钻石40飞机维护手册 DA 40 SERIES AMM 3(32)

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

A flexible hose with an internal capillary tube connects to the forward vent connector of the % outboard chamber to maintain ambient pressure within the fuel tank. The flexible hose has an outlet on the outer fuel tank access panel, on the lower surface of the wing.
%  The outboard chamber has a fuel filler in the top surface. You fill both the outboard chamber and
%  the inboard chamber through the fuel filler. The filler cap has a locking lever. You pull the locking lever up and turn the filler cap counter-clockwise to release it. You turn the cap clockwise to install it and push down the locking lever to lock it.
% The inboard fuel chamber has the outlet for the fuel feed to the engine. A finger filter prevents debris from entering the fuel system. A drain valve is located in the lower surface of the inboard % chamber. You can use this drain point for defueling the fuel tank and for doing fuel contamination tests.
%  A fuel sensor and a fuel probe attach to the inboard end of each of the inboard fuel chambers. Refer to Section 28-40 for more data on the fuel quantity indication system.
Doc # 6.02.01 Page 3
Rev. 4 09 Jan 2003

28-10-00
% 
% 
% 
% 
% 
% 
% 
% 
% 
% 
% 
%  Tank Filler 
% 
% 
% 
%  Long Range Chamber 
%  Fuel Probe 
%  Check Valve 
%  Flexible Coupling 

AIRCRAFT
Balance/Vent Hoses Capillary Balance Hose
Outboard Chamber
Balance/Vent Hoses Inboard Chamber
% Flexible Coupling % % % % % % % % % % % % %
DA 40 Series AMM
Finger Filter
Outlet Hose Outlet Hose from Left Tanks
% Figure 2: Fuel Tank System in the Right Wing, Long Range Tanks installed (O.M 40-071)
Page 4 Doc # 6.02.01 09 Jan 2003 Rev. 4
28-10-00
Fuel System
AMM

% B. Long Range Tanks (O.M 40-071)
% Figure 2 shows the fuel tank system in the right wing. The fuel tank system in the left wing is % similar.
% The DA 40 has a fuel tank in each wing. Each wing tank is made of three fuel chambers: the % inboard fuel chamber, the outboard fuel chamber and the long range fuel chamber. All fuel % chambers are interconnected. Aluminum makes the fuel chambers. Baffles in the tank prevent the % fuel from moving quickly from one end of the chamber to the other during flight.
% Each inboard fuel chamber has a capacity of 52.6 liters (13.9 US gal), each outboard fuel chamber % has a capacity of 26.1 liters (6.9 US gal) and each long range fuel chamber has a capacity of 15.9 % liters (4.2 US gal).The total fuel tank capacity of each wing is 94.6 liters (25 US gal).
% Large flexible couplings interconnect the individual fuel chambers. Worm drive clamps hold the % flexible couplings to the fuel chambers.
% Smaller diameter flexible hoses interconnect the individual fuel chambers at the top of the fuel % chambers. Two vent connections are located at the inboard end of the long range fuel chamber. % A flexible hose connects the forward vent connector to a check valve. Another flexible hose % connects the check valve to a vent connector on the outer fuel tank access panel, on the lower % surface of the wing.
% A flexible hose with an internal capillary tube connects to the forward vent connector of the long % range fuel chamber to maintain ambient pressure within the fuel tank. The flexible hose has an % outlet on the outer fuel tank access panel, on the lower surface of the wing.
% The long range fuel chamber has a fuel filler in the top surface. You fill all fuel chambers through % the fuel filler. The filler cap has a locking lever. You pull the locking lever up and turn the filler cap % counter-clockwise to release it. You turn the cap clockwise to install it and push down the locking % lever to lock it.
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：钻石40飞机维护手册 DA 40 SERIES AMM 3(32)