Page 312 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

Lost
Bus C. Cabin altitude.......................................................... Monitor
Comm CAB ALT HIGH (C) ACAWS false due to sensor ACAWS
failure failure.

D. Pilot autopilot.............................. Re-engage (as required) GROUND

E. Potential Mission Impacts....................................... Review
TAKEOFF
‡ Reduced electrical redundancy. Generator No. 4 control
relay has lost power and is no longer powering its
respective bus(es). FIRE/SMK
NORM ‡ Normal brake pressure will be on regardless of brake
selection.
‡ Radar inoperative. PRES/OXY
‡ Single source for attitude. Standby instruments also
available. ENG/PROP
‡ Single source for inertial navigation. Backup by other
navigational sources as available.
‡ VOR/ILS 2 inoperative. FUEL
‡ HF 2 inoperative.
‡ AV BAY OVERHEAT (C) ACAWS inoperative (no AAR
overheat annunciation).
SPEC ‡ NOT FOR FLIGHT ELEC
CDS gate release de-armed.
‡ Left static line retriever inoperative.
F. Fault Log................................................................ Review HYD
MC 2 AC, BIU #2 AC, CNI-SP 2, EGI 1, VOR/ILS 2
RAD ALT 2, HF 2, RADAR, CP HUD
GBE RELAY 1B/2B, BRAKE SEL VLV-NORM FLT CTRL
CP AUTOPILOT, GEN 4, NOSE GEAR WELL LTS
LAPES/CDS ARM, L STAT LINE RETRVR GEAR
SENSORS:
AV COOLING AIR DUCT TEMP
DSPLY COOLING AIR OUTLET DUCT TEMP DOR/RMP
PERF CABIN PRESSURE

AV COOLING AIR DUCT PRESS JETTISON
(End of Procedure)

Lost Bus Comm failure: If communications have failed, most ECBs stay LANDING
in their last state.

G. Brakes................................................... Select EMER (as required)
DITCHING
If ECBU 6 FAIL* occurs when the gear are retracted, the normal
brake selector valve may be stuck in the closed position. Switch to
emergency brakes for landing. Use brakes cautiously since anti- BAILOUT
skid protection will not be available. Determine takeoff/landing
distance for anti-skid inoperative.
OPER FAULT LG

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