A320飞机维护手册 AMM FUSELAGE 机身3(114)

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R  centerline, external surface. 
R  NOTE : This does not include the area under the scuff plates.____ 
R  NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-51-11-101) for____ 
R  the allowable damage limits. 
R  NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-51-11-201) for____ 
R  the correct repair procedure. 
R  5. Close-up________ 
R  Subtask 53-51-00-942-069 
R  A. Remove the ground support equipment. 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Remove the warning notice(s). 
R  (3) Remove the access platform(s).

 EFF : ALL
53-51-00Page 664
May 01/03

R Fuselage Skin around Cutout for Tail Compartment Acces Door R Figure 616/TASK 53-51-00-991-019
 EFF : ALL
53-51-00Page 665
May 01/03 CES

 TASK 53-51-00-210-018
 General Visual Inspection of the Fuselage External Surface and the Vertical Stabilizer Attachment Fitting, below the Vertical Stabilizer/Fuselage Fairings
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 535126-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific lint-free cloth No specific nonmetallic scraper No specific warning notice No specific access platform 6.0 m (19 ft. 8 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004  USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
 Material No. 15-005  AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 Material No. 15-005A  AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 Material No. 15-006  AIB TN 10138 TYPE I GRADE 3 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 EFF : ALL
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R
 CES  C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
53-55-11-000-001 Removal of the Fairings 323AL/323AR
 53-55-11-400-001 Installation of the Fairings 323AL/323AR
 ASRM 535100000 (for corrective action)

R 53-51-00-991-018 Fig. 617
 3. Job Set-up
__________
 Subtask 53-51-00-010-074

 A. Get Access WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
 BEFORE YOU START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 (1)
 Put a warning notice in position to tell persons not to operate the flight controls.

 (2)
 Put the access platform in the required position.

 (3)
 Remove the vertical stabilizer fairings 323AL, 323AR (Ref. TASK 53-55-11-000-001).

 Subtask 53-51-00-110-065
 B. Cleaning Procedure WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
 EFF : ALL
53-51-00Page 667

 WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______ AREA WHEN YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15 MINUTES. -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS.
 (1)
 Use a nonmetallic scraper to remove the old temporary protective compound from the area to be inspected.

 (2)
 Clean the area with a lint-free cloth and the CLEANING AGENTS (Material No. 11-004), and let the area dry.

 4. Procedure
_________
R (Ref. Fig. 617/TASK 53-51-00-991-018)
　
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