(2)
Remove the warning notice(s).
1EFF : ALL 1 24-56-55Page 410 1 1 Aug 01/05R 1 1 1CES 1
TASK 24-56-55-000-002
Removal of the Contactor Located in the Panel 200VU WARNING : MAKE SURE THAT NO AC OR DC POWER IS CONNECTED TO THE AIRCRAFT
_______ ELECTRICAL CIRCUITS. THERE IS A RISK OF ELECTROCUTION IF THE AC OR DC POWER STAYS CONNECTED.
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 warning notice
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-23-41-000-001 Removal of the Ceiling Panels 25-23-42-000-001 Removal of the Ceiling Panels - Forward Utility Area 24-56-55-991-002 Fig. 402
1EFF : ALL 1 24-56-55Page 411 1 1 May 01/04R 1 1 1CES 1
3. Job Set-up
__________
**ON A/C 001-049, 051-060, 101-102, 201-201,
Subtask 24-56-55-860-052
A. Safety Precautions
(1)
In the cockpit, on the overhead ELEC panel 35VU, make sure that the GALLEY pushbutton switch is released (the OFF legend is on).
(2)
Put a warning notice on the ELEC panel 35VU to tell persons not to operate the GALLEY pushbutton switch.
R **ON A/C 061-099, 103-149, 151-199, 202-299, 301-399, 401-499,
Subtask 24-56-55-860-052-A
A. Safety Precautions
(1)
In the cockpit, on the overhead ELEC panel 35VU, make sure that the GALY & CAB pushbutton switch is released (the OFF legend is on).
(2)
Put a warning notice on the ELEC panel 35VU to tell persons not to operate the GALY & CAB pushbutton switch.
**ON A/C ALL
Subtask 24-56-55-010-051
B. Removal of the Ceiling Panels
(1) Remove the ceiling panels (Ref. TASK 25-23-41-000-001) and the forward utility area ceiling panels (Ref. TASK 25-23-42-000-001).
Subtask 24-56-55-865-053
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------R **ON A/C ALL
**ON A/C 001-049, 051-060, 101-102, 201-201,
122VU ELEC/GALLEY/CTL **ON A/C ALL 1XA S26
R 122VU ELEC/GALLEY/CNTOR **ON A/C 061-099, 103-149, 151-199, 202-299, 301-399, 401-499, 7MC S28
122VU ELEC/GALY & CAB/CTL **ON A/C ALL 1XA S26
123VU FWD GALLEY/FEEDER F 123VU AFT GALLEY/FEEDER E **ON A/C 301-399, 16MC 14MC AC10AF09
R 123VU FWD GALLEY/FEEDER C 123VU FWD GALLEY/FEEDER D 1MC 2MC AE03AE02
R **ON A/C 301-399, 401-499,
R R 123VU AFT GALLEY/FEEDER A **ON A/C 401-499, 3MC AF04
R R R 123VU AFT GALLEY/FEEDER B 123VU FWD GALLEY/FEEDER D 123VU FWD GALLEY/FEEDER C 12MC 2MC 1MC AD09 AD04 AF09
4. Procedure
_________
(Ref. Fig. 402/TASK 24-56-55-991-002)
Subtask 24-56-55-020-051
A. Removal of the Contactor CAUTION : REMOVE THE CONTACTOR ONLY AND NOT THE BASE OR THE MODULE WHERE
_______
THE WIRES ARE CONNECTED.
(1)
Disconnect the electrical connector (4).
(2)
Put blanking caps on the disconnected electrical connectors.
(3)
Loosen the 6 captive screws (5). NOTE : Do not remove the captive screws (5) and the spring washers
____ (6) from the contactor (3).
(4) Remove the contactor (3).
Contactor Located in the Panel 200VU Figure 402/TASK 24-56-55-991-002
1EFF : 1 1R 1CES ALL 1 11 1 24-56-55 Page 415 May 01/04
TASK 24-56-55-400-002
Installation of the Contactor Located in the Panel 200VU
WARNING : MAKE SURE THAT NO AC OR DC POWER IS CONNECTED TO THE AIRCRAFT
_______
ELECTRICAL CIRCUITS.
THERE IS A RISK OF ELECTROCUTION IF THE AC OR DC POWER STAYS
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(132)