11-251

Question 1

A3V105. Minimum taxi distance from any obstacle is: (AFMAN 11-251)
A. 10 feet.
B. 25 feet without a wingwalker.
C. Wingtip clearance.
 D. A and B above.

Answer 1

D. A and B above.

Question 2

A3V106. During the instrument cockpit check, ensure the EHSI is within: (AFMAN 11-251)
A. 8 degrees of the magnetic compass.
B. 5 degrees of a known heading.
C. A and B above. 
D. A and B above.

Answer 2

D. A and B above.

Question 3

A3V108. During the NAVAID ground checkpoint check, the allowable bearing pointer and CDI error is: (AFMAN 11-251)
A. Plus or minus 5 degrees from the depicted course to the station.
B. Plus or minus 4 degrees from the depicted course to the station.
C. Plus or minus 8 degrees from the depicted course to the station.

Answer 3

B. Plus or minus 4 degrees from the depicted course to the station.

Question 4

A3V109. Rolling takeoffs increase takeoff roll approximately: (AFMAN 11-251)
A. 500 feet.
B. 0-150 feet. 
C. 150-300 feet.
D. 300-500 feet.

Answer 4

C. 150-300 feet.

Question 5

A3V110. You may combine the climb check with the level-off check when your cruise altitude is at or below: (AFMAN 11-251)
A. 10,000 feet.
B. 13,000 feet. 
C. FL 180.
D. You cannot combine the checks.

Answer 5

C. FL 180.

Question 6

A3V111. Unless the controller directs otherwise, initiate the break between ___ and ___ down the runway. (AFMAN 11-251)
A. The approach end, 6,000 feet. B. The approach end, 3,000 feet.
C. The desired touchdown point, halfway.
D. 1,500 feet, 3,000 feet.

Answer 6

B. The approach end, 3,000 feet.

Question 7

A3V112. Begin the closed pattern pull-up with a minimum of ___ and maintain a minimum of ___
until wings-level downwind. (AFMAN 11-251)
A. 200 KCAS, final turn airspeed.
B. 220 KCAS, 200 KCAS.
C. 240 KCAS, 200 KCAS.
D. 220 KCAS, final turn airspeed.

Answer 7

C. 240 KCAS, 200 KCAS

Question 8

A3V113. When performing an actual or simulated single-engine full-stop landing with 60% flaps,
the landing roll will be approximately: (AFMAN 11-251)
A. Twice the full-flap landing distance.
B. 500 feet longer than the full-flap landing distance.
C. Negligible compared to the full-flap landing distance.
D. 60% flap full-stop landings are not allowed

Answer 8

B. 500 feet longer than the full-flap landing distance.

Question 9

A3V114. During simulated single-engine patterns from a straight-in approach or single-engine
go-arounds, set the simulated failed engine to not less than ___ rpm. (AFMAN 11-251)
A. 50%.
B. 60%.
C. 70%.
D. Idle.
Reference: (

Answer 9

B. 60%.

Question 10

A3V115. During an actual stall indication in the traffic pattern, primary emphasis should be on
maintaining the prescribed pattern ground track. (AFMAN 11-251)
True
False

Answer 10

False

Question 11

A3V116. For traffic pattern stalls and approach-to-stall training, set the power at: (AFMAN 11-251)
A. Idle RPM minimum.
B. 60% RPM minimum. 
C. 80% RPM minimum.
D. 90% RPM minimum.

Answer 11

C. 80%

Question 12

A3V124. Maintain \_\_\_\_\_ and \_\_\_ flaps throughout a circling maneuver until aligned with the
landing runway. (AFMAN 11-251)
A. Final approach speed, 60%.
B. Final turn speed, full. 
C. Final turn speed, 60%.
D. Either B or C above.

Answer 12

C. Final turn speed, 60%.

Question 13

A3V126. For a restricted military power climb, unless accomplishing a formation rejoin, begin a smooth power reduction out of MAX between \_\_\_\_\_ KCAS and terminate afterburner by \_\_\_\_\_ KCAS. (AFMAN 11-251) 
A. 220-280, 300.
B. 240-280, 300.
C. 200-240, 300.
D. 240-300, 350.

Answer 13

A. 220-280, 300.

Question 14

A3V127. The standard VASI and PAPI have a ____ degree glideslope and a glidepath intercept point (aimpoint) approximately ___ feet beyond the runway threshold. (AFMAN 11-251)
A. 3 - 3.5, 450 feet short of the runway threshold.
B. 2.5 - 3, 750.
C. 3, 1,500.
D. 2.5, 500.

Answer 14

B. 2.5 - 3, 750

Question 15

A3V128. On normal inside downwind, slow to no less than \_\_\_\_. (AFMAN 11-251)
A. 240 KCAS.
B. 200 KCAS. 
C. final turn airspeed.
D. final approach airspeed.

Answer 15

C. final turn airspeed.

Question 16

A3V129. Prior to beginning the final turn, ensure the landing gear is down and locked and the
flaps have traveled a sufficient amount to ensure no asymmetry exists. (AFMAN 11-251)
True
False

Answer 16

True

Question 17

A3V130. With gusty winds: (AFMAN 11-251)
A. Increase the final turn, final approach, and landing speed by 1/2 the gust factor.
B. Increase the final approach and landing speed by 1/2 the gust factor.
C. Increase the final approach and landing speed by the gust factor.
D. Increase the final turn, final approach, and landing speed by the gust factor.

Answer 17

B. Increase the final approach and landing speed by 1/2 the gust factor.

Question 18

A3V131. For a normal aerobrake, increase pitch attitude to approximately \_\_\_ degrees. (AFMAN 11-251)
A. 5.
B. 7 - 7.5. 
C. 10 - 12.
D. 5-7.

Answer 18

C. 10 - 12.

Question 19

A3V132. When the crosswind component exceeds 15 knots: (AFMAN 11-251)
A. Plan to touch down on the upwind side of the runway.
B. Maintain the landing attitude and do not aerobrake.
C. Do not perform touch-and-go patterns.
D. Both A and B above.

Answer 19

D. Both A and B above.

Question 20

A3V133. After practicing an alternate landing gear extension, reset the landing gear system by
moving the gear handle: (AFMAN 11-251)
A. Down.
B. Down, then up.
C. Down, then up, and then back to the down position.
D. Any of the above.

Answer 20

C. Down, then up, and then back to the down position.

Question 21

A3V134. When accomplishing a full aft stick stall, discontinue the exercise and recover the
aircraft when: (AFMAN 11-251)
A. Bank angle exceeds 90 degrees.
B. Bank angle stabilizes over 60 degrees.
C. Definite increase in buffet intensity is attained.
D. Either A or B above.

Answer 21

D. Either A or B above.

Question 22

A3V135. Fly slow flight at an airspeed \_\_ knots below computed final approach speed
(approximately \_\_ AOA). (AFMAN 11-251)
A. 0, 0.6. 
B. 10, 0.7.
C. 10, 0.6.
D. 0, 0.7.

Answer 22

B. 10, 0.7.