Page 359 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

E. Performance data................................................................. Review
ACAWS
Determine takeoff/landing distance for anti-skid inoperative.

Prior to engine shutdown:
GROUND
F. Chocks..................................................................................... Install
The emergency brakes may fail-safe on or may be failed/ TAKEOFF
unavailable depending on the failure mode of the data bus/ECBU.
Chock the aircraft before shutting down the engines.
FIRE/SMK
NORM G. Potential Mission Impacts..................................................... Review

‡ Failed Components: PRES/OXY

MC 1 (or 2)
Anti-skid ENG/PROP
Pilot HUD CDI, markers and mode annunciators
Radar
Pilot Mode Annunciator panel lights FUEL
HDD 1 and 2
Cursor Control AAR
ADC 1
DMU
SPEC NOT FOR FLIGHT ELEC
Autopilot
Defensive System Master Control panel
Autothrottle HYD
Chute Release Electronic Control
ATCS Override FLT CTRL
Engine 4 start valve
‡ As-is Components (components which will continue to operate
in their current state, but will not respond to control/switch panel GEAR
operation):
Pilot ICS MON panel DOR/RMP
PERF GENERATOR 3 ON/OFF/RESET switch
Pilot Pitot Heat
APU Generator On/Off switch JETTISON
Standby Instrument lights
Low Speed Ground Idle switches LANDING
CNI-MU Annunciator lights
Emergency Exit Lights Control DITCHING
Pitot Heat No. 4 LL On/Off
Crew Door lights
H. Fault Log............................................................................... Review BAILOUT

MC 1 OR 2
OPER FAULT LG

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