SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Ventus-2cM
FLIGHT MANUAL
4.2.2 Refueling / Entering fuel quantity
Internal refueling system
The connecting point of the refueling system is found behind the front wing
locating tube (with the GFRP access panel removed). The ON/OFF switch for
the additional fuel pump is on the fairing of the wing locating tube on the port
side. Hence only a single loose filler hose with a quick-disconnect coupling is
required for refueling – see sketch on page 4.2.2.2 and 4.2.2.3.
November
2003
LBA-app.
Revision --
4.2.2.1
Summary of Contents for Ventus-2cM
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