返回首页
当前位置: 主页 > 通航资料 > TB >

TB20 MAINTENANCE MANUAL 28 FUEL TB20飞机维护手册 燃油(13)

时间:2011-11-02 15:43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
  
The tanks are equipped with a gage which is visible from the filler port.
The tanks are considered full (since this is not marked on the gage) when the fuel level rises to the edge of the filler port.
The filling point of each tank has a cap which may be locked and which is attached to the airframe by a chain.
The quantity of fuel is measured by four electric gage transmitters (two in each wing tank) and is displayed by two tank indicators integral with the engine monitoring cluster.
The indicators are graduated, with the zero indicating an empty tank. When the pointer of the indicator is at zero, approximately 1.3 US Gal (5 liters) of unusable fuel remains in the tank.
B. Tank cap (Figure 2)
Each tank cap is located on the upper wing surface. It blanks off an opening in the tank by which fuelling is carried out. When this cap is installed, the tank has to be sealed to prevent fuel leakage and the introduction of any foreign substance (such as water).
A safety chain is linked to the cap to prevent loss of the latter when removed.
Located near the tank cap, a placard will be installed listing tank capacity and specifications of fuel to be used.
C. Fuel tank bleed / drain (Figure 2)
The fuel tanks are equipped with a drain valve on the lower surface of each wing. The drain valve is located at the lowest point of the fuel tank to provide a collection point for contamination. The tank drains are located near the sealed inspection door 513 / 613 close to the main landing gear. Use a sample cup when removing fuel from the fuel tank drains to check for contamination.
D. Fuel system bleed S / N 731 - 9999
In addition to fuel tanks bleeding and draining points, as the system is lower than the tanks, an additional bleeding and draining point is installed under R.H. front fuselage near its intersection with wing.
AFAB
Validity : S / N 275 - 9999 28-10-00Page 2
(EA) SEP 04
 
1 - Rib
2 - Sealed inspection door
3 - Interior door on rib
4 - Filter
5 - Air inlet
6 - Gage
7 - Spar
8 - Air vent
ZONE RESERVOIR CARBURANT
 

 
Fuel tanks - Description and operation
Figure 1 - S / N 1 - 1037
 
1 - Rib
2 - Sealed inspection door
3 - Interior door on rib
4 - Sealed inspection door
5 - Fuel low level detector (Option Pre-MOD. 151, Standard Post-MOD. 151)
6 - Filter
7 - Air inlet
8 - Gage
9 - Spar
10 - Gage
11 - Air vent
ZONE RESERVOIR CARBURANT
 

 
Fuel tanks - Description and operation
Figure 1A - S / N 1038 - 9999
 

  1 - Tank cap
2 - Chain
3 - Seal
4 - Riveted base
5 - Riveted base
6 - Seal
7 - Bleeding body
 
  
 ®

5
6     1
 
中国通航网 www.ga.cn
通航翻译 www.aviation.cn
本文链接地址:TB20 MAINTENANCE MANUAL 28 FUEL TB20飞机维护手册 燃油(13)
 

------分隔线----------------------------