-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
7. Slowly release the left pedal.
R R
8. De-energize the solenoid 16CA with the 28 VDC POWER SUPPLY TOOL (355M03200001).
9. At the CAPT or F/O seat : - push the right pedal until it touches the mechanical stop (variable stop).
R R
10. Slowly release the right pedal and push the left pedal until it touches the mechanical stop (variable stop).
R R R
11. Slowly release the left pedal.
The rudder moves to the neutral position. The force you must apply to the left pedal decreases slowly and continuously, then becomes zero. On the lower ECAM display unit, on the F/CTL page :
-the pointer of the RUD indicator moves to the neutral.
NOTE : The solenoid of the artificialfeel unit is de-energized. The secondspring of the artificial feel unit is disengaged.
The rudder moves smoothly to the right.The force you must apply increasesslowly and continuously until the pedaltouches the mechanical stop. On the lower ECAM display unit, on the F/CTL page :
-
the pointer of the RUD indicator moves smoothly to the right.
The rudder moves smoothly to the left.The force you must apply to the rightpedal decreases slowly andcontinuously, then becomes zero. The force you must apply to the left pedal increases slowly and continuously until the pedal touches the mechanical stop. On the lower ECAM display unit, on the F/CTL page :
-
the pointer of the RUD indicator moves smoothly from the right mark to the left.
The rudder moves to the neutral position. The force you must apply to the left pedal decreases slowly and continuously, then becomes zero. On the lower ECAM display unit, on the F/CTL page :
-------------------------------------------------------------------------------
R R ACTION RESULT -------------------------------------------------------------------------------- the pointer of the RUD indicator moves to the neutral.
NOTE : If the feel loads are not satisfactory:____ (Ref. TSM 27 PB 101 OBSV).
5. Close-up________
Subtask 27-23-00-860-051
A. Aircraft Maintenance Configuration
(1) Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003).
(2) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 27-23-00-080-051
B. Removal of the test tool (Ref. Fig. 501/TASK 27-23-00-991-001)
R (1) Remove the 28 VDC POWER SUPPLY TOOL (355M03200001).
R (2) Make sure that the electrical connector is serviceable.
(3) Connect the electrical connector (1) to the solenoid 16CA.
(4) Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 27-23-00-410-051
C. Close Access
(1) Close the access panel 325BL (Ref. TASK 55-33-13-410-001)
(2) Close the access door 312AR.
(3) Remove the access platform(s).
Subtask 27-23-00-710-053
D. Test of the Autopilot Disengagement
(1) Do the test of the autopilot disengagement (Ref. TASK 22-10-00-710-002)
NOTE : Do the test of the autopilot disengagement only for the
____
pedals.
TASK 27-23-00-710-002
Operational Test of the Rudder-Travel Limitation Unit
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
22-61-00-710-001 Operational Test of the Rudder Travel Limiting
Function
3. Job Set-up
__________
Subtask 27-23-00-860-054
A. Not applicable
4. Procedure
_________
Subtask 27-23-00-710-051
A. Do the operational test of the variable stop of the rudder travel
limitation unit (Ref. TASK 22-61-00-710-001). R
SOLENOID - ARTIFICIAL FEEL UNLOCKING (16CA) - REMOVAL/INSTALLATION
__________________________________________________________________
TASK 27-23-17-000-001
Removal of the Artificial Feel Unlocking Solenoid 16CA
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
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(100)
