I2104. Altitude: 12,000 Heading: 360 SIMULATOR IN-FLIGHT COCKPIT SETUP Speed: 200 KIAS

Transcription

1 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

2 T-6B Basic Instruments I2100 Block STUDENT GRADE SHEET DATE INSTRUCTOR MEDIA: UDT VT- BRIEF TIME: NAME: EVENT: # MANEUVER MIF I2101 I I 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 / 2 DEBRIEFING 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 B Rev 03/30/2017

3 SIMULATOR IN-FLIGHT COCKPIT SETUP BATT/GEN/AUX BATT..On Avionics Master..On Probes Anti-Ice.On Bleed Air Inflow.Norm O2 Normal Altimeter 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

4 AIR FORCE TO 1T-6B-1 NAVY (NAVAIR) A1-T6BAA-NFM-100 SCOPE This manual contains the necessary information for safe and efficient operation of the aircraft. These instructions provide a general knowledge of the aircraft, its characteristics, and specific normal and emergency procedures. Instructions in this manual are prepared to be understandable by the least experienced crewmember that can be expected to operate the aircraft. SOUND JUDGEMENT This manual provides the best possible operating instructions under most circumstances, but it is not a substitute for sound judgement. Multiple emergencies, adverse weather, terrain, etc. may require modification of the procedures. PERMISSIBLE OPERATIONS The flight manual takes a positive approach and normally states only what can be done. Unusual operations or configurations are prohibited unless specifically covered herein. Clearance from the using command must be obtained before any questionable operation, which is not specifically permitted in this manual, is attempted. HOW TO BE ASSURED OF HAVING LATEST DATA Refer to Data Management 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 of each safety and operational supplement, and all status pages attached to formal safety and operational supplements. Clear up all discrepancies before flight. ARRANGEMENT The manual is divided into eight fairly independent sections to simplify reading it straight through or using it as a reference manual. SAFETY SUPPLEMENTS Information involving safety will be promptly forwarded in a safety supplement. Urgent information is published in interim safety supplements and transmitted by defense message system (DMS). Formal supplements are mailed. The supplement title block and status page (published with formal supplements only) should be checked to determine the supplement s effect on the manual and other outstanding supplements. OPERATIONAL SUPPLEMENTS Information involving changes to operating procedures will be forwarded by operational supplements. The procedure for handling operational supplements is the same as for safety supplements. CHECKLISTS The flight manual contains itemized procedures with necessary amplifications. The checklist contains itemized procedures without the amplification. Primary line items in the flight manual and checklist are identical. If a formal safety or operational supplement affects the checklist, the affected checklist page will be attached to the supplement. The checklist page should be cut out and inserted in case the supplement is rescinded and the page is needed. ii

5 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.

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7 instrument, fire detection system (FIRE 1 only), IRU, and VHF radio (tuning provided by the standby VHF control head). 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 ECS/pressurization UHF communications/navigation and GPS Interior and exterior lighting, except backup flight instrument 1. Descent below 10,000 ft MSL - Initiate (as required) OBOGS will be inoperative once the main battery is depleted or with battery failure. Cockpit will depressurize when power to the battery bus is lost. IF THE BATTERY AND GENERATOR FAIL, ACCOM- PLISH THE FOLLOWING: 2. AUX BAT switch - ON Backup flight instrument and VHF tuning (standby VHF control head) will be powered for approximately 30 minutes by the auxiliary battery. Plan to extend the landing gear using the emergency extension system. Emergency flaps will not be functional if the main battery has failed. With normal flap extension and a loss of power to the battery bus, flaps will retract. Landing gear and flap position indicators will not be powered. The taxi and landing lights will not be functional. 3. Land as soon as possible AIR FORCE TO 1T-6B-1 NAVY NAVAIR A1-T6BAA-NFM-100 AVIONICS FAILURES During all electronic display failures, the pilot should confirm indications in both cockpits (if occupied), reference alternate data sources or the backup instruments as applicable, and check applicable circuit breakers. In the following procedures, the term reset is used to describe the action of resetting a circuit breaker that is already open. The pilot should assess the severity of the emergency and equipment lost prior to resetting or opening 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 and MFD displays in both cockpits. Loss of a single IAC may not cause an IAC1 FAIL/IAC2 FAIL message to be displayed, but may cause loss of MFD displays in one or both cockpits, erratic MFD displays, or IAC synchronization errors. The HUD and UFCP may, or may not be operating properly. IAC data crosstalk malfunction can result in a loss of synchronization between cockpits. Loss of this synchronization may result in incorrect function of the REPEAT mode. This may occur without alerting an IAC failure. Loss of synchronization or erratic indications between shared information in each cockpit is indicative of pending or possible cross talk malfunction. Synchronization errors may present as heading, altitude and speed bug is matched settings between cockpits or altimeter synchronization errors with an associated QNH DISAGREE FMS message. Do not select REPEAT in cockpit with working MFD s. This may result in loss of all MFD information in both cockpits. If synchronization errors or erratic indications are detected on ground, takeoff is not recommended. If synchronization errors are detected without a loss of MFD information, do not select REPEAT on UFCP in either cockpit. 3-27

8 AIR FORCE TO 1T-6B-1 NAVY NAVAIR A1-T6BAA-NFM Backup flight instrument - Reference as required 2. 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: Front cockpit failures/erratic displays indicate IAC1 failure, rear cockpit failures/erratic displays indicate IAC2 failure. 4. Failed IAC circuit breaker(s) (left and right front console) - Pull, reset after 5 seconds If IAC/MFD failures, erratic displays, or IAC synchronization errors persists: 5. Land as soon as practical <6>IAC XTALK Failure 1. <6>MFD/UFP REPEAT/NORM switch - NORM 2. <6>Land as soon as practical <6>An amber IAC XTALK message may result in loss of repeat switch functionality. RPT ERROR will be posted if MFD/UFP REPEAT/NORM switch is in REPEAT position. Baro Set function, heading, altitude and airspeed bug settings, minimums on/off selection, radio altitude set height, mag/true compass setting, bingo fuel setting, clock setting and G reset feature will operate independently in each cockpit. <6>With IAC XTALK message present, Baro Set function on the UFCP will operate independently in each cockpit. Confirm PFD altimeter settings in each cockpit. IRS Failure (Loss of Attitude or Heading Display on HUD and MFD) 1. Backup flight instrument - Reference as required 2. IRS circuit breaker (left and right front console) - Check, reset if open 3. Place aircraft in straight and level unaccelerated flight and monitor alignment status 4. Land as soon as practical MFD Failure (Loss of MFD Display in Front or Rear Cockpit) Failure of a single MFD will result in PFD and EICAS display only and loss of ability to manipulate the display to the FMS MENU. 1. NORM/REPEAT switch in failed cockpit - REPEAT 2. MFD circuit breaker (left MFD right console, right and center MFD left console) - Check, reset if open 3. Backup flight instrument - Reference as required UFCP Failure (Blank UFCP Entry Windows, Data Entry Knob or System Button Non Functioning) With the UFCP inoperative, the functions not available to the pilot in the cockpit with the failed UFCP are: FMS execute, system Mag/ True heading toggle, system GS/CAS/TAS HUD speed toggle, and radio tuning with UFCP. 1. UFCP circuit breaker (left front console or left rear console) - Check, reset if open 2. Land as soon as practical Backup Flight Instrument Display Failure 1. Place aircraft in straight and level unaccelerated flight 2. STBY INST circuit breaker (left front/left rear console) - Check, reset if open 3. AFT STBY circuit breaker (left front console) - Check, reset if open If display does not return: 4. Land as soon as practical Engine Data Manager Fail (EDM FAIL Warning or EDM A INOP or EDM B INOP Advisory Resulting in Total or Partial Loss of Engine Data Manager Information) If an EDM FAIL occurs prior to start and is accompanied by red X s in the IOAT and ITT counters, refer to High IOAT at Start >80 C. 1. EDM circuit breakers (left and right front console) - Check, reset if open If engine instrument displays on EICAS page do not return: 2. Land as soon as practical 3-28