SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Ventus-2cM
FLIGHT MANUAL
(
II
)
Pneumatic valve
Panel-mounted two-way cock (should a total energy compensation
probe be used).
T.E.
=
Variometer(s)
fed
from T.E. Compensation probe
STATIC
=
Variometer(s)
fed
from Static Pressure ports
or
T.E.
=
Variometer(s)
fed
from T.E. Compensation probe
T.E.
slow
=
Variometer(s)
fed from T.E. Compensation probe
with
restrictor
With engine running and valve switched to “STATIC” or “T.E. slow”, the
reading of the variometer(s) is steadier.
(
III
) Pneumatic
valve
Panel-mounted two-way cock for feeding the ASI from either the Pitot
pressure head in the fin or in the fuselage nose.
in glide
=
Pitot head in fin
power on
=
Pitot head in nose
(
IV
) Outside air temperature indicator
When carrying water ballast, the outside air temperature (OAT) must not drop
below 2° C / 36° F.
(
V
) Stick mounted starter button
The starter motor is cut off
- with propeller not fully extended (watch signal)
- with ignition switched off (watch signal)
- with prop arresting handle not in fully forward position (watch signal)
- with an engine speed exceeding 1200 RPM
(
VI
) Fire warning signal (with test button)
With fire inside the engine compartment, signal starts flashing.
By depressing the test button, signal also flashes.
(
VII
) Emergency
switch
Description refer to page 7.3.7
(
VIII
)
Fuselage console
Description refer to page 7.3.8 and 7.3.9
(
IX
) External power receptacle (optional) not shown
Receptacle is installed on the left below the instrument panel.
With an external power source connected, the electrical system is in
working order - even with master switch OFF.
November
2003
Revision --
7.3.6
Summary of Contents for Ventus-2cM
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