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I Expect overheat.
?adar POWER switch to STBY (as
applicable).
select STBY.
ti appropriate to displayed massage(s).
7 single pitch or roll stab light:
1. MASTER RESET - Depress.
2. If light remains illuminated - No
Limitations.
f both pitch or roll stab lights:
1. Airspeed - Reduce to Stab Limits.
2. Pitch - Not Restricted.
3. Roll- 1.6TMN.
4. Wait 10 seconds for self-test.
5. PITCH CMPTR AC cb or ROLL CMPTR
AC cb - Cycle (LA1 or LBI).
6. Recheck lights.
Warning, Caution, Advisory Lights/Displays (Sheet 12 of 15)
81 ORIGINAL
WARNING/CAUTION/ADVISORY LIGHTS/DISPLAY LEGENDS
LIGHT/LEGEND CAUSE ACTION
p%FJ
CADC failure or failure of actuator to 1. MASTER RESET - Depress (10
follow schedule. seconds).
2. If light remains illuminated - Above
250 Knots, Restrict Rudder Inputs to <
IO”.
m Improper ALR-67 radar warning As briefed.
receiver operation.
WW
RWR
HOT
ALR-67 overheated. Secure ALR-67.
SAHRS
(1
SAHRS not available. Avoid IFR flight if INS is degraded.
Steady - Tracking radar detected. As briefed.
Flashing - Missile launch detected.
SDU
a
Improper operation of KY-56. As briefed.
ALARM
WW
SENSOR
COND
Overheat or pump loss in radar
coolant loop.
1. RADAR COOLING - OFF.
2. RDR - OFF.
3. APG-71 PUMP PH A, 6, C cb - Pull.
If other conditions exist that may /nd/cate aI;
ECS malfunction, either directly or
indirectly, perform ECS leak/elimination 01
smoke and fumes procedures:
4. Land as soon as practicable.
SHOOT Target meets LAR requirements. As briefed.
SMS HOT Store management system
MD) overheated.
Symmetric spoiler detctor has locked
m down spoilers.
If assoc/ated with abnormal roll andlor yaw:
I. Counter roll with at least I inch of lateral
Stick.
2. Visually check spoiler position/
operation.
Refer to Chapter 14.
Warning, Caution, Advisory Lights/Displays (Sheet 13 of 15)
82
NAVAIR Ol-l=14AAD-1
WARNING/CAUTION/ADVISORY LIGHTS/DISPLAY LEGENDS
LIGHT/LEGEND CAUSE ACTION
START
a
Starter solenoid air valve open after 1. Ensure ENG CRANK - OFF.
VALVE engine start. 2. AIRSOURCE - OFF.
If on deck:
3. Throttle - OFF.
If ainbome:
3. ENG START cb - Pull (RFI).
4. OSOGS - BACKUP.
LSTALL *
0
Engine stall and/or overtemperature. ‘1. Unload aircraft (0.59 to 1 .Og).
R STALL If greater than f. I Mach:
(HUD/MFD) l 2. Both throttles - MIL.
When I. 1 Mach or less:
‘3. Both throttles - Smoothly to IDLE.
Check EGT and FEMS engine data for
TST to determine validity of stall
message.
If EGT above 935 “C and/or engine
response abnormal:
l 4. Throttle (stalled engine) - OFF.
If EGT normal anNor airstart successful:
5. Perform engine operability check.
L TBT OT
m R TBT OT
WW
Turbine blade overtemperature. 1. Throttle - IDLE.
Check EGT gauge and FEMS
engine data on MFD for TBT to
determine validity of overtemperature
message.
If still 0verfamperefui-e:
2. Throttle - OFF.
TRANSIRECT Lack of dc output from either or both
T/R.
1. Generator - OFF/RESET, Then
NORM.
2. If both lights remain illuminated,
select EMERG GEN on MASTER TESl
panel.
3. Land as soon as practicable.
Landing gear not down with flaps down
and either throttle s 85 percent.
Lower gear.
Warning, Caution, Advisory Lights/Displays (Sheet 14 of 15)
AVAIR 0%F14AAD-1
WARNING/CAUTION/ADVISORY LIGHTS/DISPLAY LEGENDS
LIGHT/LEGEND
WW
WING
SWEEP
WSHLD HOT
CAUSE
ailure of both wing-sweep channels OI
pider detent disengaged.
:ailure of one wing-sweep channel.
:enter windshield temperature 300 “F.
%st failure in yaw SAS.
second failure in yaw SAS.
ACTION
\dvisofy light only. no loss of normal
wntfoi:
1. MASTER RESET - Depress.
MING SWEEP light and W/S legend, nc
3utomafic or manual control:
1. Airspeed - Decelerate to 0.9 or Less.
2. Check spider detent engaged.
3. MASTER RESET - Depress.
I WlNG SWEEP //ght and W/S caut/on legenc
Uuminate again:
4. WING SWEEP DRIVE NO.1 and WG
SWP DR NO.2 MANUV FLAP cb -
Pull.
5. Emergency WING SWEEP handle -
Comply With Schedule.
defer to Chapter 14.
Advisory light only:
I. MASTER RESET - Depress.
1. WSHLDAIR - OFF.
ff light remains illuminated:
2. AIRSOURCE - OFF.
3. OBOGS - BACKUP.
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F-14D 飞行手册 Flight Manual 2(92)
