R R (5) Connect the lever arm (11) to the artificial feel unit (4) as follows:
(a) Install the bush (10) in the lever arm (11).
R R (b) Move the artificial feel unit (4) at the universal joint (5). Put the shaft (31) in position at the lever arm (11).
R (c) Support the artificial feel unit (4).
(d) Align the bolt hole in the lever arm (11) with the bolt hole in the shaft (31).
(e) Install the bolt (9), the washer (12) and the nut (13).
(f) TORQUE the nut (13) to 0.8 m.daN (70.79 lbf.in).
(g) Safety the nut (13) with a new cotter pin (14).
R (6) Remove the blanking caps and connect the electrical connector (26) to the receptacle (25) of the solenoid 16CA (3).
R R (7) Make sure that the cable of the electrical connector (26) does not rub on the spar box of the vertical stabilizer (1).
Subtask 27-23-17-080-050
D. Removal of the Rigging Pins (Ref. Fig. 401/TASK 27-23-17-991-002)
(1) Remove the PIN - RIGGING (98D27207547000) (51) from the rudder cable quadrant.
(2) Remove the PIN - RIGGING (98D27207548000) (50) from the bellcrank of the rudder control unit.
Subtask 27-23-17-865-051
E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CC1, 5CC2, 14CC1, 14CC2, 15CC
Subtask 27-23-17-860-053
F. Preparation for the Test
(1)
On the overhead panel 23VU, push the FLT CTL/FAC 1 pushbutton switch and the OFF legend goes off.
(2)
On the overhead panel 24VU, push the FLT CTL/FAC 2 pushbutton switch and the OFF legend goes off.
Subtask 27-23-17-710-050
G. Do an operational test of the artificial feel loads of the rudder
(Ref. TASK 27-23-00-710-001).
5. Close-up
________ Subtask 27-23-17-410-050-A
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the access panel 325BL at the trailing edge of the vertical stabilizer (Ref. TASK 55-33-13-410-002).
(3)
Install the rudder fairing 325AL (Ref. TASK 53-55-12-400-001).
(4)
Close the access door 312AR.
(5)
Remove the warning notice(s).
(6)
Remove the access platform(s).
ARTIFICIAL FEEL AND TRIM UNIT - REMOVAL/INSTALLATION
____________________________________________________
TASK 27-23-41-000-001
Removal of the Artificial Feel and Trim Unit
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.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific blanking caps
No specific circuit breaker(s) safety clip(s)
No specific warning notices
No specific access platform 11.0 m (36 ft. 1 in.)
6137-013 1 PIN - LOCKING
98D27207547000 1 PIN - RIGGING
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2(105)