Instructor Under Training Test

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13. The minimum recovery altitude for practice ditches shall be:

A. 1500 ft AGL

B. 1500 ft MSL

C. 4000 ft AGL.

D. 4000 ft MSL.

14. Simulating a power loss after Vr shall be induced by:

A. Utilizing the engine bleed system only.

B. Pulling power lever back by IP.

C. Calling out power loss by IFE.

D. Pulling TD valve amplifier c/b at Mon AC.

15. Simulated 2-Engine approaches and landings shall be conducted during day VMC only.

A. True

B. False

16. The minimum ditching speed with a tactical crew embarked is ____.

A. Land flap ditch speed +5 kts.

B. 125 kts.

C. 1.35 Vs.

D. 140 kts.

17. No flap and 3 engine approach training is permissible during daylight hours, providing the ceiling is at least ______ ft and visibility at least _____ miles.

A. 1000 / 3

B. 1000 / 5

C. 1500 / 3

D. 1500 / 5

18. The IP may vacate the left or right seat only when:

A. The aircraft is at or above 1000 ft AGL.

B. The aircraft is on the ground with parking brakes set.

C. When the IFE is in the flight station with his head set on.

D. All of the above.

19. If aircraft buffet occurs prior to the calculated stall speed:

A. Execute recovery procedures. Confirm stall speed calculation.

B. If calculated stall speed was correct and the maneuver was flown properly, consider aborting the event.

C. Recover the aircraft and reattempt maneuver.

D. Both A and B are correct.

20. When performing an in-flight propeller system demonstration, you should:

A. Set normal rated power on the respective engine to prevent a de-couple.

B. Select the respective sync servo switch to off.

C. Select the NTS/FX valve check switch to the FX valve check position.

D. This demonstration shall be conducted in the simulator only.

21. The minimum altitude for control boost-out air-work shall be:

A. 4000 ft MSL.

B. 10,000 ft MSL.

C. 4000 ft AGL.

D. 10,000 ft AGL.

22. Use of high AOB at low altitude must take into account all of the following except :

A. Pilot experience

B. Fatigue

C. Time of Day

D. Altitude

E. All of the above must be taken into account.

23. If during an EFAR procedure the TP attempts to rotate early, stop the rotation if possible but once the nosewheel is airborne it is best the IP takes control and:

A. Continue with a 4 engine abort.

B. Lower the nosewheel to the deck until Vro is reached, then continue the take-off.

C. Continue with the EFAR procedure as a demo for the TP.

D. Continue the take-off, utilizing all 4 power levers.

24. If the VFR pattern is entered immediately after the first take-off of the day, the climb checklist shall be completed to ensure the autofeather system is deenergized.

A. True

B. False

25. When setting up a loss of Main DC, the IP/IFE will ensure:

A. A documentation MAF is written for SDRS tracking purposes.

B. Bus B is not failed in-flight with the TR 1 circuit breaker out.

C. EDCs are manually dumped to prevent overheated air cycle cooling units.

D. All of the above.

26. On stop and go landings:

A. The aircraft will be brought to a complete stop with a minimum of 6000 ft runway remaining.

B. A minimum of 2500 SHP should be used for take-off.

C. The abbreviated after landing and the take-off checklist are required before commencing the take-off.

D. All of the above.

27. During a propeller fails to feather the aft observer notices oil to creep over the wing, you should:

A. Continue the

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