Page 353 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1,8 &200 5$'$/7
BAECS A, FODS A, FMC A, DITU A, CPC A ACAWS
):' &*2 ,&6 &17/ 31/ (*, $77 +'*
BAU II #1 COMM GROUND
ECBU 7/8/13 COMM
For additional information on Potential Mission Impacts:
TAKEOFF
M. BAU II #1 FAIL* (Lost Comm).............................................. Review

N. ECBU 8 FAIL* (Lost Comm)................................................. Review FIRE/SMK
NORM O. ECBU 13 FAIL* (Lost Comm)............................................... Review

PRES/OXY
NOT FOR FLIGHT
(End of Procedure)

1.10.7.2 R AV DATA BUS FAIL* ENG/PROP
Condition:

Both channels of the data bus have failed. Failure will be preceded by FUEL
an MC failure.
Associated ACAWS: AAR
‡ MC 1 (or 2) FAIL (C)

SPEC ‡ NIU 2 FAIL (C) ELEC
‡ NIU 3 FAIL (C)
‡ INU 2 FAIL (C)
HYD
‡ ATCS DEGRADED (C)

‡ ANTI-SKID FAIL (C) (when gear is down)
FLT CTRL
NOTE

If gear was up or anti-skid was off at time of bus failure GEAR
(ACAWS inhibited when gear is up).

A. FADEC (No. 2 and No. 3)................................................ Select ALT DOR/RMP
PERF Restores proper ATCS operation and HP, MGT, NG and NP
indications.
JETTISON
B. Copilot attitude source.................................. Select ATT REF INU 1

Recovers copilot attitude reference and autopilot. LANDING

C. Copilot RAD ALT source...................................... Select RAD ALT 1
DITCHING
Restores TCAS and GCAS.

D. Icing conditions..................................................... Avoid, if practical BAILOUT

A failure of the primary vertical tail boot de-icing timer may not be
OPER reported. FAULT LG

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