Page 398 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.12.1 FLIGHT CONTROL SYSTEM FAILURE
ACAWS
Landing the aircraft without hydraulic assistance is a marginal operation
and requires skillful handling of trim tabs and engine power, plus
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WARNING TAKEOFF

Never purposely remove the hydraulic assistance from FIRE/SMK
NORM WKH ÀLJKW FRQWURO ERRVWHU DVVHPEOLHV WR VLPXODWH D
FRPSOHWH ORVV RI ERRVW DVVLVWDQFH WR WKH ÀLJKW FRQWUROV
To remove the assistance could result in an unusual PRES/OXY
NOT FOR FLIGHT
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controls.
ENG/PROP
A. Aircraft control..............................................................Maintain (PF)
Maintain aircraft control using trim tabs, engine power and FUEL
FRRUGLQDWHG HIIRUWV RI WKH SLORW DQG FRSLORW RQ WKH ÀLJKW FRQWUROV

Trim should be used with caution in conjunction with pilot inputs to AAR
normal controls to avoid over controlling.

SPEC B. Aircraft weight and speed.....................Reduce (as required) (P/CP) ELEC

Reduce the weight and speed of the aircraft as much as possible
in order to decrease control forces.
HYD
C. Controllability Check procedure.........Accomplish (as required) (PF)

FLT CTRL
NOTE

Any suspected or known structural failure that may cause GEAR
aircraft control problems will require a Controllability
Check prior to landing.
DOR/RMP
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Use normal trim and engine power to reduce control forces.
LANDING
Fly the aircraft straight to the touchdown zone.

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ground.

(End of Procedure)
BAILOUT

OPER FAULT LG

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