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If the light goes off with the switch in TEST, the
fault is in the respective electrical distribution system.
If light remains illuminated, the generatorh as
beend isconnecteda utomatically and the fault is in
IDG or generator control unit.
14.7.1.2 L or R GEN and TRANWRECT Lights
1. Generator (affected generator switch) - OFF/
RESET, Then NORM.
2. If L GEN and TRANS/RECT lights remain illuminated,
select EMERG GEN on MASTER TEST
panel.
Note
With R GEN and TRANS/RECT lights illuminated,
ac essential power is supplied by
the L GEN. Selecting EMER GEN on the
MASTER TEST panel (with R GEN and
TRANSlRECT lights) will not provide any
additional power but may cause an interrupt
as the supply is transferred from the L GEN
to the EMER GEN.
3. Land as soon as practicable.
14.7.2 Double Generator Failure
1. Both generator switches-Cycle.
If operating on emergency generator, the following important
systems are inoperative:
1. Emergency flight hydraulics
2. Outboard spoiler module and emergency flap
activation
3. OBOGS concentrator heater (OBOGS may still
function at a reducedb ut adequatele vel).
If temporary loss of combined system pressure causes
emergency generator to shift to 1 kVA mode (to drop
No. 2 essential bus):
2. EMERG generator switch-Cycle.
3. Land as soon as practicable.
NAVAIR 0%FI4AAD-1
ESSENTIAL BUSES NO. 1 (1 KVA MODE)
AICS RAMP STOW
ANGLE OF ATTACK IND
ALTITUDE LOW WARNING
BACKUP CONTR/B/U OXY LOW
BACKUP IGNITION
BACK UP OXY PRESSURE IND
BAROMETRIC ALTIMETER
CONSOLE LIGHTS (PILOT)
DC ESSENTIAL NO. 1 FEEDER
DC TEST
FIRE EXTINGUISHING
FLOOD LIGHTS
FUEL QUANTITY INDICATOR
HYDRAULIC PRESSURE
INDICATION
ICS
IFWSIF
INSTRUMENT BUS FEEDER
INSTRUMENT LIGHTS
JElTlSON (EMERGENCY)
MAIN LANDING GEAR SAFETY
RADAR ALTIMETER
RUDDER TRIM
STANDBY ATTITUDE
STORE MANAGEMENT
ENGINE INSTRUMENT GROUP
ENGINE INSTRUMENT GROUP
WHITE LIGHTS
ENGINE START
FIRE DETECTION
RELAYS
OBOGS CONTR
OBOGS CONCENTRATOR
PITCH/ROLLTRlM
PROBE LIGHT
PROCESSOR
TAIL/RUDDER/FLAP INDICATOR
TURN AND SLIP INDICATOR
VHF/UHF RADIO 1 8.2
VOICE SECURITY EQUIPMENT
WHEELS POSITION
INDICATIONS
WING POSITION INDICATIONS
AFCS
AFCSBUSFEEDER
AICS
AICS LOCKUP POWER
AIR SOURCE CONTROL
ALPHA COMPUTER
ALPHA HEATER
ANNUNCIATOR PANEL POWER
ANTI-ICE CONTROL
ANTI-ICE PROBE
ANTI-SKID POWER
ARMAMENT GAS
ARRESTING HOOK CONTROL
AUTOMATIC DIRECTION
FINDER
AUXILIARY FLAP/FLAP
CONTROL
BDHI
BINGO POWER
ESSENTIAL BUSES NO. 2
BLEED AIR LIGHT
BLEED DUCT
CABIN PRESSURE
CADC
CANOPY LIGHT
CIU
CURSOR CONTROL
DC ESSENTIAL NO. 2 FEEDER
DEKI LIGHTS
DISPLAY PROCESSORS
ECS TEMPERATURE CONTROL
EJECTION COMMAND
INDICATOR
EMERGENCY GENERATOR TEST
ENGINE AFTC
ENGINE ANTI-ICE
ENGINE ANTI-ICE VALVES
ENGINE OIL COOLING
ENGINE SECONDARY MODE
ENGINE STALL TONE
EXHAUST NOZZLE
EXTERIOR LIGHTS CONTROL
FLAP/SLAT CONTROL SHUTOFF
FLIGHT CONTROL AUTHORITY
FUEL DUMP
FUEL FEED
FUEL MANAGEMENT PANEL
FUEL PRESSURE LIGHT
FUEL TRANSFER OVERRIDE
FUEL VENT VALVE
FUEL LOW LIGHT
GENERATOR LIGHTS
GROUND ROLL BRAKING
INDICATOR
HUD
Figure 14-5. Emergency Generator Distribution (Sheet 1 of 2)
14-21 ORIGINAI
NAVAIR Ol-FI4AAD-I
HYDRAULIC PUMP SPOILER
CONTROL
HYDRAULIC VALVE CONTROL
INBOARD SPOILER CONTROL
INSTRUMENT LANDING
SYSTEMS (ARA-63)
INS
INS SYNCH
JTIDS
LADDER LIGHT
MACH TRIM
MAIN LANDING GEAR RELAYS
MFD NO. 1
MISSILE POWER HUD TEST
MISSION COMPUTER NO. 2
MOTIVE FLOW ISOLATION
NOSE GEAR STRUT LAUNCH
BAR LIGHT
NOSE WHEEL STEERING
OIL HOT LIGHTS
PEDAL SHAKER
PILOT ANNUNCIATOR PANEL
(AUX POWER)
PITCH COMPUTER
PITCH-ROLLTRIM ENABLE
PITOT HEAT
RADAR BEACON
(AN/APN-154)
ROLL COMPUTER
RUDDER TRIM
SENSOR CONTROL
SPEED BRAKES ENABLE
SPOILER INDICATOR
STARTER VALVE LIGHT
TAXI/FORMATION LIGHT
TRANSFORMER/RECTIFIER
LIGHTS
UTILITY LIGHTS
WINDSHIELD AIR
WINDSHIELD DEFOG
CONTROL
YAW SAS POWER SUPPLY
Figure 14-5. Emergency Generator Distribution (Sheet 2 of 2)
14.7.3 Double Transformer-Rectifier Failure.
　
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本文鏈接地址：F-14D 飛行手冊 Flight Manual 2(109)