The Z-9-H425 entered service in 2005.  The helicopter featured an electronic flight instrumentation system from Rockwell Collins; the glass cockpit is also from Rockwell Collins.  Maximum internal and external payloads are 1,900 kg and 1,600 kg, respectively.  The aircraft capacity is 12-13 passengers.

The H425 is the improved version of the H410A, a Z-9 variant.  After the initial flight of the H425 in December 2003, the helicopter received CAAC certification in December 2004.

Overview

Data on design, manufacture and status

Parent type: Harbin 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

Related VFS Resources

Resources related to the H425 , provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the H425 , provided by public sources across the internet.

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