(11)
Remove unwanted sealant around the scuff plates (3), (5) and (9).
(12)
Apply SEALANTS (Material No. 09-030) around and approximately 30 mm (1.1811 in.) from the edges of the scuff plates (3), (5) and (9).
(13)
Cover the scuff plates (3), (5) and (9) with a sheet of porous material.
(14)
Attach the porous material with BONDING AND ADHESIVE COMPOUNDS (Material No. 08-065) to the scuff plates (3), (5) and (9).
(15)
Connect the vacuum valve to the SPECIAL MATERIALS (Material No. 05-068).
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R Scuff Plates - Installation Procedure Figure 402/TASK 53-15-15-991-002- 12 (SHEET 1)
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R Scuff Plates - Installation Procedure Figure 402/TASK 53-15-15-991-002- 22 (SHEET 2)
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(16)
Cover the scuff plates (3), (5) and (9) and SEALANTS (Material No. 09-030) with SPECIAL MATERIALS (Material No. 05-068). You must make an overlap of 30 mm (1.2 in.) from the edge of SEALANTS (Material No. 09-030).
(17)
Connect the vacuum pump to the vacuum valve.
(18)
Operate the vacuum pump to extract the air from the scuff plates (3),
(5) and (9).
Refer to the temperature given in the table: -------------------------------------------------------------------------------TEMPERATURE TIME -------------------------------------------------------------------------------
18 deg.C (64.40 deg.F) for 48 hours 20 deg.C (68.00 deg.F) for 30 hours 23 deg.C (73.40 deg.F) for 24 hours
(19)
Disconnect the vacuum pump.
(20)
Remove the SPECIAL MATERIALS (Material No. 05-068).
(21)
Remove the vacuum valve from the SPECIAL MATERIALS (Material No. 05-068), the porous material, and SEALANTS (Material No. 09-030).
(22)
Apply SEALANTS (Material No. 09-016) on the external joints of the scuff plates (3), (5) and (9) and around the scuff plates.
(23)
Remove unwanted sealant with CLEANING AGENTS (Material No. 11-003) AND MISCELLANEOUS (Material No. 19-003).
5. Close-up
________ Subtask 53-15-15-942-050
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the applicable FWD passenger/crew door (Ref. TASK 52-10-00-410-001).
(3)
Remove the access platform(s).
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CES
MOUNT FITTING - CABIN - REMOVAL/INSTALLATION
____________________________________________
TASK 53-16-11-000-001 Removal of the Mount Fitting at FR 14
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
23-72-51-000-001 Removal of the Anti-Hijack-System Cameras 24-42-00-861-001 Energize the Ground Service Network from the External
Power 25-13-41-000-001 Removal of the Ceiling Panels 25-23-42-000-001 Removal of the Ceiling Panels - Forward Utility Area 52-10-00-010-001 Opening of the Passenger/Crew Door 52-51-11-000-001 Removal of the Cockpit Door 53-16-11-991-001 Fig. 401
3. Job Set-up
__________ Subtask 53-16-11-860-050
A. Aircraft Maintenance Configuration
(1) Energize the ground service network (Ref. TASK 24-42-00-861-001).
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Subtask 53-16-11-010-050
B. Get Access
(1)
Put an access platform in position at zone 831 (841).
(2)
Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-010-001).
(3)
Remove the Anti-Hijack-System Camera (Ref. TASK 23-72-51-000-001), if installed.
(4)
Remove the ceiling panel 221AC (Ref. TASK 25-23-42-000-001).
(5)
Remove the lining panel 211HC (Ref. TASK 25-13-41-000-001).
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