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时间:2011-03-27 12:37来源:蓝天飞行翻译 作者:航空
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28-00-00-910-001 Fuel Safety Procedures 28-10-00-910-001 Safety Procedures When You Do Work in a Fuel Tank 28-10-00-910-002 Access to the Fuel Tanks and the Work Areas 51-76-12-300-002 Repair of the Fuel Tank Fillet 57-27-11-000-001 Removal of the Access Panel (540AB, 540BB, 540CB,
 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)
 57-27-11-400-001  Installation of the Access Panel (540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)
 NTM 571185,P.Block-401
 SRM 517612,P.Block-001
 SRM 511100,P.Block 001 (for corrective action)
 SRM 512200,P.Block 001 (for corrective action)


R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 57-10-00-991-029-A  Fig. 619
 **ON A/C 301-399,
 57-10-00-991-029-B  Fig. 619A
 **ON A/C ALL
 3. Job Set-up
__________
 Subtask 57-10-00-941-069
 A. Safety Precautions
 WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
 (1)
 Obey the fuel safety precautions (Ref. TASK 28-00-00-910-001) and (Ref. TASK 28-10-00-910-001).

 (2)
 Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.

 (3)
 Install warning notices in the cockpit to tell persons not to operate the flaps or slats.

 


 Subtask 57-10-00-010-083
 B. Get Access
 (1)
 Put an access platform in position below the access panels 540AB and 640AB.

 (2)
 Remove the access panels (Ref. TASK 57-27-11-000-001), (Ref. TASK 28-10-00-910-002):

 -
For the left wing: 540AB

 -
For the right wing: 640AB.

 

 (3)
 Open the RIB2 surge doors:

 -for the left wing: 540AZ, 540BZ
 -For the right wing: 640AZ, 640BZ.

 (4)
 Install the HOOK-COVER (RIB 2 SURGE DOORS) (98D57004013000) on the forward surge doors.

 (5)
 Install the HOOK-COVER (RIB2-SURGE DOORS) (98D57004014000) on the aft surge doors.


 (6) Use a flashlight for the inspection.
 Subtask 57-10-00-110-072

 C. Preparation for the Inspection R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 619/TASK 57-10-00-991-029-A)
 **ON A/C 301-399,

 (Ref. Fig. 619A/TASK 57-10-00-991-029-B)


 Outer Wing Box - Vertical Tee Fitting - Inspection Area Figure 619/TASK 57-10-00-991-029-A
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-10-00Page 695 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1


 Outer Wing Box - Vertical Tee Fitting - Inspection Area R Figure 619A/TASK 57-10-00-991-029-B
R 1EFF : 301-399, 1 57-10-00Page 696 1 1 May 01/05 1 1 1CES 1

 **ON A/C ALL


 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 : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
 (1)
 Remove sealant from the fasteners in the inspection area.

 (2)
 Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if necessary.

 (3)
 Make sure that the surface of the inspection area is clean and smooth.

 (4)
 Do a visual check of the inspection area for damage or discontinuities.

 (5)
 Make sure that there is no:

 (a)
 Corrosion damage:

 -If you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 512200,P.Block 001) for types of corrosion, inspection, removal and corrosion protection.

 (b)
 Other damage (cracks, scratches, stress, marks, dents, bumps, ...):

 


 -If you find other damage, refer to the Structural Repair Manual (Ref. SRM 511100,P.Block 001) for damage classification and corrective action.
 1EFF : ALL 1 57-10-00Page 697 1 1 May 01/05R 1 1 1CES 1


 4. Procedure
_________
 Subtask 57-10-00-270-054

 A. Inspection R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 619/TASK 57-10-00-991-029-A)
 **ON A/C 301-399,

 (Ref. Fig. 619A/TASK 57-10-00-991-029-B)
 
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