Airbus Helicopters H215 vs Leonardo Aw139
The Airbus Helicopters H215 and the Leonardo AW139 sit in different weight and mission categories. The H215 is a larger medium twin (often considered “super-medium”) derived from the Super Puma family, typically chosen for heavier utility work such as offshore transport, search and rescue, and cargo or sling-load missions where cabin volume and lifting capability are priorities. The AW139 is a medium twin optimized for speed, efficiency, and flexible multi-mission use, widely used for corporate/VIP, EMS, law enforcement, and offshore roles where fast point-to-point transport is important. In range terms, both can be configured for strong medium-range performance, but the H215 commonly offers longer endurance in passenger/utility configurations, especially with auxiliary fuel, while the AW139’s range is competitive and often emphasized alongside higher cruise speed. For passenger capacity, the H215 generally carries more people in a high-density layout, commonly around 19 passengers, whereas the AW139 typically seats fewer, commonly up to about 15 in high-density arrangements (with fewer in VIP/EMS fits).
| Spec | AIRBUS H215 | AGUSTA / LEONARDO AW139 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 19.07 | $ 11.69 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 17 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo |
| Aircraft Name | H215 | AW139 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 468 | 573 |
| DOC / nm / Seat | $ 0.91 | $ 0.69 |
| Max Cabin Seats | 22 | 15 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 8903 | 4701 |
| Standard Cabin Seats | 19 | 15 |
| Direct Operating Cost | $ 2,708 | $ 1,929 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 142 | 165 |
| Base Aircraft Price (USD) | $27,500,000 | $15,900,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 17 |
| Max Cabin Seats | 22 | 15 |
| Standard Cabin Seats | 19 | 15 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 1A1 | PT6C-67C |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3000 | 5000 |
| Horsepower | 1820 | 1679 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 540 | 414 |
| Dimensions | ||
| Length (ft) | 61.4 | 54.7 |
| Overall Height (ft) | 16.2 | 16.4 |
| Rotor Diameter (ft) | 51.2 | 54.7 |
| Cabin Volume (cu. ft) | 473.9 | 282 |
| Baggage Volume Ext. (cu. ft) | — | 120 |