Page 358 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

‡ As-is Components (components which will continue to operate
in their current state, but will not respond to control/switch panel ACAWS
operation):
HF 1 and 2 GROUND
‡ Landing gear aural alert cannot be silenced when gear is down
DQG SRZHU OHYHUV DUH QHDU ÀLJKW LGOH
H. Fault Log.................................................................................. None TAKEOFF

NOTE
FIRE/SMK
NORM There is no fault log for this failure mode.

For additional information on Potential Mission Impacts: PRES/OXY
NOT FOR FLIGHT
I. BIU #1 FAIL* (Lost Comm).................................................... Review

J. BIU #2 FAIL* (Lost Comm).................................................... Review ENG/PROP

(End of Procedure)
FUEL

1.10.7.4 L DSPLY DATA BUS FAIL*
AAR
Condition:
SPEC Both channels of the data bus have failed. Failure will be preceded by ELEC
an MC failure.

Associated ACAWS: HYD

‡ MC 1 (or 2) FAIL (C)
‡ ADC 1 ALTITUDE FAIL (C) FLT CTRL
‡ ADC 1 AIRSPEED FAIL (C)

‡ TCAS FAULT (A) GEAR
‡ IFF 1 ALT FAIL (A)
‡ GCAS FAIL (A) DOR/RMP
PERF ‡ ADC 1 VVI FAIL (A)

A. Pilot attitude source....................................... Select ATT REF INU 2 JETTISON

Recovers pilot attitude reference.

B. Pilot air data source..................................................... Select ADC 2 LANDING
C. Autopilot........................................................................... Disengage
DITCHING
Copilot servo will disengage after one minute with no annunciation.
AP ON annunciators will erroneously indicate engaged.
BAILOUT
D. Brakes....................................................................... Use cautiously

OPER Anti-skid protection may not be available. FAULT LG

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