(1) Remove the old temporary protection compound from the area to be treated with a non metallic scraper, and clean with CLEANING AGENTS (Material No. 11-004) and a lint free cloth. Make sure that the area is dry before you continue.
4. Procedure
_________
CAUTION : DO NOT APPLY TEMPORARY PROTECTION ON THE OXYGEN SYSTEMS.
_______ MAKE SURE THAT THE TEMPORARY PROTECTION DOES NOT GET: -ON COMPOSITE PARTS, CONTROL CABLES, PULLEYS,TEFLON BEARINGS. -ON LUBRICATED SURFACES. -IN DRAIN VALVES OR OTHER ORIFICES. TEMPORARY PROTECTION ON OR IN THESE PARTS CAN CAUSE DAMAGE.
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 53-41-00-916-072
A. Temporary Protection Procedure
(Ref. Fig. 704/TASK 53-41-00-991-037)
(1) Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-005A) or STORAGE PRESERVATION (Material No. 15-006) or equivalent to the lateral frames 52A and 56 that can be seen at the sides of the AFT cargo door cutout.
R **ON A/C 151-199, 401-499,
Subtask 53-41-00-916-072-A
A. Temporary Protection Procedure
(Ref. Fig. 704/TASK 53-41-00-991-037)
(1) Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-005A) or STORAGE PRESERVATION (Material No. 15-006) or equivalent to the lateral frames 55A and 56 that can be seen at the sides of the AFT cargo door cutout.
EFF : ALL
53-41-00Page 718
Aft Cargo Door Cutout, Visible Part of Lateral FR52A and FR56.
Figure 704/TASK 53-41-00-991-037
EFF : ALL
53-41-00Page 719
May 01/04 R CES
**ON A/C ALL
5. Close-up
________ Subtask 53-41-00-410-117
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
(3)
Close the Aft cargo compartment door (Ref. TASK 52-30-00-860-002).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL
53-41-00Page 720
FLOOR PANELS - DESCRIPTION AND OPERATION
________________________________________
1. General
_______
A. Cabin Floor Panels The cabin compartment floor is a panel assembly. The floor panels are made of a honeycomb core which is bonded between reinforced composite sheets.
B. Door Threshold Floor Panels Door-threshold floor panels are installed in the cabin utility areas, adjacent the passenger/crew doors. The construction of these panels is almost the same as the cabin floor panels.
2. Component Location
__________________ R (Ref. Fig. 001)
EFF : ALL
53-42-00Page 1
Floor Panels - Component Location
Figure 001
EFF : ALL 53-42-00 Page 2
Feb 01/98
CES
PANELS - CABIN FLOOR - REMOVAL/INSTALLATION
___________________________________________
TASK 53-42-12-000-001
Removal of the Cabin Floor Panels at FR47 thru FR64
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-21-41-000-001 Removal of the Passenger Seats
25-26-42-000-001 Removal of a Partition
25-27-46-000-001 Removal of a Doghouse
25-28-41-000-001 Removal of the Textile Floor-Covering
25-28-42-000-001 Removal of the Non-Textile Floor Covering (NTF)
**ON A/C 001-049, 051-099, 101-149, 201-299,
53-42-12-991-001 Fig. 401 R **ON A/C 151-199, 401-499,
53-42-12-991-001-A Fig. 401A
**ON A/C 301-399,
53-42-12-991-001-B Fig. 401B
EFF : ALL
53-42-12Page 401
**ON A/C ALL
3. Job Set-up
__________
Subtask 53-42-12-010-050
A. Get access:
(1)
Remove the passenger seats (Ref. TASK 25-21-41-000-001). NOTE : Remove only the seats in the area as necessary.
____
(2)
Remove the partitions (Ref. TASK 25-26-42-000-001).
(3)
Remove the textile floor covering, as necessary (Ref. TASK 25-28-41-000-001).
(4)
Remove the nontextile floor covering, as necessary (Ref. TASK 25-28-42-000-001).
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM FUSELAGE 機(jī)身3(75)
