SCHEMPP-HIRTH FLUGZEUGBAU GmbH, KIRCHHEIM/TECK
Ventus-3M „Performance“
FLIGHT MANUAL
March 2019
CS 22
Revision –
4.5.6.2
b) Procedure for stopping and retracting the power plant in manual mode or with
insufficient effect of the electric propeller brake in automatic mode
o
Carry out the cooling run with approx. 20% of power until the indicated
cooling water temperature has dropped below 60°C.
o
Speed 95 -100 km/h (51-54 kt, 59-62 mph) and flap po2
o
Ignition OFF
o
Approx. 3 seconds after switching off the ignition, first stop the propeller
by actuating the manual propeller brake.
Then release the manual propeller brake again.
o
Observe the propeller in the rearview mirror: By varying the manual
force on the handle of the propeller brake, center the propeller as
precisely as possible in the retraction position with the aid of the
aerodynamic forces and then hold on tight.
(In retraction position, the power plant operating unit unit shows
)
o
Retract the engine with the manual control switch.
Caution:
If it is not possible to hold the propeller exactly in the retraction
position, the power plant can still be retracted to a large extent. In
order to prevent damage to the aircraft, the retraction should be
stopped as soon as the propeller can be heard touching the engine
doors.
o
After the flight, determine the cause why the electric propeller brake did
not work correctly and eliminate it.
Содержание Ventus-3M Performance
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