(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the slat/flap control lever.
(3)
Put the adjustable access platform in position below the work area.
4. Procedure
_________
**ON A/C 001-049, 051-061, 101-105, 201-203,
(Ref. Fig. 603/TASK 27-84-61-991-009)
Slat 1 - Trailing Edge Backlash
Figure 603/TASK 27-84-61-991-009
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 27-84-61Page 626 1 1 May 01/05 1 1 1CES 1R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 603A/TASK 27-84-61-991-009-A)
**ON A/C ALL
Subtask 27-84-61-220-102
A. Check of the Slat 1 Trailing Edge Backlash
(1)
For dimension X, at Tracks 1 thru 4, to check the slat knuckle bearings backlash:
(a)
Push the upper trailing edge of the slat down with a hand force of 25 kg (55.1155 lb). Put the load at each track position, at the trailing edge of the slat. Measure and write down the dimension X.
(b)
Pull the upper trailing edge of the slat up with a hand force of 25 kg (55.1155 lb). Put the load at each track position, at the trailing edge of the slat. Measure and write down the dimension X again.
(c)
Subtract the smaller dimension X from the larger dimension X to give you the surface-attachment spherical-bearing backlash. The difference between the two dimensions, that you wrote down, must be no more than 2.5 mm (0.0984 in.).
(2)
For dimension Y (tracks 2 and 3), to check the slat track drive system backlash:
(a)
Push the applicable track with a hand force of 25 kg (55.1155 lb) aft. Measure and write down the dimension Y.
(b)
Pull the applicable track with a hand force of 25 kg (55.1155 lb) forward. Measure and write down the dimension Y again.
(c)
Subtract the smaller dimension Y from the larger dimension Y to give you the rotary-actuator/transmission-shafts backlash. The difference between the two dimensions, that you wrote down, must be no more than 3.0 mm (0.1181 in.).
Slat 1 - Trailing Edge Backlash Figure 603A/TASK 27-84-61-991-009-A
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-84-61Page 628 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
5. Close-up
________ Subtask 27-84-61-860-057
A. Aircraft Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1) Retract the slats fully (Ref. TASK 27-80-00-866-005). Subtask 27-84-61-942-054
B. 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.
TRACK - SLAT 2, 3, 4, 5 - REMOVAL/INSTALLATION
______________________________________________
TASK 27-84-62-000-001
Removal of the Slat Tracks 5 thru 12
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 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 notice(s)
No specific adjustable access platform 3.5 m (11 ft. 6 in.)
98D27804015000 1 TOOL-BACKSTOP SLAT (TRACKS 5, 6, 7, AND 8)
98D27804016000 1 TOOL-BACKSTOP SLAT (TRACKS 9, 10, 11, AND 12)
B. Referenced Information 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵8(78)
