Page 400 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.12.1.4 Control Boost Hardover Failure
ACAWS
A. Cockpit control..................................................................Verify (PF)

Ensure cockpit control matches the hardover maneuver being GROUND
experienced.

B. Applicable CONTROL BOOST switch, BOOST..................OFF (PM) TAKEOFF

Q1 DOES HARDOVER MANEUVER STOP? FIRE/SMK
NORM
NO
Continue operation with BOOST pack OFF.
PRES/OXY
C (End of Procedure)

C. Applicable CONTROL BOOST switch, BOOST...................ON (PM) ENG/PROP

D. Applicable CONTROL BOOST switch, UTIL.......................OFF (PM)
FUEL

Q2 DOES HARDOVER MANEUVER STOP?
AAR

NO Continue operation with UTIL pack OFF.
SPEC NOT FOR FLIGHT ELEC
E (End of Procedure)

E. Applicable CONTROL BOOST switch, BOOST.................OFF (PM) HYD

NOTE

‡ Expect that greatly increased forces will be required to FLT CTRL
move the control for which the hydraulic assistance has
been turned off.
GEAR
‡ Turning the ELEVATOR CONTROL BOOST switches
OFF will alleviate an elevator hardover maneuver,
leaving the aircraft out of trim in the nose-up direction. DOR/RMP
PERF Immediate correction of trim will be required after the
CONTROL BOOST switches are placed to the OFF
position. JETTISON

F. Trim and engine power..................Use to reduce control forces (PF)
LANDING
Trim should be used with caution in conjunction with pilot inputs to
normal controls to avoid over controlling.
DITCHING
G. Flight Control System Failure procedure...................Review (P/CP)
(End of Procedure) BAILOUT

OPER FAULT LG

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