返回首页
当前位置: 主页 > 通航资料 > TB >

TB20 MAINTENANCE MANUAL 32 起落架 TB20飞机维护手册(65)

时间:2011-11-03 13:08来源:蓝天飞行翻译 作者:航空
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
  
1) Jack up the aircraft - refer to 07-10-00.
2) Disconnect main landing gear door - refer to 32-10-05.
3) Remove cotter pin (7) and washer (6). Discard cotter pin (7).
4) Disconnect compensating spring (3). Retain roller (5).
5) Unlock main landing gear manually - refer to 32-30-03. Hold it to the up position.
6) Remove cotter pin (1), washer (2), clevis pin (4) and compensating spring (3). Discard cotter pin (1).
7) Set main landing gear manually to the down position. Lock.
C. Installation of compensating spring
1) Lubricate the roller (5), clevis pin (4) and compensating spring (3) with grease (TB 04-004A).
2) If necessary, test compensating spring (3) - refer to Paragraph 3.
3) Unlock main landing gear manually - refer to 32-30-03.
4) Install compensating spring (3) with clevis pin (4), washer (2) and new cotter pin (1).
5) Set landing gear to the down position. Lock.
6) Attach compensating spring (3) to hinged strut with roller (5), washer (6) and new cotter pin (7).
7) Connect main landing gear door - refer to 32-10-05.
WARNING : BEFORE ANY LANDING GEAR RETRACTION OR "NORMAL" OR "EMERGENCY" EXTENSION PROCEDURE, AND / OR LANDING GEAR CIRCUIT-BREAKER CLOSING, MAKE SURE THAT THE LANDING GEAR IMMEDIATE SURROUNDINGS ARE CLEAR (PERSONS OR THINGS).
8) Check landing gear emergency extension.
9) Lower the aircraft to ground and remove the jacks - refer to 07-10-00.
AAAA
Validity : S / N 1 - 9999 32-30 Page 201
05 (BA) JUN 01
 
  1 - Cotter pin
2 - Washer
3 - Compensating spring
4 - Clevis pin
5 - Roller
6 - Washer
7 - Cotter pin

1
14323005AAABWZ4000 7

Compensating spring - Removal / Installation
Figure 201
AAAA
Validity : S / N 1 - 9999 32 30 05 Page 202
 
3. ADJUSTMENT / TEST - COMPENSATING SPRING (Figure 202)
A. Tools and consumable materials
- Tension bench 0 - 8851 lbf.in (0 - 1000 N.m)
B. Test procedure - Compensating spring
NOTE : Perform this test at room temperature 68°F J.: 9° (20° C ± 5°).
1) Remove compensating spring - refer to Paragraph 2.
2) Place the compensating spring on the tension bench. CAUTION : NEVER EXCEED MAXIMUM STROKE.
3) If the forces are not included within the tolerances, discard compensating spring.
4) Install compensating spring - refer to Paragraph 2.
 
       Marge mini 10% Minimum margin 10%  
           
           
           
 
中国通航网 www.ga.cn
通航翻译 www.aviation.cn
本文链接地址:TB20 MAINTENANCE MANUAL 32 起落架 TB20飞机维护手册(65)
 

------分隔线----------------------------