Term
1. When the local altimeter is at or above 29.92 the Hi Blocks in the Pensacola South MOA are from ________ ft MSL. (IFG)
A. 16,500-22,500
B. 17,000-23,000
C. 18,000-23,000
D. None of the above
Proctor Reference: T-1A IFG Pg: 22 |
|
Definition
|
|
Term
2. Additional Training (AT) Sorties may be graded as: (AETCI 36-2205)
A. U (Unsat)
B. NG (No Grade)
C. Good
D. Both A. and B.
Proctor Reference: AETCI 36-2205v5 Par: 5.3 / C-V4P-A Par: 6 |
|
Definition
|
|
Term
3. Aircrews entering on VRs 1021 through 1024 at Point A will contact _______ on VHF with position from airfield and VR route.
(AFI 11-202V3_AETCSUP_12FTWSUP)
A. Mobile Approach
B. KGPT (Gulfport) Tower
C. KMOB (Mobile Regional) Tower
D. KPQL (Trent Lott) Tower
Proctor Reference: AFI 11-202V3_AETCSUP_12FTWSUP Par: 2.1.17.7 |
|
Definition
| D. KPQL (Trent Lott) Tower |
|
|
Term
4. Who maintains overall authority and responsibility of CAP administration? (AETCI 36-2205)
A. squadron operations officer
B. SQ/CC
C. flight commander
D. flight supervisor
Proctor Reference: AETCI 36-2205 v5 Par: 3.1.3 |
|
Definition
|
|
Term
5. The flight commander, operations officer, squadron commander or designated supervisor may
approve a student's removal from CAP. (AETCI 36-2205)
A. True
B. False
Proctor Reference: AETCI 36-2205 v5 Par: 3.1.3 |
|
Definition
|
|
Term
6. Entry into the Pensacola South MOA will be: (IFG)
A. Via vectors to intercept lines A,B,C, 1, or 2 around active blocks at ATC assigned altitude
B. Via direct points A,B,C,D,E,F,H, or I to intercept transition lines A,B,C,1, or 2 around active
blocks at ATC assigned altitude
C. Via radar vectors and/or assigned altitude through inactive blocks
D. Any of the above
Proctor Reference: T-1A IFG Pg. 21 |
|
Definition
|
|
Term
7. CAP’s objective is to focus supervisory attention on a student’s progress in training, specific
deficiencies, and potential to complete the program. (AETCI 36-2205)
A. True
B. False
Proctor Reference: AETCI 36-2205 v5 Par: 3.1.1 |
|
Definition
|
|
Term
8. If unable to make the low-level entry window a new entry time must be coordinated. (AFI 11-202V3_AETCSUP_12FTWSUP)
A. True
B. False
Proctor Reference: AFI 11-202V3_AETCSUP_12FTWSUP Par: 2.1.17.
9. |
|
Definition
|
|
Term
9. On VRs 1021 through 1024, after making the required “clear to north” call on Trent Lott Tower frequency, change to__________. (AFI 11-202V3_AETCSUP_12FTWSUP)
A. Mobile Approach VHF frequency
B. Houston Center VHF frequency
C. Low-Level VHF common frequency
D. Any VHF frequency
Proctor Reference: AFI 11-202V3_AETCSUP_12FTWSUP Par: 2.1.17.7 |
|
Definition
| C. Low-Level VHF common frequency |
|
|
Term
10. 479 FTG assigned T-6 and T-1s recovering via Course Rules recover at ______ till the break. (AFI 11-202V3_AETCSUP_12FTWSUP)
A. 200 knots
B. 220 knots
C. 250 knots
D. 300 knots
Proctor Reference: AFI 11-202V3_AETCSUP_12FTWSUP Par: 5.9.7 |
|
Definition
|
|
Term
11. When in the Pensacola South MOA if the local altimeter is below 29.92, _______ ft MSL is the
highest useable working altitude (IFG)
A. 23,000
B. 22,000
C. 18,000
D. 17,000
Proctor Reference: T-1A IFG Pg. 22 |
|
Definition
|
|
Term
12. When flying on VRs 1020 through 1024 and making advisory calls in the MOA, remain on the
MOA UHF frequency until clear of the MOA then return to 255.4 MHz. (AFI 11-202V3_AETCSUP_12FTWSUP)
A. True
B. False
Proctor Reference: AFI 11-202V3_AETCSUP_12FTWSUP Par: 2.1.17.6.3 |
|
Definition
|
|
Term
13. The Lo Blocks in the Pensacola South MOA are from _________ ft MSL. (IFG)
A. 10,500-16,500
B. 11,000-17,000
C. 10,500-17,999
D. None of the above
Proctor Reference: T-1A IFG Pg. 22 |
|
Definition
|
|
Term
14. The black or blue stocking cap (i.e. “cap, knit, watch”) may NOT be worn while on the aircraft
parking ramp during external pre-/post-flight inspections. (AFI 11-202V3_AETCSUP_12FTWSUP)
A. True
B. False
Proctor Reference: AFI 11-202V3_AETCSUP_12FTWSUP Par: 6.2.10 |
|
Definition
|
|
Term
15. Units will enter students who fail to progress in the normal syllabus flow into the CR process. (AETCI 36-2205)
A. True
B. False
Proctor Reference: AETCI 36-2205v5 Par: 3.3.2 |
|
Definition
|
|
Term
16. Generally, CAP is intended as a long-term program. A student requiring an extended period of
increased supervision should be considered for additional training. (AETCI 36-2205)
A. True
B. False
Proctor Reference: AETCI 36-2205v5 Par: 3.1.5 |
|
Definition
|
|
Term
17. When a Lightning Warning exists for lightning within 10 NM of the airfield, local flying may
continue per SOF. (Ops Sup for 479 FTG) discretion. (AFI 11-202V3_AETCSUP_12FTWSUP)
A. True
B. False
Proctor Reference: AFI 11-202V3_AETCSUP_12FTWSUP Par: 5.11.3.4 |
|
Definition
|
|
Term
18. TRAWING 6 owned low level routes have a +/- ______ minute entry window. (AFI 11-202V3_AETCSUP_12FTWSUP)
A. 5
B. 4
C. 3
D. 2
Proctor Reference: AFI 11-202V3_AETCSUP_12FTWSUP Par: 2.1.17.3.1 |
|
Definition
|
|
Term
19. When in the Pensacola South MOA Contact Approach on 120.05/372.0 with intentions prior to
leaving the working area. (IFG)
A. True
B. False
Proctor Reference: T-1A IFG Pg. 21 |
|
Definition
|
|
Term
20. The standard IFR departure from Runway 07L or 07R includes a right hand turn at _____ DME to a heading of ______. (IFG)
A. 1, 150
B. 3, 220
C. 1, 160
D. 2, 150
Proctor Reference: T-1A IFG Pg. 16 |
|
Definition
|
|
Term
21. NASP ground control is authorized the use of a single clearance for multiple runway crossings
when taxi distance between runway centerline distances is less than 1000 feet. (AFI 11-202V3_AETCSUP_12FTWSUP)
A. True
B. False
Proctor Reference: AFI 11-202V3_AETCSUP_12FTWSUP Par: 5.11.3.2 |
|
Definition
|
|
Term
22. What is the minimum weather required for Course Rules at KNPA? (IFG)
A. 1500/3
B. 2000/5
C. 2500/3
D. 1500/5
Proctor Reference: T-1A IFG Pg. 25 |
|
Definition
|
|
Term
23. Aircrew will ensure they have ________ minute(s) separation behind preceding aircraft on
TRAWING 6 owned low-level routes. (AFI 11-202V3_AETCSUP_12FTWSUP)
A. 1
B. 2
C. 3
D. 4
Proctor Reference: AFI 11-202V3_AETCSUP_12FTWSUP Par: 2.1.17.2 |
|
Definition
|
|
Term
24. Pattern altitude at NASP is ____ feet MSL. (AFI 11-202V3_AETCSUP_12FTWSUP)
A. 1500
B. 1000
C. 800
D. 700
Proctor Reference: AFI 11-202V3_AETCSUP_12FTWSUP Par: 5.11.8.2.1 |
|
Definition
|
|
Term
25. Normally, students will not perform duties in excess of a 12-hour duty day. (AETCI 36-2205)
A. True
B. False
Proctor Reference: AETCI 36-2205v1 Par: 10 / C-V4P-A Par: 4.a |
|
Definition
|
|
Term
26. If Hot Brake conditions exist or are suspected taxi to the designated Hot Brake Area
(Landing/Aborting Runway Departure-End EOR) and park facing into the wind. (IFG)
A. True
B. False
Proctor Reference: T-1A IFG Pg. 43 |
|
Definition
|
|
Term
27. During normal duty hours, when are off station crews required to call their Ops Sup? (IFG)
A. Prior to takeoff
B. After landing
C. Neither A or B
D. Both A and B
Proctor Reference: T-1A IFG Pg. 27 |
|
Definition
|
|
Term
28. An operating procedure or technique which is considered essential to emphasize is a ______? (T.O. 1T-1A-1)
A. Warning
B. Procedure
C. Caution
D. Note
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE iii |
|
Definition
|
|
Term
29. Once TCAS announces "clear of conflict," the pilot should: (T.O. 1T-1A-1)
A. return to his/her ATC clearance or as directed by ATC.
B. maintain the altitude climbed/descended to, as this will maintain safe separation.
C. choose an altitude that you, as the pilot, deem necessary and fly to it.
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 1-348 |
|
Definition
| A. return to his/her ATC clearance or as directed by ATC. |
|
|
Term
30. Failure to properly set the decision height (DH) in the radio altimeter could result in __________. (T.O. 1T-1A-1)
A. nuisance warnings from the GPWS.
B. a warning given automatically at the DH or MDA depending on what approach the navigation systems are set up for.
C. an automatic warning from the GPWS at 50 feet no matter where the DH is set.
D. a & c
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 1-359 |
|
Definition
| A. nuisance warnings from the GPWS. |
|
|
Term
31. Due to weather radar system limitations, ________. (T.O. 1T-1A-1)
A. the maximum range of 300 NM should not be used when circum-navigating adverse weather.
B. do not use the turbulence mode when maneuvering or damage to the radar stabilization system could result.
C. do not rely on the system as the only means to avoid adverse weather.
D. a & b
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 1-360 |
|
Definition
| C. do not rely on the system as the only means to avoid adverse weather. |
|
|
Term
32. The weather radar system provides radar data for up to _______ NM. (T.O. 1T-1A-1)
A. 100
B. 150
C. 300
D. 600
Proctor Reference: T.O. 1T-1A-1 Pg: 1-360 |
|
Definition
|
|
Term
33. As oxygen cylinders become chilled, the pressure is reduced. A temperature drop of 100°F will reduce pressure 20%. If the pressure begins to drop while the aircraft is in level flight or descending, __________. (T.O. 1T-1A-1)
A. do nothing, this is normal at high altitudes
B. suspect an oxygen leak
C. suspect gauge failure
D. check for a similar drop in the nitrogen pressure
Proctor Reference: T.O. 1T-1A-1 Pg: 2-27 |
|
Definition
| B. suspect an oxygen leak |
|
|
Term
34. After flushing the lavatory, __________ to prevent contents from overflowing. (T.O. 1T-1A-1)
A. leave the knife valve open
B. close the knife valve
C. ensure the lid is closed
D. none of the above
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 1-412 |
|
Definition
| A. leave the knife valve open |
|
|
Term
35. The handheld HALON 1211 extinguishers in the aircraft are more effective and less toxic than other types of fire extinguishers. Therefore, it is not necessary to ventilate the aircraft after their use. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 1-413 |
|
Definition
|
|
Term
36. Resetting a popped circuit breaker in the fuel system is allowable. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 1-35 |
|
Definition
|
|
Term
37. While using the exterior inspection checklist, specific attention should be given to detect fluid leakage. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 2-5 |
|
Definition
|
|
Term
38. The exterior door handle will stow by activation of the interior handle. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2-5 |
|
Definition
|
|
Term
39. Failure to stow the exterior door handle can result in damage to the door during flight. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2-5 |
|
Definition
|
|
Term
40. How many circuit breaker panels are in the aft compartment that are required to be checked? (T.O. 1T-1A-1)
A. 1
B. 2
C. 3
D. 4
Proctor Reference: T.O. 1T-1A-1 Pg: 2-8 |
|
Definition
|
|
Term
41. The entrance door must be closed and locked prior to starting interior inspection. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: 2-2 |
|
Definition
|
|
Term
42. With respect to the door locking pins, _____ or the door may open inflight. (T.O. 1T-1A-1)
A. all eight must be white.
B. they may be half white and half red.
C. at least every other one must be white.
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 2-10 |
|
Definition
| A. all eight must be white. |
|
|
Term
43. An improperly installed escape hatch can result in loss of cabin pressure in flight. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 2-3 |
|
Definition
|
|
Term
44. Failure to remove the escape hatch lock pin will: (T.O. 1T-1A-1)
A. make hatch inoperable from the outside.
B. make hatch inoperable from the inside.
C. delay emergency ground egress from the escape hatch.
D. All of the above.
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 2-3 |
|
Definition
|
|
Term
45. To test the AHRS battery, ____________. (T.O. 1T-1A-1)
A. hold for five seconds.
B. check the AHRS BATT TEST annunciator momentarily illuminates.
C. accomplish test from both pilot and copilot's side.
D. a & b
E. All of the above.
Proctor Reference: Proctor Reference: T.O. 1T-1A-1 Pg: 2-4 |
|
Definition
|
|
Term
46. When the cabin pressure controller is set, set the altitude to _____ feet above the highest anticipated cruise altitude or according to mission requirements. (T.O. 1T-1A-1)
A. 500
B. 1,000
C. 1,500
D. 2,000
Proctor Reference: T.O. 1T-1A-1 Pg: 2-28 |
|
Definition
|
|
Term
47. Turning the manual pressure control knob past its normal range __________. (T.O. 1T-1A-1)
A. could damage the threads or needle valve seat
B. will have no affect
C. will turn off the bleed air
D. will turn on the CABIN PRESS LO annunciator
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2-10 |
|
Definition
| A. could damage the threads or needle valve seat |
|
|
Term
48. Landing with brakes applied could result in: (T.O. 1T-1A-1)
A. Blown tires
B. Potential runway departure
C. Damage to the aircraft
D. All of the above
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 1-93 |
|
Definition
|
|
Term
49. When testing the indicator lights, the following lights do not illuminate: (T.O. 1T-1A-1)
A. red landing gear unlocked indicator
B. starter DISENGAGE button
C. ENG START buttons
D. a & b
E. All of the above.
Proctor Reference: T.O. 1T-1A-1 Pg: 2-11 # 11 |
|
Definition
|
|
Term
50. After selecting the left tank during the fuel crossfeed check, these lights will illuminate: (T.O. 1T-1A-1)
A. Left boost pump light, left jet pump light, XFEED in-transit operation light
B. Right boost pump light, left jet pump light, XFEED in-transit operation light
C. Left boost pump light, right jet pump light, XFEED in-transit operation light
D. Right boost pump light, right jet pump light, XFEED in-transit operation light
Proctor Reference: T.O. 1T-1A-1 Pg: 1-416 |
|
Definition
| C. Left boost pump light, right jet pump light, XFEED in-transit operation light |
|
|
Term
51. During flight control checks, after the pilot checks the controls, the copilot must also physically check the flight controls. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: 2-14 #19 |
|
Definition
|
|
Term
52. If starting engines with battery power only, do not start the second engine until the first engine's ammeter reads below _____ amps.
(T.O. 1T-1A-1).
A. 150
B. 280
C. 400
D. Do not delay starting the second engine.
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2-15 |
|
Definition
|
|
Term
53. For generator assisted starts on the second engine, the operating engine must be at IDLE. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2-15 |
|
Definition
|
|
Term
54. The stabilizer anti-ice fail annunciator will illuminate in _____ seconds once the anti-ice switch is set to the test position. (T.O. 1T-1A-1)
A. 2
B. 3
C. 5
D. 10
Proctor Reference: T.O. 1T-1A-1 Pg: 2-16 - 5 (b) |
|
Definition
|
|
Term
55. Do not use the horizontal stabilizer anti-ice on the ground because a squat switch failure could cause damage to the ___________.
(T.O. 1T-1A-1)
A. battery
B. horizontal stabilizer
C. generators
D. All of the above
E. None of the above
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2-18 |
|
Definition
|
|
Term
|
Definition
|
|
Term
57. An external power cart is required for engine start at ambient temperatures below_____. (T.O. 1T-1A-1)
A. 5F
B. 8F
C. 5
D. 10F
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2-14 |
|
Definition
|
|
Term
58. The throttles should be set at _____ to ensure that the anti-ice valve is open when checking wing and engine anti-ice. (T.O. 1T-1A-1)
A. 65% N1
B. 65% N2
C. 70% N1
D. 70% N2
Proctor Reference: T.O. 1T-1A-1 Pg: 1-150 |
|
Definition
|
|
Term
59. When taxiing for takeoff through ice and snow, leave the flaps at _______ until approaching the runway to avoid accumulations of ice being cast off from the tires. (T.O. 1T-1A-1)
A. 0°
B. 10°
C. 30°
D. a or b
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 7-9 |
|
Definition
|
|
Term
60. An operating procedure or technique which could result in damage to equipment if not carefully followed is a _____? (T.O. 1T-1A-1)
A. Warning
B. Procedure
C. Caution
D. Note
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION iii |
|
Definition
|
|
Term
61. During a wake turbulence takeoff, allow a minimum of _____ minutes behind a large type aircraft. With an effective crosswind over _____ knots, this interval may be reduced. (T.O. 1T-1A-1)
A. 2, 5
B. 4, 5
C. 3, 10
D. 4, 10
Proctor Reference: T.O. 1T-1A-1 Pg: 2-22 |
|
Definition
|
|
Term
62. For a wake turbulence takeoff: (T.O. 1T-1A-1)
A. allow a minimum of four minutes behind jumbo (heavy) jet aircraft
B. a crosswind over 5 knots may reduce the required interval
C. remain below the flight path of the preceding aircraft
D. the pilot is authorized to reduce required intervals
Proctor Reference: T.O. 1T-1A-1 Pg: 2-22 |
|
Definition
| B. a crosswind over 5 knots may reduce the required interval |
|
|
Term
63. During takeoff and landing, to avoid obscuring visibility, the visors must be in the stowed position. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 1-12 |
|
Definition
|
|
Term
64. For extended high altitude cruise, the windshield heat should be set at _____. (T.O. 1T-1A-1)
A. LOW
B. OFF
C. HIGH
D. a or b
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 2-26 |
|
Definition
|
|
Term
65. Ignition switches should be on __________. (T.O. 1T-1A-1)
A. whenever engine anti-ice is on
B. when flight is through turbulence and/or visible precipitation
C. for all takeoffs, approaches, and landings
D. b or c
Proctor Reference: T.O. 1T-1A-1 Pg: 5-12 |
|
Definition
|
|
Term
66. With the pilot valves inoperative, which of the following is true concerning refueling? (T.O. 1T-1A-1)
A. Use single point refueling
B. Do not attempt to fly the aircraft
C. Should not be refueled
D. Either method may be used
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 1-45 |
|
Definition
| B. Do not attempt to fly the aircraft |
|
|
Term
67. Starting a descent at FL 200, maximum range descent is flown at _____, enroute descent is flown at _____, and rapid descent is flown at _____. (T.O. 1T-1A-1)
A. 250, 250, 250
B. 250, 310, 330
C. 230, 250, 330
D. 200, 250, 330
Proctor Reference: T.O. 1T-1A-1 Pg: 2-27 |
|
Definition
|
|
Term
68. Maximum range descent is _________. (T.O. 1T-1A-1)
A. idle, clean, 0.70 IMN above 35,900 ft, 230 KIAS below 35,900 ft.
B. idle, speed brakes, 0.70 above 32,300 ft, 250 KIAS below 32,300 ft.
C. idle, 180 KIAS, speed brakes, gear, 3 degrees nose low
D. idle, speed brakes, 0.78 IMN above 24,800 ft, 330 below 24,800 ft.
Proctor Reference: T.O. 1T-1A-1 Pg: 2-27 |
|
Definition
| A. idle, clean, 0.70 IMN above 35,900 ft, 230 KIAS below 35,900 ft. |
|
|
Term
69. During preflight inspection, a drop of fuel hanging on the sniffle valve ______. (T.O. 1T-1A-1)
A. is acceptable
B. is not acceptable
C. should be written up in the 781
D. a & c
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 1-45 |
|
Definition
|
|
Term
70. Use of stabilizer trim for round out in the flare could induce a strong pitch up tendency that would be difficult to control in the event that a go-around is attempted. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 2-30 |
|
Definition
|
|
Term
71. In the event of a suspected hard landing: (T.O. 1T-1A-1)
A. make an AFTO Form 781 write up with your gross weight, airspeed, and RA/VSI.
B. gear should remain down and the mission terminated.
C. if in the pattern, keep gear down and do touch and goes until bingo.
D. a & b
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2-31 |
|
Definition
|
|
Term
72. Touchdown will normally be made at approximately Vapp minus ____ KIAS. (T.O. 1T-1A-1)
A. 10
B. 8
C. 6
D. not specified.
Proctor Reference: T.O. 1T-1A-1 Pg: 2-30 |
|
Definition
|
|
Term
73. The wipers are functional at flight speeds up to _______ knots indicated airspeed. Higher speeds can cause damage to the wiper motor and possible blade separation. (T.O. 1T-1A-1)
A. 250
B. 230
C. 200
D. 165
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 1-157
74. |
|
Definition
|
|
Term
74. The takeoff trim setting mark is small and can be hard to see under many conditions. Avoid fixating on this gage while resetting trim to maintain aircraft control. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 2-35 |
|
Definition
|
|
Term
75. Failure to properly reset the trim can result in _________________. (T.O. 1T-1A-1)
A. lower than normal yoke forces
B. over-rotation
C. higher than normal yoke forces
D. All of the above.
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 2-35 |
|
Definition
|
|
Term
76. If stopping distance is critical on slippery runways, turn EFCs off to further reduce engine thrust. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: 2-31 |
|
Definition
|
|
Term
77. After landing on a snow or slush covered runway: (T.O. 1T-1A-1)
A. do not retract flaps beyond 10°.
B. leave flaps at 30 degrees if 30° flap approach was flown.
C. raise flaps to 0°.
D. constantly cycle flaps all the way to the chocks to ensure they do not get ice accumulations.
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2-35 |
|
Definition
77. After landing on a snow or slush covered runway: (T.O. 1T-1A-1)
A. do not retract flaps beyond 10°.
B. leave flaps at 30 degrees if 30° flap approach was flown.
C. raise flaps to 0°.
D. constantly cycle flaps all the way to the chocks to ensure they do not get ice accumulations.
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2-35 |
|
|
Term
78. If any system emergency affecting safety of flight is experienced prior to S1 speed, the takeoff should be aborted. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-9 |
|
Definition
|
|
Term
79. If an emergency is experienced at or after S1 speed, _____________. (T.O. 1T-1A-1)
A. the takeoff should be continued
B. abort if below Vmb
C. abort if 3000 feet is remaining
D. b or c
Proctor Reference: T.O. 1T-1A-1 Pg: 3-9 |
|
Definition
| A. the takeoff should be continued |
|
|
Term
80. If the aircraft is decelerated and engages the barrier perpendicular to the middle half, no damage to the aircraft should be expected. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 3-10 |
|
Definition
|
|
Term
81. Which statement(s) are true? (T.O. 1T-1A-1)
A. Taxi over cables lying on the runway is acceptable at slow speeds (less than 5 knots).
B. Landing should be accomplished beyond arresting cables.
C. Landing should be accomplished before arresting cables.
D. a & b
Proctor Reference: T.O. 1T-1A-1 Pg: 5-9 |
|
Definition
|
|
Term
82. If engine shutdown or failure occurs in flight, consider the use of crossfeed to balance the fuel load, unless fuel system contamination is suspected. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-14 |
|
Definition
|
|
Term
83. The base of the emergency escape hatch is 4.5 feet above the ground with the landing gear extended, use caution when using this exit. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: Warning 3-5 |
|
Definition
|
|
Term
84. With dual Remote Tuning Unit (RTU) failure, how can VHF guard (121.5) be tuned? (T.O. 1T-1A-1)
A. It is not possible.
B. Use the CDU.
C. Pulling and resetting the VHF circuit breaker.
D. Use RTU disable function.
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-44 |
|
Definition
| C. Pulling and resetting the VHF circuit breaker. |
|
|
Term
85. If UHF guard mode was on when dual RTU failure occurred, guard reception is still available. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-44 |
|
Definition
|
|
Term
86. Using the engine fire switchlights to close the fuel valve also closes the hydraulic valve. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: 1-33 |
|
Definition
|
|
Term
87. Pulling and resetting the UHF circuit breaker after dual RTU failure does what? (T.O. 1T-1A-1)
A. Turns off the squelch.
B. Returns to the frequency tuned at the time of failure.
C. Does nothing.
D. a & b
Proctor Reference: T.O. 1T-1A-1 Pg: 3-44 |
|
Definition
|
|
Term
88. NAV auto-tuning is disabled when the RMT TUNE switch is in the DSABL position. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-44 |
|
Definition
|
|
Term
89. In the event of a fuel quantity indicator failure, which of the following are true? (T.O. 1T-1A-1)
A. Both gauges' dial pointers move off scale to below the zero mark to indicate an inoperative condition
B. Both gauges dial pointers freeze at the position they were at when the failure occurred
C. The fuel gauge failure (FGAGE FAIL) annunciator illuminates
D. There will be no indication
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 1-50 |
|
Definition
| A. Both gauges' dial pointers move off scale to below the zero mark to indicate an inoperative condition |
|
|
Term
90. Securing an engine after a failure/fire on takeoff should not be accomplished prior to _______. (T.O. 1T-1A-1)
A. 400 ft AGL (1500 optional)
B. 1000 ft AGL
C. clear of obstructions
D. a & c
E. b & c
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE3-10
91. |
|
Definition
|
|
Term
91. If an engine fire occurs immediately after takeoff when using the ACM OFF procedure, the bleed air selector may be turned to NORM at any time. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 3-11 |
|
Definition
|
|
Term
92. Do not attempt to restart an engine that has been shut down due to obvious mechanical difficulties. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 3-15 |
|
Definition
|
|
Term
93. If a spin is entered: (T.O. 1T-1A-1)
A. simultaneously add full power, apply full rudder opposite spin direction, forward elevator control and neutral roll control.
B. simultaneously reduce power to idle, apply full rudder opposite spin direction, forward elevator control and neutral roll control.
C. simultaneously reduce power to idle, apply full rudder pro spin direction, forward elevator control and neutral roll control.
D. simultaneously reduce power to idle, apply full rudder opposite spin direction, aft elevator control and neutral roll control.
Proctor Reference: T.O. 1T-1A-1 Pg: 3-28 |
|
Definition
| B. simultaneously reduce power to idle, apply full rudder opposite spin direction, forward elevator control and neutral roll control. |
|
|
Term
94. During a starter assisted airstart, a relight should normally be obtained within _____ second(s) after the throttle is moved to idle.
(T.O. 1T-1A-1)
A. 1
B. 5
C. 10
D. 15
Proctor Reference: T.O. 1T-1A-1 Pg: 3-15 |
|
Definition
|
|
Term
95. During a windmilling airstart, should the temperature rise indicate a hot start, place the throttle to CUTOFF and windmill the engine for ____ seconds before attempting another start. (T.O. 1T-1A-1)
A. 10
B. 15
C. 30
D. 60
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-15 |
|
Definition
|
|
Term
96. The FMS does not recognize step-down fixes between the FAF and the MAP and will not try to comply with them. If a given approach has any stepdown fixes between the FAF and arrival at MDA, VNAV should not be used for this portion of the approach. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 1-301 |
|
Definition
|
|
Term
97. During the flight control check of the rudder, ensure that both the PF and the PM independently observe a proportional displacement of their left and right rudder pedals and a proportional rudder control surface movement. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2 |
|
Definition
|
|
Term
98. The switchlight in the fire protection group on the shroud panel is used to close the _____ on the respective engine. (T.O. 1T-1A-1)
A. main fuel line shutoff valve
B. hydraulic valve
C. electric tie in
D. a & b
Proctor Reference: T.O. 1T-1A-1 Pg: 1-32 |
|
Definition
|
|
Term
99. The autopilot is not capable of controlling the aircraft in the event of an engine failure. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: 3-14 |
|
Definition
|
|
Term
100. Rudder boost is provided by the rudder servo of the autopilot. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-14 |
|
Definition
|
|
Term
101. In the event of electrical system failure, excluding the aircraft battery, placing the battery switch to the EMER position causes the battery to power the _________________. (T.O. 1T-1A-1)
A. emergency bus
B. standby battery
C. standby bus
D. a & b
E. All of the above
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 1-64 |
|
Definition
|
|
Term
102. If smoke or fumes are emanating from the air-conditioning vents, select L ENG or R ENG in an attempt to isolate the source. Bleed air source selector must remain in each position approximately _____ seconds to allow adequate purging. (T.O. 1T-1A-1)
A. 10
B. 15
C. 20
D. 30
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-22 |
|
Definition
|
|
Term
103. With oil pressure below _____ execute engine shutdown. (T.O. 1T-1A-1)
A. 60 psi.
B. 40 psi.
C. 30 psi.
D. 83 psi.
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-15 (2) |
|
Definition
|
|
Term
104. If high oil temperature is experienced _______________. (T.O. 1T-1A-1)
A. shutdown the affected engine
B. reduce power on the affected engine
C. turn off affected engine EFC
D. increase affected engine throttle within N1 limits
Proctor Reference: T.O. 1T-1A-1 Pg: 3-17 |
|
Definition
| D. increase affected engine throttle within N1 limits |
|
|
Term
105. While trying to eliminate smoke or fumes from inside the aircraft, turning the manual pressure controller fully counterclockwise will decrease the cabin pressure to the absolute pressure regulator setting of _______ feet. (T.O. 1T-1A-1)
A. 10,000 ± 1,000
B. 10,000 ± 1,500
C. 9,500 ± 500
D. 12,500 ± 1,500
Proctor Reference: T.O. 1T-1A-1 Pg: 3-22 |
|
Definition
|
|
Term
106. Under high temperature, low altitude, high throttle setting conditions, engine oil temperature may exceed ______ when the throttles are reduced due to a reduction in cooling fuel through the fuel/oil heat exchanger. The maximum transient limit is _____ and _____ should not be exceeded for more than _______ minutes. (T.O. 1T-1A-1)
A. 115°C, 121°C, 115°C, 15
B. 121°C, 135°C, 121°C, 15
C. 121°C, 131°C, 115°C, 15
D. 121°C, 135°C, 121°C, 5
Proctor Reference : T.O. 1T-1A-1 Pg: 3-17 |
|
Definition
| B. 121°C, 135°C, 121°C, 15 |
|
|
Term
107. If you have an EFC failure: (T.O. 1T-1A-1)
A. engine spool-up time on the affected engine will be increased so you should turn off the other EFC to match the throttles.
B. similar throttle angles will yield similar thrust settings.
C. matching the throttles using the engine with the EFC off may cause overboosting of the other engine.
D. attempt to reset the EFC with the throttle in any position.
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 3-17 |
|
Definition
| C. matching the throttles using the engine with the EFC off may cause overboosting of the other engine. |
|
|
Term
108. If the fuel filter bypass annunciator is illuminated, the bypass filter is purifying the fuel to the engine. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 3-19 |
|
Definition
|
|
Term
109. Left or right fuel level low annunciator illumination indicates that approximately _____ pounds of fuel remains in the respective tank.
(T.O. 1T-1A-1)
A. 11
B. 32
C. 200
D. 325
Proctor Reference: T.O. 1T-1A-1 Pg: 3-18 |
|
Definition
|
|
Term
110. If acceptable takeoff performance can only be achieved by selecting 0 degrees flaps and/or ACM off, takeoff in the presence of potential windshear is not recommended. Windshear conditions will quickly negate these minor performance enhancements. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 7-5 |
|
Definition
|
|
Term
111. If automatic starter dropout has not occurred by ____ % N2, press the starter disengage button. (T.O. 1T-1A-1)
A. 37
B. 38
C. 45
D. 52
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 2-15 |
|
Definition
|
|
Term
112. Autopilot engagement is not possible with the pitch trim selector in the EMER position. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-23 |
|
Definition
|
|
Term
113. An operating procedure or technique which could result in personal injury or loss of life if not carefully followed is a ____? (T.O. 1T-1A-1)
A. Warning
B. Procedure
C. Caution
D. Note
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING iii |
|
Definition
|
|
Term
114. Air entering the cabin for pressurization during air conditioning emergency operation will still be hot until the bleed air selector has been turned off. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-29 |
|
Definition
|
|
Term
115. In the event of a bleed air duct failure, if the wing anti-ice switch is turned OFF and the annunciator extinguishes, flight may be continued if icing conditions are avoided. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: 3-29 |
|
Definition
|
|
Term
116. If the AIR COND FAIL annunciator illuminates, the system will switch from normal to emergency pressure mode automatically. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: 3-28 |
|
Definition
|
|
Term
117. The emergency descent procedures are intended to be used for a maximum rate descent to quickly escape the high altitude environment. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: 3-30 |
|
Definition
|
|
Term
118. The maximum zero fuel weight is _______ pounds. (T.O. 1T-1A-1)
A. 12,500
B. 13,000
C. 15,700
D. 16,100
Proctor Reference: T.O. 1T-1A-1 Pg: 5-9 |
|
Definition
|
|
Term
119. During a controllability check, the aircraft speed should be decreased to a point where full control deflection is required to maintain controlled flight. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 3-27 |
|
Definition
|
|
Term
120. Do not attempt an actual single engine go-around after selecting flaps to 30°. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 3-32 |
|
Definition
|
|
Term
121. To execute a forced landing with no power ________________. (T.O. 1T-1A-1)
A. arrive at high key approximately 4000 ft AGL over the intended landing area
B. arrive at low key approximately 2000 ft AGL abeam landing area
C. gear should be lowered at high key or delayed if altitude is low to make low key on altitude
D. All of the above
Proctor Reference: T.O. 1T-1A-1 Pg: 3-34 figure 3-8 |
|
Definition
|
|
Term
122. Electrical loads up to _____ amps are permissible for single generator operations above 32,500 feet. (T.O. 1T-1A-1)
A. 280
B. 400
C. 420
D. 480
Proctor Reference: T.O. 1T-1A-1 Pg: 3-19 |
|
Definition
|
|
Term
123. If cruising below 32,500 feet, single generator operations load capacity is _____ amps. (T.O. 1T-1A-1)
A. 200
B. 280
C. 400
D. 480
Proctor Reference: T.O. 1T-1A-1 Pg: 3-19 |
|
Definition
|
|
Term
124. When both generator master switches and the battery switch are placed to EMER, ___________. (T.O. 1T-1A-1)
A. only the standby bus is powered
B. only the emergency bus is powered
C. both the battery feed emergency bus and DC standby bus are powered
D. no buses are powered
Proctor Reference: T.O. 1T-1A-1 Pg: 3-19 |
|
Definition
| C. both the battery feed emergency bus and DC standby bus are powered |
|
|
Term
125. When both generator master switches and the battery switch are placed in EMER, the engine anti-ice valves will ________________. (T.O. 1T-1A-1)
A. open
B. closed
C. remain in the last position set by the engine anti-ice switch
Proctor Reference: T.O. 1T-1A-1 Pg: 3-19 |
|
Definition
|
|
Term
126. During a dual generator failure situation, if the generators fail to reset and flight conditions permit, attempt to reset by turning both generator switches OFF, and reset them one at a time. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 3-19 |
|
Definition
|
|
Term
127. If the DOOR UNLOCK annunciator illuminates in flight, the jump seat may check the security of the cabin door as long as he/she stays strapped in. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 3-45 |
|
Definition
|
|
Term
128. The DOOR UNLOCK annunciator indicates that: (T.O. 1T-1A-1)
A. the cabin door pins are not fully seated
B. the aft fuselage door is not fully closed and locked
C. the left nose service panel is not fully closed
D. Any of the above
E. a. or b.
Proctor Reference: T.O. 1T-1A-1 Pg: 3-45 |
|
Definition
|
|
Term
129. The CABIN PRESSURE LO warning annunciator will illuminate when the: (T.O. 1T-1A-1)
A. aircraft altitude exceeds 10,000 ± 500 feet
B. cabin altitude exceeds 9,500 ± 500 feet
C. cabin pressure exceeds 9.1 psi
D. cabin pressure exceed 9.1 ± 0.1 psi.
Proctor Reference: T.O. 1T-1A-1 Pg: 1-139 |
|
Definition
| B. cabin altitude exceeds 9,500 ± 500 feet |
|
|
Term
130. If a thunderstorm or turbulence cannot be avoided, adjust power to establish a speed of _____ KIAS or _____ Mach. (T.O. 1T-1A-1)
A. 230, .70
B. 250, .64
C. 200, .58
D. 330, .78
Proctor Reference: T.O. 1T-1A-1 Pg: 7-4 |
|
Definition
|
|
Term
131. An external power unit is required for engine start at ambient temperatures below ____°F. (T.O. 1T-1A-1)
A. 0
B. 3
C. 5
D. 10
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 7-11 |
|
Definition
|
|
Term
132. If only two pilots are onboard, crew members will exchange seats only when the autopilot is engaged. (Ref: T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 4-2 |
|
Definition
|
|
Term
133. The Pilot Flying must announce to the crew when the autopilot is engaged or disengaged. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: 4-2 #6 |
|
Definition
|
|
Term
134. Only the pilot and copilot need to monitor UHF and VHF frequencies during descent when three crew members are aboard the aircraft. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 4-3 |
|
Definition
|
|
Term
135. In the case of exceeding an aircraft limitation, you must annotate the ______ in the AFTO Form 781. (T.O. 1T-1A-1)
A. time interval the aircraft limit was exceeded
B. instrument reading of the limitation that was exceeded
C. a. & b.
D. No write-up required.
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 5-1 |
|
Definition
|
|
Term
136. Do not operate surface anti-ice systems inflight at ram air temperatures above 10°C. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: 5-11 #2 |
|
Definition
|
|
Term
137. The yaw damper must be disengaged by 200 feet AGL for all landings. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: 2-12 |
|
Definition
|
|
Term
138. During ground aborts within a given stopping distance, the same amount of heat is generated by the brakes whether the brakes are applied in one steady application or a series of short applications. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 5-12 |
|
Definition
|
|
Term
139. Maximum Braking Speed is the maximum speed from which the aircraft can be brought to a stop without exceeding the maximum brake energy limit (14.8 million foot-pounds total for takeoff or 8.1 million foot pounds for landing). (T.O. 1T-1A-1-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1-1 |
|
Definition
|
|
Term
140. When _____ million foot pounds of brake energy are absorbed per brake, thermal fused screws may release resulting in flat tires. (T.O. 1T-1A-1)
A. 4.05
B. 8.2
C. 14.2
D. 14.8
Proctor Reference: T.O. 1T-1A-1 Pg: CAUTION 5-12 |
|
Definition
|
|
Term
141. What should you do if braking effort puts you between the 8.1 million and 14.8 million foot-pounds range on the brake energy limits chart? (T.O. 1T-1A-1)
A. This should be regarded as hot brakes
B. Park the aircraft
C. Shut down engines
D. All of the above
E. None of the above
Proctor Reference: T.O. 1T-1A-1 Pg: 5-13 |
|
Definition
|
|
Term
142. What must you do if you suspect hot brakes? (T.O. 1T-1A-1)
A. Taxi only as necessary to clear the active runway
B. Do not set the parking brake
C. Do not approach the hot brakes for 30 minutes
D. All of the above
Proctor Reference: T.O. 1T-1A-1 Pg: 5-13 |
|
Definition
|
|
Term
143. Allowable asymmetric fuel conditions are: (T.O. 1T-1A-1)
A. 200 pound imbalance between wings for takeoff
B. 300 pound imbalance for all phases of flight except takeoffs
C. 100 pound imbalance between wings for takeoff and touch & goes
D. a & b
E. b & c
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 6-2 |
|
Definition
|
|
Term
144. After checking flight controls during cold weather operations, the speed brakes may not fully retract due to lack of airflow across the wing surfaces. (T.O. 1T-1A-1)
A. True
B. False
Proctor Reference: T.O. 1T-1A-1 Pg: NOTE 7-12 |
|
Definition
|
|
Term
145. Take-off rated thrust is the maximum allowable thrust (determined by %N1) and varies with _________. (T.O. 1T-1A-1)
A. pressure altitude
B. ram air temperature
C. engine bleed
D. All of the above.
Proctor Reference: T.O. 1T-1A-1 Pg: 1-18 |
|
Definition
|
|
Term
146. Increase approach speed and touchdown speed by 50% of the gust increment, not to exceed a ____ knot correction. (AFMAN 11-247)
A. 20
B. 15
C. 10
D. 5
Proctor Reference: AFI 11-247 Par: 4.2.2 |
|
Definition
|
|
Term
147. Vmcg is _____ KIAS, and is the speed which (with one engine failed) will allow directional control without deviating more than _____ feet laterally. (T.O. 1T-1A-1)
A. 88, 25
B. 89, 50
C. 88, 50
D. 89, 25
Proctor Reference: T.O. 1T-1A-1-1 Pg: A 3-3 |
|
Definition
|
|
Term
148. Center of gravity problems affecting longitudinal stability during flight should be considered prior to ________. (T.O. 1T-1A-1)
A. crossfeeding of fuel
B. personnel movement within the cabin area
C. using the auto pilot
D. lowering flaps past 10°
Proctor Reference: T.O. 1T-1A-1 Pg: WARNING 1-16 |
|
Definition
| B. personnel movement within the cabin area |
|
|
Term
149. Deviations from any flight rule are authorized only when: (AFI 11-202 Vol 3)
A. An inflight emergency requires immediate.
B. Deviation is necessary to protect lives.
C. When safety of flight dictates.
D. both a and b above.
E. all of the above.
Proctor Reference: AFI 11-202 v3 Par: 1.7 |
|
Definition
|
|
