Airbus Helicopters AS332 L1 Super Puma Mk 1

Attribution

Attribution

Designated AS332 L1e with AHCAS system installed

Overview

Data on design, manufacture and status

Design authority: Aérospatiale, Helicopter Division

Primary manufacturer: Airbus Helicopters

Parent type: Aérospatiale H225/EC225/AS332

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 Height: 4.94 m (16.2 ft)

Overall Length: 18.70 m (61.4 ft)

Overall Width: 15.60 m (51.2 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca Makila 1A1 turbine

Engine manufacturer: Turbomeca

Max continuous power: 1185 kW (1588 hp)

Take-off / rated power: 1357 kW (1819 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

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