Airbus Helicopters H225 vs Daher Tbm 960 vs Piaggio Avanti Evo
The Airbus H225 is a twin‑engine heavy helicopter designed primarily for offshore transport, search and rescue, and utility missions. It typically carries around 19 passengers (configuration dependent) and offers a practical range on the order of roughly 450–650 nautical miles, trading speed and range for vertical‑lift access to remote or confined landing sites. The Daher TBM 960 is a single‑engine turboprop airplane optimized for fast owner‑pilot or small executive travel. It usually seats 4–6 passengers (up to 6 plus pilot depending on layout) and delivers long legs, commonly around 1,000–1,700 nautical miles depending on power settings and payload, making it the range leader of the three for point‑to‑point runway operations. The Piaggio Avanti EVO is a twin‑engine turboprop aircraft aimed at efficient, high‑speed executive transport. It generally seats about 6–8 passengers and offers mid‑to‑long range, typically around 1,200–1,700 nautical miles, combining jet‑like cruise speeds with turboprop economics, but requiring suitable runways.
| Spec | AIRBUS H225 | Daher TBM 960 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | — |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 8 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Piaggio |
| Aircraft Name | H225 | TBM 960 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | — |
| Max Cabin Seats | 28 | — | 7 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 | 3775 |
| Standard Cabin Seats | 19 | 4 | 6 |
| Direct Operating Cost | $ 2,963 | $ 744 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 330 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $ 7,695,000 |
| Aircraft Type | — | Turbo Prop | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 8 |
| Max Cabin Seats | 28 | — | 7 |
| Standard Cabin Seats | 19 | 4 | 6 |
| Lavatory | — | No | No |
| Galley Location | — | MID | — |
| Cabin Pressure (psi) | — | 6.2 | 9 |
| SL Cabin Altitude (ft) | — | 14390 | 24000 |
| Galley / Refreshment | — | — | No |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | PT6A–66B |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 3500 | 3600 |
| Horsepower | 2100 | 850 | 850 |
| No. of Engines | 2 | — | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 49 | ISA + 28 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 63.4 | 35.3 | 47.3 |
| Overall Height (ft) | 16.3 | — | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | — |
| Wingspan (ft) | — | 42.1 | 47.1 |
| Cabin Width (ft) | — | 4 | 6.1 |
| Cabin Height (ft) | — | 4.1 | 5.8 |
| Cabin Length (ft) | — | 13.4 | 14.9 |
| Cabin Width - Floor (ft) | — | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 |