-
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.8 m (5 ft. 11 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C 001-049, 051-099, 101-149, 201-299,
 53-35-00-991-004 Fig. 601 R **ON A/C 151-199, 401-499,
 53-35-00-991-004-A Fig. 601A
 EFF : ALL
53-35-00Page 601

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
**ON A/C 301-399,
 53-35-00-991-004-B Fig. 601B R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 53-35-00-991-005 Fig. 602
 **ON A/C 301-399,
 53-35-00-991-005-A Fig. 602A
 **ON A/C ALL
 53-35-00-991-006 Fig. 603
 3. Job Set-up
__________
 Subtask 53-35-00-010-052

 A. Get Access
 (1) Put the access platform in position in the zone 190.
 EFF : ALL
53-35-00Page 602

 4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 201-299,
 Subtask 53-35-00-210-051
 A. Do an inspection of the wing to fuselage fairings and the belly fairing access panels for missing fasteners. (Ref. Fig. 601/TASK 53-35-00-991-004, 602/TASK 53-35-00-991-005, 603/TASK 53-35-00-991-006)
 NOTE : You can temporarily replace a missing fastener by a fastener from
____ another panel. Make sure that the replacement fastener has the same thread size and the same length as the missing one. Obey the criterias in the subsequent table when you remove a fastener from any other panel.
 |-------------|----------------------------------|----------------------------| | Panel FIN | Belly Fairing Missing Fasteners | | | | Description | | |-------------|----------------------------------|----------------------------| | 7504MM | No missing fastener permitted. | | | 7505MM | | | | | | | |-------------|----------------------------------|----------------------------| | 193AB/194AB | No missing fastener permitted. | | | 193BB/194BB | | | | | | | |-------------|----------------------------------|----------------------------| | 191BB/192FB | Missing fasteners are not | Replace the missing | | | permitted on the FWD edge of each| fasteners before 10 flight | | | panel. | cycles | | | Missing fasteners are permitted, | | | | only if in accordance with the | | | | subsequent condition: | | | | - that a minimum of two fasteners| | | | in the first fastener positions| | | | are installed on all corners of| | | | each panel (count from the | | | | corner). | | |-------------|----------------------------------|----------------------------| | 191AB/191AT | Missing fasteners are not | Replace the missing | | 191LB/192AB | permitted on the FWD edge of each| fasteners before 10 flight | | 192AT/192LB | panel. | cycles | | | Two missing fasteners are | | | | permitted, only if in accordance | |
 EFF : ALL
53-35-00Page 603

 Belly Fairing Access Panels and Wing to Fuselage Fairings - Right Side Figure 601/TASK 53-35-00-991-004
R EFF : 001-049, 051-099, 101-149, 201-299, 53-35-00Page 604 May 01/05
 CES

 Belly Fairing Access Panels and Wing to Fuselage Fairings - Right Side Figure 601A/TASK 53-35-00-991-004-A
R EFF : 151-199, 401-499, 53-35-00Page 605 Aug 01/05
 CES

R  Belly Fairing Access Panels and Wing to Fuselage Fairings - Right Side 
R  Figure 601B/TASK 53-35-00-991-004-B 
R  EFF :  301-399,  53-35-00 Page 606 
May 01/04
 CES 

 Belly Fairing Access Panels and Wing to Fuselage Fairings - Left Side Figure 602/TASK 53-35-00-991-005
R  EFF : 001-049, 051-099, 101-149, 151-199, 53-35-00Page 607 201-299, 401-499, Aug 01/05
 CES

R  Belly Fairing Access Panels and Wing to Fuselage Fairings - Left Side 
R  Figure 602A/TASK 53-35-00-991-005-A 
R  EFF :  301-399,  53-35-00 Page 608 
　
中國航空網 www.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(104)