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49. What will the standby attitude indicator be powered by if the right 115 volt ac bus fails?
50. The APU fire detection/extinguishing systems operates from . . . . power, provided the . . . .
switch is ON.
51. The bleed air shutoff valves are closed when the fire and bleed air test switch is placed to TEST
A and TEST B positions. How do you get the valves back open?
a.
b.
52. True/False: The canopy can be jettisoned in the closed position only.
53. Why would you not pull the manual override handle in flight before ejection?
54. What conditions must be met to utilize the emergency jettison button?
a.
b.
55. The . . . . switch must be in the . . . . position to use the selective jettison system.
56. What occurs when the unlighted MASTER CAUTION light is pressed?
57. True/False: For cautions with voice alert, the master caution tone comes on after the voice alert.
58. What two ways can you stop any BIT test in progress and return the equipment to normal
operation?
a.
b.
A1-F18EA-NFM-000
X-30-9 ORIGINAL
59. What two systems require additional switchology other than pressing the associated button
when performing initiated BIT checks?
a.
b.
60. How much has the fuel quantity in tank 1 been reduced in the F/A-18F aircraft?
61. True/False: The rear cockpit does not have an internal canopy switch or an internal manual
canopy handcrank.
62. True/False: There are provisions for normal landing gear extension from the rear cockpit.
63. The leg restraint lines must be buckled at all times during flight to ensure . . . . and to enhance
. . . .
64. Failure to route the restraint lines properly through the garters could cause: . . . ..
65. True/False: High gain nosewheel steering should be used on takeoff roll up to 50 KIAS.
66. On a section takeoff, turns into the wingman will not be made at altitudes less than . . . . feet
AGL.
67. True/False: The second section may commence the takeoff roll after the first section has rolled
1,000 feet.
68. True/False: Before descent it is necessary to preheat the windshield by increasing defog airflow.
69. True/False: For optimum braking above 40 KIAS, with anti-skid, full brake pressure should be
used.
70. True/False: Ensure anti-skid is OFF for all shipboard operations.
71. Nosewheel steering low mode (may/may not) be engaged while the launch bar is down (circle
correct answer).
72. A carrier landing pattern starts with a level break at . . . . . feet, on the . . . . bow of the ship.
73. True/False: The seat rocket thrusters may ignite spilled fuel or hydraulic fluid and may injure
ground crew in the immediate vicinity.
74. True/False: If you must land with the launch bar extended, you should request that the field
arresting gear cables be removed.
75. A time critical situation exists if you have directional control problems during takeoff. If you
suspect nosewheel steering failure, the first thing you should do is . . . . .
76. If the aircraft begins to settle after a catapult launch and the settling cannot be stopped you
must . . . ..
77. What are the emergency procedures if you have lost thrust on takeoff?
A1-F18EA-NFM-000
X-30-10 ORIGINAL
78. True/False: It is unlikely that a blown nose tire will FOD an engine.
79. During flight brief consideration of takeoff abort possibilities, the following items should be
considered.
a. Weight
b. Speed
c. Runway length remaining
d. All of the above
80. When making an arrested abort, allow time for the arresting hook to extend; as a guide, lower
the hook . . . . feet before the cable.
81. If the landing gear fails to retract you should perform the following:
a. Pull the landing gear control circuit breaker.
b. Cycle the gear and pull negative g's.
c. Put the landing gear handle down and do not cycle
d. Press on - it's probably a false light.
82. What two methods may be used to retain both hydraulic systems if the engine core is rotating:
a.
b.
83. True/False: If the right engine is being rotated with crossbleed to provide normal systems
operation and fuel flow on the left engine is reduced below 2,000 pph (as during landing) the right
engine hydraulic pump may not provide sufficient flow for nosewheel steering and normal brakes.
84. True/False: Most engine stalls are self clearing.
85. True/False: Engine stalls may produce audible bangs.
86. True/False: If a stalled engine will not clear, you may shut down the engine and attempt a
restart.
87. What airspeed may be required to maintain 12% windmilling rpm?
88. True/False: Engine crossbleed may not be used to achieve a 12% rpm for engine restart.
89. With one engine windmilling below 12%, the remaining engine should be operated at or above.
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 2(126)