(2)
Put the access platform in position.
(3)
Open the access door 312AR.
Subtask 27-44-54-865-053
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
4. Procedure_________
(Ref. Fig. 501/TASK 27-44-54-991-002)
Subtask 27-44-54-720-051
A. Functional Test of the Pressure-Off Brakes (2):
(1) Cut and remove the lockwire which safeties the plug (3) to the screw (5) at the THS actuator motor (6).
(2) Remove the plug (3) from the manual drive input of the THS actuator (1).
(3) Remove and discard the O-ring (4) from the plug (3).
R R (4) Use a torque wrench to between 1.0 and 10.0 m.daN (88.49 and 884.95 lbf.in) for the subsequent test.
R R (5) Put the torque wrench in position at the manual drive input, apply a torque of minimum 7.2 m.daN (53.0973 lbf.ft). Make sure that the pressure-off brakes do not move.
R R R NOTE : The static break-out torque must be a minimum of 7.2 m.daN____ (53.0973 lbf.ft). - If the static break-out torque is between 6.5 m.daN (47.9351 lbf.ft) and 7.2 m.daN (53.0973 lbf.ft), replace the THS actuator within the next A-Check (500 F/H) (Ref. TASK 27-44-51-000-001) and (Ref. TASK 27-44-51-400-001). - If the static break-out torque is less than 6.5 m.daN (47.9351 lbf.ft), replace the THS actuator before next flight (Ref. TASK 27-44-51-000-001) and (Ref. TASK 27-44-51-400-001).
R (6) Remove the torque wrench.
R (7) Apply COMMON GREASE (Material No. 04-015) to the new O-ring (4).
R (8) Use the CONE - MOUNTING, THS ACTUATOR (0U145506) and put the O-ring (4) on the plug (3).
R (9) Install the plug (3) in the manual drive input.
R (10) TORQUE the plug (3) to between 1.4 and 1.6 m.daN (10.32 and 11.79 lbf.ft).
R (11) Safety the plug (3) to the screw (5) at the motor (6) with lockwire 0.6 mm (0.024 in.).
Functional Test of the Pressure-Off Brakes Figure 501/TASK 27-44-54-991-002
1EFF : 1 1R 1CES ALL 1 11 1 27-44-54 Page 504 May 01/98
5. Close-up
________ Subtask 27-44-54-865-054
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 15CE1, 16CE1, 19CE1, 19CE2, 19CE3
Subtask 27-44-54-410-051
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the access door 312AR.
(3)
Remove the warning notice(s).
(4)
Remove the access platform(s).
TRANSDUCER - THS ACTUATOR POSITION - REMOVAL/INSTALLATION
_________________________________________________________
TASK 27-44-56-000-001
Removal of the Position Transducer from the THS Actuator 9CE
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 CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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3(177)
