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%rpm and . . . . PPH fuel flow to utilize the crossbleed airstart capability.
90. True/False: Hydraulic system 2A failure is the only single hydraulic system failure which
requires pilot action.
A1-F18EA-NFM-000
X-30-11 ORIGINAL
91. Hydraulic system 1A does not power which of the following;
a. Right Aileron
b. Right Trailing Edge Flap
c. Leading Edge Flaps
d. Left Trailing Edge Flaps
92. True/False: With HYD 2A failure, anti-skid is available.
93. With HYD 2A failure what type of landing should be considered?
a. Normal landing
b. Formation landing
c. Long field arrestment
d. Short field arrestment if practical
94. True/False: Gravity fuel flow is sufficient to sustain minimum afterburner operation.
95. True/False: You are in the spooldown restart envelope at 450 KIAS, 23,000 feet and N2 50%.
96. True/False: You are in the windmill restart envelope at .75 Mach, 25,000 feet and 14%N2.
97. True/False: A crossbleed restart is recommended at .68 Mach and 10,000 feet.
98. True/False: As a last resort, you may attempt an APU restart at 250 KIAS and 10,000 feet.
99. True/False: An APU restart should be one of the first procedures you utilize after an engine
failure.
100. Deleted.
101. True/False: One generator is insufficient to carry the total aircraft electrical load.
102. The battery will provide limited dc power for approximately . . . . minutes.
103. Deleted.
104. If the cabin temperature knob is full clockwise with the cabin temperature switch in MAN,
cockpit temperature can reach as high as . . . . °F.
105. True/False: The most probable source of visible smoke or fumes in the cockpit is from the
engine bleed or residual oil in the ECS ducts.
106. True/False: With both generators inoperative and a good battery your landing gear position
indicator will function normally.
A1-F18EA-NFM-000
X-30-12 ORIGINAL
107. True/False: With both generators inoperative and a good battery your hydraulic pressure
indicator will be inoperative.
108. True/False: Weight must be off the main landing gear or landing gear handle must be up for
the emergency jettison system to be operational.
109. True/False: Failure of FCS channels 1 and 3 will not affect the flying qualities of the aircraft.
110. True/False: With FLAPS OFF caution, a reset of the system may cause the leading edge and
or trailing edge flaps to retract.
111. True/False: If the trailing edge flaps are failed in the 0° position, final approach airspeed is not
significantly affected.
112. True/False: A single-engine landing is made at HALF flaps.
113. With 1,000 feet per minute sink rate, at 130 to 150 KIAS, the minimum altitude for a successful
ejection is . . . . feet in the F/A-18F at 0° angle of bank.
114. Deleted.
115. The correct procedure for an APU ACCUM caution airborne is:
116. List the steps for an out-of-control (OCF).
117. Thunderstorm penetration should be made between optimum cruise and . . . . . . . KIAS below
35,000 feet, and no less than . . . . KIAS above 35,000 feet.
118. What precautions must be observed when using the windshield rain removal?
119. The COM-NAV functions not available when MC 1 has failed are:
120. True/False: The right and left DDIs are physically and functionally interchangeable.
121. The bank angle scale pointer, on the HUD, is limited at ... and ...when the limit is exceeded.
122. The velocity vector represents:
123. True/False: Do not lock the gyro in the caged position with the pull to cage knob if the gyro is
spinning.
124. Using Stall Speed chart:
Mil power
Gross weight - 42,900 pounds
Gear/flaps - DOWN
Determine - Stall Speed 0° Bank= . . . .
125. Determine - Stall Speed 45° Bank= . . . .
A1-F18EA-NFM-000
X-30-13 ORIGINAL
126. Using Landing Approach Speed chart:
Gross weight - 42,900 pounds
Flaps - HALF
127. Determine - Recommended Approach Speed= . . . .
128. What action must the pilot take in order to slew the moving map with the TDC?
a.
b.
129. The GYRO position on the INS mode selector switch
a. Connects the gyros to the attitude heading reference system in order to complete an inflight
alignment
b. Enables the mission computer to use the gyros in computations for air-to-air weapons delivery
c. Is the attitude mode where the INS operates in the gyro mode
d. All of the above
130. REJ 1 removes what from the HUD display?
131. If you see the following in the upper left corner of the HSI display or MPCD, what does it tell
you?
237/108
18:00
NLC
a. Your aircraft is 108 miles from Lemoore TACAN on the 237° radial
b. Your aircraft is 108 miles from Lemoore TACAN on the 057° radial
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 2(127)