Page 172 - (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
R XSHIP ISOL C GROUND
The right wing isolation valve Icing conditions........................... Avoid
and the divider valve are in D
the AUTO or CLOSE mode, The cargo compartment air
commanded closed by the FRQGLWLRQHU DQG XQGHUÀRRU KHDW DUH TAKEOFF
controller and are closed inoperative and the empennage E
according to the feedback ice protection zone HEAT FAIL
position switch. (C) ACAWS is inhibited in this F FIRE/SMK
NORM FRQ¿JXUDWLRQ ,I LFH DFFXPXODWLRQ
is suspected, refer to Landing with
Ice Accumulation procedure. PRES/OXY
NOT FOR FLIGHT
RADALT 1 (or 2) FAIL G
The respective radar altimeter RAD ALT 1 or 2 ECB (420 or 825)........
has failed. ...................................... PULL, RESET H ENG/PROP

If the ACAWS does not clear:
I
Select the other radar altimeter. FUEL
RADALT SAME
Pilot and copilot have the same Radar altimeter...................................... L
radar altitude source selected. ............... Change source (as required) AAR
RAMP/DOOR CNTL CLOSED M
SPEC The RAMP/DOOR switch RAMP/DOOR switch .....................OFF ELEC
(loadmaster station) is in N
CLOSE position.
RAMP OPEN HYD
O
The ramp is not in the closed No crew action required.
and locked position. FLT CTRL
REFUEL XFD VALVE NOT CLSD P
The fuselage tank transfer (TO, RFL XFEED VLV CLOSE ECB (509).... GEAR
FROM) switches are in the ...................................... PULL, RESET R
CLSD, OFF position and the
fuselage tank transfer valve RFL XFEED VLV OPEN ECB (508)......
has not closed or ...................................... PULL, RESET S DOR/RMP
PERF has failed open. Fuselage tank transfer switches... Cycle

Cycle the fuselage tank transfer T JETTISON
(TO, FROM) switches on the
REFUEL CONTROL panel.
U
If the cross-ship manifold is pressurized: LANDING
Monitor fuselage tank quantity to ensure V
that fuel is not leaking into the tank. DITCHING

W
BAILOUT
X

OPER FAULT LG

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