Page 300 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.10.5.1 ECBU 1 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
Comm ‡ ADC 1 FAIL (C) PRES/OXY
failure ‡ P AMU FAIL (C)
‡ P PITOT HEAT FAIL (C) ENG/PROP

‡ PUSHER OFF (C)
‡ P HUD FAIL (C) FUEL
‡ HDD 1 FAIL (A)
‡ HDD 3 FAIL (A) AAR

‡ CNBP FAIL (A)
IFF 1 ALT FAIL (A)
SPEC ‡ NOT FOR FLIGHT ELEC
‡ IFF 2 ALT FAIL (A)
‡ GCAS FAIL (A)
HYD
‡ BAU I #3 FAIL* (A)
‡ BAU I #5 FAIL* (A)
FLT CTRL
$ 'LVSOD\V 5HFRQ¿JXUH DV UHTXLUHG
HDD 1 and 3 failed.
GEAR
B. Pilot air data source................................... Select CADC 2
Recovers IFF altitude, GCAS and roll/yaw axes of autopilot.
DOR/RMP
PERF C. ELEV TAB power selector switch................. Select EMER
Normal elevator trim failed.
JETTISON
D. Autopilot......................... Select PITCH OFF (as required)
Autopilot pitch axis unusable due to inoperative normal
elevator trim. LANDING
( 6ORZ ÀLJKW $YRLG EHORZ DSSURDFK VSHHGV
Stick pusher inoperative. Stall warning operative but DITCHING
degraded at high sideslip angles.

F. EMER EXIT LIGHT....................................... EXTINGUISH BAILOUT
Prevents drain on aircraft batteries.
OPER FAULT LG

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