Also carries the British Army designation AH.Mk.1

Overview

Data on design, manufacture and status

Design authority: Société Nationale Industrielle Aérospatiale

Primary manufacturer: Westland Helicopters Ltd

Parent type: SNIAS SA.341

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Fenestron/Shrouded tail rotor

Crew required: 1-2

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Turbomeca Astazou IIIN2 turbine

Engine manufacturer: Turbomeca

Weights and Performance

Data on aircraft weight and flight characteristics

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Related Public Resources

Resources related to the SA.341B Gazelle, provided by public sources across the internet.

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