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HelicoptersEcureuilIntroduced 2015

Airbus Helicopters

H125

The Airbus H125 (formerly AS350 B3e) is a single-engine light utility turbine helicopter renowned for its exceptional high-altitude and hot-day performance. It holds the record for the highest landing ever made on a helicopter, on the summit of Mount Everest. The H125 is widely used for utility, sling load, firefighting, EMS, and VIP transport operations worldwide.

  • Everest Summit landing record holder
  • Outstanding hot-and-high performance
  • Arriel 2D FADEC turboshaft engine
  • Versatile utility and EMS platform
  • Large cabin for the category
  • Fenestron tail rotor option on some variants
Airbus Helicopters H125

H125 key specifications

Range
335 nm
Cruise speed
130 kts
Passengers
up to 6
Max take-off weight
4,960 lb
Engines
1 × Turboshaft
Overview

About the H125

The Airbus H125 — long known as the AS350 Ecureuil, or AStar in North America — is the definitive single-engine utility helicopter and the benchmark for aerial work. Its combination of high power margins, hot-and-high performance and a rugged airframe has made it the aircraft of choice for load-lifting, firefighting, powerline and survey work, mountain operations and high-end tourism, and in 2005 an AS350 famously became the only helicopter to land on the summit of Mount Everest.

Powered by a Turbomeca/Safran Arriel 2D engine, it carries up to six and offers a large, flexible cabin and strong external-load capability. Operators value its simplicity, availability and the vast global support network built over decades of production.

The H125 is the right helicopter when the mission demands performance and payload in demanding environments from a single, economical airframe. Operators who need twin-engine redundancy for passenger transport over water or congested areas will step up to an H135 or H145; those whose work is utility, aerial and high-altitude flying consistently return to the H125.

Gallery

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At a glance

Performance

Max Range
335 nm
Cruise Speed
130 kt
Max Seats
6
MTOW
4,960 lbs

Full specifications

Operator and certification details for the H125, plus the complete performance, dimensions, weights and powerplant sheet — free with an account.

Country of Origin
France
Engines
1 × Turboshaft
Engine Model
Safran Arriel 2D
IFR Certified
Varies
Single-Pilot
Yes

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

View plans

Value & depreciation

How a helicopter like the H125 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 H125. 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 H125 cost of ownership with our free calculator.

Ownership & ROI calculator

Model the true economics of owning or chartering the H125. Pre-filled with realistic defaults for this type — adjust any assumption and the results update instantly.

Model the economics of the H125

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 H125 compares

Side by side with the most similar helicopters.

Performance
Range
335 nm
335 nm
330 nm
360 nm
Cruise speed
130 kt
130 kt
133 kt
125 kt
Max speed
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Service ceiling
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Rate of climb
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Capacity & dimensions
Max seats
6
8
7
5
Crew
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Max takeoff weight
4,960 lbs
5,070 lbs
5,250 lbs
3,609 lbs
Length
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Cabin height
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Powerplant
Engines
1 × Turboshaft
1 × Turboshaft
1 × Turboshaft
1 × Turboshaft
Engine model
Safran Arriel 2D
Safran Arriel 2D
Rolls-Royce M250-C47E/4
Safran Arrius 2R

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

Beyond the spec sheet

Buying or operating the H125? Get an independent acquisition recommendation, or see how fleet management keeps operations, maintenance, crew and compliance in one place.

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