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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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 Subtask 53-12-11-210-052
 D. Inspection of the Adhesive Tape 
R R  (1) Make sure that the adhesive tapes are clean and in the correct condition. If necessary, repair the related adhesive tape (Ref. TASK 53-12-00-300-001).
 Subtask 53-12-11-210-054
 E. Inspection of the Shims (Ref. Fig. 404/TASK 53-12-11-991-004) 
R R  (1) Examine the shims between FR1 and FR12. If the shims are damaged, do the steps that follow:
 (a) Remove the shims with a non metallic scraper.
 (b) Clean the area between the shims and the structure with CLEANING AGENTS (Material No. 11-003) and a MISCELLANEOUS (Material No. 19-003).
 (c) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) on the surface between the shims and the structure.
 (d) Install the shims on the structure.

 EFF : ALL

53-12-11Page 408


R R  Shims from FR1 thru FR12 Figure 404/TASK 53-12-11-991-004
 EFF :  ALL  53-12-11 Page 409 Feb 01/01
 CES 


 4. Procedure
_________

 Subtask 53-12-11-420-050
 A. Installation of Panels from FR1 thru FR6 (Ref. Fig. 401/TASK 53-12-11-991-001, 402/TASK 53-12-11-991-002)
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Put the floor panels (2) in position.


 (3) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (1). R (4) Install the screws (1) and TORQUE to between 0.15 and 0.20 m.daN
 (13.27 and 17.69 lbf.in).
 (5)
 Put the floor panels (4) in position.

 (6)
 Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (3).

 (7)
 Install the screws (3) and TORQUE to between 0.15 and 0.20 m.daN


 (13.27 and 17.69 lbf.in).
 Subtask 53-12-11-420-051

 B. Installation of Panels from FR6 thru FR12 (Ref. Fig. 401/TASK 53-12-11-991-001, 403/TASK 53-12-11-991-003)
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Make sure that the adhesive tape (15) is in position.


 (3) Put the floor panels (12) in position.
 Subtask 53-12-11-420-053

 C. Installation of Panels from FR6 thru FR12
 (1)
 Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (11).

 (2)
 Install the screws (11) and TORQUE to between 0.15 and 0.20 m.daN


 (13.27 and 17.69 lbf.in).
 EFF : ALL

53-12-11Page 410


 5. Close-up________
 Subtask 53-12-11-420-052 
R  A. Installation of the Component
 (1) Install the textile floor covering.
 (2) Install the cockpit carpet. 
R  (3) Install the third occupant seat (Ref. TASK 25-11-41-400-001). 
R  (4) Install the captain/first officer seat (Ref. TASK 25-11-51-400-001).
 Subtask 53-12-11-942-050
 B. Close Access
 (1) Remove the ground support and maintenance equipment, the special and
 standard tools and all other items.
 (2) Close the passenger/crew door (Ref. TASK 52-10-00-010-001).
 (3) Remove the access platform(s).

 EFF : ALL

53-12-11Page 411


 PANELS - CABIN FLOOR - REMOVAL/INSTALLATION
___________________________________________
 TASK 53-12-12-000-001
 Removal of the Cabin Floor Panels from FR12 thru FR24
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 3.50 m (11 ft. 6 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-28-41-000-001 Removal of the Textile Floor-Covering 25-28-42-000-001 Removal of the Non-Textile Floor Covering (NTF) 25-31-41-000-001 Removal of the FWD Galley Unit (6475MM) 25-31-41-000-002 Removal of the FWD Galley Unit (6478MM or 6479MM) 25-32-41-000-001 Removal of the MID RH Galley Unit (7000MM) 25-41-41-000-001 Removal of the Lavatory A 25-41-42-000-001 Removal of the Lavatory B 25-41-44-000-001 Removal of the Lavatory H 25-42-41-000-001 Removal of the Lavatory H 52-10-00-010-001 Opening of the Passenger/Crew Door 53-12-12-991-004 Fig. 401
 **ON A/C 001-003,
 
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