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Air Force Instruction – Download as PDF File .pdf), Text File .txt) or read online. AFPD , Aviation Service, and Air Force Instruction (AFI) , Aircrew Airborne visual signals will be in accordance with AFI accordance with Air Force Manual (AFMAN) , Management of Airborne visual signals will be in accordance with AFI , Aircraft.

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While flying practice instrument approaches in VMC, if the pilot acknowledges reaching PWC minimums and states intentions to crewmembers, he may continue to published minimums.

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AFI engine malfunction. The AOA gage is marked with a white diamond at 8. The PT6A engine is a reverse-flow design, with airflow entering the engine: What are the RCRs for dry, wet, and icy runway conditions respectively?

Once takeoff trim is set, the TAD will make no further trim inputs until: You are required to refer to the checklist to complete each individual item to ensure all items are completed. During flap deployment or retraction, the flap position pointer moves: During an instrument trail departure, until join up or level off, each aircraft or element will call: AFI T-6 Vol 3 10 With operations group commander approval, aircrews may conduct operations at non-towered, public-use airfields, with the which of the following restrictions: To possibly discriminate between a fire or overheat condition: Ari when passing even thousands of feet i.

Set attitude nose high on EADI.

AFMAN fuel filler cap, wingtip If excess altitude is too great to dissipate with a slip, S-turn, or by lowering the gear early, one technique is to make degree turns prior to high key. With operations group commander approval, aircrews may conduct operations at non-towered, public-use airfields, with the which of the following restrictions: AOA being higher af the downward moving propeller blade than on the upward moving propeller blade.

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If the nose is yawed to the right, the nose tends to pitch down. Flap position is controlled by a three-position flap selector marked: Landing distance charts assume what type of braking? Normal cockpit indications when the emergency extension system is used are: The fuel auto balance system provided by the EDM detects fuel imbalances: If there is a generator malfunction in flight: If the generator control switch GEN has been set to on in either cockpit, and the occupant of the other cockpit selects ON: Adverse yaw is the tendency of the aircraft to yaw away from direction of aileron input.

Components of the oil system include the following system s: Actual or simulated instrument approaches and landings as lead or wing. AFI T-6 Vol 3.

The generator provides 28 volts DC, which is sufficient to power: Preflight testing of the auxiliary battery power level is ari Operations Group Commander approval is required to fly formation at night.

Smoothly advance the PCL to max.

During an ELP, fly towards base key maintaining knots. If in other than fingertip or route when radio failure occurs and a planned rejoin will not shortly follow, the NORDO aircraft should: AFMAN Maintaining flight path deconfliction and proper position as directed by 1 If in other than fingertip or route when radio failure occurs and a planned rejoin will not shortly follow, the NORDO aircraft should: Once extended, the speed brake remains extended until: AFMAN on or slightly above Typical reactions from a clockwise-turning propeller as viewed from the pilot’s seat include: AFI T-6 Vol 3 15 When leading fingertip formation, limit maneuvering to knots minimum airspeed, approximately 90 degrees of bank, and 2 to 3 Gs.

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Study questions 1a

If a start attempt is aborted after fuel has been introduced: The AOA gage is marked with a white triangle at 4. Initiate recovery from a power-on stall when: A good visual reference for proper downwind spacing at feet AGL is: If the fuel imbalance exceeds 30 pounds for more than 2 minutes: Study questions 1a Updated: If excess altitude is too great to dissipate with a slip, S-turn, or by lowering the gear early, one technique is to make degree turns prior to high key.

The AOA gage is marked with a green arc at 10 to 11 units, which indicates: The reduction gearbox RGB is driven by the power turbine, which is driven by hot gases from the gas generator section. Pressing and holding the trim interrupt button: During normal operation, the hydraulic system operates the: Normal flap qfi and indication are unavailable anytime: