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(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(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 green lines between the EXT PWR and AC 1(2) are present.
(5)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002)
(6) De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
Subtask 24-22-55-710-054
R D. Test of the Generator Line Contactor (GLC) FOR 9XU1, 9XU2 NOTE : This test is for GLC 1. For the GLC 2, use the indications between
____
the parentheses.
(1)
Start the engine 1(2) automatically (Ref. TASK 71-00-00-710-003).
(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 green line between GEN 1(2) and AC 1(2) is present.
(5)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002)
(6)
Stop the engine 1(2) (Ref. TASK 71-00-00-710-028).
5. Close-up
________ Subtask 24-22-55-410-051
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 L lower side of the panel 120VU.
(3)
Install the Third Occupant 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 AUXILIARY GENERATION (APU GENERATOR, GCU OR GAPCU)
_____________________________________________________ DESCRIPTION AND OPERATION
_________________________
1. General
_______
The AC auxiliary generation comes from the APU generator. This generator
can:
-in flight, replace either or both engine generator(s) in case of failure,
- on the ground, supply the aircraft electrical network when the electrical ground power unit is not available.
2. Component Location
__________________
**ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
(Ref. Fig. 001)
**ON A/C 063-099, 106-149, 153-199, 206-299, 301-399,
(Ref. Fig. 001A)
R **ON A/C 401-499,
R (Ref. Fig. 001B)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
(Ref. Fig. 002)
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF.
-------------------------------------------------------------------------------1XS GCU-APU 91VU 121 811 24-23-34 2XS P/BSW-ELEC/APU GEN 35VU 210 831 24-23-00 3XS GLC-APU 120VU 212 831 24-23-55 8XS GEN-APU 310 24-23-51
42XS CT-AC, APU GEN 120VU 212 831 24-23-00
The APU generator is installed in the APU compartment. It is attached to the APU gearbox by a button hole flange.
AC Auxiliary Generation (APU Generator GCU) Component Location Figure 001 (SHEET 1)
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AC Auxiliary Generation (APU Generator GCU) Component Location Figure 001 (SHEET 2)
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AC Auxiliary Generation (APU Generator GCU)
Component Location
Figure 001A (SHEET 1)
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AC Auxiliary Generation (APU Generator GCU)
Component Location
Figure 001A (SHEET 2)
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R AC Auxiliary Generation (APU Generator GAPCU)
R Component Location
R Figure 001B (SHEET 1)
R 1EFF : 401-499, 1 24-23-00Page 6 1 1 Aug 01/05 1 1 1CES 1 中國航空網 m.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(136)
