Page 213 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

,I HQJLQH FOLPERXW ÀLJKW SDWK LV QRW UHTXLUHG DIWHU WKH JHDU LV XS
lower the nose as desired, maintaining the climb dive marker above ACAWS
the horizon and accelerating to normal climb speed.

H. FLAPS...........................................................................Retract (PM) GROUND

WARNING
TAKEOFF
6HOHFWLQJ WKH ÀDS OHYHU WR D SRVLWLRQ OHVV WKDQ
percent increases V MCA by up to 36 knots because of the
reduction in rudder boost pressure and the ATCS power FIRE/SMK
NORM UHVWRUDWLRQ VFKHGXOH 2EVHUYH WKH PLQLPXP ÀDSV XS
safety speed of 135 knots, which is approximately the
worst case V MCA ZLWK ÀDSV XS DQG ORZ ERRVW 2SHUDWLQJ PRES/OXY
NOT FOR FLIGHT
WKH ÀDSV DQG JHDU WRJHWKHU LQFUHDVHV WKH PLQLPXP
control speed due to reduction in available hydraulic
pressure. ENG/PROP

5HWUDFW WKH ÀDSV DFFRUGLQJ WR WKH IROORZLQJ VFKHGXOH
FUEL
GWT Retraction Schedule

AAR
5DLVH ÀDSV ZKHQ DFFHOHUDWLQJ WKURXJK 9
FUSS
(135 KIAS).
SPEC 100,000 to %HJLQ ÀDS UHWUDFWLRQ ZKHQ DFFHOHUDWLQJ WKURXJK ELEC
140,000 135 KIAS and end at V FUSS (V OBS + 25 knots).
%HJLQ UDLVLQJ ÀDSV DW 9035 9 OBS + 5 knots) in
! 10 percent increments for each 5 knot increase in HYD
airspeed ending at FUSS (V +25).
OBS
FLT CTRL

After FLAPS are retracted and best climb airspeed established:
GEAR
I. Power levers...........................................................MAX CONT (PF)

J. Applicable Emergency procedure................................... Accomplish DOR/RMP
PERF Conduct Emergency procedures when time and crew workload

permit. JETTISON

K. Climb speed..................................................................Maintain (PF)
LANDING
If 3-engine climbout Àight path is required, climb at 3-engine best
climb speed.
DITCHING
If 3-engine climbout Àight path is not required, climb at normal
climb speeds.
BAILOUT
(End of Procedure)

OPER FAULT LG

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