Overview

Data on design, manufacture and status

Latest or last design authority: Aérospatiale, Helicopter Division
Originally designed by Société Nationale Industrielle Aérospatiale

Latest or last primary manufacturer: Airbus Helicopters
Originally manufactured by Société Nationale Industrielle Aérospatiale

Parent type: Aérospatiale SA.330 Puma

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1-2

Crew seating: Side-by-side

Landing gear: Wheels (all retractable)

Overall Dimensions

Data on aircraft size

Overall Width: 15.09 m (49.5 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca TURMO IV C turbine

Engine manufacturer: Turbomeca

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 7400 kg (16314 lb)

Related VFS Resources

Resources related to the SA.330 J Puma, provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.

Related Public Resources

Resources related to the SA.330 J Puma, provided by public sources across the internet.

Images