Page 308 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.10.5.5 ECBU 5 FAIL*
ACAWS
Condition:

The ECBU has failed or lost bus communication with the MC. GROUND

Q1 ARE MULTIPLE ACAWS DISPLAYED? TAKEOFF

NO
Conventional failure: All ECBs lose power and multiple failures FIRE/SMK
NORM Lost DUH HYLGHQW RQ WKH ÀLJKW GHFN 7KH $&$:6 DVVRFLDWHG ZLWK D
conventional failure are:
Bus PRES/OXY
Comm ‡ GEN 3 FAIL (C)
failure ‡ P HUD FAIL (C)
ENG/PROP
‡ NORM BRAKES FAIL (C) (if selected on)

NOTE FUEL
ACAWS is not valid, system is functional.
AAR
‡ EMER BRAKES FAIL (C) (if selected on)
SPEC ‡ NOT FOR FLIGHT ELEC

NOTE
ACAWS is not valid, system is functional.
HYD

‡ PUSHER OFF (C)
‡ GCAS FAIL (A) FLT CTRL

‡ TCAS FAIL (A)
‡ DIGITAL MAP FAIL (A) GEAR

P CNI-MU FAIL (A)
‡ CNI SP 1 FAIL (A) DOR/RMP
PERF ‡ VOR/ILS 1 FAIL (A)

JETTISON
‡ ADC 2 DEGRADED (A)

‡ RAD ALT 1 FAIL (A)
LANDING
A. Performance data.................................................. Review

Determine takeoff/landing distance for anti-skid DITCHING
inoperative.

B. Brakes........................................................ Use cautiously
BAILOUT
Anti-skid protection may not be available.
OPER FAULT LG

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governed by the statement on the
BACK title page of this document. CHARTS