Page 311 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

FLT STN CB LTS
DIGITAL MAP ACAWS
CHUTE RELEASE, SPTU 1, CP PITOT HEAT 4
EXT MASS MEM UNIT GROUND
R POD E-TRAIL/R-TEST
R POD TRAIL
TAKEOFF
(End of Procedure)

1.10.5.6 ECBU 6 FAIL* FIRE/SMK
NORM Condition:

The ECBU has failed or lost bus communication with the MC. PRES/OXY

Q1 ARE MULTIPLE ACAWS DISPLAYED? ENG/PROP

NO Conventional failure: All ECBs lose power and multiple failures FUEL
DUH HYLGHQW RQ WKH ÀLJKW GHFN 7KH $&$:6 DVVRFLDWHG ZLWK D
Lost conventional failure are:
Bus AAR
Comm ‡ RADAR FAIL (C)
‡
INU 1 FAIL (C)
SPEC failure NOT FOR FLIGHT ELEC
‡ CP AP FAIL (C)
‡ CP HUD FAIL (C)
HYD
‡ GCAS FAIL (C)
‡ GEN 4 FAIL (C)
FLT CTRL
‡ CAB ALT HIGH (C)

NOTE
GEAR
ACAWS is not valid, system is functional.

‡ TCAS FAULT (A) DOR/RMP
PERF ‡ RADALT 2 FAIL (A)

‡ HF 2 FAIL (A) JETTISON
‡ CNI SP 2 FAIL (A)
‡ VOR/ILS 2 FAIL (A)
LANDING
A. Pilot attitude source........................ Select ATT REF INU 2
Recovers pilot autopilot and GCAS.
DITCHING
B. CNI-MU NAV CTRL.......................................................Set
Select INS No. 2 for INAV 1 sensor on CNI- BAILOUT
MU INAV CTRL SENSORS page 2 of 3. Then
reselect desired solution for INAV 1 on page 1
OPER of 3. FAULT LG

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