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less than expected thrust. gauges and FEMS engine data for nomtal rpm
FF, and temperatures. If no anomalies
message is false alarm triggered by the hook
If not associated with a RATS check, recon
FEMS data and abort.
\\\\~~~~~~~-~-~rr---------------------
NAVAIR Ol-F14AAD-1
Warning, Caution, Advisory Lights/Displays (Sheet 9 of 15)
78
WARNING/CAUTION/ADV~SORY LlGHTS/DlSPLAY LEGENDS
1J GHTILEGEND CAUSE ACTION
LOCK Radar locked on target. Pilot option.
L MACH # Mach number signal to designated
R MACH # engine has failed.
In flight - Remain below 1 .I TNM. Small
throttle reductions below MIL at high Mach
WV
can result in engine stall.
On deck - Assess operational Impact of
speed restriction for mission.
MACH TRIM Failure of Mach trim actuator to follow 1. MASTER RESET.
program.
WW
2. Retrim manually.
MASTER
i
Actuated by any caution light on Push to reset after discrete MSG noted.
CAUTION
caution panel.
MC1
a MC2
Improper operation of mission
computer.
Backup operation selected automatically.
M-7
MC1 HOT
m
Mission computer overheated. Backup operation selected automatically.
MC2 HOT
WFD)
L Nl OSP
a
Engine fan rpm exceeds 106 percent. 1. Throttle - IDLE.
Fl Nl OSP Check rpm gauge for N2 and FEMS
engine data on MFD for Nf to
WFD)
determine validity of overspeed
message.
If overspeed continues:
2. ENG MODE SELECT - SEC.
If ovwspeed condition persists:
3. Throttle - OFF.
4. Refer to Single-Engine Cruise
Operations.
Engine core rpm exceeds 107.7
m percent.
WW
5. Land as soon as practicable.
1. Throttle - IDLE.
Check rpm gauge for N2 and FEMS
engine data on MFD for Nt to determine
validity of overspeed message.
If overspeed continues
2. ENG MODE SELECT - SEC.
If overspeed condition persists:
3. Throttle - OFF.
4. Refer to Single-Engine Cruise Operations.
5. Land as soon as practicable.
Warning, Caution, Advisoty Lights/Displays (Sheet 10 of 15)
WARNING/CAUTION/ADVISORY LIGHTS/DISPLAY LEGENDS
a
Nosewheel steering is engaged. Disengage when approprtate.
NWS
ENGAGE
Engine oil temperature limits
&i-iJtJ tempemt”m,
exceeded or high scavenge oil
On deck:
1. Throttle - OFF.
In flight:
1. Oil pressure - Check.
2. Throttle - 85parcantrpm.
3. If after 1 minute, light still Illuminated
- Throttle OFF.
4. Land as soon as practicable.
5. Refer to SingleEngine Cruise Operations.
6. Relight engine for landing if necessary.
UR OIL LO Designated engine oil level Is Alert ground personnel: servtclng required.
approximately 2 quarts low Postflight. :
WD) engine at idle.
B
L or R oil press <I 1 psi. 1. Throttle (affected englne) 7 IDLE.
If oil pressure below 15 psi, above 65 psi. or
engine vlbtation:
If shutdown feasible:
2. Throttle (affected engine) - OFF.
3. Refer to SIngleEngine Crulsa Operation
(Chapter 14).
If shutdown not feasible:
2. RPM - Set Minimum Rpm.
3. Avokl high-g or large throttle movements.
4. Land as soon as practicable.
m Low percent oxygen. 1. BACKUP OXY PRESS - Check.
Channel 1 or 2 inoperative. If single pitch or roll stab Ilght:
1. MASTER RESET - Depress.
2. If light remains lllumlnatad -
No Limitations.
If both pitch or roll stab lights:
I. All-speed - Reduce to Stab Limits.
2. Pitch - Not Restricted.
3. Roll - 1.6 TMN.
4. Wait IO seconds for self-test.
5. PITCH CMPTR AC cb or ROLL CMPTR AC
ob - Cycle (LA1 or LBi).
6. Recheck lights.
Warning, Caution, Advboty Lights/Displays (Sheet 11 of 15)
ORIGINAL
NAVAIR 0%F14AAD-1
1 LIGHT/LEGEND 1 CAUSE
WARNING/CAUTION/ADVISORY LIGHTS/DISPLAY LEGENDS
I
ACTION
Computer/mechanical malfunction or I
ramp misposittoning.
Refer to INLET light.
RATS RATS operation enabled.
RCV ALG-165 is receiving threat
identification signal.
Flaps fail down, airspeed 225 knots;
total temperature 388 ‘F, 2.4 M
(HUDNFD)
RDP FAN Radar data processor fan failure.
Radar operation on ground is possible. I
a
I RDR HOT Radar system overheated.
WW
Warning or caution message(s) being
displayed on MFD.
I m Channel 1 or 2 inoperative. I
1. Tailhook - DOWN.
ff conditions permit
2. ANTI ICE CONTR HOOK CONT/
WSHLDIAIR cb - Pull (8C2).
14 s briefed.
1. Reduce speed.
2. Check FLAP handle.
3. MASTER RESET.
　
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