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Tecnam P2006T - Page 225

Tecnam P2006T
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Page 7 - 43
Section 7 – Airframe and Systems description
ELECTRICAL SYSTEM
4
th
Edition, Rev 0
The second ones allow, through a relay, for realizing the parallel connection be-
tween the pertinent generator bus and the battery bus. Setting these ones to OFF,
the pertinent generator bus (and related avionic bus supplied) is separated from the
battery bus and from opposite generator bus.
When both generators are correctly operating and all above mentioned switches
are in ON position, all the busses are connected to the generators.
The ignition switches, two for each engine and grouped on the over head panel,
are instead independent from the airplane electrical system (generation and distri-
bution); they only control and open the engine electrical circuit
WARNING
If ignition switches are turned ON, a propeller movement can
cause the engine starting with consequent hazard for people
nearby.