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The 5-kVA emergency generator will automatically activate
and power the essential ac and dc No. 1 and No.
2 and AFCS buses. See Figure 14-6 for listing of inoperable
dc-powered equipment.
14.7.4 TRANSIRECT Light. The TRANSIRECT
light will illuminate if either or both T/R malfunction. If
one T/R fails, the operating T/R will assume the dc load.
If both TiRs fail, the emergency generator will go on the
line and tie to essential dc buses No. 1 and No. 2. Land
as soon as practicable.
Popped circuit breakers should not be reset more !han
once or be held depressedu nless the associatede quipment
is absolutely an operational necessity. A popped
circuit breaker indicates an equipment malfunction or
an overload condition. Repeated resets or forced depressions
ofpopped circuit breakers can result in equipment
damage and/or serious electrical tire.
The losso f oneg eneratora nd failure to tie the acm ain
buses will illuminate the affected GEN light. The
TRANYRECT light will also illuminate bccausc the
affected generator’s associated T/R is not receiving ac
power to convert. Upon observing a TRANWXECT
light, the pilot can check that the aircrafl is actually
experiencing a T/R failure and not a bus tie failure. If
the seat adjust, white floods, or instrument lights are still
operative with the R GEN light illuminated, the bus is
tied. If the throttles are operating on the boosted mode
with a L GEN light illuminated, the bus is tied.
If the hydraulict ransferp ump is operatinga ndp ressure
dropst ob ehvecn2 ,000a nd 1,100p si (dependenutp ont he
load placed on the generator),t he emergencyg enerator
will automatically shift to the 1 -kVA mode andpoweronly
the csscntial ac and dc No. 1 bttscs. If combined hydraulic
pressures ubsequentlyr ecovers,t he EMERG generator
switch must be cycled through OFF/RESET to NORM to
regaint he essentiaal c and dc No. 2 and AFCS buses.
14.7.5 Electrical Fire. Electrical tires may be indicated
by visual or audible arcing or an ozone odor in the
cockpit and popping circuit breakers. Electrical tires
produced by 400 “F air leaks can result in any one or
combination of the following:
1. Pinballing caution/advisory lights and instrument
indications.
2. CADC associated caution/advisory lights.
3. Uncommanded movement of electrically controlled
components (SAS, spoilers, wing sweep,
throttles).
4. Complete electrical failure.
5. Smoke, fumes, and/or heat in the cockpit.
The most effective method to extinguish an electrical
fire is to secure all electrical power. However, some
conditions may not permit securing the emergency generatora
fter both main generatorsa re securedN. ight/IFR
flight or ECS-duck-leak-induced electrical fires are
cases where securing all electrical power is not feasible.
NAVAIR Ol-F14AAD-1
ACM LIGHT EMERGENCY GENERATOR MULTI-FUNCTIONAL DISPLAYS
AIRBORNE SELF-PROTECTION COOLING 2AND3
JAMMER FLIGHT HYDRAUUC BACKUP NFO CONSOLE LIGHT
AIR SOURCE CONTROL GROUND POWER COOLING OUTBOARD SPOILER
ALE-39 CHAFF/FLARE INTERLOCK CONTROL AND PUMP
ALR-67 GROUND TEST POSITION LIGHTS
AMC BlT GUN POWER RADAR COMPONENTS
ANIAWW-I HUD CAMERA RECONNAISSANCE
ANNUNCIATOR PANEL DIM HV POWER SUPPLY EQUIPMENT
CONTROL IFF AIR-TO-AIR RIGHT MAIN TRANSFORMER
ANTENNA LOCK INS BAllERY POWER RECTIFIER
ANTENNA HYDRAULIC SERVO INTERFERENCE BLANKER RIGHT DC TEST
INTEGRATED TRIM SAHRS
ANTI-COLLISION LIGHT INlERRUFllON FREE DC BUS SEAT ADJUST
ASW 27 IRST SOLENOID POWER SUPPLY
AUTO THROTTLE JTlDS DATA PROCESSOR AND
BEAM PS
STATION 1.1 A, AND B AIM-9
BATTERY HEATER
BOL CHAFF DISPENSERS
COOLING POWER
BRAKE ACCUMULATOR
LEFT/RIGHT AICS HEATER STATION 1, 3, 4, 56, AND 8
SHUTOFF VALVE
LEFT MAIN DECODER RELAY POWER
COUNTING ACCELERATOR
TRANSFORMEWRECTlFlER STEADY POSITION LIGHTS
DATA LINK LIQUID COOUNG STORES MANAGEMENT
DATA PROCESSORS MASTER ARM PROCESSOR
DATA STORAGE SET MASTER TEST STORM FLOOD LIGHTS
DEHYDRATOR MISSILE POWER RELAY UNlT SUPPLEMENTAL POSITION
DEU MISSION COMPUTER NO. 1 LIGHTS
DIGITAL DISPLAY ENABLE
ELECTRICAL COOLING
MONlTOR BUS CONTROL TELEVISION CAMERA SET
MULTI-FILTER ASSEMBLY
Figure 14-6. Failure of Both Transformer-Rectifiers Equipment Inoperative List
*l. L and R generators-OFF.
Note
OBOGS concentrator heater power will be
lost. OBOGS may still function at a reduced
but adequatele vel.
If associatedw ith any other direct or indirect indication
of ECS malfunction, perform ECS Leak/Elimination of
Smoke and Fumes procedure, paragraph 14.8.1
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F-14D 飞行手册 Flight Manual 2(110)
