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(41)

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
  
6 - Protection valve
7 - Check valve
8 - Shuttle valve
9 - Spool valve
10 - Pump
11 - Low pressure valve
12 - Air intake
13 - Filter
14 - Motor shaft
15 - L.H. main gear actuator
16 - Emergency valve control
17 - Configuration and control panel
18 - Emergency valve
Extension and retraction - Landing gear system during extension
Key to Figure 4
 
Extension and retraction - Landing gear system during extension
Figure 4
 
1 - Nose gear actuator
2 - R.H. main gear actuator
3 - Pressure switch
4 - Reservoir
5 - High pressure valve
6 - Protection valve
7 - Check valve
8 - Shuttle valve
9 - Spool valve
10 - Pump
11 - Low pressure valve
12 - Air intake
13 - Filter
14 - Motor shaft
15 - L.H. main gear actuator
16 - Emergency valve control
17 - Configuration and control panel
18 - Emergency valve
Extension and retraction - Landing gear system in "extended and locked" position
Key to Figure 5
 
Extension and retraction - Landing gear system in "extended and locked" position
Figure 5
 
I AAAA
Validity : Electrohydraulic generator
"PRESTOLITE"
32-30-00 (AM) Page 13
JUN 02
 
1 - Nose gear actuator
2 - R.H. main gear actuator
3 - Pressure switch
4 - Reservoir
5 - High pressure valve
6 - Protection valve
7 - Check valve
8 - Shuttle valve
9 - Spool valve
10 - Pump
11 - Low pressure valve
12 - Air intake
13 - Filter
14 - Motor shaft
15 - L.H. main gear actuator
16 - Emergency valve control
17 - Configuration and control panel
18 - Emergency valve
Extension and retraction - Landing gear system "emergency extension"
Key to Figure 6
 
Extension and retraction - Landing gear system "emergency extension"
Figure 6
Ity 7AA Validity Electrohydraulic generator "PRESTOLITE" 32 30 00 (AM) JUN 0125
 
PAGE INTENTIONALLY LEFT BLANK
 
I AAAA
Validity : Electrohydraulic generator
"PRESTOLITE"
32-30-00Page 16
(AnA) JUN 02
 
EXTENSION AND RETRACTION
DESCRIPTION AND OPERATION
1. GENERAL
The landing gear maneuver system includes the following elements :
- main landing gear actuating cylinder,
- nose landing gear actuating cylinder,
- main landing gear hinged strut,
- nose landing gear hinged strut,
- main landing gear compensating spring,
- nose landing gear compensating actuator,
- end of travel microswitch.
2. LOCATION
COMPONENT QTY AREA ACCESS DOOR REFERENCE
 
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(41)
 
------分隔线----------------------------