A. Removal of the Electronic Assembly NOTE : The subsequent worksteps are necessary if you remove the
____
electronic assembly of a rudder trim actuator with the part number R 6137-3. If you remove the electronic assembly of a rudder trim R actuator with the part number 6137-4 or 6137-5, refer to the next R subtask.
(1)
Disconnect the electrical connectors (7) from the plugs (8) on the rudder trim actuator 10CC (10).
(2)
Put blanking caps on the plugs (8) and the electrical connectors (7).
(3)
Cut and remove the lockwire from the screws (9).
(4)
Hold the electronic assembly (6) and remove the screws (9).
(5)
Remove the electronic assembly (6) from the rudder trim actuator (10).
(6)
Remove and discard the packing (5).
Subtask 27-22-51-020-053
B. Removal of the Electronic Assembly
R R NOTE : The subsequent worksteps are necessary if you remove the____ electronic assembly of a rudder trim actuator with the part number 6137-4 or 6137-5.
(1) Disconnect the electrical connectors (6) from the plugs on the rudder trim actuator (2).
(2) Put blanking caps on the plugs and the electrical connectors (6).
(3) Hold the electronic assembly (4) and remove the screws (5).
(4) Remove the electronic assembly (4) from the rudder trim actuator (2).
(5) Remove and discard the packing (3).
TASK 27-22-51-400-002
Installation of the Electronic Assembly of the Rudder Trim Actuator (10CC)
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.
WARNING : PRESSURIZE ONLY THE HYDRAULIC SYSTEM(S) THAT IS (ARE) NECESSARY FOR
_______ THE TASK. ISOLATE THE OTHER HYDRAULIC SYSTEM(S) BEFORE YOU SUPPLY HYDRAULIC POWER TO THE AIRCRAFT.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 2 ACCESS PLATFORM 6M (20 FT) - ADJUSTABLE
No specific 2 WARNING NOTICE R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) R
6137-013 1 PIN - LOCKING
98D27207547000 1 PIN - RIGGING
98D27207548000 1 PIN - RIGGING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
22-96-00-710-001 22-97-00-710-001 27-22-00-710-002 29-00-00-864-001 55-33-13-000-001 Operational Test of the AFSOperational Test of the LAND CAT III CapabilityOperational Test of the Rudder Trim ActuationPut the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionRemoval of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
55-33-13-010-002 Opening/Removal of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and
325BR
55-33-13-400-001 Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and
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