Page 310 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

Lost
Bus XDUCER
Comm UNDERDECK UTIL/CREW ENTRANCE LTS ACAWS
failure
FLT STN CB LTS
DIGITAL MAP GROUND
CHUTE RELEASE, SPTU 1, CP PITOT HEAT 4
EXT MASS MEM UNIT TAKEOFF
R POD E-TRAIL/R-TEST
R POD TRAIL
(End of Procedure) FIRE/SMK
NORM
Lost Bus Comm failure: If communications have failed, most ECBs stay
in their last state. PRES/OXY
NOT FOR FLIGHT
J. Performance data.................................................................. Review
Determine takeoff/landing distance for anti-skid inoperative. ENG/PROP

K. Brakes....................................................................... Use cautiously
Anti-skid protection may not be available. FUEL

Prior to engine shutdown:
AAR
L. Chocks..................................................................................... Install
SPEC The emergency brakes may or may not be available depending on ELEC
the failure mode of the data bus/ECBU. Chock the aircraft before
shutting down the engines.

M. Potential Mission Impacts.................................................... Review HYD
‡ Generator No. 3 will remain as-is; control not functional.
FLT CTRL
NOTE

GEN 3 OFF (A) ACAWS only indicates GEN switch GEAR
position. Verify condition on system status page.

‡ Chute release (bomb rack) inoperative. DOR/RMP
PERF ‡ Copilot lower left pitot heat will remain as-is; control not
functional.
JETTISON
‡ Right AR pod emergency trail/response test function lost.
N. Fault Log............................................................................... Review
LANDING
MC 1 AC, BIU #1 AC, CNI-SP 1, RAD ALT 1
P HUD, VOR/ILS 1, P CNI-MU DITCHING
GBE RELAY 3A/4A, GEN 3
ELEV TAB CNTL-NORM, PITOT HEAT MON
BRAKE SEL VLV-EMER, NORM/EMER BRAKE XDUCER BAILOUT
UNDERDECK UTIL/CREW ENTRANCE LTS
OPER FAULT LG

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