Page 297 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

INSTRUMENTS
ACAWS
STAND-BY INSTRUMENTS:
‡ Attitude

Powered by Utility Battery bus regardless of BTRY switch GROUND
position.

‡ Airspeed/altitude (vibrator) TAKEOFF

Powered by Utility Battery bus regardless of BTRY switch
position. FIRE/SMK
NORM ‡ Magnetic compass

Electrical power not required. PRES/OXY
‡ Pilot and copilot inclinometers

Electrical power not required. ENG/PROP
PFD:
‡ Airspeed and altitude indications may be erroneous in icing FUEL
conditions
‡ CDI and bearing pointers not functional AAR

PANEL CONTROLS/DISPLAYS
SPEC NOT FOR FLIGHT ELEC

NOTE

Functionality of operable panels (to include soft panels) HYD
may be severely limited due to loss of associated
component power.
FUNCTIONAL HARD PANELS: FLT CTRL
‡ GEAR (landing and taxi lights failed)

‡ HYDRAULIC (engine pump control only; all other controls failed) GEAR
‡ 3LORW DQG FRSLORW 5() 02'( ÀLJKW GLUHFWRU IDLOHG

‡ APU DOR/RMP
PERF ‡ BLEED AIR

‡ ELECTRICAL JETTISON
‡ ENGINE START (engine 1 and 4 start valves inoperative)

‡ FADEC (PMA supplies electrical power for switches) LANDING
‡ ICE PROTECTION (pilot and copilot pitot heat, NESA, propeller
ice protection and vertical tail pneumatic boot failed)
DITCHING
NOTE
BAILOUT
The fuel and mode annunciator panels are powered, but
not functional due to associated component failures.
OPER FAULT LG

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