Page 136 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.2.3 ADVISORIES B
ACAWS
Alert/Condition Crew Action
FS A/C DUCT HOT C GROUND
The BA/ECS has detected an AIR COND FLT STA MAN switch... ON
air conditioning supply duct D
overtemp. Temperature control switch........DECR TAKEOFF
Decrease set temperature as E
required to clear the ACAWS.

If the ACAWS does not clear: F FIRE/SMK
NORM AIR COND FLT STA POWER switch....
..................................................... OFF
FS A/C WATER SEP BLKD G PRES/OXY
NOT FOR FLIGHT
Clogged or iced water separator Increase temperature to possibly melt
is detected. the ice. H ENG/PROP
FS AUTOTEMP CNTL FAIL
Automatic temperature control AIR COND FLT STA MAN switch... ON I
has failed and the air conditioner FUEL
temperature control valve has
defaulted to a hold mode. L
FUEL FILTER 1 (2, 3 or 4) AAR
7KH UHVSHFWLYH HQJLQH IXHO ¿OWHU On the ground: M
SPEC impending bypass is detected 0DLQWHQDQFH UHTXLUHG EHIRUH ÀLJKW ELEC
by the NIU. Inhibited if the
HQJLQH IXHO ¿OWHU LPSHQGLQJ ,Q ÀLJKW N
bypass switch fault is detected. No crew action required
FUEL MGMT CNTL A (or B) FAIL O HYD
Respective channel A (or B) If channel A fails:
Avionics bus FMC interface Systems lost ............................. Review FLT CTRL
power loss or FMC 1553B data P
bus communication failure. All TK PRI (SEC) FLCV FAIL (A)
ACAWS are disabled. The TK 1
(2, 3, or 4) XFER PMP FAIL (C) R GEAR
ACAWS are disabled, the AUX/
EXT XFER PMP FAIL (C) ACAWS
are operative for crossfeed S DOR/RMP
operations only.
PERF
If operation of the FLCV must be veri¿ed:
T JETTISON
Fuel.......... Transfer into suspected tank

)XHO ÀRZ 0RQLWRU U
If channel B fails: LANDING
No crew action required. V
FUEL PRESS XDUCER FAIL DITCHING
The FMC has detected a failure No crew action required.
of the fuel manifold pressure W
transducer. BAILOUT
X

OPER FAULT LG

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