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时间:2011-03-27 08:44来源:蓝天飞行翻译 作者:admin
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 5. Close-up________
 Subtask 53-15-11-860-051
 A. Close Access
 (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
 (2) Make sure that the work area is clean and clear of tool(s) and other items.
 (3) Remove the access platform(s).

 EFF : ALL
53-15-11Page 804


 SCUFF PLATES - DOOR ENTRANCE - REMOVAL/INSTALLATION
___________________________________________________ TASK 53-15-15-000-001 Removal of the FWD Passenger/Crew Door Scuff Plates
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific non metallic scraper No specific non metallic wedge No specific access platform 4.00 m (13 ft. 1 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-10-00-010-001 Opening of the Passenger/Crew Door 53-15-15-991-001 Fig. 401
 3. Job Set-up
__________ Subtask 53-15-15-941-050
 A. Get Access
 (1)
 Put the access platform in zone 831 or 841.

 (2)
 Open the applicable FWD passenger/crew door 831 or 841 (Ref. TASK 52-10-00-010-001).


 EFF : ALL
53-15-15Page 401
Aug 01/01
R
 CES  4. Procedure


_________
 Subtask 53-15-15-020-050

 A. Removal of the Scuff Plates
 (Ref. Fig. 401/TASK 53-15-15-991-001)

 CAUTION : MAKE SURE THAT YOU DO NOT DAMAGE THE FUSELAGE WHEN YOU REMOVE
_______
 THE SCUFF PLATES.

R NOTE : The scuff plates can become damaged during the subsequent removal
____ R procedure.
 (1)
 Remove the screws (1) and the cover strip (2).

 (2)
 Remove the sealant between the scuff plates (3) (5) and (9) with a non metallic scraper.

 (3)
 Remove the screws (6) and (8), the nuts (4), and the washers (7) from the scuff plates (3), (5) and (9).

 (4)
 Blow air on the scuff plates (3), (5) and (9) with a hot air blower. NOTE : Do not let the temperature of the scuff plates increase by

____ more than 100 +50 -0 deg.C (212.00 +90.00 -0.00 deg.F).

 (5)
 Carefully put a non metallic wedge between the fuselage and the scuff plates (3), (5) and (9).

 (6)
 Remove the scuff plates (3), (5) and (9). NOTE : If the scuff plates (3), (5) and (9) are damaged, discard


____
 them.

 EFF : ALL
53-15-15Page 402


R  FWD Passenger/Crew Door Scuff Plate Figure 401/TASK 53-15-15-991-001
 EFF :  ALL  53-15-15 Page 403 Nov 01/00
 CES 

 

 TASK 53-15-15-400-001
 Installation of the FWD Passenger/Crew Door Scuff Plates
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific scotch brite
 No specific vacuum pump
 No specific vacuum valve

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific adhesive tape
 No specific porous material
 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. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
 Material No. 09-016  USA MIL-PRF-81733D TYPE II CLASS B
 CORROSION INHIBITING FILLET CONSISTENCY
 (Ref. 20-31-00)

 Material No. 09-030 D 80-T-50-4005 SEAL TAPE (Ref. 20-31-00) R Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 EFF : ALL
 
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