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AircraftHelicoptersH225 Super Puma
HelicoptersSuper Puma / H225Introduced 2004

Airbus Helicopters

H225 Super Puma

The Airbus H225 (formerly EC225 Super Puma) is a long-range twin-engine heavy helicopter used for offshore oil-and-gas transport, search and rescue, and VIP missions. Powered by two Turbomeca Makila 2A1 engines with a five-blade Spheriflex rotor, it carries up to 19 passengers over long over-water distances with advanced autopilot and de-icing systems.

  • Long-range twin-engine heavy helicopter
  • Two Turbomeca (Safran) Makila 2A1 engines
  • Five-blade Spheriflex main rotor
  • Seats up to 19 for offshore transport
  • Full de-icing and 4-axis autopilot
  • SAR and VIP configurations available
Airbus Helicopters H225 Super Puma

H225 Super Puma key specifications

Range
540 nm
Cruise speed
142 kts
Passengers
up to 19
Max take-off weight
24,251 lb
Engines
2 × Turboshaft
Overview

About the H225 Super Puma

The Airbus Helicopters H225 Super Puma — part of the Super Puma / H225 family — is a helicopter aimed at point-to-point access without the need for a runway. It entered service in 2004 and is now an established, widely-supported design, developed in France.

On performance, it offers a maximum range of about 540 nautical miles and a cruise of roughly 142 knots. It seats up to 19 passengers and is powered by 2 Safran Makila 2A1 engines.

Its 540 nm range makes it well matched to short-haul hops and local operations. It is flown by a two-pilot crew and is approved for IFR flight. For buyers weighing the H225 Super Puma, compare its specifications and operating profile against the closest alternatives below before requesting a quote.

Gallery

At a glance

Performance

Max Range
540 nm
Cruise Speed
142 kt
Max Seats
19
MTOW
24,251 lbs

Full specifications

Operator and certification details for the H225 Super Puma, plus the complete performance, dimensions, weights and powerplant sheet — free with an account.

Country of Origin
France
Engines
2 × Turboshaft
Engine Model
Safran Makila 2A1
IFR Certified
Yes
Single-Pilot
Two-crew

20 more specifications — performance, dimensions, weights and powerplant — are free with an account.

View plans

Value & depreciation

How a helicopter like the H225 Super Puma typically holds value — indicative, class-typical retention of a new example against age. Run your own year and hours in the valuation calculator for a specific estimate.

At 5 years
~73%
of typical new value retained
At 10 years
~54%
of typical new value retained
At 15 years
~40%
of typical new value retained

Indicative only — actual value depends on hours, maintenance-program status, avionics, condition and the current market.

Pricing & seller quotes

Aggregated market pricing and multi-seller quotes — shared with verified partners.

Pricing is shared with verified partners

We aggregate live market pricing and seller quotes for the H225 Super Puma. Request a quote and our team will send tailored pricing and availability — or sign in if you’re an approved partner.

Prefer a quick public estimate? Estimate the H225 Super Puma cost of ownership with our free calculator.

Ownership & ROI calculator

Model the true economics of owning or chartering the H225 Super Puma. Pre-filled with realistic defaults for this type — adjust any assumption and the results update instantly.

Model the economics of the H225 Super Puma

Create a free account to see the true cost per flight hour and annual ownership cost. Upgrade for the full five-year ROI projection, charter profitability and a client-ready report.

True cost per flight hour
Fully-burdened ownership cost from fuel to financing — free.
Five-year ROI projection
Revenue, EBITDA, equity, ROI, NPV & IRR modelled out five years.
Charter profitability
Private, hybrid and full-charter scenarios side by side.
Compare aircraft
Acquisition, cost/hour and ROI across multiple types.

How the H225 Super Puma compares

Side by side with the most similar helicopters.

Performance
Range
540 nm
539 nm
430 nm
430 nm
Cruise speed
142 kt
151 kt
145 kt
150 kt
Max speed
Locked — sign in to view
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Service ceiling
Locked — sign in to view
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Rate of climb
Locked — sign in to view
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Capacity & dimensions
Max seats
19
19
10
12
Crew
Locked — sign in to view
Locked — sign in to view
Locked — sign in to view
Locked — sign in to view
Max takeoff weight
24,251 lbs
26,500 lbs
10,630 lbs
13,228 lbs
Length
Locked — sign in to view
Locked — sign in to view
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Locked — sign in to view
Cabin height
Locked — sign in to view
Locked — sign in to view
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Locked — sign in to view
Powerplant
Engines
2 × Turboshaft
2 × Turboshaft
2 × Turboshaft
2 × Turboshaft
Engine model
Safran Makila 2A1
GE CT7-8A
Pratt & Whitney Canada PW210A
Safran Arrano 1A

6 more specs per aircraft — ceiling, climb, cabin, dimensions and more — are free with an account.

Beyond the spec sheet

Buying or operating the H225 Super Puma? Get an independent acquisition recommendation, or see how fleet management keeps operations, maintenance, crew and compliance in one place.

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