Page 321 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.10.5.10 ECBU 10 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
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Lost conventional failure are:
Bus ‡ ANTI-SKID FAIL (C) (when gear is down) PRES/OXY
Com
failure ‡ BAU II #4 FAIL* (C)
‡ UTIL SUCT PRESS LO (C) ENG/PROP
‡ F/ODS B FAIL (A)
‡ ADF 2 FAIL (A) FUEL

A. ANTI SKID switch....................................................... OFF
Use brakes cautiously since anti-skid protection not AAR
available.

SPEC NOT FOR FLIGHT ELEC
B. Performance data................................................... Review
Determine takeoff/landing distance for anti-skid inoperative.

C. SUCTION BOOST PUMPS, UTIL switch................... OFF HYD
Pump not powered.
FLT CTRL
D. UNDERFLOOR switch........... OFF (below 15,000 ft MSL)
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air leak detection operative. GEAR

E. Potential Mission Impacts...................................... Review
‡ Utility hydraulic suction boost pump not functional. Utility DOR/RMP
PERF hydraulic pressure may momentarily drop to lower than
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JETTISON
‡ Fuel cross-ship manifold pressure indication lost.

‡ Fuselage tank transfer pump inoperative. Fuel may be
transferred using cabin differential pressure. LANDING

‡ Fuel dumping will be at reduced rate (right fuel dump
valve failed as-is).
DITCHING
‡ 2LO FRROHU ÀDS 1R IDLOHG DQG 1R ZLOO QRW FORVH

‡ Engine No. 3 auxiliary feather pump inoperative.
BAILOUT

OPER FAULT LG

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