Aug 01/05
R
CES 3. Job Set-up
__________
Subtask 25-00-00-010-093
A. Get Access
(Ref. TASK 25-00-00-200-001)
4. Procedure
_________
Subtask 25-00-00-220-066
A. Identify the Damage Limits (Ref. TASK 25-00-00-200-001)
(1)
If the length of a damaged area is more than 25 mm (0.98 in.):
-the minimum distance to another damaged area or repaired area in the same panel is 50 mm (1.97 in.)
-If the distance to another damaged area is less than 50 mm (1.97 in.), both damaged areas must be considered as a single damage.
(2)
Type of repair patch:
-GILLPATCH III
Subtask 25-00-00-340-099
B. Do the Repair
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ 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. 834/TASK 25-00-00-991-046)
NOTE : Do not use the patch to overlap another repair.
____
(1) Remove the damaged material from the core and the edge of the lining panel.
EFF : ALL 25-00-00Page A873
Aug 01/05
R
CES
CC Honeycomb Linings, Filler/Patch - Damage Not Through from the Edge Figure 834/TASK 25-00-00-991-046
EFF : ALL 25-00-00Page A874 Aug 01/05 R CES
(2)
Make smooth and deburr the edges of the repair with a emery cloth
grade 80-120.
(3)
Clean the repair area with CLEANING AGENTS (Material No. 11-010) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
(4)
Make sure that the repair area is dry.
(5)
Cut a patch to the applicable dimensions.
NOTE : The repair patch must be 38 mm (1.5 in.) larger than the
____
damaged area in all directions.
(6)
Deburr the edges of the patch with a emery cloth grade 80-120.
(7)
Make sure that the repair area is dry.
(8)
Remove the protective foil from the patch.
NOTE : Obey the manufacturers instructions.
____
(9)
Put the patch over the damaged area on the view side of the panel and push it into position.
(10) Fill the
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115)
or
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115A)
or
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115B)
or
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115C)
into the prepared area.
NOTE : Obey the manufacturers instructions.
____
NOTE : The quantity of filler used must ensure a minimum width of 10
____
mm (0.4 in) from the edge.
(11) Make the edge of the cured repaired area smooth with a emery cloth grade 80-120.
EFF : ALL 25-00-00Page A875
Aug 01/05
R
CES 5. Close-up
________ Subtask 25-00-00-410-087
A. Close Access (Ref. TASK 25-00-00-200-001)
EFF : ALL 25-00-00Page A876
Aug 01/05
R
CES TASK 25-00-00-340-029
Protection of Cargo Compartment Linings with S-Glass Patch - All Cargo Compartment Linings with Honeycomb Core
1. Reason for the Job
__________________
This task gives a procedure to bond a protection patch (S-glass layer) on the view side of the cargo compartment sidewalls, ceiling and partition panels to make them stronger.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM EQUIPMENT/FURNISHINGS 設備1(88)
