Page 411 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

WARNING
ACAWS

With structural damage there is a possibility of a split
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TAKEOFF
Determine minimum airspeed (no slower than landing speed) by
gradually slowing the aircraft in 5 knot increments until the desired
speed is attained or a control problem is encountered. Evaluate the FIRE/SMK
NORM control capabilities in turns and simulated landing approaches. Any
impending control problems are indicated by an excessive rolling,
yawing or pitching moment. PRES/OXY

ARE AIRCRAFT CONTROL PROBLEMS
Q1 ENG/PROP
ENCOUNTERED?
NO FUEL
H. Airspeed................................ Increase a minimum of 5 kts
I Maintain airspeed a minimum of 5 knots above
the speed at which the problem was encountered AAR
until touchdown.
SPEC NOT FOR FLIGHT ELEC
(End of Procedure)

I. Aircraft ...............................................Land at normal landing speed
HYD
(End of Procedure)

FLT CTRL
1.12.5 WING/EMPENNAGE ICE PROTECTION
SYSTEM FAILURES GEAR

Wing/empennage ice protection system failures generally are due to a
zone overheat indicated by a OVRHEAT (C) ACAWS or an inadequate DOR/RMP
zone heat indicated by a HEAT FAIL (C) ACAWS. The ACAWS indicates
PERF the type of failure and associated crew action.
JETTISON
A. Icing conditions........................................................................... Exit

LANDING
IS AN OVRHEAT (C) ACAWS PRESENT THAT
Q1
INDICATES A ZONE OVERHEAT?
DITCHING
NO
B. Affected zone........................................... Manually isolate
C BAILOUT

OPER FAULT LG

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