-
Speed Patches (on View Side) Repair Method (Damage Through) - All Cargo Compartment Linings with Honeycomb Core, but not Ceiling Panels (Ref. TASK 25-00-00-340-015)
-Patches and Filler Repair Method (Damage Through) - All Cargo Compartment Linings with Honeycomb Core (Ref. TASK 25-00-00-340-020)
-
Speed Patch Repair Method (Damage not Through) - All Cargo Compartment Lining with Honeycomb Core (Ref. TASK 25-00-00-340-021)
-
Speed Patches and Filler Repair Method (Damage Through) - All Cargo Compartment Linings with Honeycomb Core, but not Ceiling Panels (Ref. TASK 25-00-00-340-022)
-Patches, Filler and Rivets Repair Method (Damage Through) - All Cargo Compartment Linings with Honeycomb Core (Ref. TASK 25-00-00-340-023)
-Speed Patches and Filler Repair Method (Damage not Through) - All Cargo Compartment Linings with Honeycomb Core (Ref. TASK 25-00-00-340-025)
-Stainless Steel-Patch Repair Method (Damage not Through) - All Cargo Compartment Linings with Honeycomb Core (Ref. TASK 25-00-00-340-026)
EFF : ALL 25-00-00Page A813
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-Speed Patch and Filler to the Edge Repair Method (Damage Not Through from the Edge) - All Cargo Compartment Linings with Honeycomb Core (Ref. TASK 25-00-00-340-028)
Subtask 25-00-00-420-083
F. Installation of the Repaired Lining(s) if they are removed to do the Repair Procedure.
(1) Install the repaired linings
(a)
FWD cargo compartment:
-
(Ref. TASK 25-54-11-400-001)
-
(Ref. TASK 25-54-12-400-001)
-
(Ref. TASK 25-54-12-400-002)
-
(Ref. TASK 25-54-12-400-003)
(b)
AFT cargo compartment:
-
(Ref. TASK 25-55-11-400-001)
-
(Ref. TASK 25-55-11-400-002)
-
(Ref. TASK 25-55-11-400-003)
-
(Ref. TASK 25-55-12-400-001)
-
(Ref. TASK 25-55-12-400-002)
-
(Ref. TASK 25-55-12-400-003)
Subtask 25-00-00-918-050
G. Put the aircraft back to its initial configuration.
(1) If necessary, install new placards on the repaired linings (Ref. TASK 11-00-00-400-007) and
-FWD cargo compartment (Ref. AMM 11-35-25 P.Block 001)
-AFT cargo compartment (Ref. AMM 11-36-25 P.Block 001)
5. Close-up
________
Subtask 25-00-00-410-077
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
(3)
Close the cargo compartment door (Ref. TASK 52-30-00-860-002).
EFF : ALL 25-00-00Page A814
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CES Subtask 25-00-00-862-080
B. De-energize the ground service network (Ref. TASK 24-42-00-862-001).
EFF : ALL 25-00-00Page A815
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CES TASK 25-00-00-340-003
Repair to the Flanges of the Cargo-Compartment Decompression Panels
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 1 PLATE - PRESSURE No specific 1 WARNING NOTICE
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific emery cloth, grade 80-120 No specific prefabricated molding block No specific waxed paper Material No. 05-007 USA MIL-C-9084 TYPE VIII B CLASS 2,
GLASSCLOTH, EPOXY LAMINATES (Ref. 20-31-00)
Material No. 08-001 USA DOD-A-82720 GENERAL PURPOSE ADHESIVE HONEYCOMB FILLER (Ref. 20-31-00)
Material No. 08-005 USA L-T-100 TYPE I SEALING TAPE OBSOLETE-USE 08-005A ,B,C, (Ref. 20-31-00)
Material No. 08-060 USA MIL-T-4053 TAPE, PRESSURE SENSITIVE,GLASSCLOTH (Ref. 20-31-00) Material No. 11-010 USA TT-I-735 GRADE A ISOPROPYL ALCOHOL (Ref. 20-31-00)
EFF : ALL 25-00-00Page A816
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C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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