(4)
Check the slat lower-trailing edge to 'D' nose gap as follows:
(a)
For the slat 1, measure the dimension L at points F, G, H, J and
K.
(b)
For the slats 2 thru 5, measure the dimension L at points F, G and H.
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 27-80-00Page 608 1 1 May 01/05 1 1 1CES 1
(c) The dimension L must be 5.0 mm (0.1968 in.) +/- 2.0 mm (0.0787 in.).
R **ON A/C 151-199, 301-399, 401-499,
Subtask 27-80-00-220-051-B
A. Permitted Aerodynamic Tolerances between the Slats 1 thru 5
(1)
Check the slat end step tolerances as follows:
(a) For the slat 1, measure and write down the slat end step dimensions:
-
at the inboard end of slat 1 at points 1 and 4 (2 dimensions)
-
at the outboard end of slat 1 at points 1, 2, 3, and 4 (4 dimensions).
(b)
For the slats 2 thru 5, measure and write down the slat end step dimensions at points 1, 2, 3, and 4 (20 dimensions).
(c)
Compare the 26 dimensions:
-21 of the 26 dimensions measured must be between the general tolerance limits given in the table J
-3 of the 26 dimensions measured can be between the general tolerance limits given in the table J +/- 0.5 mm (0.0196 in.)
-2 of the 26 dimensions measured can be between the general tolerance limits given in the table J +/- 1.5 mm (0.0590 in.).
(2)
Check the slat upper-trailing edge to 'D' nose step tolerances as follows:
(a)
For the slat 1, measure and write down the dimension X at points A, B, C, D and E (5 dimensions).
(b)
For the slats 2 thru 5, measure and write down the dimension X at points B, C and D (12 dimensions).
(c)
Compare the 17 dimensions X:
-14 of the 17 dimensions X must be between +/- 0.5 mm (0.0196 in.) of each other
-3 of the 17 dimensions X can be between +/- 1.0 mm (0.0393 in.) of each other.
(3)
Check the slat lower-trailing edge to 'D' nose step tolerances as follows:
(a)
For the slat 1, measure and write down the dimension Y at points F, G, H, J and K (5 dimensions).
(b)
For the slats 2 thru 5, measure and write down the dimension Y at points F, G and H (12 dimensions).
(c)
Compare the 17 dimensions Y:
-11 of the 17 dimensions Y must be between +/- 1.0 mm (0.0393 in.) of each other
-4 of the 17 dimensions Y can be between +/- 2.0 mm (0.0787 in.) of each other
-2 of the 17 dimensions Y can be between +/- 3.0 mm (0.1181 in.) of each other.
(4)
Check the slat lower-trailing edge to 'D' nose gap as follows:
(a)
For the slat 1, measure the dimension L at points F, G, H, J and
K.
(b)
For the slats 2 thru 5, measure the dimension L at points F, G and H.
(c)
The dimension L must be 5.0 mm (0.1968 in.) +/- 2.0 mm (0.0787 in.).
**ON A/C ALL
Subtask 27-80-00-865-072
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV, 9CV, 11CV
Subtask 27-80-00-860-068
C. Aircraft Maintenance Configuration
(1) Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control lever.
1EFF : ALL 1 27-80-00Page 610 1 1 May 01/04R 1 1 1CES 1
5. Close-up
________ Subtask 27-80-00-942-062
A. 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 access platform(s).
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
SLATS ELECTRICAL CONTROL AND MONITORING - DESCRIPTION AND OPERATION
___________________________________________________________________
1. General_______
The electrical control and monitoring system of the slats has:
-
a manually operated slat/flap control lever
-
a Command Sensor Unit (CSU) 51CV
-
two Slat and Flap Control Computers (SFCC1 and SFCC2) 21CV, 22CV
-
two electrically controlled valve blocks 25CV(26CV) installed on the slats Power Control Unit (PCU) 6001CM (Ref. 27-84-00)
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(48)
