____ (745.0058 hPa) instead of a pressure plate.
EFF : ALL 25-00-00Page A820
Aug 01/05
R
CES
(i) Remove the unwanted resin. NOTE : Refer to the manufacturer's instructions for the curing
____
times.
(10)
Make sure the thickness of the repair is not more than 0.8 mm (0.0314 in.).
(11)
If necessary, correct the thickness with a emery cloth, grade 80-120 .
(12)
If necessary, cut the repair to the correct shape (ref. detail A).
(13)
Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-060) to the rear side of the repair.
(14)
Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-005) to the rear side of the repair.
5. Close-up
________ Subtask 25-00-00-420-058
A. Install the applicable Panels in the cargo compartments
(1)
Install the decompression panels (Ref. TASK 25-68-41-960-001).
(2)
Install the FWD cargo-compartment partition at FR24 (Ref. TASK 25-54-11-000-001).
(3)
Install the ceiling panels in the FWD cargo compartment (Ref. TASK 25-54-12-000-002).
(4)
Install the ceiling panels in the AFT cargo compartment (Ref. TASK 25-55-12-000-002).
Subtask 25-00-00-410-054
B. 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 A821
Aug 01/05
R
CES
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items. Subtask 25-00-00-862-059
C. De-energize the ground service network (Ref. TASK 24-42-00-862-001).
EFF : ALL 25-00-00Page A822
Aug 01/05
R
CES TASK 25-00-00-340-004
Filler Repair Method (Damage not Through) - All Cargo Compartment Linings with Honeycomb Core
1. Reason for the Job
__________________
Refer to the AMM task 25-00-00-200-001
2. Job Set-up Information
______________________
A. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific emery cloth, grade 80-120 Material No. 08-115 AIB AIMS 08-08-001
CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00) Material No. 08-115A AIB AIMS 08-08-001
CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00) Material No. 08-115B AIB AIMS 08-08-001
CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00) Material No. 08-115C D DAN 1282
CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00) Material No. 11-010 USA TT-I-735 GRADE A
ISOPROPYL ALCOHOL (Ref. 20-31-00) Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-00-00-200-001 Cargo Compartment Linings with Honeycomb Core -
General Repair/Protection Information 25-00-00-991-038 Fig. 824
3. Job Set-up
__________
Subtask 25-00-00-010-058
A. Get Access
(Ref. TASK 25-00-00-200-001)
EFF : ALL 25-00-00Page A823
Aug 01/05
R
CES 4. Procedure
_________
Subtask 25-00-00-220-063
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 should be considered as a single damage.
Subtask 25-00-00-340-055
B. Repair of the Core and/or Edge of the Cargo Compartment Lining with
Filler
(Ref. Fig. 824/TASK 25-00-00-991-038)
(1)
Remove the damaged material from the lining panel.
(2)
Deburr the edges with emery cloth, grade 80-120
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE
_______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
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(75)
