(b)
Remove the tie-down point (6) from the structure (1).
**ON A/C 201-220, 222-223, 225-227, 229-299, 301-399,
Subtask 25-55-41-020-053-A
D. Removal of the Tie-Down and Net Attachment Fittings from the Ceiling Area of the BULK Cargo-Compartment
**ON A/C 203-220, 222-223, 225-227, 229-299,
(Ref. Fig. 404/TASK 25-55-41-991-004) **ON A/C 201-202, 301-399,
(Ref. Fig. 404B/TASK 25-55-41-991-004-A) **ON A/C 201-220, 222-223, 225-227, 229-299, 301-399,
(1)
Remove the cargo net(s) (9), if installed:
(a)
Disconnect the net fittings (8) from the tie-down and net attachment fittings of the cargo-compartment floor and ceiling areas.
(b)
Remove the cargo net(s) (9).
(2)
Remove the tie-down points (3): NOTE : The removal procedure for all the tie-down points (3) is the
____ same. Therefore, the removal procedure for one tie-down point
(3) only is given here.
(a)
Remove the screws (4) from the tie-down point (3).
(b)
Remove the tie-down point (3) from the spacer (2).
(c)
If necessary, remove the spacer (2): 1 Remove the screws (5) from the spacer (2).
_
2 Remove the spacer (2) from the structure (1).
_
R EFF : 201-220, 222-223, 225-227, 229-299, 25-55-41Page 438 301-399, Aug 01/05
CES
(3) Remove the tie-down points (6): NOTE : The removal procedure for all the tie-down points (6) is the
____ same. Therefore, the removal procedure for one tie-down point
(6) only is given here.
(a)
Remove the screws (7) from the tie-down point (6).
(b)
Remove the tie-down point (6) from the structure (1).
(4) Remove the stanchion fittings (10). NOTE : The removal procedure for all the stanchion fittings (10) is
____ the same. Therefore, the removal procedure for one stanchion fitting (10) only is given here.
(a)
Remove the screws (11) from the stanchion fitting (10).
(b)
Remove the stanchion fitting (10) from the structure (1).
R EFF : 201-220, 222-223, 225-227, 229-299, 25-55-41Page 439 301-399, Aug 01/05
CES **ON A/C ALL
TASK 25-55-41-400-001
Installation of the Tie-Down and Net Attachment Fittings of the AFT and BULK Cargo-Compartments
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-metal scraper
No specific access platform 2.1 m (6 ft. 11 in.)
No specific access platform 2.3 m (7 ft. 7 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (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. 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
25-55-41Page 440
Aug 01/05
R
CES C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the
Yellow Electric Pump
52-30-00-860-006 Open the Bulk Cargo-Compartment Door
52-30-00-860-008 Close the Bulk Cargo-Compartment Door
**ON A/C 001-049, 051-099, 101-149, 201-299,
25-55-41-991-001 Fig. 401 R **ON A/C 151-199, 401-499,
25-55-41-991-001-A Fig. 401A
**ON A/C 301-399,
25-55-41-991-001-B Fig. 401B
**ON A/C 001-049, 051-099, 101-149, 201-299,
25-55-41-991-002 Fig. 402 R **ON A/C 151-199, 401-499, 中國(guó)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(cè) AMM EQUIPMENT/FURNISHINGS 設(shè)備4(48)
