A320飞机维护手册 AMM FUSELAGE 机身2(101)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

R  ports (to drain away any water that collects when the doors are open) and 
R  the panel sides. To reduce downward heat transmission, the bottom of the 
R  panel, below the heater element, is filled with insulation. The 
R  electrical connector is installed on the bottom of the panel. The 
R  installation of these panels is almost the same as the cabin floor 
R  panels.

 CES  PANELS - CABIN FLOOR - REMOVAL/INSTALLATION

___________________________________________
 TASK 53-32-12-000-002
 Removal of the Cabin Floor Panels
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
24-42-00-861-001  Energize the Ground Service Network from the External Power
 25-27-51-000-001  Removal of the Heated Floor Panel 5DS (6DS), 15DS (16DS)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 53-32-12-991-002 Fig. 401
 **ON A/C 301-399,

 53-32-12-991-002-A Fig. 401A
 **ON A/C ALL

 3. Job Set-up
__________
 Subtask 53-32-12-861-050

 A. Energize the ground service network
 (Ref. TASK 24-42-00-861-001).

 EFF : ALL
53-32-12Page 401

 Subtask 53-32-12-010-050

 B. Get access.
 (1) Remove the necessary equipment and furnishing to get access to the cabin floor panels.
 4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 401/TASK 53-32-12-991-002)
 **ON A/C 301-399,

 (Ref. Fig. 401A/TASK 53-32-12-991-002-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 53-32-12-020-050
 A. Removal of the floor panels.
 NOTE : This procedure is applicable for all floor panels.

____
 (1)
 Pull the cord (1) up to remove the sealant from between the floor panel joints.

 (2)
 Remove the screws (3).

 (3)
 Remove the floor panels (4). NOTE : Identify the floor panels. This will help the installation

____
 procedure.

 EFF : ALL
53-32-12Page 402

 Cabin Floor Panel Installation - FR35 thru FR47 Figure 401/TASK 53-32-12-991-002 
R  EFF : 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,  53-32-12 Page 403 Aug 01/05
 CES 

 

R R  Cabin Floor Panel Installation - FR35.8 thru FR47.5 Figure 401A/TASK 53-32-12-991-002-A 
R  EFF :  301-399,  53-32-12 Page 404 May 01/04
 CES 

 

R  **ON A/C 301-399, 
R  Subtask 53-32-12-020-050-A 
R  A. Removal of the floor panels. 
R  NOTE : This procedure is applicable for all floor panels.____ 
R  (1) Pull the cord (1) up to remove the sealant from between the floor 
R  panel joints. 
R  (2) Remove the screws (3). 
R  (3) Remove the floor panels (4). 
R  NOTE : Identify the floor panels. This will help the installation____ 
R  procedure. 
R  (4) If necessary remove the heated floor panels, 15DS (16DS), at the AFT 
R  emergency exits (Ref. TASK 25-27-51-000-001). 

 CES  **ON A/C ALL

 TASK 53-32-12-400-002
 Installation of the Cabin 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 R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
 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
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FUSELAGE 机身2(101)