Page 303 - (KU)01-75GAJ-1.5 - Change 1

INTRO

EP'S (KU)01-75GAJ-1.5 FIGURES
Lost
Bus ‡ Autothrottle and ATCS override switches inoperative
Comm (BAU I #2). ACAWS
failure ‡ Degraded mission capability due to loss of displays (CP
HUD, HDD 2, HDD 4, CP AMU, CP CNI-MU, observer
CNI-MU). GROUND

‡ Low speed ground idle not available (BAU I #2).
‡ UHF 2 secure failed TAKEOFF
‡ Radar cooling fans and heater failed; radar may
eventually fail. FIRE/SMK
NORM ‡ Copilot inclinometer indicator lighting failed.
BAU I #1, BAU I #2 and BAU I #4 lighting (to include
‡
CNIMU mode annunciators) degraded. PRES/OXY
‡ Floodlighting degraded.
‡ TAWS failed. ENG/PROP
G. BAU I #1 FAIL*....................................................... Review

H. BAU I #2 FAIL*....................................................... Review FUEL

I. BAU I #4 FAIL*....................................................... Review
J. Fault Log................................................................. Review AAR

CP AMU, CP/OBS CNI-MU, ADC 2, GBE RELAY 1A/2A
SPEC NOT FOR FLIGHT ELEC
HDD 2/4, CP HUD
NESA, DIMMER UNIT 2, R OVHD FAN, RADAR HTR/FANS
&3 3,727 +($7 &3 7$7 5 $2$ +($7(56 HYD
R ICE DET, UHF 2 SECURE VOICE, SAR HOMER,
DSDTS FLT CTRL
BAU I #1/#2/#4, TAWS
(End of Procedure)
GEAR
Lost Bus Comm failure: If communications have failed, most ECBs stay
in their last state.
DOR/RMP
K. Potential Mission Impacts..................................................... Review
PERF
‡ Copilot upper right pitot heat and NESA will remain as-is; control
not functional. JETTISON
L. Fault Log............................................................................... Review
LANDING
CP AMU, CP/OBS CNI-MU, ADC 2, GBE RELAY 1A/2A
HDD 2/4, CP HUD
NESA, DIMMER UNIT 2, R OVHD FAN, RADAR HTR/FANS DITCHING
&3 3,727 +($7 &3 7$7 5 $2$ +($7(56
R ICE DET, UHF 2 SECURE VOICE, SAR HOMER, DSDTS BAILOUT
BAU I #1/#2/#4, TAWS

OPER (End of Procedure) FAULT LG

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