The AC312 is a 4 ton twin-turbine civil variant of the Harbin H425.  With side by side seating arrangement, the cabin layout is [2 pilot + 12 pax].  In air medical service, the cabin layout may be [1-2 pilot + 4 stretchers + 1 med] or [1-2 pilot + 2 stretchers + 4 meds].

The AC312 is operated with either AVIC ENGINE WZ-8, or TURBOMECA Arriel 2C powerplants.  Avicopter's AC312 obtained CAAC Type Certificate and Production Certificate, and passed the evaluation conducted by Aircraft Evaluation Group (AEG).

Maximum internal and external payloads are 1590 kg and 907 kg, respectively.  The maximum fuel weight is 915 kg.

Overview

Data on design, manufacture and status

Parent type: Avicopter Z-9

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Fenestron/Shrouded tail rotor

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

Landing gear: Wheels (all retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

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Related Public Resources

Resources related to the AC312 , provided by public sources across the internet.

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