(3)
Put the links of the chain on the pinion until:
-there are 33.5 links (320 mm (12.5984 in.)) between the pitch trim shaft, the gearset unit and the end of the shaft.
(4)
Remove the RIGGING PIN - THS MECHANICAL CONTROL (98D27407532000) (11) from the tension regulator.
(5)
Adjust the tension of the cables (Ref. TASK 27-41-00-820-002).
**ON A/C 301-399,
Subtask 27-41-00-820-051-A
D. If the dimension you measured is not correct:
-adjust the distance between the shaft of the THS actuator input pinion,
and the end of the shaft.
Do these steps:
(1)
Lock the tension regulator with the RIGGING PIN - THS MECHANICAL CONTROL (98D27407532000) (11).
(2)
In the FWD Cargo Compartment, remove the ceiling panel 131EC (Ref. TASK 25-54-12-000-002) and the partition 131PW (Ref. TASK 25-54-12-000-001).
(3)
Remove the recirculation filter LH side (Ref. TASK 21-21-41-000-001)
(4)
Remove the locking clips from the turnbuckles and loosen the cables (Ref. Detail B).
R R R (5) Put the links of the chain on the pinion until : - there are 33.5 links (320 mm (12.5984 in.)) between the pitch trim shaft, the gearset unit and the end of the shaft.
R R (6) Remove the RIGGING PIN - THS MECHANICAL CONTROL (98D27407532000) (11) from the tension regulator.
R (7) Adjust the tension of the cables (Ref. TASK 27-41-00-820-002).
R (8) Install the locking clips on the turnbuckles (Ref. Detail B).
R **ON A/C ALL
Subtask 27-41-00-710-050
E. Do the operational test of the THS actuator (Ref. TASK 27-44-00-710-003).
5. Close-up________
Subtask 27-41-00-410-056
A. Installation of the protective covers
(1) Install the protective covers (2) and (5).
(2) Tighten the fasteners (1).
(3) Install the washers (3) and the screws (4).
Subtask 27-41-00-942-055
B. Put the aircraft back to the serviceable condition.
(1) On the center pedestal, remove the PITCH TRIM CONTROL LOCKING (98D27403500000).
(2) Make sure that the zero adjustment is correct (Ref. TASK 27-41-00-220-003).
(3) 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 27-41-00-410-053
C. Close Access
(1)
Install the floor panel 211EF (Ref. TASK 53-12-11-400-001).
(2)
Install the floor panels 241FF and 241BF (Ref. TASK 53-32-12-400-002).
(3)
Close the access doors 811 and 312AR.
(4) Remove the access platform(s).
**ON A/C 301-399,
Subtask 27-41-00-410-053-A
C. Close Access
(1)
Install the floor panel 211EF (Ref. TASK 53-12-11-400-001).
(2)
Install the ceiling panel 131EC (Ref. TASK 25-54-12-400-002) and the partition 131PW (Ref. TASK 25-54-12-400-001).
(3)
Install the recirculation filter LH side (Ref. TASK 21-21-41-400-001).
(4)
Close the access doors 811 and 312AR.
(5) Remove the access platform(s).
**ON A/C ALL
Subtask 27-41-00-862-053
D. De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
TASK 27-41-00-720-001
Functional Test of the THS-Actuator Overtravel Related to the Mechanical Indicator
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 FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY
_______ OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
1. Reason for the Job__________________
Refer to the MPD TASK: 274400-02
2. Job Set-up Information______________________
A. Referenced Information
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵3(83)
