Page 329 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

‡ Booster hydraulic system aileron/elevator/rudder control boost
shutoff valves will remain as-is; CONTROL BOOST,BOOST ACAWS
switches not functional.

NOTE GROUND

Flight control boost shutoff valve AIL/ELEV/RUD UTIL
SWITCH OFF (C) ACAWS indicate switch position only. TAKEOFF
G. Fault Log.............................................................................. Review

AIL/ELEV/RUD SOV-BOOSTER FIRE/SMK
NORM AIL/ELEV/RUD TAB POSN XMTR, AUX HYD PRESS SENS

CGO DOME/FLOOR LTS, CVR, FUEL DRAIN PWR PRES/OXY
NOT FOR FLIGHT
FUEL LEVEL CNTL VLVS, FUEL MGMT CNTL B
HF 1 DC, IFF 2, IRCM CNTL, R AUX XFER PUMP ENG/PROP
R EXT TK FWD PMP, RWS, SPR/XSHIP VLVS, STICK PUSHER
TK 1 BOOST PUMP, TK 1/2/3/4 XFEED VLVS, TK 3 XFER PUMP
POD/HOSE ILLUM LTS, FORM SIG RLY FUEL

(End of Procedure) AAR
1.10.5.13 ECBU 13 FAIL*
SPEC Condition: ELEC

ECBU 13 has failed or lost bus communication with the MC.
HYD

Q1 ARE MULTIPLE ACAWS DISPLAYED?
FLT CTRL

NO Conventional failure: All ECBs lose power and multiple failures
DUH HYLGHQW RQ WKH ÀLJKW GHFN 7KH $&$:6 DVVRFLDWHG ZLWK D GEAR
Lost conventional failure are:
Bus
Com ‡ TECU FAIL (C) DOR/RMP
PERF failure ‡ DE-ICE TIMER CH 2 FAIL (A)

‡ TACAN 2 FAIL (A) JETTISON

‡ IFF 1 FAIL (A)
‡ UHF 2 FAIL (A) LANDING

A. Stick pusher..................................... Select PUSHER OFF
Stick pusher failed. DITCHING
B. Potential Mission Impacts...................................... Review

‡ TACAN 2, all secure, and IFF No. 1 failed. BAILOUT
‡ CMDS programmer inoperative. Use CMDS BYPASS
OPER mode. FAULT LG

Use, copying and/or disclosure is 1 -289
governed by the statement on the
title page of this document. BACK CHARTS