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AS332 Super Puma vs H225M / EC725 Caracal

AS332 Super Puma vs H225M / EC725 Caracal at a glance — top speed 327 vs 324 km/h, range 851 vs 930 km, max takeoff weight 9,150 vs 11,200 kg, built 890 vs 90 units.

Aérospatiale AS332 Super Puma military helicopters side profile drawing
Airbus Helicopters H225M / EC725 Caracal military helicopters side profile drawing
🇩🇪🇫🇷 H225M / EC725 Caracal
Specifications
AS332 Super Puma H225M / EC725 Caracal
Origin country 🇫🇷 France 🇩🇪 Germany🇫🇷 France
Category Military Helicopters Military Helicopters
Manufacturer Aérospatiale Airbus Helicopters
First flight 13 September 1978 27 November 2000
Year introduced 1981 2005
Number produced 890 units 90 units
Average unit price -- $70 million
Wing area 206.1 m² -- m²
Wingspan 16.2 m 16.2 m
Height 5.0 m 4.6 m
Length 16.8 m 19.5 m
Maximum speed 327 km/h 324 km/h
Operational range 851 km 930 km
Service ceiling 5,180 m 6,100 m
Max. takeoff weight 9,150 kg 11,200 kg
Empty weight 4,660 kg 5,330 kg
Total thrust 2 x 1,376 kW 2 x 1,776 kW
Performance Radar Chart

Detailed Comparison

The Airbus H225M Caracal is a direct, heavy-duty evolution of the Aérospatiale AS332 Super Puma airframe, engineered to solve the survivability and payload deficits identified by French forces operating older Puma variants in hostile environments. While the AS332 established the European medium-lift utility baseline in the 1980s, producing 890 units, the H225M was procured specifically for dedicated Combat Search and Rescue (CSAR) and special operations.

Development and Design

The AS332 emerged in the 1970s as a utility transport, prioritizing crashworthiness, a monocoque tail boom, and a widened fuselage over the legacy SA 330. It relies on a four-blade rotor and Turbomeca Makila 1A2 turboshafts.

The H225M was developed in the late 1990s after the French Air Force demanded a more survivable CSAR platform. Eurocopter upgraded the dynamic system with a five-blade composite main rotor utilizing a new airfoil to reduce vibration during high-speed, low-altitude ingress. The airframe integrates modular armor plating, dual-channel Full Authority Digital Engine Control (FADEC), and an all-glass cockpit. The H225M also natively integrates the HForce Generic Weapon System, coupling a Thales Scorpion helmet-mounted sight with Wescam electro-optics to guide Hellfire missiles, a capability absent from base AS332 variants.

Specifications and Performances

The transition from utility to dedicated combat platform required structural and propulsion overhauls.

  • Weight and Payload: The H225M operates with a Max Takeoff Weight of 11,200 kg, a 2,050 kg increase over the AS332's 9,150 kg MTOW, to accommodate armor, sensors, and weaponry.
  • Power: To prevent this weight from degrading flight characteristics, Airbus integrated Makila 2A1 engines. These produce 1,776 kW each, a 29% thrust increase over the AS332’s 1,376 kW output.
  • Altitude: The H225M extends the service ceiling from 5,180 m to 6,100 m, an aerodynamic modification driven by high-altitude extraction requirements.

Deployment and usage

The AS332 operates globally in utility, MEDEVAC, and maritime patrol roles. The French Army deployed it during the 1994 Rwanda intervention, and the Swedish and Spanish air forces utilized it for MEDEVAC in Afghanistan. It remains heavily utilized in civilian offshore oil transport.

The H225M is deployed into higher-threat environments. The French Air Force inserted Caracals into Lebanon for Opération Baliste in 2006 and later into Kabul. Combat feedback from Afghanistan forced a 2013 upgrade cycle, adding SAGEM FLIR, Nexter door guns, and low-temperature FADEC modifications. Export usage reflects its combat designation: Mexico utilizes armed EC725s for counter-cartel operations, losing one airframe to hostile fire during Operation Jalisco in 2015.

Conclusion

The AS332 retains the edge in mass-procurement utility transport and uncontested maritime patrol. It delivers standard medium-lift capabilities at a volume and operating cost the Caracal is not designed to match. However, for contested airspace, the H225M is the definitive choice. Air forces executing CSAR or special operations infiltration require the H225M; its $70 million acquisition cost buys the Makila 2A1 engines, structural armor, and integrated HForce targeting required to survive and operate in deep-penetration missions where an AS332 would be compromised.

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Frequently Asked Questions

Which is faster, the AS332 Super Puma or H225M / EC725 Caracal?
The AS332 Super Puma is faster with a maximum speed of 327 km/h compared to the H225M / EC725 Caracal's 324 km/h, a difference of 3 km/h.
Which has longer range, the AS332 Super Puma or H225M / EC725 Caracal?
The H225M / EC725 Caracal has a longer range at 930 km compared to the AS332 Super Puma's 851 km.
Which can fly higher, the AS332 Super Puma or H225M / EC725 Caracal?
The H225M / EC725 Caracal has a higher service ceiling at 6,100 meters (20,013 ft) compared to the AS332 Super Puma's 5,180 meters (16,994 ft).
Which is heavier, the AS332 Super Puma or H225M / EC725 Caracal?
The H225M / EC725 Caracal has a higher maximum takeoff weight at 11,200 kg compared to the AS332 Super Puma's 9,150 kg.
Which is larger, the AS332 Super Puma or H225M / EC725 Caracal?
The H225M / EC725 Caracal is longer at 19.5 meters compared to the AS332 Super Puma's 16.8 meters.
Which entered service first, the AS332 Super Puma or H225M / EC725 Caracal?
The AS332 Super Puma entered service first in 1981, 24 years before the H225M / EC725 Caracal which entered service in 2005.
Which has been built in greater numbers, the AS332 Super Puma or H225M / EC725 Caracal?
The AS332 Super Puma has been produced in greater numbers with 890 units compared to 90 units of the H225M / EC725 Caracal.