(7)
 Remove the access platform(s).

 (8)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

R 1EFF : 106-149, 159-199, 211-299, 301-399, 1 27-21-41Page 447 1401-499, 1Aug 01/05 1 1 1CES 1R Servo Actuator Connection at the Rudder with Bolt PN D55370020800 R Figure 407/TASK 27-21-41-991-010

 1EFF : ALL 1 27-21-41Page 448 1 1 Nov 01/04 1 1 1CES 1

 RUDDER - INSPECTION/CHECK_________________________
 TASK 27-21-41-200-001
 Inspection/Check of the Rudder
 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 GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______ GEAR.
 1. Reason for the Job__________________
 Because the free movement is more than the limits.
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  warning notice 
R  B. Expendable Parts 
R R R  -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R  1  bushes  27-21-04 15A-040

R C. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
27-21-41-000-001
27-21-41-400-001
55-36-41-000-001
55-36-41-400-001

R  55-46-11-000-001
R  55-46-11-400-001 CMM 55-41-13 27-21-41-991-007

R  27-21-41-991-009
R  27-21-41-991-008
3. Job Set-up
__________
 Subtask 27-21-41-941-055Removal of the RudderInstallation of the RudderRemoval of the Hinge Arm Fittings No. 1 thru No. 7Installation of the Hinge Arm Fittings No. 1 thru No. 7 Removal of Rudder Hinge Bearing No. 6 Installation of Rudder Hinge Bearing No.6(for corrective action)Fig. 601 Fig. 602 Fig. 603
 A. Put a warning notice in position to tell persons not to operate the flight controls.
 Subtask 27-21-41-010-053
 B. Remove the rudder (Ref. TASK 27-21-41-000-001).
 Subtask 27-21-41-860-055
 C. Replacement Information
 (1) Do a check of the rudder attachment parts for wear, damage and corrosion.
R (a) If it is necessary to replace the bushes of the rudder hinge
R fittings, the actuator attach fittings, or the fork assy:
R (Ref. Fig. 601/TASK 27-21-41-991-007)
R and
R (Ref. Fig. 602/TASK 27-21-41-991-009)

 -Refer to the Component Maintenance Manual (Ref. CMM 55-41-13) for the correct procedure.
R (b) If it is necessary to replace the rudder hinge bearing No. 6:
R (Ref. Fig. 601/TASK 27-21-41-991-007)
R - (Ref. TASK 55-46-11-000-001) and (Ref. TASK 55-46-11-400-001).

R  Fits and Clearances of the Rudder Hinge Fittings Figure 601/TASK 27-21-41-991-007
 1EFF : 1 1 1CES  ALL  1 111 27-21-41 Page 603 Nov 01/03

R Fits and Clearances of the Actuator Attach Fittings and the Fork Assy R Figure 602/TASK 27-21-41-991-009
 1EFF : ALL 1 27-21-41Page 604 1 1 Feb 01/02 1 1 1CES 1

R R  (c) If it is necessary to replace rudder hinge arm attach fittings: (Ref. Fig. 603/TASK 27-21-41-991-008) - (Ref. TASK 55-36-41-000-001) and (Ref. TASK 55-36-41-400-001).
 4. Procedure_________
 (Ref. Fig. 601/TASK 27-21-41-991-007)
 Subtask 27-21-41-220-050 
R R  A. Measurement of the Fits and Clearances of the Rudder Hinge Fittings (Ref. Fig. 601/TASK 27-21-41-991-007)
 -------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | B | 17.987 | 18.000 | | | 17.977 | | | | OD 1 |(0.7081) |(0.7086) | | |(0.7077) | | | | | | | 0.000 | 0.031 | | | 0.066 | | | | | (0.0000)| (0.0012)| | |(0.0025)| | B | 18.000 | 18.018 | | | | 18.043 | | | ID 2 |(0.7086) |(0.7093) | | | |(0.7103) | | -------------------------------------------------------------------------------
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱2(14)