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109. Illumination of the WING SWEEP warning light means:
110. Illumination of the WING SWEEP advisory light means:
111. Transient failures in the CADC may be reset by:
112. The CADC is self-tested in
113. List the caution, advisory, and warning lights activated by the CADC directly or via the AFCS:
a. e.
d. h.
114. When instrumentt eath asb eens electedo n the MASTER TEST panel,t he EIG indicationsa fler 5 secondsa re:
a. RPM
b. EGT
c. FUEL
d. FLOW
ORIGINAL 39.12
NAVAIR 0%FMAAD-1
115. A degrademd odeo f EIG operationis indicatebdy
116. Maneuvefrl apsc anb e lowereda t anyw ing-sweeap ngleb etween2 0’ and
117.T he maneuverinfgla p thumbwheewl ill lowert he mainf laps ,
and the slats
theauxiliatyflaps . . . ,
. Useo fthe maneuvering&vice(dso eso r doesn ot)p utm orer estrictiveg htahons
on the aircraft.
118.W hati s the meaningo f the fogowing( besideCs ADC failure)?
a. FLAPc autionli ght
b. REDUCES PEEDw arning (1)
(3)
119.P owerf or emergenceyx tensioonf thel andingg earis s uppliebdy
120.T hem inimumb ottlep ressurfeo r accomplishinegm ergenceyx tensioonf the landingg earis psib ut
minimump reflightb ottlep ressuries psia t 70 OF( 21.T).
121. Full lateralt rim in the direction of stick displacemenwt ill reducem aximums poilerd eflectiont o
ou that side.
122. Full slata symmetroy f 17’ canr esulti n ano ut-of-controsl ituationa t
evenw ith 55Oo f spoilersa vailable.
units AOA or greater,
123. Ther udderp edals hakeirs armedw ith mainf lapsg reaterth an
computeor perating.
124. With DIG engagedlb, ll-upD LC positionsth ei nboards poilersa t
GP
Oandthe
0a ndt heh orixontasl tabt railing
125. Thei nitialp ositionf or spoilenw henD LC is engageids
126. Thec orrectp ositioningfo r stabilizerws henD LC is givena fit&downc ommand(f rom trim) is
trailing edge
127.F ull rudderthrowo fi ’ correspondtos f inches of rudderp edatl ravel.
128. Controls urfacea uthorityo f the stabilitya ugmentatiosny stemis :
Pitch i 0
Roll f 0
Yaw l 0
129. Theg earh andleis downa ndt het hreeg earp ositionin dicatorss howt he geard own,b ut the transitionli ght
is illuminatedW. hatd oesth is indicatea ndw hata ctions houldb et aken?
39-13 ORIGINAL
130. The ANTI SKID SPOILER BK switch is OFF and the BRAKE light is illuminated. This would indicate:
a.
b.
131. The BRAKE light (ANTI SK.ID SPOILER BK switch OFF) operateso nly when the brakesa re depressedo r
the parking handle is pulled.
a. True
b. False
132. The two procedures for lowering the launch bar are:
133. Nosewheel steering cannot be engaged until weight is on wheels.
a. True
b. False
or
134. With the nosewheel <70°, the nosewheel assumes the position commanded by the rudder pedals when
nosewheel steering is engaged.
a. Tnre
b. False
135. BLEED DUCT light indicatest emperaturesin excesso f OFb etweene nginea ndp rimary heat
exchanger or greater than OF between primary heat exchanger and the ECS turbine.
136. The ram air door can be openedo nly if the or button is depressedo n the ECS
control panel.
137. TheramairdoorautomaticallycloseswithselectionofLENG,RENG,orBOTHENGontheECScontrolpanel.
a. True
b. False
138. The ram air door requires secondst o go full open.
139. The RIO has a low-cockpit-pressure caution light (CABIN PRESS) that illuminates if or
140. With the OBOGS light on, each flightcrewmember should have hours of oxygen at 20,000 feat (8,000
feet cabin altitude).
141. Pullmg the emergency oxygen actuator releases gaseous oxygen charged to psi and will provide approximately
a -minute supply.
142. Windshield rain removal is accomplished by blowing 390 OF air over the outside of the windshield. If the
tempemtute sensor detects an overtempemture condition, the.WSHLD HOT advisory light will ifhrminate
and
143. Maximum allowable headwind for the open canopy is
ORIGINAL 39-14
kllOtS.
NAVAIR 0%FUAAD-1
144.W hent he canopyis j ettisonedt,h e sill locksa rer eleasebdy
145.T hec anopyp neumatirce servoimr ustb e servicedb y grounds ervicingu nit.
aTme
b. Fslse
146. Thep ilot cant ell thep ositiono f the commande jectionle verb y
147. TheR IO cane jectb othh imselfa ndt hep ilot with EJECTC MD handles ett o PILOT.
a. True
b. False
148. Thep ilot cane jectb othh imselfa ndt heR IO with theE JECTC MD handles ett o MCO.
aTrue
b. False
149.I n the eventt he canopyd oesn ot separatetir n the aimraftw hene ither tlightcmwmembehra s initiated
ejection‘,Y tuwght he canopy”e jectionw ill not occur.
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F-14D 飞行手册 Flight Manual 3(92)
