(2)
Close the access door 812.
(3) Remove the access platform(s). Subtask 24-34-00-860-051
B. Put the aircraft back to its initial configuration.
(1)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
(2)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
TRANSFORMER RECTIFIER (1PE) - REMOVAL/INSTALLATION
__________________________________________________ TASK 24-34-51-000-001 Removal of the Essential Transformer Rectifier (1PE)
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
No specific circuit breaker(s) safety clip(s)
No specific insulating sleeve
No specific access platform 1.8 m (5 ft. 11 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-34-51-991-002 Fig. 401
3. Job Set-up
__________ Subtask 24-34-51-010-050
A. Aircraft Maintenance Configuration
(1)
Put an access platform at the avionics compartment door 812.
(2)
Open the access door 812.
(3)
Open the access panel of the AC/DC emergency power center 106VU.
Subtask 24-34-51-865-050
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
R 106VU ESS TR/SPLY 4PE C01 R
4. Procedure
_________
(Ref. Fig. 401/TASK 24-34-51-991-002)
Subtask 24-34-51-020-050
A. Removal of the Essential Transformer Rectifier
(1)
Remove the protective caps from the output terminals (8).
(2)
Remove the nuts (5), (10) and the washers (6), (9).
(3)
Disengage the lugs (7) from the output terminals.
(4)
Put an insulating sleeve on the lugs.
(5)
Disconnect the connectors (4).
(6)
Put blanking caps on the connectors.
(7)
Remove the screws (3) and the washers (2).
(8)
Remove the transformer rectifier (1).
R Essential Transformer Rectifier Figure 401/TASK 24-34-51-991-002
1EFF : 1 1 1CES ALL 1 111 24-34-51 Page 403 Feb 01/00
TASK 24-34-51-400-001
Installation of the Essential Transformer Rectifier (1PE)
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific access platform 1.8 m (5 ft. 11 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-24-00-710-001 Operational Test of the Emergency Generation System 24-34-51-991-002 Fig. 401
3. Job Set-up
__________
Subtask 24-34-51-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position at the access door
812. 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM ELECTRICAL POWER 电源2(40)
