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c. Your aircraft is 18 miles from Lemoore TACAN on the 057° radial, 108° magnetic heading
d. Your aircraft is 18 miles from Lemoore TACAN on the 108° radial, 237° magnetic heading
132. During a data link ACLS (SPN-42) approach the HUD displays:
a. A TD box overlying the touchdown point
b. A fly-to tadpole symbol
c. Fly-to needles (similar to ILS)
d. A course arrow and elevation steering bar
133. True/False: During an ILS approach the standby attitude indicator displays the ILS needles.
A1-F18EA-NFM-000
X-30-14 ORIGINAL
134. What is the internal fuel capacity of the F/A-18E . . . . pounds, F/A-18F: . . . . pounds.
135. State the following limitations:
a. Maximum steady state EGT -
b. Maximum start EGT -
c. Maximum EGT fluctuation (stabilized power) -
d. Maximum rpm fluctuation (stabilized power) -
e. Maximum transient rpm (N2)
f. Maximum nozzle fluctuation
136. State the ranges for the following:
a. Ground idle rpm -
b. Flight idle rpm -
c. Maximum oil pressure (2 minutes after start with ambient temperature below -18°C, 0°F)
Minimum oil pressure (ground idle) -
d. Inflight oil pressure:
(1) Idle -
(2) 95% rpm -
(3) Military -
137. The maximum speeds of the following are:
a. Refueling probe -
b. Gear retraction/extension -
c. Gear emergency extension -
d. Trailing edge flaps -
e. Canopy open -
A1-F18EA-NFM-000
X-30-15 ORIGINAL
138. State the following limitations:
a. Maximum gross weight field takeoff -
b. Maximum landing weight (field landing - flared) -
c. Maximum weight (touch and go)
d. Maximum air refueling altitude -
e. Maximum closure on refueling drogue -
f. Maximum time at negative g -
g. Minimum time between negative g maneuvers -
139. If the velocity vector begins to flash slowly but is not HUD limited:
a. Selected ordnance has been released.
b. The mission computer may be displaying a degraded velocity vector
c. The waterline symbol is HUD limited
d. STBY attitude indicator is providing HUD attitude information
140. The HUD landing display (elongated horizon bar, AOA bracket, waterline symbol, steering
display) will be presented
a. When selected through the HUD control panel
b. When selected on the right DDI
c. When gear is down and NAV master mode is selected
d. Any time that the gear is down
141. True/False: While using NAV master mode, the pilot has the option to cage or uncage the
velocity vector on the HUD.
142. At what altitude will the cockpit begin to pressurize?
143. What action should be taken if FCS HOT caution light comes on in flight?
a.
b.
A1-F18EA-NFM-000
X-30-16 ORIGINAL
144. When the G XMT switch is placed to COMM 1 or COMM 2 the
a. Selected radio will receive/transmit on 243.0 only
b. Selected radio will receive only 243.0
c. Selected radio will transmit only 243.0
145. The hydraulic pumps are located on the . . . . and maintain the hydraulic pressure at
approximately . . . . psi.
146. The HYD 2 priority valves close at approximately . . . . psi.
147. Placing the HI mode selector switch to NORMAL displays compass rose aligned with the
aircraft
a. Magnetic ground track
b. Magnetic heading
148. By what method are external tanks pressurized on the ground?
149. What indication does the pilot have to indicate low or lost motive flow pressure?
150. Fuel is transferred from external tanks by:
a. The passing of motive flow fuel through an ejector pump which utilizes the venturi principle
to induce fuel flow.
b. Bleed air to pressurize each external tank.
c. Electrically powered boost pumps located inside each tank.
d. AMAD driven boost pumps that utilize the venturi principle to induce the flow from each tank.
151. True/False: In the F/A-18F there is no provision to raise the landing gear from the rear cockpit.
152. With a failure of hydraulic system 2A, what alternate method exists for extending the air
refueling probe?
153. Fuel dump is accomplished by:
a. Motive flow (ejector pumps)
b. Electrical pump powered by essential bus
c. AMAD driven boost pump
d. Variable displacement pumps driven by hydraulic system 2A
154. Normal brake system pressure is provided by hydraulic system . . . ..
A1-F18EA-NFM-000
X-30-17 ORIGINAL
155. What optical indications of NWS failure will the pilot have available besides the MASTER
CAUTION light?
a.
b.
156. Where is the manual canopy crank handle located inside the F/A-18 cockpit?
157. Depending on aircraft attitude and power setting, the fuel dump rate is about . . . .
pounds/minute.
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 2(128)