-
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 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific warning notices No specific access platform 5.5 m (18 ft. 1 in.) 98D27403500000 1 PITCH TRIM CONTROL LOCKING 98D27407532000 1 RIGGING PIN - THS MECHANICAL CONTROL
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 27-41-42-991-003 Fig. 403
3. Job Set-up
__________
Subtask 27-41-42-860-053
A. Aircraft Maintenance Configuration
(1)
Put the access platform in position.
(2)
Remove the access panel 311AL and open the access door 312AR.
(3)
Make sure that the pitch-trim control wheel in the cockpit is in the zero position.
(4)
Lock the pitch trim control wheel with the PITCH TRIM CONTROL LOCKING (98D27403500000).
(5)
Put the warning notices in the cockpit to tell persons not to operate the pitch controls.
(6)
Make sure that the Green and Yellow hydraulic systems are depressurized and put them in the maintenance configuration (Ref. TASK 29-00-00-864-001).
(7)
Put the warning notices in position to tell persons not to pressurize the Green and the Yellow hydraulic systems.
Subtask 27-41-42-865-053
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
1EFF : ALL 1 27-41-42Page 419 1 1 May 01/04R 1 1 1CES 1
4. Procedure
_________
(Ref. Fig. 403/TASK 27-41-42-991-003) Subtask 27-41-42-020-051
A. Removal of the Springs of the Cable Tension Regulator
(1)
Remove the bolts (3). (5), (6) and the washers (4).
(2)
Remove the cover (2) from the cable tension regulator (10).
(3)
Put the RIGGING PIN - THS MECHANICAL CONTROL (98D27407532000) in the rocker assembly (12) of the cable tension regulator (10).
(4)
Remove the cotter pins (7) and the washers (8).
(5)
Carefully remove the springs (9) from the bolts (11).
1EFF : ALL 1 27-41-42Page 420 1 1 May 01/04R 1 1 1CES 1
Springs of the Cable Tension Regulator Figure 403/TASK 27-41-42-991-003
1EFF : 1 1R 1CES ALL 1 11 1 27-41-42 Page 421 May 01/04
TASK 27-41-42-400-002 Installation of the Springs of the Cable Tension Regulator WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
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
______________________
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱3(111)
