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时间:2011-03-21 13:47来源:蓝天飞行翻译 作者:admin
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 Subtask 27-26-41-710-050
R D. Test
 (1)
 Remove the rigging pin 98D27207516330, or 98D27207549000 from the yaw damper bellcrank.

 (2)
 Remove the warning notice(s).


R  (3) Do the operational test of the rudder hydraulic actuation (Ref. TASK 27-24-00-710-001).


 5. Close-up________
 Subtask 27-26-41-860-053
 A. Put the aircraft back to the serviceable condition.
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Apply a layer of SPECIAL MATERIALS (Material No. 05-027) to the adjacent structure.
 (3) Make sure that the drain holes in the adjacent structure are not blocked. 
R  Subtask 27-26-41-410-050-A 
R  B. Close Access 
R R  (1) Make sure that the work area is clean and clear of tool(s) and other items. 
R  (2) Close the access panel 325BL (Ref. TASK 55-33-13-410-002). 
R  (3) Remove the access platform(s).

 

 CENTERING SPRING ROD - YAW DAMPER SERVO ACTUATOR - INSPECTION/CHECK
___________________________________________________________________
 TASK 27-26-41-280-001
 Removal of the Centering Spring Rod of the Yaw Damper for Workshop Test

 1.
 Reason for the Job

__________________
 Refer to the MPD TASK: 272100-04


 2.
 Job Set-up Information


______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-26-41-000-001  Removal of the Centering Spring Rod for the Actuator of the Yaw Damper Servo 27-26-41-400-001 Installation of the Centering Spring Rod for the Actuator of the Yaw Damper Servo CMM 272641
 3. Job Set-up
__________
 Subtask 27-26-41-020-051

 A. Remove the centering spring rod of the yaw damper (Ref. TASK 27-26-41-000-001).
 4. Procedure
_________ Subtask 27-26-41-280-050 R A. Do a check of the centering spring rod of the yaw damper in the workshop R (Ref. CMM 272641).
 5. Close-up
________
 Subtask 27-26-41-420-051

 A. Install the centering spring rod of the yaw damper (Ref. TASK 27-26-41-400-001).


 SERVO ACTUATOR - YAW DAMPER (3CC1,3CC2) - REMOVAL/INSTALLATION
______________________________________________________________
 TASK 27-26-51-000-001
 Removal of the Yaw Damper Servo Actuator (3CC1) and (3CC2)
 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 blanking caps No specific circuit breaker(s) safety clip(s) No specific drainage container No specific warning notices No specific drainage container 4.0 l (1.0566 USgal) No specific adjustable access platform 6.0 m (19 ft. 8 in.) 98D27207516000 1 RIGGING PIN SET 98D27207549000 1 PIN - RIGGING
 1EFF : ALL 1 27-26-51Page 401 1 1 Aug 01/01R 1 1 1CES 1


 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-00-00-864-001  Put the Related Hydraulic System in the Depressurized
 Configuration before Maintenance Action
 29-00-00-910-002  Safety Procedures of the Hydraulic System
 29-14-00-614-001  Depressurization of the Hydraulic Reservoirs
 55-33-13-010-002  Opening/Removal of the Trailing Edge Access-Panels
 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and
 325BR
 27-26-51-991-001  Fig. 401
 3. Job Set-up__________

 (Ref. Fig. 401/TASK 27-26-51-991-001)
 Subtask 27-26-51-010-050-A
 A. Get Access
 (1) Put the adjustable access platform in position. 
R R R  (2) Open the access panel 325BL (for 3CC1) and/or 325BR (for 3CC2) at the trailing edge of the vertical stabilizer (Ref. TASK 55-33-13-010-002).
 
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