-
maximum 2.0 mm (0.0787 in.) above wing surface (out of wind).

 (2)
 Measure the step tolerances of the pressure-relief panel ends across the line of flight. These must be as follows:

 (a) For the panel ends:
 -
maximum 1.2 mm (0.0472 in.) above or below the adjacent panel end (DIM X)

 -
maximum 1.2 mm (0.0472 in.) above or below the adjacent wing surface (DIM Y).

 (3)
 Measure the clearance between the D-nose skin and the leading edges of the pressure-relief panels. The clearance must be between 0.5 mm (0.0196 in.) and 3.5 mm (0.1377 in.).

 (4)
 Measure the clearance at the inboard and outboard edges of the pressure-relief panels. The clearance must be between 0.5 mm (0.0196 in.) and 5.5 mm (0.2165 in.).

R  (5) Measure the clearance at the trailing edges of the pressure-relief 
R  panels between: 
R  - the wing-skin and the edges of the panels (that are parallel to the 
R  panel leading edges), the clearance must be between 0.5 mm (0.0196 
R  in.) and 5.5 mm (0.2165 in.) 
R  - the wing-skin and the edges of the panel cut-outs (that are not 
R  parallel to the panel leading edges), the clearances must be 
R  between 0.5 mm (0.0196 in.) and 7.0 mm (0.2755 in.). 
R  **ON A/C ALL 
R  5. Close-up________ 
R  Subtask 57-41-37-865-074 
R  A. Remove the safety clip(s) and the tag(s) and close this(these) circuit 
R  breaker(s): 
R  5CV, 7CV. 
R  Subtask 57-41-37-942-060 
R  B. Removal of Equipment 
R  (1) Remove the warning notice(s). 
R  (2) Remove the safety barriers. 
R  (3) Remove the access platform(s). 
R  (4) Remove the ground support and maintenance equipment, the special and 
R  standard tools and all other items.

 TASK 57-41-37-000-003

 Removal of the Access Panel 522AT(622AT)
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
 -
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 circuit breaker(s) safety clip(s)
 No specific safety barriers
 No specific warning notice
 No specific access platform 3.2 m (10 ft. 6 in.)

 1EFF : ALL 1 57-41-37Page 412 1 1 Aug 01/04R 1 1 1CES 1

 B. Referenced Information

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
27-80-00-866-004 Extending the Slats on the Ground
 **ON A/C 001-003, 051-052,
 57-41-37-991-018 Fig. 401 R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 57-41-37-991-018-A Fig. 401A
 **ON A/C ALL
 3. Job Set-up
__________
 Subtask 57-41-37-941-060

 A. Safety Precautions
 (1) Put the safety barriers in position.
 Subtask 57-41-37-860-064

 B. Aircraft Maintenance Configuration
 (1)
 Fully extend the slats (Ref. TASK 27-80-00-866-004).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever.

 (3)
 Put a warning notice in the cockpit to tell persons not to operate the slats.

 (4)
 Put the access platform in position below the applicable access panel 522AT(622AT).

 Subtask 57-41-37-865-069
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
　
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 WINGS 機翼2(134)