| CPC H01R 13/20 (2013.01) [B64C 27/04 (2013.01); G01K 7/22 (2013.01); G05D 1/0808 (2013.01); H01R 9/2491 (2013.01); H01R 43/205 (2013.01); H01R 2201/26 (2013.01)] | 20 Claims |

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1. An aircraft comprising:
pilot flight controls;
a flight control computer coupled to the pilot flight controls, the flight control computer configured to receive input signals from the pilot flight controls and generate control signals according to the input signals; and
an engine comprising an engine control computer and a power converter, the engine control computer coupled to the flight control computer, the flight control computer further configured to transmit the control signals to the engine control computer, the power converter comprising power terminals and a battery connector, the battery connector comprising:
an antispark circuit coupled to the power terminals;
a charge pin coupled to the antispark circuit; and
power pins coupled to the power terminals, the charge pin being longer than each of the power pins.
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