(Ref. Fig. 401B/TASK 53-22-14-991-001-A)
EFF : ALL
53-22-14Page 402
FWD Cargo-Compartment Floor-Panels Figure 401/TASK 53-22-14-991-001-B
R EFF : 001-049, 051-099, 101-101, 106-149, 201-299, 53-22-14 Page 403 May 01/05
CES
FWD Cargo-Compartment Floor-Panels Figure 401A/TASK 53-22-14-991-001
R EFF : 102-105, 53-22-14 Page 404 May 01/05
CES
R FWD Cargo-Compartment Floor-Panels Figure 401B/TASK 53-22-14-991-001-A
R EFF : 151-199, 53-22-14 Page 405 May 01/01
CES
**ON A/C 301-399,
(Ref. Fig. 401C/TASK 53-22-14-991-001-C) R **ON A/C 401-499,
R (Ref. Fig. 401D/TASK 53-22-14-991-001-D)
R **ON A/C 001-049, 051-099, 101-101, 106-149, 201-299, 301-399, 401-499,
Subtask 53-22-14-020-050-A
A. Removal of the Floor Panels:
(1)
Find the end of the cord (7).
(2)
Pull the cord (7) up to remove the sealant from between the floor panels (1).
(3)
Remove the sealant from between the cutouts and the tiedown positions with a nonmetallic scraper.
(4)
Remove the screws (2).
(5) Remove the floor panels (1) and the seals (3) and (6).
**ON A/C 102-105, 151-199,
Subtask 53-22-14-020-050
A. Removal of the Floor Panels:
(1)
Find the end of the cord (7).
(2)
Pull the cord (7) up to remove the sealant from between the floor panels (1).
(3)
Remove the sealant from between the cutouts and the tiedown positions with a nonmetallic scraper.
(4)
Remove the screws (2).
(5)
Remove the floor panels (1) and the seals (3), (4), (5) and (6).
FWD Cargo-Compartment Floor-Panels Figure 401C/TASK 53-22-14-991-001-C
R EFF : 301-399, 53-22-14 Page 407 Aug 01/05
CES
R R FWD Cargo-Compartment Floor-Panels Figure 401D/TASK 53-22-14-991-001-D
R EFF : 401-499, 53-22-14 Page 408 Aug 01/05
CES
**ON A/C ALL
TASK 53-22-14-400-001
Installation of the FWD Cargo-Compartment Floor-Panels
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific lint free cloth No specific nonmetallic scraper No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific FIBER GLASS CORD 1.1MM DIA. (DAN107-1) Material No. 05-002 USA MIL-P-8116
PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 09-005 USA MIL-S-81733 CLASS C
CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00) Material No. 11-003 USA ASTM D 740
METHYL-ETHYL-KETONE (Ref. 20-31-00)
EFF : ALL
53-22-14Page 409
Aug 01/05
R
CES
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump
**ON A/C 001-049, 051-099, 101-101, 106-149, 201-299,
53-22-14-991-001-B Fig. 401
**ON A/C 102-105,
53-22-14-991-001 Fig. 401A
**ON A/C 151-199,
53-22-14-991-001-A Fig. 401B
**ON A/C 301-399,
53-22-14-991-001-C Fig. 401C R **ON A/C 401-499,
R 53-22-14-991-001-D Fig. 401D **ON A/C ALL
3. Job Set-up
__________
Subtask 53-22-14-860-050
A. Aircraft Maintenance Configuration
(1) Make sure that the aircraft is in the same configuration as for the removal task.
EFF : ALL
53-22-14Page 410
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-101, 106-149, 201-299,
(Ref. Fig. 401/TASK 53-22-14-991-001-B)
**ON A/C 102-105,
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2(30)
