CAA (now FAA) Approved Type Certificate 410. All data references are the same as for the Pitcairn PCA-2.  The engine is upgraded to the 420-hp Wright R-975-E-2, improving performance.

Overview

Data on design, manufacture and status

Design authority: Pitcairn Autogiro Company

Primary manufacturer: Pitcairn Autogiro Company

Parent type: Pitcairn PCA-2/3

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Gyroplane

Compound type: N/A compounded with 1 propulsors

Lift devices: 1 Single main rotor

Dedicated control device: 1 Rudder

Crew required: 1 in Tandem 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

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Related Public Resources

Resources related to the PA-21 , provided by public sources across the internet.

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