Page 405 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.12.2.1 Asymmetrical Flap Positioning
ACAWS
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fail to move in either direction, it may be due to engagement of the
HPHUJHQF\ ÀDS EUDNH GROUND

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TAKEOFF
'R QRW DWWHPSW IXUWKHU PRYHPHQW RI WKH ÀDSV LQ ÀLJKW

FIRE/SMK
NORM WARNING

PRES/OXY
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NOT FOR FLIGHT
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FRQGLWLRQ RI WKH ÀDSV PD\ UHVXOW 7KLV PDQXDO UHVHW LV IRU ENG/PROP
ground use only.

(End of Procedure)
FUEL

1.12.2.2 Wing Flap Position Indicator Failure
AAR
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or if indicator is beyond 100 percent after movement of the FLAPS
SPEC OHYHU VXVSHFW LQGLFDWRU UDWKHU WKDQ ÀDS V\VWHP IDLOXUH ELEC

A. Pitch attitude...............................................................Observe (PF)
HYD
Flaps movement is indicated by a change in the pitch attitude of the
aircraft.
FLT CTRL
B. Hydraulic pressure........................................................Observe (PF)

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K\GUDXOLF SUHVVXUH GURS LQGLFDWHV WKDW WKH ÀDSV DUH PRYLQJ RU D GEAR
hydraulic leak or failure exists in the actuating system.

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PERF 'XULQJ ÀDS H[WHQVLRQ WKH SLORW PD\ GLUHFW D FUHZPHPEHU WR PDNH

D YLVXDO LQVSHFWLRQ RI WKH ÀDS SRVLWLRQ RU XVH WKH $08 35()/,*+7 JETTISON
0(18 SDJH IRU ÀDS SRVLWLRQ LQGLFDWLRQ

(End of Procedure) LANDING

DITCHING
1.12.2.3 Wing Flap Cable Break

A. Overriding the Flap Selector Valve procedure.................Accomplish BAILOUT

(End of Procedure)
OPER FAULT LG

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