(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)
　
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