(6)
 Disconnect the inflation hose (16) from the fuselage union (15).

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 CES

 (7)
 Put blanking plugs on the disconnected line ends.

 (8)
 Put blanking caps on the disconnected electrical connectors.

 (9)
 Remove the escape slide enclosure (7) from the aircraft. NOTE : Make sure that all related components (seal attach plate (12),

____ seal strips(9), screws (10), countersunk washers (11)), removed with the escape slide enclosure (7) are kept together. They are made to operate as a complete assembly.
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 CES  TASK 25-62-42-920-001 Offwing Escape-Slide - Remove for Restoration

 1.
 Reason for the Job

__________________
 Refer to the MPD TASK: 256242-02

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-62-42-000-001 Offwing Escape-Slide - Removal 25-62-42-400-001 Offwing Escape-Slide - Installation
 3. Job Set-up
__________ Subtask 25-62-42-010-058
 A. Get Access
 (1) Remove the offwing escape-slide (Ref. TASK 25-62-42-000-001).
 4. Procedure
_________ Subtask 25-62-42-920-051
 A. Workshop Procedure
 (1) Do the restoration of the offwing escape-slide, and refer to the manufacturers Component Maintenance Manual (CMM) for the correct procedures.
 5. Close-up
________ Subtask 25-62-42-410-057
 A. Close Access
 (1) Install a serviceable or replacement offwing escape-slide (Ref. TASK 25-62-42-400-001).
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 CES  TASK 25-62-42-400-001

 Offwing Escape-Slide - Installation
 1. Reason for the Job__________________
 Self Explanatory
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific 1 ACCESS PLATFORM 2M (6 FT)
 No specific Torque Wrench : range 0.20 to 3.60 m.daN

 (2.00 to 26.00 lbf.ft) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER FOR FIN 7504MM No specific 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE FOR FIN 7505MM No specific 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE No specific 1 WARNING NOTICE 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
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
 33-51-00-710-001  Operational Test of Emergency Lights by 'TEST EMER LIGHT SYS' Pushbutton
 52-30-00-860-001  Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump
 52-30-00-860-002  Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump
 25-62-42-991-005  Fig. 402
 FOR FIN 7505MM
 25-62-46-400-001  Inflation Reservoir, Offwing Escape-Slide -Installation
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 CES  -------------------------------------------------------------------------------

REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
27-50-00-866-009 Retraction of the Flaps on the Ground
 3. Job Set-up
__________
 Subtask 25-62-42-860-050
 A. Aircraft Maintenance Configuration
 (Ref. Fig. 402/TASK 25-62-42-991-005)

 (1)
 Make sure that the ground service is energized (Ref. TASK 24-42-00-861-001).

 (2)
 Make sure that the AFT cargo compartment door is open (Ref. TASK 52-30-00-860-001).

 (3)
 Make sure that the ACCESS PLATFORM 2M (6 FT) is in position adjacent to the AFT cargo compartment exit.
　
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