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If wing ancV0.r e&ma! fuel remaining:
3. WINGIEXTTRANS - ORIDE.
4. Land as soon as practicable.
‘PEk
cz3
Sump tank boost pump discharge fess 1. Both throttles - MILPower or Less.
than 9 psi. 2. Restore aircraft to 1 .Og flight.
RPRFEUSESL
If both lights remain on:
3. Increase positive g’s to > l.Og.
,4. Descend below 25,000 feet.
5. Maintain cruise power settings or less.
6. Land as soon as possible.
If one light remains on:
3. .No afterburner above 15,000 feet.
4. Fuel distribution - Monitor.
5. Land as soon as practicable.
L GEN
lIlIIIl
Generator failure and/or 1. Gemmtor - DFF/RESET,ThsnNORM.
R GEN disconected from its ac bus. If generator does not reset:
2. Generator - TEST.
m Firing logic met. Pilot’s trigger will Ire Pilot optton.
weapon when squeezed.
Combined or flight pump discharge Refer to Chapter 14 for appropriate
pressure 2,100 psi or less. procedure.
Wamlng, Caution, Advisory Lights/Displays (Sheet 7 of 15)
76
--
WARNING/CAUTION/ADVISORY LIGHTS/DISPLAY LEGENDS
LIGHT/LEGEND CAUSE ACTION
m
CADC fsilure or failure of actuators to
HZ TAIL
1. MASTER RESET - Depress.
AUTH
follow schedule. If fight mmalns illuminated:
2. ROLL STAB AUG - OFF.
3. Above 400 knots, restrict lateral control
to onequarter throw.
4. ROLL STAB AUG - ON for Landing.
5. Do not select OV SW after landing.
IFF
Mode 4 interrogation received; no reply As briefed.
generated.
Improper IFF transponder operation.
IFF ZERO (MFD)
As briefed.
m,
Inlet guide vanes off schedule. AICS fail operation mode in use.
Stall margin may be very slightly reduced but
WW
still remains satisfactory and greater than
that in SEC mode.
High-power thrust may be reduced.
Improper operation of inertial
IMU
Secondary navigation mode is in use.
WW
measurement unit.
INS
Improper operation of inerttal Secondary navigation mode is in use.
CM=‘)
navlgstlon system.
INTEG
Power loss or discrepancy between MASTER RESET.
TRIM
Input slgnal and posltlon
Computer malfunctton or ramp ‘1. Avoid abrupt throttle movements.
mlsposltlonlng. ‘2.. Decelerate below 1.2 TMN.
‘3. Affected INLET RAMPS - STOW.
If RAMPS light remains illuminated:
4. Throttle - 80 percent or Less.
5. Affected AICS cb - Pull.
6. Affected INLET RAMPS - AUTO.
7. Land as soon as practicable.
If INLET light only illuminated, attempt AICS
pivgmm reset:
4. Decelerate betow 0.5 TMN.
5. Affected AlCScb - cycle.
If INLET light goes of??
6. Affected INLET RAMPS - AUTO.
If INLET LIGHT remains Mumhated:
6. Affected AlCScb - Pull.
7. Affected INLET RAMPS - AUTO.
6. Remain below 1.2 TMN.
u- WARNING/CAUTION/ADVISORY LIGHTS/DISPLAY LEGENDS
LIGHT/LEGEND CAUSE ACTION
INLET
liIIz3 ICE
Icing condition exists in inlet or
ENGlPROBE ANTI-ICE switch is on.
1,. Select ORIDUON.
When clear of Mng conditions:
2. ANTI-ICE - AUTO/OFF.
IPF
IRSTS HOT
WW
JTID HOT
WD)
JTIDS is failed, a momentary glitch,
or 20-percent duty cycle has been
exceeded.
Infrared search and track system
overheated.
Possible loss of cooling air or a high
JTIDS transmit duty cycle.
Select IPF RESET on JTIDS control panel.
Secure system.
Secure system.
cIIzz.2
With RIO CANOPY light, canopy *I. Canopy - BOOST CLOSE.
LADI unlocked. ‘2. EJECT CMD - PILOT.
CANOPY 3. Airspeed and altitude - Below 200
Knots/15.000 Feet.
4. Seats and visors - DOWN.
5. If canopy has departed aircraft, perform
controllability check.
m
LADI
CANOPY
LAUNCH
BAR
(Ground)
LAUNCH
BAR
(Flight)
Without RIO CANOPY light, ladder
not stowed.
Launch bar unlocked, engines less
than MIL thrust.
Launch bar not locked in up position
or cocked nosegear.
6. Land as soon as possible.
1. Airspeed minimum.
2. Obtain in-flight visual check if possible.
3. Land as soon as practicable.
As appropriate.
1. Landing gear - Leave Down.
2. Obtain visual inspection.
If nosegear cocked, refer to Landing Gear
Malfunction guide.
If launch bar down or visual inspect/on not
available:
3. Request removal of arresting cables for
Reid landing.
L LO THR
R LO THR
WW
4. Request removal of cmssdeck pendants
I and 4 for CV landing.
Designated engine may be producing If associated with RATS check, monitor englnr
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F-14D 飞行手册 Flight Manual 2(90)
