Airbus Helicopters H145 vs Airbus Helicopters H215 vs Airbus Helicopters H225
The Airbus Helicopters H145 is a light twin in the company’s lineup, optimized for short to medium missions such as EMS, law enforcement, and utility work. It typically carries around 6 to 9 passengers depending on configuration and fuel fit, and its practical mission range is generally in the few-hundred–nautical-mile class. The H215 is a medium, workhorse-class twin derived from the Super Puma family, aimed at passenger transport, logistics, and utility missions with higher payload than the H145. It is commonly configured for roughly 19 to 22 passengers and offers a longer practical range than the H145, often around the mid-hundreds of nautical miles, mission-dependent. The H225 sits at the larger end of the same family as a heavy/large transport twin, targeting offshore energy, SAR, and high-capacity transport. It typically accommodates about 19 to 24 passengers in transport layouts and generally provides the longest range of the three, often in the upper-hundreds of nautical miles depending on payload, reserves, and optional tanks.
| Spec | AIRBUS H145 | AIRBUS H215 | AIRBUS H225 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 9.31 | $ 19.07 | $ 20.87 |
| Min Crew | 1 | 2 | 2 |
| Total Seats | 10 | 21 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters |
| Aircraft Name | H145 | H215 | H225 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 468 | 454 |
| DOC / nm / Seat | $ 0.93 | $ 0.91 | $ 0.99 |
| Max Cabin Seats | 9 | 22 | 28 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 8903 | 11929 |
| Standard Cabin Seats | 8 | 19 | 19 |
| Direct Operating Cost | $ 1,210 | $ 2,708 | $ 2,963 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 130 | 142 | 142 |
| Base Aircraft Price (USD) | $10,200,000 | $27,500,000 | $ 29,500,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 2 |
| Total Seats | 10 | 21 | 21 |
| Configuration | Green Interior | — | — |
| Max Cabin Seats | 9 | 22 | 28 |
| Standard Cabin Seats | 8 | 19 | 19 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Arriel 2E | Makila 1A1 | Makila 2A1 |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3000 | 3500 |
| Horsepower | 894 | 1820 | 2100 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | — | 540 | 684 |
| Dimensions | |||
| Length (ft) | 44.8 | 61.4 | 63.4 |
| Overall Height (ft) | 13 | 16.2 | 16.3 |
| Rotor Diameter (ft) | 36.1 | 51.2 | 53.2 |
| Cabin Volume (cu. ft) | 166 | 473.9 | 547 |
| Baggage Volume Ext. (cu. ft) | 46.8 | — | — |