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