Page 301 - (KU)01-75GAJ-1.5 - Change 1

INTRO

EP'S (KU)01-75GAJ-1.5 FIGURES
Lost
Bus G. Potential Mission Impacts...................................... Review
Comm ACAWS
failure ‡ Standby altimeter may be inaccurate in sideslip
conditions if freezing conditions encountered (Pilot Pitot
Heat No. 3 Lower Right Fail). GROUND
‡ RUDDER trim inoperative.
‡ Degraded mission capability due to loss of displays (P
HUD, HDD 1, HDD 3, P AMU, CNBP). TAKEOFF
‡ Pilot inclinometer indicator lighting failed.
‡ BAU I #3 and BAU I #5 lighting degraded. FIRE/SMK
NORM ‡ Floodlighting degraded.

‡ Avoid icing conditions. Pilot upper left and lower right PRES/OXY
pitot failed, Pilot TAT probe and left AOA vane heat failed.
H. BAU I #3 FAIL*....................................................... Review
ENG/PROP
I. BAU I #5 FAIL*........................................................ Review

J. ECBU 1 Fault Log................................................... Review FUEL

P AMU, CNBP, HDD 1/3
P HUD, ADC 1, L OVHD FAN AAR
3 3,727 +($7 3 7$7 / $2$ +($7(56
FLT STN UTIL/RDG LTS, EMER EXIT LTS CNTL
SPEC NOT FOR FLIGHT ELEC
L ICE DET, DIMMER UNIT 1, RUD HI BOOST CNTL
RUD TAB PWR, ELEV TAB PWR-NORM
BAU I #3/#5 HYD
SPTU 2
FLT CTRL
(End of Procedure)
Lost Bus Comm failure: If communications have failed, most ECBs stay
in their last state. GEAR
K. Potential Mission Impacts..................................................... Review

‡ Pilot pitot heat will remain as-is; Control not functional. DOR/RMP
PERF L. ECBU 1 Fault Log................................................................. Review

JETTISON
P AMU, CNBP, HDD 1/3
P HUD, ADC 1, L OVHD FAN
3 3,727 +($7 3 7$7 / $2$ +($7(56 LANDING
FLT STN UTIL/RDG LTS, EMER EXIT LTS CNTL
L ICE DET, DIMMER UNIT 1, RUD HI BOOST CNTL DITCHING
RUD TAB PWR, ELEV TAB PWR-NORM
BAU I #3/#5 BAILOUT
SPTU 2

OPER (End of Procedure) FAULT LG

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