DA 40 NG AFM
Airplane
Description
Doc. # 6.01.15-E
Rev. 3
01-Jul-2014
Page 7 - 33
A gascolator is located at the bottom side of the fuselage which is the lowest point of the
entire fuel system. A drain valve (pull to drain) is mounted to the gascolator, to allow the
remove of water and sediment which has collected in the fuel system.
A capacity probe measures the fuel quantity in each tank. The indication is non-linear,
therefore proportional calculations to determine the remaining fuel quantity or direct
calculations of fuel consumption are not possible. Information about the fuel consumption
can be found in Chapter 5 - PERFORMANCE.
Long Range Tank (if installed)
The tank chamber has a capacity of approx. 5 US gal (19 liter). The ventilation system
of the main and the auxiliary tank remains unchanged.
When the fuel quantity indicator reads zero, only the unusable fuel remains in the tank.
The useable capacity of each tank is 19.5 US gal, the maximum quantity that can be
indicated is 14 US gal. Up to an actual quantity of 14 US gal the indication is correct. At
an actual quantity above 14 US gal the indication remains at 14 US gal.
NOTE
When the fuel quantity indicator reads 14 US gal, the correct
fuel quantity must be determined with the alternate mean for
fuel quantity indication. If this measurement is not carried out,
the fuel quantity available for flight planning is 14 US gal.
Содержание DA 40 NG
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Страница 240: ...Mass Balance DA 40 NG AFM Page 6 8 Rev 3 01 Jul 2014 Doc 6 01 15 E 6 4 2 LOADING DIAGRAM...
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Страница 288: ...Airplane Description DA 40 NG AFM Page 7 28 Rev 3 01 Jul 2014 Doc 6 01 15 E Long Range Tank Schematic...
Страница 316: ...Handling DA 40 NG AFM Page 8 8 Rev 3 01 Jul 2014 Doc 6 01 15 E...
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