FLIGHT MANUAL TSA-M, VARIANT S6
Doc.-No.: P400-006.000 E Page: 7-41 Revision: 10
Date of Issue: 07. October 2008 Date of Rev.: 06.07.2020
Engine-Master-
Switch:
Turns ON or OFF all electrical devices needed for
engine-operation (starter, propeller-pitch-control,
engine-
instruments and similar) by connecting them to
the battery or external-
alternator. This switch is
mechanically coupled to the „Batt“-Master-
turn ON the engine-bus with the „Gen“-master-switch,
the „Batt“-master-switch also needs to be turned ON. To
turn OFF the „Batt“-master-switch, the engine-
needs to be turned OFF. This makes certain, that the
external-
alternator is only turned ON, when the battery
is also turned ON.
Ignition-Switch: The key-
switch can be set to „OFF“, „RIGHT“, „LEFT“
and „BOTH“. It operates the ignition-
circuits and the
electrical engine-starter.
TCU-Isolation-Switch: This switch separates the waste-gate-
turbo-control-
unit when necessary. The switch is
protected against accidental activation because it only
needs to be operated in the event of a TCU-malfunction.
The normal operating position is the DOWN (protected)
setting. To disconnect the actuator, set the switch to the
Avionics-Master-
activates the avionics-bus. It is designed as a 20A-
Auxiliary-Fuel-
Pump(s):
The auxiliary-fuel-
pump is turned ON and OFF with this
switch when needed. The aux.-fuel-
same time as the main-fuel-
pump. If the switch is set to
ON, then the green indication-light on the announciator-
Fuel-Transfer-Pump: activates the automatic control for fuel transfer fro
left wing-tank (when installed) to the right wing
(=automatic fuel-transfer) (see section about the fuel-
Propeller-Pitch-
Rotary-
switch for adjusting the propeller’s pitch (see
section about the propeller)
Fire-Warning Warning light with push-button for alarm indication of fire
in the engine compartment by red light and acoustic
alarm signal, push to check function (see section 7.11.5)
To Next Page
Loading...
Need help?
General
