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,
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FUSELAGE 機身1(91)
