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时间:2011-03-27 08:50来源:蓝天飞行翻译 作者:admin
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 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  53-41-00Page A652

Nov 01/04
R
 CES


 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
53-35-11-000-001 Removal of the Wing-to-Fuselage Fairings 53-35-11-400-001 Installation of the Wing-to-Fuselage Fairings 53-35-13-000-001 Removal of the Belly Fairing Access Panels 53-35-13-000-002 Removal of the Quick-Release Access Panels from the
 Belly Fairing Structure 53-35-13-400-001 Installation of the Belly Fairing Access Panels 53-35-13-400-002 Installation of the Quick-Release Access Panels on
 the Belly Fairing Structure ASRM 53-45-12-201 (for corrective action) 53-41-00-991-044 Fig. 633
 3. Job Set-up
__________
 Subtask 53-41-00-010-136
 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)
 Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever when you work near the flaps/slats.

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

 (3)
 Put an adjustable access platform in position at the belly fairing.

 (4)
 Remove these fairings/access panels:

 -
the wing-to-fuselage fairings (Ref. TASK 53-35-11-000-001),

 -
the quick-release access panels (Ref. TASK 53-35-13-000-002).

 


 -and the belly fairing access panels (Ref. TASK 53-35-13-000-001).
 EFF : ALL 53-41-00Page A653

Nov 01/04
R
 CES  Subtask 53-41-00-110-087


 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.
 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) Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint free cloth.
 4. Procedure
_________
 (Ref. Fig. 633/TASK 53-41-00-991-044)
R **ON A/C 001-049, 051-099, 101-149, 201-299,
 Subtask 53-41-00-210-104
 A. Inspection
 (1) Examine the the fuselage external surface and the belly fairing support structure between FR30 thru FR53, under the belly fairing for:
 -corrosion,
 -cracks
 -and other damage.
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-45-12-201) for
____
 the correct repair procedure.

 

 Fuselage External Surface inside the Belly Fairing and Belly Fairing Support Structure Figure 633/TASK 53-41-00-991-044
 EFF : ALL 53-41-00Page A655 Nov 01/04 R CES


R **ON A/C 151-199, 401-499,
 Subtask 53-41-00-210-104-A
 A. Examine the the fuselage external surface and the belly fairing support structure between FR27 and FR57, under the belly fairing for:
 -corrosion,
 -cracks
 -and other damage.
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-45-12-201) for the
____
 correct repair procedure.

 **ON A/C 301-399,
 Subtask 53-41-00-210-104-B
 A. Inspection
 (1) Examine the the fuselage external surface and the belly fairing support structure between FR35.3 thru FR48, under the belly fairing for:
 -corrosion,
 -cracks
 -and other damage.
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-45-12-201) for
 
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