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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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 CES


 Wash Basin Waste-Flap Area Figure 813/TASK 25-00-00-991-031- 14 (SHEET 1) 
R  EFF : 004-049, 053-099, 101-105, 151-199, 301-399, 401-499,  25-00-00 Page 870 Aug 01/05
 CES 

 

 Wash Basin Waste-Flap Area Figure 813/TASK 25-00-00-991-031- 24 (SHEET 2) 
R  EFF : 004-049, 053-099, 101-105, 151-199, 301-399, 401-499,  25-00-00 Page 871 Aug 01/05
 CES 

 

 Wash Basin Waste-Flap Area Figure 813/TASK 25-00-00-991-031- 34 (SHEET 3) 
R  EFF : 004-049, 053-099, 101-105, 151-199, 301-399, 401-499,  25-00-00 Page 872 Aug 01/05
 CES 

 

 Wash Basin Waste-Flap Area Figure 813/TASK 25-00-00-991-031- 44 (SHEET 4) 
R  EFF : 004-049, 053-099, 101-105, 151-199, 301-399, 401-499,  25-00-00 Page 873 Aug 01/05
 CES 

 

 (d) Apply the prepared adhesive, item of the DCIN900 VARICOR repair kit to the repair area of the wash basin.
 NOTE : Obey the manufacturers instructions.
____
 (e)
 Put the replacement part (3) in position with a light pressure and set it with a PLIERS - NOSE, SOFT, LONG or a wooden block.

 (f)
 Let the repair cure at a temperature of:
 20 deg.C (68.00 deg.F) for 6 hours,
 25 deg.C (77.00 deg.F) for 4 hours,
 30 deg.C (86.00 deg.F) for 3 hours

 

 NOTE : Obey the manufacturers instructions.
____
 (g) Remove the pliers or the wooden block and the masking tape.
 (3)
 Make the repair area smooth with:

 -
the abrasive paper, grain 180,

 -
the abrasive paper, grain 220,

 -
the abrasive paper, grain 320
 and


 -
the abrasive fleece
 of the DCIN900 VARICOR repair kit.

 


 (4)
 Release the flap (1) and make sure that it closes correctly.

 (5)
 Clean and polish the wash basin (Ref. TASK 12-21-12-100-009).


 5. Close-up
________ Subtask 25-00-00-942-076
 A. Close-up
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.


 Subtask 25-00-00-862-070
 B. De-energize the ground service network
 (Ref. TASK 24-42-00-862-001).


R  EFF : 004-049, 053-099, 101-105, 151-199, 25-00-00Page 874 301-399, 401-499, Aug 01/05
 CES R **ON A/C ALL

 

R TASK 25-00-00-370-001 R Repair of Painted Components R 1. Reason for the Job
__________________ R Self Explanatory R 2. Job Set-up Information
______________________
R A. Fixtures, Tools, Test and Support Equipment
R -------------------------------------------------------------------------------R REFERENCE QTY DESIGNATION R -------------------------------------------------------------------------------
R No specific 2 GUN - AIR SPRAY, STANDARD PAINT R No specific 2 NOZZLE DIA 1.5 MM (1/16 IN)
R B. Consumable Materials
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R No specific R No specific R No specific R Material No. 08-074 R R Material No. 11-010 R R Material No. 16-046 R R Material No. 16-047 R R Material No. 19-003 R
emery cloth, 320-400 grade
masking paper
4 mm (0.16 in.) DIN cup

MASKING TAPE (Ref. 20-31-00)
USA TT-I-735 GRADE A
ISOPROPYL ALCOHOL (Ref. 20-31-00)
D DAN 1278
PRIMER (Ref. 20-31-00)
F ASNA3687
DECORATIVE PAINT (INTERNAL APPLIC.) (Ref. 20-31-00)
USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)


R EFF : ALL 25-00-00Page 875 Aug 01/05
 CES R C. Referenced Information


R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 24-42-00-861-001 R R 24-42-00-862-001 R R 25-13-00-370-001 R FAR 25.853(a-1)
R 3. Job Set-up
__________ Energize the Ground Service Network from the External Power De-energize the Ground Service Network Supplied from the External Power Painting of the Internal Cockpit Surfaces
R Subtask 25-00-00-861-089
R A. Energize the ground service network R (Ref. TASK 24-42-00-861-001). R Subtask 25-00-00-010-097 R B. If necessary, remove the component you will repair from the aircraft
R (refer to the related AMM chapter). R 4. Procedure
 
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