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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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____ than 100 +50 -0 deg.C (212.00 +90.00 -0.00 deg.F).
R  EFF : 001-049, 051-099, 101-149, 221-221, 53-45-15Page 412 224-224, 228-228, 301-399, May 01/05
 CES


 Scuff Plate of the BULK Cargo-Compartment Door Figure 404/TASK 53-45-15-991-003 
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 CES 

 

 (4)
 Loosen the scuff plate sections (1) and (4) with a nonmetallic wedge. CAUTION : MAKE SURE THAT YOU DO NOT DAMAGE THE FUSELAGE WHEN YOU

_______
 REMOVE THE SCUFF PLATES.


 (5)
 Remove the scuff plate sections (1) and (4). NOTE : You must install new scuff plates if the scuff plates you


____ remove were not installed with a release agent. (The release agent provides for easier removal).
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 CES

 TASK 53-45-15-400-002


 Installation of the Scuff Plates at the BULK Cargo-Compartment Door
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific vacuum pump No specific vacuum valve
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific adhesive tape, 3M Scotch 471F-15, Blue No specific porous felt Material No. 05-013A C Z-24.223
 RELEASE AGENT (Ref. 20-31-00) Material No. 05-068 D 80-T-31-2910 VACUUM FOIL (Ref. 20-31-00) Material No. 08-065 USA MIL-T-60394 TYPE I CLASS I DOUBLE SIDED ADHESIVE TAPE (Ref. 20-31-00)
 Material No. 09-013  USA MIL-PRF-81733 TYPE I CLASS A CORROSION INHIBITING BRUSH CONSISTENCY (Ref. 20-31-00)
 Material No. 09-030 D 80-T-50-4005 SEAL TAPE (Ref. 20-31-00) Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00) Material No. 16-001 ANTI-CORROSION PRIMER (POLYURETHANE ) (Ref. 20-31-00) Material No. 16-003 F ASNB70720 COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)
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 CES


 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
51-76-11-300-001 52-30-00-860-008 53-42-17-400-001 51-75-12-300-003  Repair of the SealingClose the Bulk Cargo-Compartment DoorInstallation of the BULK Cargo-Compartment Floor-PanelsRepair of Minor Paint Damage (Topcoat Only) (for corrective action) 
R  **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
 53-45-15-991-003  Fig. 404 
R  **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228, 301-399,
 53-45-15-991-004 53-45-15-991-005  Fig. 405Fig. 406
 3. Job Set-up__________
 Subtask 53-45-15-860-051
 A. Aircraft Maintenance Configuration
 (1) Make sure that the aircraft is in the same configuration as for the removal task.
 4. Procedure_________ 
R  **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
 (Ref. Fig. 404/TASK 53-45-15-991-003) 
R  **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228, 301-399,
 (Ref. Fig. 405/TASK 53-45-15-991-004, 406/TASK 53-45-15-991-005) 

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 CES


 Scuff Plate Attachment Figure 405/TASK 53-45-15-991-004 
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 CES 

 

 Installation and Application of Sealant to the Scuff Plates Figure 406/TASK 53-45-15-991-005
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 CES  Subtask 53-45-15-916-051


 A. Preparation for Installation
 (1) Clean the scuff plate mating surface of the fuselage skin with CLEANING AGENTS (Material No. 11-003).

 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.
 
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