Areas of the Moisture-Removing Oil Coating
 Figure 002

R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 51-23-00Page 4 1301-399, 1May 01/05 1 1 1CES 1

 Areas of the Moisture-Removing Oil Coating
 Figure 002A

R 1EFF : 151-199, 401-499, 1 51-23-00Page 5 1 1 Aug 01/05 1 1 1CES 1

R R  Fuselage External Areas - Coatings Figure 003
 1EFF : 1 1 1CES  ALL  1 111 51-23-00 Page 6 Aug 01/04

R  Areas of Moisture Removing Oil Coating (External) Figure 004
 1EFF : 1 1 1CES  ALL  1 111 51-23-00 Page 7 Feb 01/04

 C. Wing Internal Areas
 (Ref. Fig. 005)

 1EFF : ALL 1 51-23-00Page 8 1 1 May 01/04R 1 1 1CES 1

 Wing - Coatings Figure 005
 1EFF : 1 1R 1CES  ALL  1 11 1 51-23-00 Page 9 Feb 01/04

 D. Wing External Areas
 (Ref. Fig. 005) R

R E. Stabilizer Coatings R (Ref. Fig. 006)

 Stabilizer - Coatings Figure 006
 1EFF : 1 1R 1CES  ALL  1 11 1 51-23-00 Page 12 Feb 01/04

 F. Engine Pylon and Nacelle Coatings (Ref. Fig. 007)
 1EFF : ALL 1 51-23-00Page 13 1 1 May 01/04R 1 1 1CES 1

 External Coatings - Pylon and Nacelle CFM56 Figure 007
 1EFF : 1 1R 1CES  ALL  1 11 1 51-23-00 Page 14 Feb 01/04

 COATINGS APPLICATION - GENERAL - MAINTENANCE PRACTICES
______________________________________________________
 TASK 51-23-00-370-001
 Application of Paint and Protective Coatings - Fuselage Internal Areas
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 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.
 WARNING : DO NOT GET THE COMPOUND ON YOUR SKIN.
_______ IF YOU DO:
 -RUB IT OFF IMMEDIATELY WITH A CLEAN CLOTH
 -WASH THE SKIN WITH SOAP AND RINSE WITH CLEAN WATER.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 1 ACCESS PLATFORM 2M (6 FT) No specific 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE No specific 1 WARNING NOTICE

 B. Consumable Materials

 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 13-002  USA MIL-C-5541 MIL-C-81706 CLASS I/A
 CHEMICAL CONVERSION COATING YELLOW ALUMINUM
 (Ref. 20-31-00)

 Material No. 15-004  USA MIL-C-16173 GRADE 3
 CORROSION PREVENTIVE COMPOUND (Ref. 20-31-00)
R Material No. 15-007 AIB TN 10138 TYPE II GRADE 1
R  CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND
R (Ref. 20-31-00) Material No. 16-002 GB BAEP 3536 POLYURETHANE TOPCOAT GREY (FOR INTERNAL APPLIC.) (Ref. 20-31-00) Material No. 16-006 ANTI-CORROSION PRIMER (EPOXY-IMPRVD ADHESION) (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
21-20-00-010-001 Removal of the Air-Conditioning Distribution Ducts 21-20-00-410-001 Installation of the Air-Conditioning Distribution
 Ducts 25-23-43-000-001 Removal of the Upper Sidewall Panel(s) 25-23-43-400-001 Installation of the Upper Sidewall Panel(s) 25-23-44-000-001 Removal of the Lower Sidewall-Panels (Dado Panels) 25-23-44-400-001 Installation of the Lower Sidewall-Panels (Dado
 Panels) 25-23-45-000-002 Removal of the Door Frame Linings at the Right FWD Passenger/Crew Door 25-23-45-000-003 Removal of the Door Frame Linings at the Left AFT Passenger/Crew Door 25-23-45-000-004 Removal of the Door Frame Linings at the Right AFT Passenger/Crew Door 25-23-45-000-005 Removal of the Door Frame Linings at the Left FWD Passenger/Crew Door 25-23-45-400-005 Installation of the Door Frame Linings at the Right
 AFT Passenger/Crew Door
 25-23-45-400-006 Installation of the Door Frame Linings at the Left
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM STANDARD PRACTICES AND STRUCTURES(7)