Designation format taken from Airbus Helicopters website (i.e. EC225 not EC 225). Sometimes referred to as Super Puma LP

Overview

Data on design, manufacture and status

Design authority: Airbus Helicopters

Primary manufacturer: Airbus Helicopters

Parent type: Airbus Helicopters 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

Crew seating: Side-by-side

Landing gear: Wheels (all retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 4.97 m (16.3 ft)

Overall Length: 19.50 m (64.0 ft)

Overall Width: 16.20 m (53.1 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca Makila 2A1 turbine

Engine manufacturer: Turbomeca

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 11000 kg (24251 lb)

Max Gross Weight (airborne): 11200 kg (24692 lb)

Max Range: 1135 km (613 nm)

Max Endurance: 5.6 hrs (5.6 hrs)

Related VFS Resources

Resources related to the H225/EC225/EC225e Super Puma Mk II+, provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
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Web files from vtol.org
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Webpages from vtol.org
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Related Public Resources

Resources related to the H225/EC225/EC225e Super Puma Mk II+, provided by public sources across the internet.

Images