SCHEMPP-HIRTH FLUGZEUGBAU GmbH, KIRCHHEIM/TECK
Ventus-3M „Performance“
FLIGHT MANUAL
March 2019
Revision –
7.10.1
7.10
Power plant system
The engine and the propeller (see engine and propeller manual for construction
and data) are attached to the propeller mount and connected by individual V-belts.
This unit is rotatably mounted at two points to the fuselage steel frame with rubber
elements for vibration damping and is rotated around a pivot point in the fuselage.
The arresting wire is attached to the propeller pylon.
An electrical spindle drive, anchored to the fuselage deck and linked to the pylon,
extends and retracts the latter.
The doors of the engine compartment are automatically opened and closed by a
linkage while the pylon extends / retracts.
The most important functions and displays for the operation of the power plant are
summarized in the power plant control system. The corresponding operating unit
for the pilot is mounted in the instrument panel. See page 7.3.5 and following for
further description of the power plant control system.
As additional control elements for the power plant, the pilot must also operate the
fuel shut-off valve, the throttle lever and, if necessary, the manual propeller brake.
After the engine has been stopped in flight, the further retraction of the power plant
is normally carried out by the power plant control system without any further action
of the pilot. After the ignition is switched off, the propeller is stopped, slowly turned
into the retraction position with assistance from the air stream, held there and then
the power plant retracts.
If necessary, the pilot can accelerate the alignment of the propeller by selectively
actuating the starter motor.
The stopping and the positioning of the propeller as well as retraction of the power
plant during flight can also be carried out by the pilot without automatic operation
with the aid of the manual propeller brake.
Содержание Ventus-3M Performance
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