The Chinese revamp of the Changhe Z-8, announced a Airshow China 2002.  The WZ6 engines were replaced with P&WC PT6A-67B turboshafts.

Overview

Data on design, manufacture and status

Parent type: No type defined

Aircraft status: Status unknown

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 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 Z-8F , provided by the Vertical Flight Society.
Forum Proceedings
 
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Related Public Resources

Resources related to the Z-8F , provided by public sources across the internet.

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