_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(Ref. Fig. 827/TASK 25-00-00-991-043)
(1)
Carefully remove the damaged material from the lining.
(2)
Remove the rough edges with emery cloth, grade 80-120.
(3)
Clean the area with CLEANING AGENTS (Material No. 11-010) and a lint free cotton cloth MISCELLANEOUS (Material No. 19-003)
(4)
Do an inspection of the component interface and/or the adjacent area. NOTE : Make sure that all components behind the lining you will
____
repair are not damaged.
(5)
Cut two repair patches to the applicable dimensions. NOTE : The repair patch (1) must be 38 mm (1.5 in.) larger than the
____
damaged area in all directions.
NOTE : The repair patch (2) must be 50 mm (2.0 in.) larger than
____
repair patch (1) in all directions.
EFF : ALL 25-00-00Page A837
Aug 01/05
R
CES
CC Honeycomb Linings, Two Patches - Damage Through Figure 827/TASK 25-00-00-991-043
R EFF : CES ALL 25-00-00 Page A838 Aug 01/05
NOTE : Do not use the patch to overlap another repairs.
____
(6)
Deburr the edges of the two repair patches with emery cloth grade 80-120..
(7)
Remove the protective backing from the repair patch (1).
(8)
Put the patch (1) over the damaged area and push it in position.
(9)
Remove the protective backing from the repair patch (2).
(10) Put the repair patch (2) over the patch (1) and push it in position.
5. Close-up
________ Subtask 25-00-00-410-073
A. Close Access
(Ref. TASK 25-00-00-200-001)
EFF : ALL 25-00-00Page A839
Aug 01/05
R
CES TASK 25-00-00-340-019
Replacement of Cargo Compartment Ceiling Panel, Side Wall Panel and Partition Panel
1. Reason for the Job
__________________
Refer to the AMM task 25-00-00-200-001
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 1 CUTTER - THIN BLADE No specific 1 KNIFE - SHAPED
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific emery cloth, 80-120 grade Material No. 11-010 USA TT-I-735 GRADE A
ISOPROPYL ALCOHOL (Ref. 20-31-00) Material No. 16-053 D DAN 1282-02
FILLER FOR CORE AND EDGE (2 PARTS) (Ref. 20-31-00) Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-00-00-200-001 Cargo Compartment Linings with Honeycomb Core -
General Repair/Protection Information SIL 25-097
EFF : ALL 25-00-00Page A840
Aug 01/05
R
CES 3. Job Set-up
__________ Subtask 25-00-00-010-082
A. Get Access
(Ref. TASK 25-00-00-200-001)
4. Procedure
_________ Subtask 25-00-00-340-088-A
A. Replacement
(1) Remove all anchor-nuts, clip-nuts and other items from the damaged panel.
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE
_______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
CAUTION : MAKE SURE THAT THE THICKNESS OF THE NEW PANEL IS THE SAME
_______ AS THE THICKNESS OF THE REMOVED PANEL. IF IT IS NOT THE SAME, THERE WILL NOT BE SUFFICIENT FIRE-PROTECTION IN THE CARGO COMPARTMENT.
(2)
Cut the semi-finished replacement material (according to the (Ref. SIL 25-097)) with a CUTTER - THIN BLADE or a KNIFE - SHAPED to the necessary dimension.
(3)
Smooth and deburr the edges with emery cloth, 80-120 grade .
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM EQUIPMENT/FURNISHINGS 設(shè)備1(79)
