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b. False
23. Normal ranges of nozzle position are:
a. IDLE weight on wheels
b. In-flight MRT
c. MNA/Ei
d. MAXAD
24. What interlocks must be satisfied to activate the nozzle to the full-open position to reduce residual thrust?
a.
25. Minimum rpm for ground start of the Fl lo-GE-400 engine is percent rpm.
26. Maximum allowable EGT for ground starting the Fl IO-GE-400 engine is T.
27. The starting temperature limits are the same for both ground starts and aimtarts.
a. True
b. False
28. At EGT readings of “C *lo, a warning tone is present in the pilot earphones.
29. At T, the EGT chevrons begin to flash.
30. A hot engine should not be started until EGT is below T airborne.
3 1. Zero- or negative-g flight is limited ,to a maximum of
seconds in afterburner in or&r not to
seconds in military power or less aud
32. Above rpm, the MEC should shut off ibe1 flow to the Fl lO-GE-400 engine.
33. If the throttle boost system fails, the throttles automatically revert to manual mode, and the throttle mode switch
returns to MAN.
a. True
b. False
34. What pilot action is requiredt o reset the boost mode of throttle control subsequentto reversiont o the manual
mode?
35. is the controllmg parameter for the APCS.
39.7 ORIGINAL
NAVAIR Q1-Fl4AAD-1
36. Autothrottle engagement range is between and percent rpm.
37. If the autotbrottlesa re disengagedb y any means,t he AUTO THROT light illuminates for a lo-secondd uration.
a. True
b. False
38. Engine rpmmust be above percent to supply suf6cient power forthe main engine ignition system.
39. When attempting a crossbleedo r normal grounds tart,t he ENG CRANK switch will not reengageif the engine
is spooling down and engine rpm is between and percent
40. During spooklown airstarts, hung starts in the low rpm range (less than 45 percent) can be assisted with
.Hung~inthemid-rpmrange(5Oto6opercent)canbecorrected by
41. If the IGV linkage breaks, the IGVs assume a position, which is near normal for
power settings.
42. The number of delta Ps to cheek on each engine during preflight is
43. During an engine ground tire or abnormal start, be sure that the BACK UP IGNITION switch is in the
position.
44. The L or R FIRE warning lights illuminate when the respective entire sensing loop is heated approximately
“F or when any 6-inch section is heated to approximately OF.
45. What procedures should be followed to check oil level if it was not checked within 5 to 30 minutes after
shutdown?
46. During preflight, the oil sight gauge is always a reliable indicator of oil level.
a. True
b. False
47. TheNo. bearing receives priority lubrication in the event of a loss of oil.
48. During cold starts,o il pressureg reatert han 80p si shouldn ot be exceededfo r more than minute(s).
49. The electrical source for the oil pressure indicator is
50. The OIL PRESS warning light will illuminate. when the pressure drops below
when pressure rises above
psi and extinguishes
psi.
5 1. The L or R OIL HOT warning light indicates that the supply oil temperature has exceeded
the scavenge pump temperature has exceeded
52. The INLET ICE caution light illuminates when or
53. In AUTO, pitot probe heat is available only with weight off wheels.
a. ‘he
b. False
or
ORIGINAL 39-a
NAVAIR Ql-FMAAD-1
54. which of the following would result io illumination of the FUEL PRESS caution light?
a. Failure of a motive flow pump.
b. Failure of a main foe1 pump stage.
56. Failure of the second stage on the main engine fuel pump will have what effect on engine operation?
55. Failure of a motive flow fuel pump will have what effect on the engine and fuel system operation?
57. The loss of an engine-driven boost pump will have what effect on operation of both engines?
58. Selecting either AFT or FWD with the foe1 FEED switch performs what functions in the fuel system?
a. C. e.
59. The JJR FUEL LOW light ilhuninates with approximately pounds remaining in the respective
feed group.
60. AutomaticshutoffofwinganddroptrmkhansfaoccurswithwING/ExTTRANsswitchineitherA~orORIDE
a. True
b. False
61. The engine boost pump is powered by
62. To increase bingo fuel specifications, the engine mode select switch may be placed in
during descents or
63. The BINGO caution light illuminates when
64. Is vent tank fuel quantity included in the fuel totaker on the AFT and L indicator readings7
65. When should the FEED switch be activated to FWD or AFT7
66. What medium is used to actuate the feed tank interco~ect valve, wing motive tlow shut-off valves, and fuel
dump valve7
67. Wing foe1 is transferred by:
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F-14D 飞行手册 Flight Manual 3(90)
