Page 403 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

Q3 NOTE
ACAWS
‡ The ELEV TRIM switches on the control
wheels will not operate the emergency system.
Emergency operation is controlled by the GROUND
pedestal mounted NOSE up, NOSE down TRIM
switch only.
TAKEOFF
‡ Tab movement may be slower in emergency
than in normal.
FIRE/SMK
NORM D. Elevator trim tab switch on pedestal..................................
............................................................Trim (as required) (PF)
PRES/OXY
NOT FOR FLIGHT

Q2 IS TRIM TAB FUNCTIONING IN EMER?
ENG/PROP

NO
No further action is required.
FUEL
(End of Procedure)

E. ELEV TAB power selector switch........................OFF (PF)
AAR

SPEC Q3 IS FAILURE IN A NOSE UP CONDITION? ELEC

NO F. Bank..........................As necessary to lower the nose (PF) HYD

Q4 G. Airspeed....................................Reduce (as required) (PF)
H. FLAPS.......................................Extend (as required) (PM) FLT CTRL

Extend as structural limitations permit to provide
increasing stall margin as airspeed is reduced. 100 GEAR
SHUFHQW ÀDSV ZLOO LQFUHDVH WKH QRVH GRZQ PRYHPHQW
and reduce required control forces.
DOR/RMP
PERF I. Flight Control System Failure procedure................. Review

(End of Procedure)
JETTISON

Q4 IS FAILURE IN A NOSE DOWN CONDITION?
LANDING

NO
J. Power.........................................Reduce (as required) (PF)
DITCHING
EoP K. Airspeed....................................Reduce (as required) (PF)
L. Flight Control System Failure procedure................ Review
BAILOUT
(End of Procedure)

OPER (End of Procedure) FAULT LG

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