays, orIAC synchronization errors. The HUD and UFCP may, ormay not be operating properly.

IAC data crosstalk malfunction can result in a loss of syn-chronization between cockpits. Loss of this synchronizationmay result in incorrect function of the REPEAT mode. Thismay occur without alerting an IAC failure.

Loss of synchronization or erratic indications betweenshared information in each cockpit is indicative of pendingor possible cross talk malfunction. Synchronization errorsmay present as heading, altitude and speed “bug” is matchedsettings between cockpits or altimeter synchronization errorswith an associated ”QNH DISAGREE” FMS message.

Do not select REPEAT in cockpit with work-ing MFD’s. This may result in loss of allMFD information in both cockpits.

NOTE• If synchronization errors or erratic indica-

tions are detected on ground, takeoff is notrecommended.

• If synchronization errors are detected withouta loss of MFD information, do not selectREPEAT on UFCP in either cockpit.

3-28 Change 1

AIR FORCE TO 1T-6B-1NAVY NAVAIR A1-T6BAA-NFM-100

1. Backup flight instrument - Reference as required2. NORM/REPEAT switch - NORM (both cockpits)3. IAC1 and IAC2 circuit breakers (left and right front

console) - Check, reset if open

If IAC/MFD failures or erratic displays persists:

NOTEFront cockpit failures/erratic displays indi-cate IAC1 failure, rear cockpit failures/erraticdisplays indicate IAC2 failure.

4. Failed IAC circuit breaker(s) (left and right front con-sole) - Pull, reset after 5 seconds

If IAC/MFD failures, erratic displays, or IAC synchroniza-tion errors persists:

5. Land as soon as practical

<6>IAC XTALK Failure1. <6>MFD/UFP REPEAT/NORM switch - NORM

NOTE<6>An amber IAC XTALK message mayresult in loss of repeat switch functionality.RPT ERROR will be posted if MFD/UFPREPEAT/NORM switch is in REPEAT posi-tion. Baro Set function, heading, altitude andairspeed bug settings, minimums on/offselection, radio altitude set height, mag/truecompass setting, bingo fuel setting, clock set-ting and G reset feature will operate inde-pendently in each cockpit.

<6>With IAC XTALK message present,Baro Set function on the UFCP will operateindependently in each cockpit. Confirm PFDaltimeter settings in each cockpit.

IRS Failure (Loss of Attitude or Heading Display on HUD and MFD)

1. Backup flight instrument - Reference as required2. IRS circuit breaker (left and right front console) -

Check, reset if open3. Place aircraft in straight and level unaccelerated flight

and monitor alignment status

4. Land as soon as practical

MFD Failure or Avionics Bus Failure

FOR MFD FAILURE WITH NO OTHER INDICATIONS:

NOTEFailure of a single MFD will result in PFDand EICAS display only and loss of ability tomanipulate the display to the FMS MENU.

1. NORM/REPEAT switch in failed cockpit - REPEAT2. MFD circuit breaker (left MFD right console, right and

center MFD left console) - Check, reset if open

FOR MFD FAILURE WITH OTHER AVIONICS FAIL-URES, BUT WITHOUT GEN BUS OR BATT BUSWARNING:

3. FWD/AFT AVI circuit breakers (left and right frontconsole) - Check, reset if open

4. Backup flight instruments - Reference as required

IF FWD AVIONICS GEN BUS REMAINS INOPERA-TIVE:

5. Land as soon as practical

UFCP Failure (Blank UFCP Entry Windows, Data Entry Knob or System Button Non Functioning)

NOTEWith the UFCP inoperative, the functions notavailable to the pilot in the cockpit with thefailed UFCP are: FMS execute, system Mag/True heading toggle, system GS/CAS/TASHUD speed toggle, and radio tuning withUFCP.

1. UFCP circuit breaker (left front console or left rearconsole) - Check, reset if open

2. Land as soon as practical

Backup Flight Instrument Display Failure1. Place aircraft in straight and level unaccelerated flight2. STBY INST circuit breaker (left front/left rear con-

sole) - Check, reset if open3. AFT STBY circuit breaker (left front console) -

Check, reset if open

If display does not return:4. Land as soon as practical