Page 291 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

‡ RPS overhead console
‡ BAU I #2 ACAWS
‡ Smoke detection

‡ Standby instrument lights GROUND
‡ Standby altimeter (vibrator)
‡ Standby attitude indicator (gyro) TAKEOFF
‡ UHF COMM No. 1 (also secure voice)

‡ Utility lights FIRE/SMK
NORM ‡ VHF communication No. 1 antenna

Electrical power is not required for: PRES/OXY
ANTI-ICING AND DE-ICING:

‡ Engine inlet and oil cooler inlet and torque meter shaft and ENG/PROP
inlet guide vane anti-icing

FLIGHT CONTROLS: FUEL

‡ Normal boost (rudder boost pressure reduced to low boost)
‡ :LQJ ÀDSV K\GUDXOLF RYHUULGH AAR

SPEC NOT FOR FLIGHT ELEC
NOTE
'XH WR WKH ORVV RI SRZHU WR WULP WDE V\VWHP D QR ÀDS
landing is recommended.
HYD
FLIGHT INSTRUMENTS:

‡ Magnetic compass FLT CTRL
‡ Pilot and copilot inclinometer

LANDING GEAR AND BRAKES: GEAR
‡ Landing gear system (hydraulic override)

‡ Normal brake system (no anti-skid) DOR/RMP
PERF ‡ Nose wheel steering

MISCELLANEOUS: JETTISON

‡ Cargo door and ramp (manual)
‡ Crew oxygen system LANDING
‡ Emergency lights (self contained battery)

‡ Fuel available from main tanks (gravity feed) DITCHING
‡ Standby altimeter/airspeed indicator (gyro)
‡ Continued engine operation BAILOUT
(End of Procedure)

OPER FAULT LG

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