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INTRO
EP'S (KU)01-75GAJ-1.5 FIGURES
Lost
Bus procedures. Use caution when dumping to avoid large
Com fuel imbalances. ACAWS
failure UTIL and BSTR RUD PRESS HI/LO (C) ACAWS and
system status page pressure indications inoperative.
Flap position indicator inoperative. Visually verify GROUND
ÀDS SRVLWLRQ ZKHQ H[WHQGLQJ DQG UHWUDFWLQJ 5XGGHU
HI/LO boost control should function normally. The
pressure gauge on the rudder booster panel assembly TAKEOFF
at approximately FUS STA 1023 can be used to verify
booster pressure.
FIRE/SMK
NORM Auxiliary hydraulic pump and pressure indications
failed. Emergency brakes will fail after accumulator is
discharged. Recharge accumulator using manual hand PRES/OXY
pump and direct reading pressure sight gauge.
Utility hydraulic system aileron/elevator/rudder control ENG/PROP
boost shutoff valves failed open.
GPS 2 unavailable because of antenna electronics
power failure. No GPS functionality with EGI 2. FUEL
Electronic control of chute release inoperative.
$LU GHÀHFWRUV IDLO LQ FXUUHQW SRVLWLRQ FDQQRW H[WHQG AAR
retract. Monitor airspeed if extended.
Exterior lighting degraded: Upper strobe, covert
SPEC NOT FOR FLIGHT ELEC
anticollision light, loading lights, pod/hose illumination
lights and main landing gear wheel-well inspection lights
failed.
HYD
UHF DF unusable.
HF 2 inoperative.
FLT CTRL
F. BAU II #3 FAIL*....................................................... Review
G. Fault Log................................................................ Review GEAR
ADS CNTL, AIL/ELEV/RUD SOV-UTIL
AIR DEFLECT-EXT/RETR DOR/RMP
PERF AUX HYD PMP RELAY, BAU II #3
CGO RAMP/DOOR-OPEN/CLOSE, FLT DATA RECORDER JETTISON
FUEL MGMT CNTL A, HF 2 DC PWR
L AUX XFER PMP, L EXT TK FWD PMP, LOADING LTS
MAIN GEAR WELL LTS LANDING
RUD BSTR/UTIL HYD PRESS SENS, STICK PUSHER
TK 2 BOOST PMP, TK 4 XFER PUMP, TOP STROBE DITCHING
UHF/DF ANT SEL SW, WING FLAP POSN SENS
(End of Procedure) BAILOUT
Lost Bus Comm failure: If communications have failed, most ECBs stay
OPER in their last state. FAULT LG
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