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时间:2011-03-27 08:47来源:蓝天飞行翻译 作者:admin
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May 01/04
R
 CES

 TASK 53-31-00-220-006


 Special Detailed Inspection of Splice Plate at Circumferential Skin Splice at FR47, from Stringer 10, LH/RH, to Crown Centerline
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 533140-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific abrasive cloth, grade 280 No specific warning notice No specific access platform 5.5 m (18 ft. 1 in.) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004  USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
 Material No. 19-003  USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 EFF : ALL  53-31-00Page A650

May 01/04
R
 CES


 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
51-75-12-300-001 Repair of Major Paint Damage on Light Alloy and
 Composite Material 51-75-12-300-003 Repair of Minor Paint Damage (Topcoat Only) ASRM 51-11-00-001 ASRM 51-22-00-001 ASRM 53-31-11-001 NTM 533140-Part.6 ASRM 51-73-00-001 (for corrective action) ASRM 51-74-00-001 (for corrective action) 53-31-00-991-045 Fig. 629
 3. Job Set-up
__________
 Subtask 53-31-00-860-060
 A. Aircraft Maintenance Configuration
 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)
 Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever when working near the flaps/slats.

 (2)
 Put the warning notice on the slat/flap control lever to tell persons not to operate the slats.


 Subtask 53-31-00-010-084
 B. Get Access
 (1) Put the access platform in position adjacent to FR47.
 EFF : ALL 53-31-00Page A651

May 01/04
R
 CES


 Subtask 53-31-00-860-059

 C. Preparation of the Inspection Areas (Ref. Fig. 629/TASK 53-31-00-991-045)
 (1) Make sure that the outer surface of the inspection area is clean and smooth.
 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
_______ 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.
 (2)
 If necessary, clean the outer surface of the inspection area with the CLEANING AGENTS (Material No. 11-004) and a MISCELLANEOUS (Material No. 19-003). Make sure the inspection area is dry before you continue.

 (3)
 If necessary, make the outer surface of the inspection area smooth with the abrasive cloth, grade 280.

 (4)
 Do a visual inspection of the outer surface of the inspection area. Look for damage, and defects in the shape of the external surface.

 (5)
 If you find damage :

 (a)
 Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification of the damage.

 (b)
 If you find corrosion damage:

 -
refer to the ASRM (Ref. ASRM 51-22-00-001) for the general corrosion data

 -
refer to the ASRM (Ref. ASRM 51-74-00-001) for the repair of the corroded areas.

 

 


 EFF : ALL 53-31-00Page A652

May 01/04
R
 CES


 Circumferential Skin Splice at FR47, from STGR10 LH/RH to Crown Centerline Figure 629/TASK 53-31-00-991-045
 
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