Page 321 - (KU)01-75GAJ-1.5 - Change 1
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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
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Engine No. 3 auxiliary feather pump inoperative.
BAILOUT
OPER FAULT LG
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