Page 297 - (KU)01-75GAJ-1.5 - Change 1
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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
Use, copying and/or disclosure is 1 -257
governed by the statement on the
title page of this document. BACK CHARTS