An aircraft powering system is provided which includes an aircraft electrical connector (100) is provided with features to allow facile engagement with an aircraft and strong retention forces. The aircraft powering system may include the aircraft electrical connector having a unique biasing mechanism (104) and modular construction, wherein the biasing mechanism is configured to place differential forces onto mating electrical connectors from an aircraft. The biasing mechanism may be operatively coupled to a handle (118) or trigger, which may be easily engageable by an operator.
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