(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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