Aircraft overview

The Airbus Helicopters H215 / H225 Super Puma represents the current heavy end of the Super Puma family, a twin engine, multi purpose helicopter line that began with the AS332 Super Puma, first flown in 1978. The H225, formerly EC225, first flew in 2000 and entered service in the mid 2000s. The H215 is the modernized civil and governmental continuation of the AS332 L1e line. Both serve missions where long range, high payload, twin engine redundancy and all weather capability are central, including offshore transport, search and rescue, utility lift, firefighting, law enforcement and military support.

Performance & specifications

Typical cruise speed is about 140 knots, with the H225 commonly quoted at around 452 nautical miles of range with standard fuel, depending on reserves, payload and equipment. Service ceiling is generally listed at up to 20,000 feet. The H215 is powered by two Safran Makila 1A1 turboshafts, while the H225 uses two Safran Makila 2A1 engines. Maximum takeoff weight is approximately 18,960 lb for the H215 and 24,251 to 24,692 lb for H225 configurations. External lift capability and installed mission equipment vary materially by aircraft, so logbook and configuration review is essential.

Cabin & avionics

The cabin is sized for utility rather than light corporate use, typically seating up to 19 passengers in transport layout, with large sliding doors and provisions for stretchers, rescue gear, cargo or mission consoles. Offshore aircraft may include emergency flotation, life rafts, HUMS, weather radar, satellite tracking and crash resistant seating. Avionics are Airbus centered, not Garmin Perspective or G1000. Typical equipment includes a digital flight deck, dual flight management systems, automatic flight control with 4 axis autopilot capability, TAWS, TCAS options, radar and comprehensive systems monitoring. Later and upgraded aircraft may feature Airbus Helionix architecture, depending on model and retrofit status.

Buying & value

Used market buyers should distinguish carefully between H215, H225 and earlier AS332 or EC225 designations, as weights, engines, avionics and support status differ. Key diligence items include offshore corrosion exposure, gearbox and main rotor component life, Makila engine condition, HUMS data, airworthiness directive compliance, mission equipment approvals and records after any heavy maintenance or conversion. H225 values are influenced by oil and gas demand, SAR contracts and fleet standardization, while H215 aircraft often appeal to operators needing Super Puma capability with lower acquisition complexity. Common upgrades include modern avionics, HUMS enhancements, mission interiors, flotation systems, hoists and firefighting equipment.