钻石40飞机维护手册 DA 40 SERIES AMM 3(36)

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(2)  Install the fuel filler assembly: S Make sure that the mounting in the outboard chamber (Standard Tanks installed) or long range chamber (Long Range Tanks installed) is correctly aligned with the hole in the top surface of the wing. S Install the spacer ring onto the tank filler mounting. S Install a new O-ring seal in position over the spacer ring. S Install the bonding cable. S Install the 6 screws which attach the fuel filler to the outboard tank. S When all six screws are installed, then tighten the screws.  If necessary, move the tank assembly to give correct alignment. Use a fuel resistant sealing compound (DP300). Make sure that the O-ring is correctly positioned. At the position noted in 2.A.(9). Finger tight only. Tighten opposite screws. 
(3)  Connect the electrical cable to the fuel probe in the long range chamber.  Only if the Long Range Tanks are installed. At the in-line connector. 

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Detail Steps/Work Items  Key Items/References 
(4)  Connect the vent hose and the capillary hose to the vent outlets: S If necessary, remove the access panel from the lower surface of the wing. S Push the capillary hose onto the overboard vent pipe. S Install the clip which attaches the capillary hose to the pipe. S Push the vent hose onto the overboard vent pipe. S Install the clip which attaches the vent hose to the pipe. S Install the access panel.  Refer to Section 52-40. Refer to Section 52-40. 
(5)  Attach the bonding cable to the inboard end of the inboard fuel chamber: S Put the bolt up through the bonding tag on the inboard chamber. S Move the bonding cable into position on the bolt. S Install the washer and nut onto the bolt. S Tighten the bolt. 
(6)  Connect the electrical cable to the fuel probe in the inboard chamber.  At the in-line connector. 
(7)  Connect the electrical cable to the fuel level sensor in the inboard chamber.  At the in-line connector. 
(8)  Install the access panel at the wing root rib: S Put the access panel into position on the studs. S Install the 11 washers and nuts. S Tighten the nuts. 

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Detail Steps/Work Items  Key Items/References 
(9)  Install the drain valve: S Install a new O-ring onto the drain valve assembly. S Install the drain valve assembly into the mounting at the bottom of the inboard fuel chamber. S Secure the drain valve assembly with lock-wire. S Install the access panel.  Refer to Section 52-40. 
(10)  Install the wing onto the airplane.  Refer to Section 57-10. 
(11)  Refuel the airplane.  Refer to Section 12-10. Look specially for fuel leaks from the tank assembly which you have installed. 
(12)  Test the fuel storage system.  Refer to Paragraph 4. 

4. Test the Fuel Storage and Distribution System
Do this test when you have removed/installed a major component of the fuel system, or if there is any trouble with the fuel supply to the engine.
A. Equipment
Item  Quantity  Part Number 
25 liter (minimum) calibrated fuel container.  1  Commercial. 
Stopwatch.  1  Commercial. 

B. Procedure
You need two persons to do this test, one person in the airplane cockpit and one person at the engine bay.
Detail Steps/Work Items  Key Items/References 
(1)  Make sure that both the left and right fuel tanks are full. Refuel if necessary.  Refer to Section 12-10. 
(2)  Select the fuel selector in the cockpit to OFF. 
　
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