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Note 1: Long power cable runs to a remote main battery* may need to route ignition bus power
through a dedicated 16 AWG cable to the battery. This avoids sharing a long power cable with the
starter motor, a combination that can exaggerate power dips and inhibit ignition operation while
cranking. Low battery, cold temperatures, small cable size, poor terminations, etc. can induce a
similar affect.
* Typical in RV10s, some canards, and others.
Note 2: The power test switch lets the operator turn aircraft power OFF for testing the ignition
internal alternators
– see Operating Notes and Ignition Checks earlier in the manual. The power
test switch can be configured several ways and is largely a matter of installer/operator preference.
1) If using switchable circuit breakers (vs. fuses) the breaker itself can be used as a power test
switch - one breaker per ignition.
2) A dedicated power test switch can also be used. One such implementation to consider is a
momentary push button switch (non-latching, normally closed
– push to open, one switch per
ignition) that offers the following advantages:
a) A push button is not likely to be mistaken, by sight or by feel, for other switches.
b) It cannot inadvertently be left in the OFF position.
c) It can be located close to kill switch for ergonomic one-handed operation.
d) Can pair with either key switch or toggle switches as shown below.
Power
Right
Power
Left
KILL
Right
KILL
Left
START
LEFT
BOTH
RIGHT
OFF
Power
Left
Power
Right