Bristol Sycamore HR.14

Royal Air Force (RAF) SAR version.

Source: ”Helicopters & Autogyros of the World”, Paul Lambermont with Anthony Pirie, Second edition 1970, Cassell & Company Ltd, SBN 304 93390 2

and,

Source: ”Bristol 171 Sycamore”, BAe Systems Heritage Team, BAe Systems Heritage Web site, Last accessed 11 Jul 2018 (with kind permission from BAe)

Attribution

Overview

Data on design, manufacture and status

Design authority: Bristol Aeroplane Company, Helicopter Division

Primary manufacturer: Bristol Aeroplane Company, Helicopter Division

Parent type: Bristol Type 171 Sycamore

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

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Related Public Resources

Resources related to the Sycamore HR.14, provided by public sources across the internet.

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