Page 351 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

A. FADEC (No. 1 and No. 4)................................................ Select ALT
ACAWS
Restores proper ATCS operation and HP, MGT, NG and NP
indications.
GROUND
B. Pilot attitude source....................................... Select ATT REF INU 2

Recovers pilot attitude reference and autopilot.
TAKEOFF
C. Pilot RAD ALT source.......................................... Select RAD ALT 2

Restores TCAS and GCAS. FIRE/SMK
NORM D. Stick pusher.................................................... Select PUSHER OFF

PRES/OXY
NOT FOR FLIGHT
Stick pusher failed.

E. Icing conditions...................................................... Avoid, if practical ENG/PROP

Wing/empennage A/I valve failure may not be detected. If icing
conditions cannot be avoided, monitor wing/empennage ice FUEL
protected surfaces for lack of ice shedding.

F. Aircraft hydraulic systems..................................................... Monitor
AAR
Periodically scan aircraft and utility hydraulic reservoir for signs
RI ÀXLG ORVV RU OHDNDJH 0RQLWRU XWLOLW\ UXGGHU ERRVW SUHVVXUH IRU
SPEC indication of utility system pressure (rudder pressure will be in low ELEC
ERRVW ZLWK ÀDSV UHWUDFWHG 8WLOLW\ V\VWHP SUHVVXUH LQGLFDWLRQ DQG
HYD PMP 1 and 2 PRESS LO (C) ACAWS failed.
HYD
G. OIL COOLER FLAPS (No. 1 and No. 2).................... Select Manual

2LO FRROHU ÀDSV 1R DQG ZLOO IXOO\ H[WHQG FLT CTRL
H. OIL COOLER FLAP (No. 4)....................................... Manual/OPEN

2LO FRROHU ÀDS 1R QRW IDLO VDIH WR RSHQ OLNH 1R DQG 2LO GEAR
FRROHU ÀDSV 1R DQG FDQQRW EH FORVHG 0RQLWRU UHPDLQLQJ RLO
temperatures.
DOR/RMP
PERF Prior to landing:

I. Landing gear................................ Use Landing Gear Selector valve JETTISON

Refer to Landing Gear Malfunctions, Overriding the Landing Gear
Selector Valve procedure. LANDING

J. Landing gear............................................................... Visually verify
DITCHING
Visually verify landing gear position before landing or before
exceeding limiting speeds after gear retraction. Left main gear
indication failed. BAILOUT

K. Potential Mission Impacts..................................................... Review
OPER FAULT LG

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