Page 313 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

H. Potential Mission Impacts..................................................... Review
ACAWS
‡ Generator No. 4 will remain as-is; control not functional.

NOTE
GROUND
GEN 4 OFF (A) ACAWS only indicates GEN switch
position. Verify condition on system status page.
TAKEOFF
I. Fault Log............................................................................... Review

MC 2 AC, BIU #2 AC, CNI-SP 2, EGI 1, VOR/ILS 2 FIRE/SMK
NORM RAD ALT 2, HF 2, RADAR, CP HUD
GBE RELAY 1B/2B, BRAKE SEL VLV-NORM
CP AUTOPILOT, GEN 4 PRES/OXY
NOSE GEAR WELL LTS
LAPES/CDS ARM, L STAT LINE RETRVR ENG/PROP
SENSORS:
AV COOLING AIR DUCT TEMP
DSPLY COOLING AIR OUTLET DUCT TEMP FUEL
CABIN PRESSURE
AV COOLING AIR DUCT PRESS

(End of Procedure) AAR

SPEC NOT FOR FLIGHT ELEC
1.10.5.7 ECBU 7 FAIL*

Condition: HYD

The ECBU has failed or lost bus communication with the MC.
FLT CTRL
Q1 ARE MULTIPLE ACAWS DISPLAYED?

GEAR
NO Conventional failure: All ECBs lose power and multiple failures
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Lost conventional failure are: DOR/RMP
PERF Bus

Comm ‡ P AUTOPILOT FAIL (C) JETTISON
failure ‡ INU 2 FAIL (C)

‡ APU GEN FAIL (C) (if operating)
LANDING
A. Copilot attitude source.................... Select ATT REF INU 1

Recovers copilot attitude reference and autopilot.
DITCHING
B. CNI-MU NAV CTRL.......................................................Set
Select INS No. 1 for INAV 2 sensor on page 2 of BAILOUT
3. Then reselect desired solution for INAV 2 on
page 1 of 3.
OPER FAULT LG

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