A320飞机维护手册 AMM FUSELAGE 机身2(27)

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R  necessary. 
R  4. Procedure_________ 
R  Subtask 53-21-00-210-091 
R  A. Inspection 
R  (Ref. Fig. 638/TASK 53-21-00-991-062) 
R  (1) Do a general visual inspection of the fuselage skin around the 
R  forward emergency-exit skin cutout . This inspection is applicable 
R  from FR35 to FR35.3 and from STGR8 to STGR23, external surface left 
R  and right sides. 
R  (2) Make sure that there is no: 
R  (a) Corrosion damage: 
R  - If you find corrosion damage, refer to the Structural Repair 
R  Manual (Ref. SRM 512200 P.Block 001) for types of corrosion, 
R  inspection, removal and corrosion protection.

 

R Skin Around the Forward Emergency Exit - from FR35 to 35.3 and from STGR8 to R STGR23, External Surface R Figure 638/TASK 53-21-00-991-062
 EFF : 301-399, 53-21-00Page B602 Aug 01/05
 CES  CES  PANELS - CABIN FLOOR - REMOVAL/INSTALLATION

R  (b) Other damage (cracks, scratches, stress, marks, dents, 
R  bumps,...): 
R  - If you find other damage, refer to the Structural Repair Manual 
R  (Ref. SRM 511100 P.Block 001) for damage classification and 
R  corrective action. 
R  5. Close-up________ 
R  Subtask 53-21-00-410-097 
R  A. Close Access 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Remove the access platform(s).

 

___________________________________________
 TASK 53-22-12-000-001
 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)
 **ON A/C 001-049, 051-099, 101-149, 201-299,
 53-22-12-991-001 Fig. 401 R **ON A/C 151-199, 401-499,
 53-22-12-991-001-A Fig. 401A
 **ON A/C 301-399,

 53-22-12-991-001-B Fig. 401B
 **ON A/C ALL

 3. Job Set-up
__________
 Subtask 53-22-12-861-050

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

 EFF : ALL
53-22-12Page 401

 Subtask 53-22-12-010-050

 B. Get access.
 (1) Remove the necessary equipment and furnishings to get access to the cabin floor panels.
 4. Procedure
_________
 **ON A/C 001-049, 051-099, 101-149, 201-299,

 (Ref. Fig. 401/TASK 53-22-12-991-001) R **ON A/C 151-199, 401-499,
 (Ref. Fig. 401A/TASK 53-22-12-991-001-A)
 **ON A/C 301-399,

 (Ref. Fig. 401B/TASK 53-22-12-991-001-B) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 53-22-12-020-050
 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 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
53-22-12Page 402

 Cabin Floor Panel Installation - FR24 thru FR35 Figure 401/TASK 53-22-12-991-001 
R  EFF :  001-049, 051-099, 101-149, 201-299,  53-22-12 Page 403 May 01/05
 CES 

 

 Cabin Floor Panel Installation - FR24 thru FR35 Figure 401A/TASK 53-22-12-991-001-A 
R  EFF :  151-199, 401-499,  53-22-12 Page 404 Aug 01/05
 CES 

 

R R  Cabin Floor Panel Installation - FR24 thru FR35.8 Figure 401B/TASK 53-22-12-991-001-B 
R  EFF :  301-399,  53-22-12 Page 405 May 01/04
 CES 

 

R  **ON A/C 301-399, 
R  Subtask 53-22-12-020-050-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 
　
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