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Closing Nozzles.
3. CANOPY DEFOG/CABIN
AIR lever - CANOPY DEFOG.
4. ECS - MAN/FULL HOT (CONT).
If light goes auf:
5. Throttles - IDLE.
6. ECS - As Desired.
If light remains illuminafed:
7. Secure systems.
I
Continuous-wave emitter detected. As briefed.
DEU HOT (MFD)
Data entry unit oveheated. Expect loss of DEU.
DPI HOT
Display processor overheated. Pull cb’s lG2,1G4,1G6,3F4,4F3,4F6.
DP2 HOT (MFD)
DSS HOT
W=W
Data storage set overheated. Expect loss of DSS.
EMERG JETT
When depressed with weight off wheels, None.
PUSHBUTTON/
activates emergency stores jettison
ACK LIGHT
signal to the SMS and illuminates light
for 5 seconds. Jettison function is
disabled with weight on wheels.
Warntng, Caution, Advisory LlghtslDlsplays (Sheet 4 of 15)
WARNING/CAUTION/ADVISORY LIGHTS/DISPLAY LEGENDS
LIGHT/LEGEND
ENG
FIRE EKT
WW
CAUSE
Low-extinguisher agent
pressure.
ACTION
Report to maintenance.
L ENG SEC
a
Engine mode control in secondary. If engine transfers to set mode:
R ENG SEC I. Throttle - Less Than MIL.
2. ENG MODE SELECT - Cycle.
If PRI mode restored:
3. Maintain constant subsonic airspeed in
level flight.
4. Affected L or R AICS cb - Cycle.
If engine fwmelfls in SEC:
3. ENG MODE SELECT - SEC.
4. Avoid abrupt throttle movements.
5. Land as soon as practicable.
LFIRE *
0
Fire/overheat condition in englne If HUDh4FD message:
R FIRE
nacelle.
Message is a repeat of a discrete from the
(HUD/MFD)
fire detect system. If FIRE warning light is off
and FIRE DET TEST checks 4.0, then
assume message was incorrect and keep
engine on line.
If FIRE warning light and message:
‘I. Throttle (affected engine) - IDLE.
‘2. AIRSOURCE - OFF.
l 3. OBOGS - BACKUP.
fflight goes OFF and no secondary
Indications:
l 4. MASTER TEST - FIRE DET TEST.
If light remains illumlnafed, FlRE DET TEST
fails, or other secondary indications:
l 5. FUEL SHUT OFF - Pull.
‘6. Throttle - OFF.
‘7. Climb and decelerate.
l 6. Fire extinguisher - Depress.
‘9. Refer to SingleEngIne Cruise
Operations.
10. Land as soon as possible.
11. If fire persists - Eject.
Wamlng, Cautlon, Advlsory Lights/Displays (Sheet 5 of 15)
ORIGINAL
WARNlf
LIGHT/LEGEND
WFD)
i/CAUTION/ADVISORY LIGHTS/DISPLAY LEGENDS
CAUSE
Yap position disparity with
ommanded position or flap/slat
Isymmetry.
NAVAIR OMl4AAD-1
ACTION
1. Airspeed - Below 225 Knots.
2. FLAP handle - Ensure Full Up.
3. MASTER RESET - Depress.
4. While holding MASTER RESET
pushbutton depressed, maneuver flap
thumbwheel - Full Forward.
5. Check FLAP light out.
If after landing/takeoff flap transition, or
~ilfuminatton after above procedures:
1. MASTER RESET - Depress.
2. If light still illuminated, check FLAP
handle and indicator position, then
proceed with appropriate steps below.
Flap handle up and t7aps not fully retracted:
1. Flap handle - EMER UP.
Flap handle up and flaps indicaUng full up:
1. Flaps - Cyde.
Flap handle down and flaps not f&y
extendeti
I. Wing sweep - Ensure at 20”.
Flap handle down and flaps down:
,I. Wing sweep - Ensure at 20”.
2. MASTERRESET - Depress.
Flap and slat asymmetry:
Refer to Chapter 14.
Check engine gauges.
If invalid, report anomaly to maintenance:
ff valid petfom the following:
*I. Throttle - IDLE or Above.
‘2. BACKUP IGNITION switch - ON.
If hung start or no starl:
l 3. Throttle - Cycle OFF, Then IDLE.
Warning, Cautlon, Advisory LlghtdDlspltiya (Sheet 0 of 15)
75 ORIGINA
\\\\\~\~~\~~~~~~~~~-----.-------
NAVAIR 0%F14AAD.1
WARNING/CAUTION/ADVISORY LIGHTS/DISPLAY LEGENDS
LIGHT/LEGEND CAUSE ACTION
giii%J
Engine flameout. If sf/// hung or no start:
l 4. ENG MODE SELECT - SEC.
If one engine is operable, perfom, a
WW
crossbleed airstart.
If both engines flamed out//noperafive o
crossbleed not possible:
‘5. Airspeed - 450 Knots.
6. OBOGS - BACKUP.
When stari complefe:
7. BACKUP IGNITION - OFF.
8. ENG MODE SELECT - PRI.
9. OBOGS - ON.
When primary mode restored:
10. Maintain constant subsonic Mach in level
flight.
il. Affected AICS cb - Cycle.
LL%L
lIlIlll
Usable fuel in L and AFT or R and FWD 1. DUMP switch - OFF.
fuselage tanks 1,000 pounds. 2. Fuel distribution - Check.
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F-14D 飞行手册 Flight Manual 2(89)
