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If an OIL HOT caution is set, the parameter
which triggered the caution should be highlighted in
red on the ENG format. If AMAD OIL TEMP is
high, securing the GEN (ac output) greatly reduces
the heat load imparted to the AMAD oil and may
prevent heat-related damage to the generator. If an
OIL HOT caution was caused by extended ground
operations with OAT greater than 103°F, increasing
the affected engine rpm should clear the caution
within 20 seconds (normal operating system).
Prolonged operation of a hot AMAD may result in
an engine bay fire.
GROUND
1. Throttle affected engine - INCREASE RPM
TO 74%
2. ENG format - Identify out of limit parameter.
If caution removed in 20 seconds -
3. Continue mission, monitoring OIL TEMPs
until airborne.
If caution remains -
3. Throttle affected engine - OFF
INFLIGHT
*1. Throttle affected engine - IDLE
If caution removed -
2. Land as soon as practical.
If caution remains at IDLE -
2. ENG format - Identify out of limit parameter.
If AMAD OIL TEMP hot -
3. GEN switch affected side - OFF
If more than 5 minutes to landing -
4. Throttle affected engine - OFF
5. Restart for landing.
POST-FLIGHT
If caution on for more than 5 minutes -
1. Throttle affected engine - OFF
L OIL PR
R OIL PR
²Engine left (right),
Engine left (right)²
· Designated engine oil pressure out of limits.
Zero oil pressure without the L/R OIL PR caution
indicates the oil pressure transmitter has failed
and the oil pressure switch is detecting oil pressure
greater than 35 psi. Flight may be continued.
*1. Throttle affected engine - IDLE
If caution still on after 10 seconds -
2. Throttle affected engine - OFF
3. Restart for landing.
ONBD JAM DEGD · ALE-50 has detected a failure during a periodic
BIT. Information
ONBD JAM HI B · Failure of high band function of ALE-50. Information
ONBD JAM LO B · Failure of low band function of ALE-50. Information
ONBD JAM OVRHT · ALE-50 overheat. 1. JAMMER switch - OFF (if practical)
L OVRSPD
R OVRSPD
²Engine left (right),
Engine left (right)²
· Designated fan or compressor rpm high. *1. Throttle affected engine - IDLE
2. Land as soon as practical.
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 25 of 55)
V-12-27 ORIGINAL
DDI Cautions and Caution Lights
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
PARK BRAKE
· Parking brake still set when throttles are advanced.
The caution is set when both throttles are advanced
past 27° THA if the PARK BRK handle is
set and the INS is on.
Even if PARK BRAKE caution is extinguished inflight,
the possibility exists that the parking brake
may still be engaged.
GROUND
1. PARK BRK handle - RELEASE
INFLIGHT
1. PARK BRK handle - CYCLE AND CHECK
FULLY STOWED
Whether or not the caution clears -
2. Make a fly-in arrested landing.
L PITOT HT
R PITOT HT
· Designated pitot tube, AOA probe, or AOA probe
cover heater malfunction.
If displayed immediately after takeoff, the caution
may also be an indication of a WonW proximity
switch failure on the corresponding side.
1. PITOT ANTI ICE switch - ON
After landing -
2. PITOT ANTI ICE switch - AUTO
POS/ADC
· INS velocities unreliable.
Position keeping supplied by the air data function.
POS/ADC is not as reliable a position keeping
source as the INS or GPS.
1. Position keeping - SELECT POS/TCN
PROBE UNLK · Air refueling probe not fully retracted with
PROBE switch in RETRACT.
1. Airspeed - Maintain below 300 KCAS.
2. PROBE switch - CYCLE
R-LIM OFF · Roll rate limiting failed. 1. Use no more than ½ lateral stick with tanks or
A/G stores on the wings.
RACK UNCPL · BRU-32 rack(s) failed to lock or unlock during
rack test. 1. Do not takeoff.
FIRE EXTGH
READY
Light
· Fire extinguisher bottle armed. (FIRE light or
APU FIRE light depressed.)
If FIRE light unintentionally depressed -
1. Identify affected light.
2. FIRE light - RESET
REFUEL DR · Ground refueling door not properly secured.
(Only activated with WonW.)
1. Ensure ground crew secure door prior to takeoff.
If caution remains -
2. Do not takeoff.
RIG · Flight controls out of rig.
(Only activated with WonW.) 1. Do not takeoff.
S/W CONFIG
· Software incompatible and/or engine FADEC
software mismatched.
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 2(30)