The AC310 is a 1 ton piston helicopter, developed by Avicopter and certificated by CAAC in 2012.  Closely resembles the Schweizer 300C.  The AC310 has a fully articulated 3-blade rotor and a 2-3 seat cockpit.

The maximum payload is 431.5 kg.  The helicopter can be equipped with a standard fuel tank of 114 L and/or an Auxiliary tank of 72 L.

Overview

Data on design, manufacture and status

Design authority: AVICOPTER PLC

Primary manufacturer: AVICOPTER PLC

Parent type: No type defined

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 1-2 in Side-by-side arrangement

Landing gear: Skids

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Related VFS Resources

Resources related to the AC310 , provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the AC310 , provided by public sources across the internet.

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