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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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If the nose is yawed to the left, the nose tends to pitch up. Barrel rolls or over-the-top maneuvers while on the wing.

AFMAN when passing even thousands of feet i. The reduction gearbox RGB is driven by the power turbine, which is driven by hot gases from the gas generator section. Preflight testing of the auxiliary battery power level is accomplished: If a start attempt is aborted after fuel has been introduced: If the generator control switch GEN has been set to on in either cockpit, and the occupant of the other cockpit selects ON: AFI execute rapid, shallow wing rock.

AFMAN Maintaining flight path deconfliction and proper position as directed by 1 If in other than fingertip ari route when radio failure occurs and a planned rejoin will not shortly follow, the NORDO aircraft should: AFI engine malfunction.

wfi

Landing distance charts assume what type of braking? During flap deployment or retraction, the flap position pointer moves: With operations group commander approval, aircrews may conduct operations at non-towered, public-use airfields, with the which of the following restrictions: 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: Study questions 1a Updated: Normal flap operation and indication are unavailable anytime: AFMAN on or slightly above Typical reactions from a clockwise-turning propeller as viewed from the pilot’s seat include: Actual or simulated instrument approaches and landings as lead or wing.

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Study questions 1a

Set attitude nose high on EADI. Check VSI and altimeter to verify climb and raise gear and flaps. The formation signal for attention in the afo is to: Once takeoff trim is set, the TAD will make no further trim inputs until: Components of the oil system include the following system s: Pressing and holding the trim interrupt button: Operations Group Commander approval is required to fly formation at night.

Initiate recovery from a power-on stall when: The control and performance concept procedural steps are in order: You are required to refer to the checklist to complete each individual item to ensure all items are completed.

The AOA gage is marked with a white diamond at 8.

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The fuel auto balance zfi provided by the EDM detects fuel imbalances: Typical reactions from a clockwise-turning propeller as viewed from the pilot’s seat include: When leading fingertip formation, limit maneuvering to knots minimum airspeed, approximately 90 degrees of bank, and 2 to 3 Gs.

If in other than fingertip or route when radio failure occurs and a planned rejoin will not shortly follow, the NORDO aircraft should: If the fuel imbalance exceeds 30 pounds for more than 2 minutes: Flap position is controlled by a three-position flap selector marked: Once extended, the speed brake remains extended until: The AOA gage is marked with a white triangle at 4.

Because the circling approach is generally flown at a lower altitude than the overhead pattern, proper displacement will appear to be much wider than normal.

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. 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 aif to high key.

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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. The PT6A engine is a reverse-flow design, with airflow entering the engine: The AOA gage is marked with a green arc at 10 to 11 units, which indicates: Adverse yaw is the tendency of the aircraft to yaw away from direction of aileron input. To possibly discriminate between a fire or overheat condition: A good visual reference for proper downwind spacing at feet AGL is: During normal operation, the hydraulic system operates the: AFMAN Because the circling approach is generally flown at a lower altitude than the overhead pattern, proper displacement will appear to be much wider than normal.

There is no mechanical connection between the gas generator section and the RGB.

Flashcards – Study questions 1a

Practice lost wingman procedures while on the wing. If the nose is pitched down, a left yaw tends to develop.

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. Close trail as wingman. AFI T-6 Vol 3. If a solo student experiences an engine failure, the student may attempt a forced landing with the following restriction: If the nose is yawed to the right, the nose tends 111-205 pitch down.