Page 326 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

H. Stick pusher.................................................... Select PUSHER OFF
ACAWS
Stick pusher failed.

I. Potential Mission Impacts...................................................... Review GROUND

‡ Auxiliary hydraulic pump will remain as-is. Pull HYD PUMP AUX
SYS MCB (AFT 245, LWR AC R2 #10), if required.
TAKEOFF
‡ Cargo ramp door electronic control inoperative. Manual control
available with auxiliary hydraulic hand pump.
FIRE/SMK
‡ Utility hydraulic system aileron/elevator/rudder control boost
NORM shutoff valves will remain as-is; CONTROL BOOST,UTIL
switches not functional.
PRES/OXY
NOT FOR FLIGHT

NOTE
ENG/PROP
Flight control boost shutoff valve AIL/ELEV/RUD UTIL
SWITCH OFF (C) ACAWS indicates switch position only.
FUEL
‡ Electronic control of chute release inoperative.
‡ $LU GHÀHFWRUV IDLO LQ FXUUHQW SRVLWLRQ FDQQRW H[WHQG UHWUDFW
Monitor airspeed if extended. AAR
‡ Pod/hose illumination lights will remain as-is.
SPEC ‡ UHF DF unusable. ELEC

J. Fault Log............................................................................... Review
HYD
ADS CNTL, AIL/ELEV/RUD SOV-UTIL
AIR DEFLECT-EXT/RETR
AUX HYD PMP RELAY, BAU II #3 FLT CTRL
CGO RAMP/DOOR-OPEN/CLOSE, FLT DATA RECORDER
FUEL MGMT CNTL A, HF 2 DC PWR GEAR
L AUX XFER PMP, L EXT TK FWD PMP, LOADING LTS
MAIN GEAR WELL LTS
RUD BSTR/UTIL HYD PRESS SENS, STICK PUSHER DOR/RMP
PERF TK 2 BOOST PMP, TK 4 XFER PUMP, TOP STROBE

UHF/DF ANT SEL SW, WING FLAP POSN SENS JETTISON

(End of Procedure) LANDING

1.10.5.12 ECBU 12 FAIL* DITCHING

Condition:
BAILOUT
The ECBU has failed or lost bus communication with the MC.
OPER FAULT LG

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