Page 64 - (KU)01-75GAJ-1.5 - Change 1

INTRO

EP'S (KU)01-75GAJ-1.5 A FIGURES

1.2.2 CAUTIONS B
ACAWS
Alert/Condition Crew Action
IRCM FAIL C GROUND
The IR jammer has CNI-MU IRCM PWR..................... OFF
experienced a failure. D
0LVVLRQ SUR¿OH 5HYLHZ
ISO DC BUS OFF* E TAKEOFF

Isolated dc bus voltage is less Fault Log.................................. Review
than 12 volts and the BTRY FIRE/SMK
NORM switch is ON or the Essential F
dc bus is not off.
L AC BUS OFF* G PRES/OXY
NOT FOR FLIGHT
Left ac bus is not being GENERATOR switch (No. 1)........... Off
powered and power is If the ACAWS does not clear:
available. H ENG/PROP
GENERATOR switch (No.1)..................
..................................... Do not turn ON
Fault Log.................................. Review I FUEL
L AUX XFER PMP FAIL
The pressure switch senses CROSS FEED switches (all)........ CLSD L
less than 23 psig, the L AUX AAR
transfer FROM switch is on, CROSS SHIP switch.................... Open
there is more than 100 pounds Transfer FROM switches (all except L M
SPEC of fuel indicated in the tank, AUX)............................................... OFF ELEC
and fuel is not being de-fueled,
transferred (to tanks or AR pod) Transfer TO switches................... CLSD N
or dumped.
Pump pressure............................. Verify HYD
OR O
If pump pressure is less than 23 psi:
The L AUX transfer FROM L AUX transfer FROM switch......... OFF
switch is on, there is more than P FLT CTRL
100 pounds of fuel indicated in L AUX XFER PUMP ECB (239).... PULL
the tank, fuel is being defueled,
transferred (to tanks or AR Do not turn the pump on or reset R GEAR
pod) or dumped and the FMC the ECB until proper inspection and
detects low pump electrical repairs have been performed.
current.
Set up another fuel supply, as required. S DOR/RMP
PERF Total usable fuel.................. Recalculate

The fuel in the L AUX tank is T JETTISON
unusable.
If the ACAWS clears or pump pressure U
is greater than or equal to 23 psi: LANDING
Continue pump operation. V
L AV DATA BUS FAIL* DITCHING
Both channels of the data bus L AV DATA BUS FAIL* procedure........... W
have failed. Failure will be ............................................ Accomplish
preceded by an MC failure. BAILOUT
Normal landing gear extension X
is inoperative.
OPER FAULT LG

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