• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 13:47来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
 -------------------------------------------------------------------------------
2 bush 27-24-04 20 -100A 2 bush 27-24-04 20A-100 3 bolt 27-24-04 20 -060A 3 bolt 27-24-04 20A-060 4 bush 27-24-04 20 -110 4 bush 27-24-04 20A-110
 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
27-24-51-000-001 Removal of the Rudder Servo Control
 1025GM/2025GM/3025GM
 27-24-51-400-001 Installation of the Rudder Servo Control
 1025GM/2025GM/3025GM

R CMM 55-41-13 (for corrective action) 27-24-51-000-001 Removal of the Rudder Servo Control 1025GM/2025GM/3025GM (for corrective action) 27-24-51-000-003 Removal of the Rudder Servo Control Eye End (for corrective action) 27-24-51-400-001 Installation of the Rudder Servo Control 1025GM/2025GM/3025GM (for corrective action) 27-24-51-400-003 Installation of the Rudder Servo Control Eye End (for corrective action) 27-24-51-991-005 Fig. 601


 3. Job Set-up__________
 Subtask 27-24-51-010-053
 A. Remove the rudder servo control (Ref. TASK 27-24-51-000-001).
 4. Procedure_________
 (Ref. Fig. 601/TASK 27-24-51-991-005)
 Subtask 27-24-51-220-050 
R  A. Measure of the Fits and Clearances
 (1) Do an inspection of the two ends of the servo-control bearings. 
R R  (a) Make sure that the inner dimensions of the two servo-control bearings (6) are between 19.037 mm (0.7494 in.) and 19.050 mm (0.7500 in.). 
R R  (b) Replace the servo-control bearing(s) (6) if the dimensions are not correct (Ref. TASK 27-24-51-000-003) and (Ref. TASK 27-24-51-400-003). 
R R  (c) Replace the servo-control if you find wear (Ref. TASK 27-24-51-000-001) and (Ref. TASK 27-24-51-400-001).
 (2) Continue with the check of the fits and clearances in the subsequent tables (for section C-C and section D-D).
 -------------------------------------------------------------------------------
| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | C,D | 22.984 | 23.000 | | | 22.984 | | | | OD 2 |(0.9048) |(0.9055) | | |(0.9048) | | | | | | | 0.000 | 0.037 | | | 0.037 | | | | | (0.0000)| (0.0014)| | |(0.0014)| | C,D | 23.000 | 23.021 | | | | 23.021 | | | ID 1 |(0.9055) |(0.9063) | | | |(0.9063) | | -------------------------------------------------------------------------------
NOTE : No wear is permitted between the bush (1) and the bush (2).____

 

R  Rudder Servo Control Figure 601/TASK 27-24-51-991-005
 1EFF : 1 1 1CES  ALL  1 111 27-24-51 Page 603 May 01/05

 

 (3) If necessary, replace the bush (1) (Ref. CMM 55-41-13) and/or the bush (2).
 Subtask 27-24-51-220-051
 B. Measurement of the Fits and Clearances
 -------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | C,D | 19.024 | 19.037 | | | 19.024 | | | | OD 3 |(0.7489) |(0.7494) | | |(0.7489) | | | | | | | 0.000 | 0.034 | | | 0.034 | | | | | (0.0000)| (0.0013)| | |(0.0013)| | C,D | 19.037 | 19.058 | | | | 19.058 | | | ID 2 |(0.7494) |(0.7503) | | | |(0.7503) | | -------------------------------------------------------------------------------
NOTE : No wear is permitted between the bolt (3) and the bush (2).
____
 (1) If necessary, replace the bolt (3) and/or the bush (2).
 Subtask 27-24-51-220-052
 C. Measurement of the Fits and Clearances
 -------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | C,D | 19.024 | 19.037 | | | 19.024 | | | | OD 3 |(0.7489) |(0.7494) | | |(0.7489) | | | | | | | 0.000 | 0.034 | | | 0.034 | | | | | (0.0000)| (0.0013)| | |(0.0013)| | C,D | 19.037 | 19.058 | | | | 19.058 | | | ID 4 |(0.7494) |(0.7503) | | | |(0.7503) | | -------------------------------------------------------------------------------
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵2(151)