(5)
(3)
Put blanking caps on the disconnected electrical connectors.
(4)
Remove the screws (6), the washers (7) and the mini inverter (8).
EFF : ALL
25-44-41Page 403
Static Inverter - Razor Supply Figure 401/TASK 25-44-41-991-001
R EFF : 001-049, 051-099, 101-105, 151-152, 201-206, 25-44-41 Page 404 May 01/05
CES
Mini Inverter - Razor Supply Figure 401A/TASK 25-44-41-991-001-A
R EFF : 106-149, 153-199, 207-299, 301-399, 401-499, 25-44-41 Page 405 Aug 01/05
CES
**ON A/C ALL
TASK 25-44-41-400-001
Installation af the Static Inverter - Razor Supply
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from
the External Power 25-23-42-000-002 Removal of the Ceiling Panels - Aft Utility Area 25-23-42-400-002 Installation of the Ceiling Panels - Aft Utility Area 25-44-00-710-001 Operational Test of the Razor Supply System
R **ON A/C 001-049, 051-099, 101-105, 151-152, 201-206,
25-44-41-991-001 Fig. 401
EFF : ALL
25-44-41Page 406
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R **ON A/C 106-149, 153-199, 207-299, 301-399, 401-499,
25-44-41-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
**ON A/C 001-049, 051-099, 101-105, 151-152, 201-206,
Subtask 25-44-41-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
(2)
Make sure that the ceiling panel 261CC is removed (Ref. TASK 25-23-42-000-002).
R **ON A/C 106-149, 153-199, 207-299, 301-399, 401-499,
Subtask 25-44-41-860-050-A
A. Aircraft Maintenance Configuration
(1) Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
EFF : ALL
25-44-41Page 407
**ON A/C 001-049, 051-099, 101-105, 151-152, 201-206,
Subtask 25-44-41-865-052
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
2001VU LAV SHAVER SOCKET 1MT 01 E
OR
2001VU LAV SHAVER SOCKET 1MT 01 C
R **ON A/C 106-149, 153-199, 207-299, 301-399, 401-499,
Subtask 25-44-41-865-053
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
2000VU LAV LIGHT 1LQ 01 C
OR
2000VU TOILET LIGHT 1LQ 01 C
**ON A/C ALL
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-105, 151-152, 201-206,
Subtask 25-44-41-420-050
A. Installation of the Static Inverter 2MT
(Ref. Fig. 401/TASK 25-44-41-991-001)
(1) Put the static inverter (3) in position and install the washers (1) and the screws (2) (Ref. TASK 20-28-00-912-004).
EFF : ALL
25-44-41Page 408
(2)
TORQUE the screws (2) to between 0.37 and 0.48 m.daN (32.74 and 42.47 lbf.in).
(3) 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 EQUIPMENT/FURNISHINGS 设备3(108)
