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R R (4) Make sure that the electrical connectors are clean and in the correct condition.
R R (5) Remove the blanking caps and connect the electrical connectors (17). Do this on the bottom of the rudder travel limitation unit (5).
R R R (6) Install the bonding leads (36) with the bolt (35) and the nut (34) if removed (Ref. TASK 20-28-00-912-004). Do this on the electrical connectors (17).
R R (7) Safety the electrical connectors (17) to the bonding leads (36) with the lockwire MISCELLANEOUS (Material No. 19-018)
R R R (8) Apply the STRUCTURE PAINTS (Material No. 16-021) to the connections of the bonding leads (36) and the electical connectors (17).
**ON A/C ALL
Subtask 27-23-51-080-050
D. Removal of the Rigging Pins
(1) Remove the PIN - RIGGING (98D27207545000) (32) from the bellcrank assy (4).
(2) Remove the PIN - RIGGING (98D27207545000) (32) from the levers (6),(16) of the travel limitation unit 4CC (5).
(3) Remove the PIN - RIGGING (98D27207546000) (33) from the bellcrank assembly of the servo actuator 1025GM.
Subtask 27-23-51-865-051
E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CC1, 5CC2, 14CC1, 14CC2, 15CC
Subtask 27-23-51-860-055
F. Preparation for the Test
(1)
Make sure that the travel range of the rudder (2), the rudder travel limitation unit (5) is clear of tools and other items.
(2)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(3)
On the overhead panel 23VU, push the FLT CTL/FAC 1 pushbutton switch and the OFF legend goes off.
(4)
On the overhead panel 24VU, push the FLT CTL/FAC 2 pushbutton switch and the OFF legend goes off.
Subtask 27-23-51-710-050
G. Do the operational test of the rudder travel limiting function (Ref. TASK 22-61-00-710-001).
5. Close-up
________ Subtask 27-23-51-410-050
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the warning notice(s).
(3)
Close the access panels 325DL, 325DR.
(4)
Remove the access platform(s).
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TASK 27-23-51-000-002
Removal of the Electronic Module of the Rudder Travel Limitation Unit
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
__________________
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 8.0 m (26 ft. 3 in.)
98D27207545000 3 PIN - RIGGING
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 27-23-51-991-002 Fig. 402
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3. Job Set-up
__________ Subtask 27-23-51-861-051
A. Energize the aircraft electrical circuits. (Ref. TASK 24-41-00-861-002) Subtask 27-23-51-865-056
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