Page 330 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

Lost
Bus ‡ Engine No. 4 auxiliary feather pump inoperative.
Com ‡ Engine No. 1 start valve will not open. ACAWS
failure
‡ Bleed air manifold pressure reads erroneously low due
to sensor failure. GROUND
‡ 2LO FRROHU ÀDS 1R DQG 1R ZLOO QRW UHWUDFW DQG 1R
will not extend.
TAKEOFF
‡ AR manifold pressure indication is lost.

C. TECU FAIL*........................................................... Review
FIRE/SMK
NORM D. Fault Log................................................................ Review

FADEC 3A/4B, PROP 4 AUX PUMP PRES/OXY
OIL FLAP 2 EXTEND, OIL FLAP 1/4 RETRACT
START VLV 1, UNFTHR SOLENOID 1/2/3/4 ENG/PROP
UHF 2, VHF 2, TACAN 2
DEICE TIMER UNIT B
SKE, IFF 1, VHF 2 SECURE, CMDS PROGRAM FUEL
STICK PUSHER
SENSORS: AAR
FLT STN CTRL VLV OUTLET DUCT TEMP
SPEC NOT FOR FLIGHT ELEC
L BLD AIR CROSS-SHIP MANIFOLD DUCT
PRESS
FLT STN TURBINE OUTLET DUCT PRESS
JTSN INTLK RELAY A HYD
TECU
(End of Procedure) FLT CTRL

Lost Bus Comm failure: If communications have failed, most ECBs stay
in their last state. GEAR
E. Stick pusher.................................................... Select PUSHER OFF

Stick pusher failed. DOR/RMP
PERF F. OIL COOLER FLAP (No. 2)................................................... Manual

Flap will remain at 100 percentG. Potential Mission JETTISON
Impacts..................................................... Review

‡ UHF 2, VHF 2 and TACAN 2 power will remain as-is; CNI-MU LANDING
ON/OFF control not functional.
‡ CMDS programmer power will remain in the last commanded DITCHING
state. If CMDS operation was not established before failure use
CMDS BYPASS mode.

‡ Engine No. 4 auxiliary feather pump inoperative. BAILOUT
‡ Engine No. 1 start valve will not open.
OPER FAULT LG

1 -290 Use, copying and/or disclosure is
governed by the statement on the
BACK title page of this document. CHARTS