Page 38 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.2.2 CAUTIONS B
ACAWS
Alert/Condition Crew Action
ANTI-SKID FAIL C GROUND
The ANTI SKID switch is If ACAWS occurs after touchdown:
ON, the parking brake is not Do not turn ANTI SKID switch OFF. D
set, the EMER BRAKE SEL
switch is in Normal, the left If the ACAWS does not clear: TAKEOFF
or right main gear is not UP Power levers........................ MAX REV E
and a fault sensed in the Braking....................... Apply cautiously
anti-skid system by the BIT All other occurrences: F FIRE/SMK
NORM or the parking brake valve is ANTI SKID switch......................... OFF
not OPEN. This ACAWS may
illuminate momentarily after a Performance data..................... Review G PRES/OXY
soft touchdown when opposing Determine takeoff and landing
rear main wheels spin-up more
than three seconds apart; this distances for anti-skid inoperative. H ENG/PROP
is a normal condition.
APU GEN FAIL
APU generator trips off line EXT PWR/APU switch.................. OFF I FUEL
due to an over or under
voltage, over or under EXT PWR/APU switch.................. APU L
frequency, or feeder fault. Resets the APU generator. AAR
If the ACAWS does not clear: M
SPEC NOT FOR FLIGHT ELEC
EXT PWR/APU switch.................. OFF
Continue with the APU generator N
inoperative.
APU OVRTEMP O HYD
APU EGT exceeds 710º C. AIR COND POWER (either FLT STA or
CARGO COMPT or both) switch(es)........ FLT CTRL
........................................................ OFF P

Reduce the APU loading.
R GEAR

S DOR/RMP
PERF

T JETTISON

U
LANDING

V
DITCHING
W
BAILOUT
X

OPER FAULT LG

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