(a) If they are in good condition:
1 Make a mark on each rear cable.
_
2 Pull the cables to the front until the position of the index
_ agrees with the value found on the graph.
3 Keep the cables pulled and make a new mark on each cable then
_
release the cables.
4 Measure the length between two marks of each cable
_ R - if the length is more than 32 mm (1.2598 in.), shorten the
control cables (Ref. TASK 27-41-00-820-003). R - if the length is less than 32 mm (1.2598 in.), replace the R rear control cables (Ref. TASK 27-41-44-000-001) (Ref. TASK
27-41-44-400-001).
Adjustment of the Cables Figure 505/TASK 27-41-00-991-006
1EFF : 1 1R 1CES ALL 1 11 1 27-41-00 Page 533 May 01/04
Adjustment Graph Figure 506/TASK 27-41-00-991-008
1EFF : 1 1R 1CES ALL 1 11 1 27-41-00 Page 534 May 01/04
(7)
Remove the PIN - RIGGING (0U190360) (5).
(8)
Energize the aircraft electrical circuit (Ref. TASK 24-41-00-861-002).
(9)
Pressurize the Green and Yellow hydraulic systems (Ref. TASK 29-23-00-863-001) and (Ref. TASK 29-24-00-863-001).
(10)
Operate the THS fully more than ten times and put it in the zero position.
(11)
Install the PIN - RIGGING (0U190360) (5).
(12)
Depressurize the Green and Yellow hydraulic systems (Ref. TASK 29-23-00-864-001) and (Ref. TASK 29-24-00-864-001).
(13)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
(14)
Make sure that the position of the index (4) agrees with the values found on the graph with a tolerance of + or - 1 graduation (+ or -5.C).
(15)
Make sure that the pitch-trim control-wheels stay at zero.
(16)
With a tensiometer, measure the tension of the two cables at a distance no less than 200 mm (7.8740 in.) from the tension regulator (2). Do this step two times to make sure that you get the same tension value.
(17)
Make sure that the tension value is 20 +8 -4 daN (45 +18 -9 lbf).
5. Close-up
________ Subtask 27-41-00-860-057
A. Put the aircraft back to its initial configuration.
(1)
Install the locking clips on the turnbuckles (3) of each cable. Make sure that the number of threads on each side of the end fitting is the same.
(2)
Remove the PIN - RIGGING (0U190360) (5).
(3)
Remove the warning notice(s).
1EFF : ALL 1 27-41-00Page 535 1 1 May 01/04R 1 1 1CES 1
(4) Make sure that the work area is clean and clear of tool(s) and other items.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-41-00-410-054
B. Close Access
(1)
Install the cabin floor panels 241FF, 241BF (Ref. TASK 53-32-12-400-002).
(2)
Close the access doors 312AR, 811, 812, 824, 825, 826 (Ref. TASK 52-41-00-410-002).
(3) Remove the access platform(s).
**ON A/C 301-399,
Subtask 27-41-00-410-054-A
B. Close Access
(1)
In the FWD cargo compartment, install the ceiling panel 131EC (Ref. TASK 25-54-12-400-002) and the partition 131PW (Ref. TASK 25-54-12-400-001).
(2)
Install the recirculation filter, LH side (Ref. TASK 21-21-41-400-001)
(3)
Close the access doors 312AR, 811, 812, 824, 825, 826 (Ref. TASK 52-41-00-410-002).
(4)
Remove the access platform(s).
R **ON A/C ALL
TASK 27-41-00-820-003
Shortening of the THS Control Cable
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 TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
CAUTION : MAKE SURE THAT THE AIRCRAFT IS IN THE TEMPERATURE CONDITIONS (STABLE
_______
AMBIENT TEMPERATURE) SPECIFIED IN THE AIRCRAFT MAINTENANCE
CONFIGURATION PARAGRAPH.
CHANGES IN THE TEMPERATURE CAN CAUSE INCORRECT MEASUREMENTS.
1. Reason for the Job
__________________
Do this procedure when it is no longer possible to adjust the length of the THS control cables (turnbuckles on the stops).
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 FLIGHT CONTROLS 飛行操縱3(90)
