The aircraft was built by Doman and later financed by Curiss Wright (as a development vehicle). The aircraft was designated as the CW-40 by Curtiss Wright.

The aircraft was an 8 place machine.

Tthe aircraft also served as the prototype fro the LZ-5 (YH-31).

Overview

Data on design, manufacture and status

Design authority: Doman Helicopters Inc.

Primary manufacturer: Doman Helicopters Inc.

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 in Side-by-side arrangement

Landing gear: Wheels (non-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 LZ-4 (CW-40), provided by the Vertical Flight Society.
Forum Proceedings
 
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Related Public Resources

Resources related to the LZ-4 (CW-40), provided by public sources across the internet.

Images