SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Arcus M
FLIGHT MANUAL
(
II
)
ON/OFF switch for the redundancy engine control system
Upward
position: Engine operation with redundancy system
Downward position: regular Engine operation
(
III
)
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
With engine running and valve switched to “STATIC” or “T.E. slow”, the
reading of the variometer(s) is steadier.
(
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 an engine speed exceeding 2000 RPM
- with ignition off:
However it is possible to support the vertical positioning of the propeller with
the starter although the ignition is switched off. The propeller moves in small
steps by pressing the starter button. In this process an engine start is not
possible.
(
VI
) Fire warning signal (with test button)
With fire inside the engine compartment, signal starts flashing.
October 2011
Revision --
7.3.17
