Page 259 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

I F. FLAPS lever........................................................ 20% (PM)
ACAWS
WARNING

GROUND
Do not raise the FLAPS lever above 20 percent
during the go-around. Low boost will be set, and
WKHUH PD\ EH LQVXI¿FLHQW UXGGHU FRQWURO DYDLODEOH TAKEOFF
for full two-engine power. Gross weight should
be below 120,000 pounds.
FIRE/SMK
NORM G. Accelerate..........................................................................
(gear up) or 165 KIAS (gear down) (PF)
..........................V
MCA2
PRES/OXY
Initially trade altitude for airspeed if possible.
WARNING
ENG/PROP

With No. 3 and No. 4 engines failed, delay
hydraulic gear retraction until the aircraft is well FUEL
under control and 165 KIAS is maintainable.
Raising the gear may reduce available hydraulic AAR
SUHVVXUH QHHGHG WR RSHUDWH WKH ÀLJKW FRQWUROV

H. GEAR...................................................Up, if possible (PM)
SPEC NOT FOR FLIGHT ELEC
After establishing a positive rate of climb.

(End of Procedure) HYD
I. Power levers..................................................TAKEOFF (as required) (PF)
FLT CTRL
Set inboard immediately, followed by outboard as rudder control
permits.
GEAR
J. FLAPS lever.................................................................................20% (PM)

WARNING
DOR/RMP
PERF
Do not raise the FLAPS lever above 20 percent during
the go-around. Low boost will be set, and there may be JETTISON
LQVXI¿FLHQW UXGGHU FRQWURO DYDLODEOH IRU IXOO WZR HQJLQH
power. Gross weight should be below 120,000 pounds.
LANDING
K. Accelerate....................................................................165 KIAS (PF)

Initially trade altitude for airspeed if possible. DITCHING

L. GEAR .................................................................Up, if possible (PM)
BAILOUT
After establishing a positive rate of climb.

OPER (End of Procedure) FAULT LG

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