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a. True
b. False
150.T lleream safetyp insp ere jections eat.
151.C ommande jectionb y either flightcrewmembewr ill eject the RIO in __ secondsa nd the pilot
swondsla ter.
152. For a high-altitode jectiont,h e seati s allowedto ike-fall to f. feet.
153. All exteriorli ghtingc ontrolse xcepfto r the lighta rel ocatedo n theM ASTERL IGHT paneol n the
pilot consolea, ndt he exteriorl ightsm asters witcho n the outboardth rottle.
154. Whent he wing.9a res wepta ft of
-
the positionli ghtsa red isableda ndt heg lovev ane
positionli ghtsa reo perable.
155. Whent he ANTI-COLLISIONl ights witchi s ON, the positionli ghtsf lashers witchi s disabled.
156. A properin dicatorli ghtst esth ast he MASTERC AUTION lighto n steady.
a.TlUe
b. False
157.T heR IO canm onitorS Wt onesb y selectiono f positiono n theI CS panel.
158.T hes tandbya ttitudein dicatoris capableo f providingr eliablea ttitudei nformationw ithin for
upb minutesa ftera completelo sso f power.
159. Ond eckt bea llowabler rorb etweenth ep ilota ndR IO altimeterre adingis feeta t fielde levation.
39.15 ORIGINAL
160. The angle-of-attack indicator is checked during
indications are:
a. hiicator -
b. Indexer -
and the indexer during .proper
161. In the landing cont&uration, 15 units AOA is equivalent in aimpeed for:
a 48,000 pounds (DLC not engaged) = KIAS
b. 48,000p ounds (DLC engaged/neutral=) KIAS
c. 50,000 pounds (DLC not engaged) = KL4s
162 . With an ahspeed indicator failure, list the angle of attack to fly for the following conditions (drag index 8):
a. Catapult
b. Climb (MIL) SL to combat ceiling.
c. Cruise at OPT. ALT.
d. Endurance at OPT. ALT.
163. Stores jettison is controlled by which aircraft system?
164. ACM jettison requires MASTER ARM ON.
a True
b. False
165. Selective jettison can be completely controlled by either flightcmwmember.
a. True
b. False
166. In the emergency jettison mode, the weight-on-wheels interlock is bypassed.
a. True
b. False
167. Emergency jettison mode will jettison Sidewinders.
a. True
b. False
168. Sidewinder is jettisoned by ftig the motor and sating the warhead.
a. True
b. False
ORIGINAL 39-16
NAVAIR WF14AAD-1
169. The pretaxi (weighton-wheels) OBC master test is a complete check of the SMS.
a. True
b. False.
170. Selection of any pulse dogfight mode automatically provides stab out aircmft reference.
a. True
b. False
171. The pilot must clear maintenance display prior to running OBC for current test results
a. True
b. False
172. FornormalUHPoperationwiththeARC-182,theAMEMswitchshouldbeinthe
position.
173. With track files established in TWS, the HUD and MPDs provide the pilot complete steering information to
the centroid of the targets.
a. True
b. False
174. The navigation system may be updated by five methods; they are:
a. d.
b.
C.
e.
175. In TACAN BIT, the range and bearing on the HSD and BDHI should indicate
0
nm and
176. The target designator (diamond) is valid to f O off the nose.
177. With MASTER ARM OFF, the HUD and VDI armament legend will appear with
178. To obtain an attack presentation,t he air-to-air button must be selectedo n the PDCP.
a. True
b. False
179. The COOLING AIR light refers to air cooling out of tolerance while the SENSOR COND light indicates
liquid cooling out of tolerance.
a. True
b. False
39-l 7 ORIGINAL
NAVAlR 01.Fl4AAD-l
180. The TID is orieoted to north, with selection of GND STAB on the TID mode switch.
181. Which of tbe following presentationsa re available to tbe pilot:
a. IRSTS
b. PS
c. PDS
d. AU of tbe above.
182. A acronym indicates * failure of tbe SMS, thus preventing normal separation of stores in any
launch mode.
183. The RADAR COOLING switch in tbe RIO cockpit controls liquid coolant to
184. Hostile area altitude is entered in tbe pseudo file to properly reject eltitude line return.
185. Wind is automatically computed by the system in the INS mode.
a. True
b. False
186. A wind of 35 lmots and 057” relative to the duty runway representsa headwind compone.nto f
knots and crosswind of ImOtS.
187. A blinking SHOOT cue indicates
188. Hydraulic power to drive tbe gun comes f?nrn the System.
ORIGINAL 39-18
PART XI
Performance Data
Foraimaftperformamedataandchats,refertoNAVAIROl-F14AAP-l.l.

NAVAIR 01.F14AAP1
INDEX
Page Page
No. No.
A
Abnormalstart. ................. 12-l
Aborted takeoff ................. 13-l
　
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