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engine generators, the APU generator or an external
power source.
The DC electrical system is supplied from the AC
electrical system or from the batteries as a back up
source.
An Emergency Generator, driven by the Blue Hydraulic
System pressurized by the Ram Air Turbine in emergency
configuration, can supply part of the AC and DC
electrical systems in case of loss of normal supply.
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ELECTRICAL SYSTEM GENERAL INTRODUCTION
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24 - ELECTRICAL POWER
24-00-00 ELECTRICAL SYSTEM LOCATION
CONTENTS:
AC Normal Generation
AC Emergency Generation
Static Inverter
DC Normal Generation
DC Emergency Generation
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ELECTRICAL SYSTEM LOCATION
AC NORMAL GENERATION
There are 2 engine driven Integrated Drive Generator
(IDGs).
The IDG is an assembly of two parts:
- the drive : Constant Speed Drive (CSD)
- the generator.
Each IDG is installed on the associated engine
accessory gearbox.
The AC Auxiliary Power Unit (APU) generator is located
in the APU compartment.
The external power receptacle is fitted forward the
nose landing gear bay.
AC EMERGENCY GENERATION
The AC Emergency Generation consists of a Constant
Speed Motor (CSM) and an AC generator which form an
assembly called Constant Speed Motor/Generator
(CSM/G).
The CSM/G is located in the main landing gear bay.
STATIC INVERTER
The Static Inverter is located in the right lateral
avionics compartment.
DC NORMAL GENERATION
The two batteries (BAT 1 and BAT 2) and the two main
Transformer Rectifiers (TR1 and TR2) are located in
the right lateral avionics compartment.
DC EMERGENCY GENERATION
The Essential Transformer Rectifier (ESS TR) is located
in the left lateral avionics compartment.
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24-00-00 ELECTRICAL SYSTEM DIAGRAM
DESCRIPTION
CONTENTS:
MAIN AC Generation
Emergency Generator
AC Transfer
AC Distribution
DC Generation
DC Distribution
Batteries
Static Inverter
Ground/Flight Buses
Galleys
Main Electrical Configurations
Self Examination
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ELECTRICAL SYSTEM DIAGRAM DESCRIPTION
MAIN AC GENERATION
ENGINE GENERATORS
The aircraft electrical system is supplied by two
engine driven generators regulated in speed by
integrated drives.
Generator 1 is driven by engine 1.
Generator 2 is driven by engine 2.
Engine generator characteristics are: 115 Volts, 400
Hertz, 90 KVA.
APU GENERATOR
A third AC generator driven by the APU can replace
one or both main engine generators throughout the
flight envelope.
APU generator characteristics are: 115 Volts, 400
Hertz, 90 KVA.
EXTERNAL POWER
　
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