(2)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 (3)
 On the ECAM control panel, push the ELEC key to get the ELEC system page.

 (4)
 On the lower ECAM display unit, make sure that the A/C electrical configuration is correct.

 (5)
 Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002)

 (6)
 De-energize the aircraft electrical circuits supplied from the APU (Ref. TASK 24-41-00-862-002).

 5. Close-up
________
 Subtask 24-23-55-410-050

 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the access door (8) on the L lower side of the panel 120VU.

 (3)
 Install the Tthird Ooccupant seat (Ref. TASK 25-11-41-400-001).

 (4)
 Remove the warning notice(s).

 (5)
 Close the access door 121AL.

 (6)
 Remove the access platform(s).

 AC EMERGENCY GENERATION (CSM/G,GCU) - DESCRIPTION AND OPERATION
_______________________________________________________________
 1. General
_______
 The AC emergency generation enables part of the distribution network to be
 recovered in case of:
 -loss of the two main generation sources and,
 -unavailability of the auxiliary generation.
 2. Component Location
__________________
 (Ref. Fig. 001, 002, 003)

 -------------------------------------------------------------------------------FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I ATA I I I I DOOR I REF. -------------------------------------------------------------------------------2XE GLC-EMER 106VU 125 812 24-24-55
 -------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF.
 -------------------------------------------------------------------------------1XE CONTROL UNIT-CSM/G 125 812 24-24-34 8XE CSM/G 148 734 24-24-51 14XE ANN-EMER ELEC PWR/RAT/&/EMER GEN 21VU 211 831 24-24-00 15XE CNTOR-AC ESS BUS SWITCHING 106VU 125 812 24-24-55 23XE P/BSW-EMER ELEC PWR/EMER GEN TEST 21VU 211 831 24-24-00 24XE P/BSW-EMER ELEC PWR/MAN ON 21VU 211 831 24-24-00 33XE TIMER 106VU 125 812 24-24-00
 3. System Description
__________________
 **ON A/C 001-049, 051-099, 101-105, 201-203,
 (Ref. Fig. 004)
R **ON A/C 106-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 004A)

R  AC Emergency Generation - Component Location Figure 001
 1EFF : 1 1 1CES  ALL  1 111 24-24-00 Page 2 Feb 01/00

 AC Emergency Generation - Component Location
 Figure 002
 1EFF :  ALL  1  24-24-00 Page 3 
1  1  Feb 01/98
 1  1
 1CES  1

 AC Emergency Generation - Component Location
 Figure 003
 1EFF :  ALL  1  24-24-00 Page 4 
1  1  Feb 01/98
 1  1
 1CES  1

 Electrical Emergency Generating System - Schematic
 Figure 004

R 1EFF : 001-049, 051-099, 101-105, 201-203, 1 24-24-00Page 5/6 1 1 May 01/05 1 1 1CES
1

 Electrical Emergency Generating System - Schematic
 Figure 004A

R 1EFF : 106-149, 151-199, 204-299, 301-399, 1 24-24-00Page 7/8 1401-499, 1Aug 01/05 1 1 1CES

 **ON A/C ALL
 4. Component Description_____________________ The emergency generation system is mainly composed of: - a Constant Speed Motor/Generator (CSM/G) including a hydraulic motor and an AC generator, - a Generator Control Unit (GCU). A hydraulic motor drives the emergency generator. A servo valve speed regulator controls the speed: it transforms the oil flow of the Blue hydraulic system into constant speed for the generator. When emergency conditions are met, this Blue system is supplied by a Ram Air Turbine (RAT).
 NOTE : The Blue hydraulic system is supplied by an electric pump in normal____ configuration.
 A. Constant Speed Motor/Generator
 (1) Hydraulic motor: - Powered by the Blue hydraulic circuit (RAT in emergency configuration ; electrical hydraulic pump in test), - speed regulation by servovalve, - integrated solenoid control valve.
 (2) AC generator: - Three phase 115V/200 V - 400 Hz (12000 rpm), - output power: 5 KVA continuously, - oil cooled. 
R  **ON A/C 051-052, 
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM ELECTRICAL POWER 電源1(158)