DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE:
CHAPTERPAGE 26
MAINTENANCE MANUAL STEMME S12
FUEL SYSTEM
Design
2 FRP-tanks in wing center section + 1 feeder
tank, 1 electrical fuel transfer pump for each
wing-tank + 2 electrical pumps from feeder tank
to the engine.
Maximum fuel volume 126.0 l ( 2%)
33.28 US gal.
27.72 Imp.gal.
Unusable fuel 1.4 l
0.37 US gal.
0.31 Imp.gal.
NOTICE
For more technical data, please refer to the S12 Aircraft Flight Manual.
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