Page 139 - (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
FUSELAGE TK EMPTY C GROUND
The fuselage tank fuel quantity Fuel.......................................................
readings are valid, the fuselage ....Select alternate supply (as required) D
tank fuel quantity is less than
100 pounds, and the fuselage TAKEOFF
tank manifold pressure is less E
than 23 psi. FIRE/SMK
NORM OR F
The fuselage tank quantity
readings are invalid and G PRES/OXY
NOT FOR FLIGHT
the fuselage tank manifold
pressure is less than 23 psi.
FWD AR PUMP FAIL H ENG/PROP

The fuselage tank forward air FWD AR PUMP START ECB (504)......
refueling pump has failed. Aerial .................................................... PULL I
refueling may still be conducted, FUEL
EXW ÀRZ PD\ EH UHGXFHG FWD AR PUMP switch ................ OFF
Do not turn the pump on or reset L
the ECB until proper inspection AAR
and repairs have been performed. M
SPEC FWD CGO HIU FAIL ELEC
The BIT has detected a fault in Use a different HIU.
the forward cargo HIU. N
FWD CGO ICS CNTL PNL FAIL HYD
MC has lost communication Use a different ICS CONTROL panel. O
with the forward cargo ICS
CONTROL panel. FLT CTRL
FWD CGO ICS CNTL PNL FAULT P
MC has detected an invalid Use a different ICS CONTROL panel, GEAR
switch/knob/etc. input from the as required. R
forward cargo ICS CONTROL
panel.
GCAS FAIL S DOR/RMP
PERF The BIT has detected a GCAS On the ground:

software fault. T JETTISON
Current altimeter............................. Set
If the ACAWS does not clear:
U
0DLQWHQDQFH UHTXLUHG EHIRUH ÀLJKW LANDING
,Q ÀLJKW V
The system automatically shuts off. DITCHING
Source systems.......... Verify operation W

GCAS............................................. ON BAILOUT
X

OPER FAULT LG

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