Also known as Super Cougar

Empty weight accuracy within + 2% —Manual of H225 TD 2016


Data on design, manufacture and status

Design authority: Eurocopter Group

Primary manufacturer: Airbus Helicopters

Parent type: Eurocopter H225/EC225/AS332

Aircraft status: Operational


Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: TBA

Crew seating: Side-by-side

Landing gear: Wheels (all retractable)

Layout and Dimensions

Data on aircraft size

Overall Dimensions
Overall Height: 4.97 m 16.3 ft
Overall Length: 19.50 m 64.0 ft
Overall Width: 16.20 m 53.1 ft
Airframe Dimensions
Airframe Length:  
Airframe Width: 4.10 m 13.5 ft
Airframe Height:  
Landing Gear Dimensions
Landing Gear Base: 5.25 m 17.2 ft
Landing Gear Track: 3.00 m 9.8 ft
Cabin Dimensions
Cabin Internal Height:  
Cabin Internal Length:  
Cabin Internal Width:  

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 11,000 kg 24,251 lb
Max Gross Weight (airborne): 11,200 kg 24,692 lb
Max Take-off Weight: 11,000 kg 24,251 lb
Empty Weight: 5,594 kg 12,333 lb
Useful Load: 5,406 kg 11,918 lb
Empty Weight Fraction: 0.509
Climb Performance
Max Rate of Climb:  
Hover Performance
Hover Ceiling IGE:  
Hover Ceiling OGE:  
Max Level Flight Speed:  
Never Exceed Speed:  
Service Ceiling:  
Range and Endurance
Max Range:  
Max Endurance:  

Engine Details

Aircraft powerplant (lift and/or propulsion)

Provided powerplant data is for uninstalled, sea level, static operations.

Number of engines: 2
Designation: Turbomeca Makila 2A1 turbine
Manufacturer: Turbomeca
Normal Ratings
Max continuous:  
Take-off / rated:  
OEI Ratings
OEI contingency:  
OEI continuous:  
OEI 30-second: 1776 kW 2381 hp
OEI intermediate:  

Primary Lift Device

Data on primary lift devices such as main rotors

Main Rotor Characteristics
Direction of Rotation: Unknown
Hub Type:  
Main Rotor Blade Characteristics
Blade Construction:  
Blade Chord:  
Blade Tip Geometry:  
Blade Twist:  
Number of Blades:  
Main Rotor Derived Characteristics
Disc Area:  
Disc Loading:  
Main Rotor Blade Derived Characteristics
Blade area per blade:  
Tip Speed:  

Primary Control Device

Data on primary control devices such as tail rotors

Tail Rotor Characteristics
Configuration: Unknown
Direction of Rotation: Unknown
Tail Rotor Blade Characteristics
Number of Blades:  
Blade Construction: N/A
Blade Chord:  
Blade Twist:  
Tail Rotor Derived Characteristics
Disc Area:  
Tail Rotor Blade Derived Characteristics
Tip Speed:  
Blade Area (per blade):  

Related VFS Resources

Resources related to the H225M/EC725 Caracal, provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the H225M/EC725 Caracal, provided by public sources across the internet.