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A320飞机维护手册 AMM WINGS 机翼3(51)

时间:2011-03-27 12:43来源:蓝天飞行翻译 作者:航空 点击:
  
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 574000) for the

____
 correct repair procedure.

 (2) Examine each slat attachment bolt on slat tracks 7 or 8 as follows: NOTE : Remove one of the attachment bolts, examine it and install it
____ correctly before removing a different bolt for inspection. Do not remove more than one attachment bolt at any time.


R R  Slat 3, Track 7 - Inspection Details Figure 605/TASK 57-44-00-991-011
 1EFF : 1 1 1CES  ALL  1 111 57-44-00 Page 626 May 01/98

 

R R  Slat 3, Track 8 - Inspection Details Figure 606/TASK 57-44-00-991-012
 1EFF : 1 1 1CES  ALL  1 111 57-44-00 Page 627 May 01/98

 

 Details of the Slat Track 7 Link Sideplates and Bolts Figure 607/TASK 57-44-00-991-004
 1EFF : ALL 1 57-44-00Page 628 1 1 Nov 01/99R 1 1 1CES 1


 Details of the Slat Track 8 Link Sideplates and Bolts Figure 608/TASK 57-44-00-991-005
 1EFF : ALL 1 57-44-00Page 629 1 1 Nov 01/99R 1 1 1CES 1


 (a)
 Remove one of the slat attachment bolts on slat tracks 7 or 8 (Ref. TASK 27-84-65-000-001).

 (b)
 Examine the attachment bolt. Make sure that:


 -there is no corrosion or damage
 -
the shank of the bolt is not worn

 -
the bolt hole is not worn or damaged.
 NOTE : If necessary, discard the worn/damaged bolt and install a

 

____
 replacement item.

 (c)
 Install the slat attachment bolt (Ref. TASK 27-84-65-400-002).

 (d)
 Do steps (a) thru (c) for each attachment bolt on the slat tracks 7 and 8 attachment links and side plates.


R **ON A/C 106-149, 228-299, 301-399, 401-499,
 Subtask 57-44-00-210-055-A
 B. Inspection
 (1)
 Do an inspection of the slat track 7 and 8 attachments in the areas shown.

 (2)
 Make sure that there is no corrosion, cracks or damage and that the sealant is in a seviceable condition.


 NOTE : If necessary, refer to the ASRM (Ref. ASRM 574000) for the
____
 correct repair procedure.

 **ON A/C ALL
 5. Close-up
________
 Subtask 57-44-00-410-056

 A. Close Access
 (1) Remove the access platform(s).


 Subtask 57-44-00-865-065
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 57-44-00-860-051
 C. Aircraft Configuration
 (1) Retract the slats fully (Ref. TASK 27-80-00-866-005). Subtask 57-44-00-942-064
 D. Removal of Equipment
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the safety barriers.

 (3)
 Remove the warning notice(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 


 SKINS AND PLATING - CLEANING/PAINTING
_____________________________________
 TASK 57-44-11-300-001
 Cleaning and Painting of the Slat No. 3. Slat
 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.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Reason for the Job
__________________
R 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 notices
 No specific SCOTCHBRITE-pad
 No specific access platform 3 m (9 ft. 10 in.)

 

 B. Consumable Materials

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
R Material No. 07-003
R ABRASION RESISTANT COATING (TEFLON POLYURET) (Ref. 20-31-00) Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 
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