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STEMME S6

STEMME S6
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FLIGHT MANUAL TSA-M, VARIANT S6
Doc.-No.:P400-006.000 E Page: 4-22 Revision: 6
Date of Issue: 07. October 2008 Agency approved Date of Rev.: 26.09.2011
4.7.3 Cruise / Cross-Country-Flying
4.7.3.1 Cruise (Powered)
1.
Throttle
SET cruise-power according to MAP
2. Propeller-RPM ADJUST according to manifold-air-
pressure-gauge ==> see RPM-table
in section 4.1
3. Flaps Set to „CRUISE“ for fast cruise.
Set to „NEUTRAL“ for normal cruise
4.
Trim
SET according to air-speed
5. Cowl-flaps REDUCE according to throttle,
altitude, air-temperature and similar
6. Oil-temp. / CHT MONITOR continuously. If
necessary adjust cowl-flaps.
Recommended oil-temp. and CHT
for cruise is 194-212°F / 90-100°C
7. Fuel-management
(with optional left tank installed)
MONITOR
4.7.3.2 Fuel-Management
The integral-fuel-tanks are located in the inner-wing-section with automatic fuel-
extraction. The only way to control the fuel-extraction is by using the fuel-shut-
off-valve to interrupt the fuel-flow or the auxiliary-fuel-pump (which assists the
main-fuel-pump). The correct extraction of fuel can be monitored with the two
fuel-gauges and one low-fuel-caution-light.
The fuel-tank-system consists of one main-tank with a feeder-compartment in
the right wing. An auxiliary-tank in the left wing may be installed optionally.
If the engine is running, the feeder-compartment is filled automatically from the
main-tank by a pump. If the feeder-compartment is completely filled, then fuel
flows back into the right main-tank. The fuel-transfer-pump of the optional
auxiliary-tank also transports fuel into the feeder-compartment. Fuel is only
taken from the optional auxiliary-tank if less than 2/3 - 3/4 of the maximum
amount of fuel remains in the main tank and the fuel-transfer-pump is switched
ON.

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