A. Reactivation of the Channel 1 of the Rudder Travel Limitation Unit R (1) On the panel 187VU, install the relay 13CC1.
(2) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CC1.
Subtask 27-23-00-810-050
B. Do the trouble shooting of the rudder travel limitation unit you deactivated (Ref. TSM 22 PB 101)
5. Close-up
________
Subtask 27-23-00-410-053
A. Close Access R (1) Close the access door 824.
(2) Remove the access platform(s).
Subtask 27-23-00-862-053
B. Put the aircraft back to its initial configuration.
(1)
Remove the warning notice(s).
(2)
De-energize the ground service network
(Ref. TASK 24-42-00-862-001).
ARTIFICIAL FEEL AND RUDDER TRAVEL LIMITING - ACTUATION - ADJUSTMENT/TEST
________________________________________________________________________ TASK 27-23-00-710-001 Operational Test of the Rudder Artificial-Feel Loads WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY
_______ OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
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
__________________
This test makes sure that the operation of the artificial feel unit of the rudder is correct in manual mode and when the autopilot operates.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
No specific access platform 2.80 m (9 ft. 2 in.)
No specific access platform 5.87 m (19 ft. 3 in.)
355M03200001 1 28 VDC POWER SUPPLY TOOL
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
22-10-00-710-002 Operational Test of Autopilot Disengagement and Locking Devices of the Side Stick Controller and Rudder Pedals
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
R 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
R Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the Electric Pump 29-24-00-864-001 Depressurize the Yellow Hydraulic System 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 55-33-13-010-001 Opening of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR 55-33-13-410-001 Closing of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR TSM 27 PB 101 OBSV (for corrective action) 27-23-00-991-001 Fig. 501
3. Job Set-up
__________
Subtask 27-23-00-010-051
A. Get Access
(1)
Put the access platform at the zone 325.
(2)
Open the access panel 325BL (Ref. TASK 55-33-13-010-001).
(3)
Put the access platform at the zone 312.
(4)
Open the access door 312AR to get access to the +28VDC supply
Subtask 27-23-00-480-051
B. Installation of the Test Tool
(Ref. Fig. 501/TASK 27-23-00-991-001)
(1)
Disconnect the electrical connector (1) from the rudder artificial feel solenoid 16CA.
(2)
Put blanking caps on the disconnected electrical connectors.
(3)
Connect the 28 VDC POWER SUPPLY TOOL (355M03200001) to the solenoid 16CA .
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