Page 323 - (KU)01-75GAJ-1.5 - Change 1
P. 323
INTRO
EP'S (KU)01-75GAJ-1.5 FIGURES
If gear was up or anti-skid was off at time of failure, then
anti-skid will be failed (ANTI-SKID FAIL (C) ACAWS ACAWS
when gear is lowered). In this case, use brakes cautiously
since anti-skid protection not available.
GROUND
I. Performance data................................................................. Review
Determine landing distance for anti-skid inoperative. TAKEOFF
J. OIL COOLER FLAP (No. 3)................................................... Manual
FIRE/SMK
Flap will extend to and remain at 100 percent.
NORM
K. Potential Mission Impacts...................................................... Review
PRES/OXY
NOT FOR FLIGHT
2LO FRROHU ÀDS 1R ZLOO IXOO\ H[WHQG DQG 1R ZLOO QRW FORVH
HYDRAULIC panel switch for UTIL HYD suction boost pump is ENG/PROP
inoperative. (OFF light indicates switch position only.)
Normal brake pressure may bleed off when setting parking
brake (parking brake valve will remain as-is). Ensure aircraft is FUEL
chocked and use emergency brake pressure for parking.
Engine No. 3 auxiliary feather pump inoperative. AAR
Fuselage tank transfer pump inoperative. Fuel may be
transferred using cabin differential pressure.
SPEC L. Fault Log............................................................................... Review ELEC
)$'(& % % 3523 $8; 3803 HYD
F/ODS CH B, R DUMP VLV, ADF 2, HF 2
LDG LTS RETRACT/EXTEND, LEADING EDGE LTS
UTIL HYD SUCT PUMP, PARK BRAKE VALVE FLT CTRL
ANTISKID
OIL FLAP 2/3 RETRACT, OIL FLAP 3 EXTEND GEAR
MISSLE WARNING, ALE TAIL, HF 2 SECURE VOICE
BAU II #4 DOR/RMP
PERF FUS TK XFER PUMP
SENSORS:
CGO AIR COND FLOW CTRL VLV OUTLET DUCT TEMP JETTISON
FLOOR HEAT SUPPLY DUCT TEMP
CGO OVRHD RECIRC FAN DUCT PRESS LANDING
CGO TURBINE OUTLET DUCT PRESS
R BLD AIR CROSS-SHIP MANIFOLD DUCT PRESS
DITCHING
(End of Procedure)
BAILOUT
OPER FAULT LG
Use, copying and/or disclosure is 1 -283
governed by the statement on the
title page of this document. BACK CHARTS