Page 290 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

‡ Standby altimeter (vibrator)
‡ Standby attitude indicator (gyro) ACAWS
‡ Utility battery control

Avionics Battery bus powers: GROUND
‡ AV BAT meter

‡ Cargo compartment IR lighting TAKEOFF
‡ DC voltmeter (avionics battery)
‡ FADEC 1 and 4 (starting) FIRE/SMK
NORM ‡ Emergency engine shutdown 1 and 4

With BTRY switch ON and only battery power available, the following PRES/OXY
NOT FOR FLIGHT
avionics and isolated dc bus systems will be powered in addition to
items powered by the Utility and Avionics Battery buses:
ENG/PROP
‡ Air data system 1 and 2
‡ APU generator control
FUEL
‡ APU run control

‡ APU start control
AAR
‡ BA/ECS channel 1

SPEC ‡ ‡ BAU II #1 and #2 ELEC
BIU #1 and #2
‡ Cockpit lighting
HYD
‡ CNI SP 2
‡ Engine generator control
FLT CTRL
‡ Engine start valve 2 and 3
‡ FADECs
‡ Fire and overheat detection GEAR

‡ FIRE handle (1, 2, 3 and 4) (fuel, oil and hydraulic)
‡ Get Home Control DOR/RMP
PERF ‡ EGI 1 and 2

‡ Ground beta enable time delay relay (A and B) (1, 2, 3 and 4) JETTISON

‡ HDD display 1 and 2
‡ Pilot and copilot ICS LANDING

‡ Landing gear control
‡ MC 1 and MC 2 DITCHING
‡ NIU 1, 2, 3 and 4
‡ Pilot CNI-MU BAILOUT

‡ Reading lights
OPER ‡ RPS main instrument panel FAULT LG

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governed by the statement on the
BACK title page of this document. CHARTS