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A1-F18EA-NFM-000
X-30-5 ORIGINAL
30.4 NATOPS EVALUATION QUESTION BANK
1. What is the F/A-18's operating weight?
2. What is the takeoff gross weight (operating weight plus full internal fuel, ammo, 2 AIM-7s, 2
AIM-9s)?
3. What is military thrust of the F414-GE-400 engine?
4. What is afterburner thrust of the F414- GE-400 engine?
5. When will you get engine ignition?
a.
b.
c.
d.
6. When will you get afterburner ignition?
a.
b.
7. How is a limited amount of fuel provided for negative G or inverted flight?
8. True/False: The F/A-18's IDLE rpm is the same on the ground as inflight.
9. Which one of the following caution and advisory displays will not activate the ªengine left (right)º
voice alert?
a. L or R OVRSPD
b. L or R EGT HIGH
c. L or R BOOST LO
d. L or R OIL PR
10. What are the modes of operation of the automatic throttle control (ATC)?
a.
b.
11. What conditions must be met to engage the approach mode of the automatic throttle control?
a.
A1-F18EA-NFM-000
X-30-6 ORIGINAL
12. What conditions must be met to engage the cruise mode of the automatic throttle control?
a.
b.
13. Which fuel tanks are transfer tanks?
a.
b.
c.
14. Which fuel tanks are feed tanks?
a.
b.
15. What does a TK PRES LO or TK PRES HI caution display on the DDI indicate?
a. On the ground -
b. Inflight -
16. Normal internal fuel is transferred using . . . .
17. External fuel is transferred by . . . .
18. True/False: With external tank control switch in stop transfer and hook handle down, fuel will
transfer when FUEL LO caution display comes on.
19. What two fuel valves close when an engine fire light is pressed?
a.
b.
20. List four events which individually will cause fuel dump to stop.
a.
b.
c.
d.
21. True/False: The fuel low level indicating system is completely independent of the fuel quantity
indicating system.
A1-F18EA-NFM-000
X-30-7 ORIGINAL
22. What fuel state illuminates the FUEL LO light, MASTER CAUTION light, and activates fuel
low voice alert?
23. True/False: There is no voice alert associated with BINGO fuel.
24. Either AMAD may be driven pneumatically through an . . . . by the APU, opposite engine bleed
air, or external air.
25. Each AMAD mechanically drives a . . . . . . . . ., . . . . . . . . ., and . . . . . . . . ..
26. True/False: Operation of APU is totally automatic after the APU switch is placed ON.
27. What provides electrical power for APU ignition and start control circuits?
28. What is used to start the APU?
29. True/False: If ATS caution is on when a DDI comes on, shut down the affected engine to avoid
starter damage.
30. What is the cockpit warning of a single TR failure?
31. What is indicated by the BATT SW light coming on in the air with the battery switch on?
32. What seven circuit breakers are located in the cockpit?
33. True/False: The exterior lights master switch must be on for operation of the position and
formation lights, but not for the strobe lights.
34. What failure(s) will illuminate the emergency instrument light and the BATT SW caution light?
35. The right or HYD system 2 provides power to:
36. What are the primary flight controls?
37. What does pressing the T/O trim button in flight do?
38. What is the FCS reset button used for?
39. With the spin switch in NORM, when will the spin recovery mode be activated?
40. On takeoff, accelerating with the flaps switch in HALF, at what speed will the flaps begin AUTO
scheduling?
41. True/False: Once EMERG has been selected on FCS COOL switch, selection of NORM will
switch FCC A and right TR cooling back to avionics air.
42. Rudder toe-in is a function of flap switch position and . . . . with maximum toe-in being . . . ..
43. True/False: Stabilator position on the FCS status display on the DDI shows a (+) for trailing
edge up (or nose up), and a (-) for trailing edge down (or nose down).
A1-F18EA-NFM-000
X-30-8 ORIGINAL
44. What occurs with gear handle UP, airspeed below 175 KCAS, altitude less than 7,500 feet, and
rate of descent greater than 250 feet per minute?
a.
b.
45. True/False: Pressing and holding the nosewheel steering button a second time will select the
high mode (±75°) and NWS HI is displayed on the HUD.
46. True/False: The hook light remains on except when the hook is up and latched.
47. Normally, what kind of power is needed to fold or spread the wings?
48. Is it normal to have L PITOT HT and R PITOT HT advisories displayed on the DDI while on
the ground with pitot heat switch in AUTO?
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 2(125)