Page 253 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

CAUTION ACAWS

Blade angle scheduling at the GND IDLE power lever GROUND
position is a function of indicated airspeed and is
designed to make engine out stops easier to control.
7KH EHQH¿WV RI WKLV VFKHGXOLQJ DUH QRW DYDLODEOH LI WKH TAKEOFF
power levers are brought below FLT IDLE above 115
knots when crosswinds from opposite the failed engine
side are above 15 knots. FIRE/SMK
NORM (End of Procedure)

PRES/OXY

1.7.9.4 Go-around with One Engine Inoperative
ENG/PROP
A. Go-around.................................................................Announce (PF)

B. G/A switch........................................................................Press (PF)
FUEL
C. Power levers...................................... TAKEOFF (as required) (PF)

Anticipate rudder and aileron input as asymmetric power is applied. AAR

D. Bank angle......................... Set 2º to 5º into operating engines (PF)
SPEC NOT FOR FLIGHT ELEC
Initially set 2º to 5º angle of bank away from the shutdown engine,
then stabilize angle of bank and rudder for zero sideslip.
HYD
( &OLPE GLYH PDUNHU 6HW WR ÀLJKW GLUHFWRU FRPPDQG 3)

F. FLAPS............................................................................... 50% (PM)
FLT CTRL
G. GEAR..................................................................................UP (PM)

H. RUDDER trim.................................................Set (as required) (PF) GEAR

Add rudder trim to reduce pedal forces and provide increased
rudder capability should a second engine fail on the same side. DOR/RMP
PERF I. FLAPS...........................................................UP, passing FUSS (PM)

JETTISON
(End of Procedure)

LANDING
1.7.10 TWO-ENGINE OPERATION

DITCHING
The loss of engines No. 1 and No. 2 results in the loss of the utility
hydraulic system functions and will require special planning and
procedures. Reference systems affected by various two-engine failure BAILOUT
combinations.

OPER FAULT LG

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