Page 138 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.2.3 ADVISORIES B
ACAWS
Alert/Condition Crew Action
FUS TK FLCV FAIL CLSD C GROUND
The fuselage tank FLCV has FUS TK FLCV PRI ECB (919).... PULL
failed in the closed position. It D
is not possible to transfer any FUS TK FLCV SEC ECB (488)... PULL
more fuel into the fuselage tank Do not turn the pump on or close TAKEOFF
through the FLCV. the ECBs until proper inspection E
and repairs have been performed. FIRE/SMK
NORM Fuselage tank TO switch........... CLSD F

Fuel for aerial refueling.........................
.........................Select alternate supply G PRES/OXY
NOT FOR FLIGHT
Fuel may be slowly transferred
(approximately 60 gpm) into H ENG/PROP
the fuselage tank through
KDOI LQFK RUL¿FHV LQ WKH DHULDO
refueling pump check valves I
by pressurizing the cross- FUEL
ship manifold and opening an
interconnect valve. Monitor the L
fuselage tank quantity closely AAR
and limit it to 18,500 pounds
maximum. M
SPEC FUS TK PRI SOL FAIL ELEC

The primary solenoid of the No crew action required. N
fuselage tank FLCV has failed
and secondary solenoid is HYD
functioning. O
FUS TK QTY ERROR FLT CTRL
The fuselage tank fuel quantity TECU ECB (449).......... PULL, RESET P
indication is erroneous because
of invalid TECU calibration If the ACAWS does not clear:
constants. REFUEL CONTROL panel fuselage R GEAR
tank quantity......................... Disregard

Total usable fuel................ Recalculate S DOR/RMP
PERF FUS TK QTY FAIL

The fuselage tank fuel quantity Manually track the fuselage tank fuel T JETTISON
indication has failed. quantity based on the last known
value.
FUS TK SEC SOL FAIL U LANDING

The secondary solenoid of the No crew action required.
fuselage tank FLCV has failed V
and the primary solenoid is DITCHING
functioning.
W
BAILOUT
X

OPER FAULT LG

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