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时间:2011-03-21 08:20来源:蓝天飞行翻译 作者:admin
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25-00-00-200-001  Cargo Compartment Linings with Honeycomb Core -
General Repair/Protection Information 25-00-00-991-027 Fig. 822 25-00-00-991-042 Fig. 833
 EFF : ALL  25-00-00Page A867

Aug 01/05
R
 CES  3. Job Set-up


__________
 Subtask 25-00-00-010-090
 A. Get Access
 (Ref. TASK 25-00-00-200-001)

 4. Procedure
_________
 Subtask 25-00-00-220-060
 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)
 Types of repair patch:


 (a) You can use the subsequent repair patches to do the repair.
 -a sheet of Stainless Steel 0.6 mm (0.024 in.) to 2 mm (0.08 in.) with
 -
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-010A) or

 -
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-001) or

 -
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-066)


 Subtask 25-00-00-340-095
 B. Do the Repair
 WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
 MATERIAL.
 THIS MATERIAL IS DANGEROUS.

 EFF : ALL 25-00-00Page A868

Aug 01/05
R
 CES  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. 833/TASK 25-00-00-991-042)
 NOTE : Do not use the patch to overlap another repair.
____
 (1)
 Remove the damaged area from the panel.

 (2)
 Smooth and deburr the repair with 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.

 NOTE : The overlap of patches is not permitted
____
 (6)
 Deburr the edges of the patch with emery cloth grade 80-120.

 (7)
 Apply:


 -BONDING AND ADHESIVE COMPOUNDS (Material No. 08-010A)
 - or BONDING AND ADHESIVE COMPOUNDS (Material No. 08-001)
 - or BONDING AND ADHESIVE COMPOUNDS (Material No. 08-066)

 on one side of the repair patch.
 (8)
 Put the repair patch over the damaged area and push it into position.

 (9)
 Let the repair dry.
 NOTE : Obey the manufacturers instructions.

 

____
 (10) Follow the curing recommendations of the selected adhesive.
 EFF : ALL 25-00-00Page A869

Aug 01/05
R
 CES


 CC Honeycomb Linings, Stainless Steel Patch - Damage Not Through Figure 833/TASK 25-00-00-991-042
 EFF : ALL 25-00-00Page A870 Aug 01/05 R CES


 (11) On, or before the time limit (400 FH) of this temporary repair, replace the repair with a permanent repair. (Ref. Fig. 822/TASK 25-00-00-991-027) ________
5. Close-up
 Subtask 25-00-00-410-084
 A. Close Access
 (Ref. TASK 25-00-00-200-001)

 EFF : ALL 25-00-00Page A871

Aug 01/05
R
 CES  TASK 25-00-00-340-028


 Speed Patch and Filler to the Edge Repair Method (Damage Not Through from the Edge) - All Cargo Compartment Linings with Honeycomb Core
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific emery cloth grade 80-120. No specific GILLPATCH III 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
 
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