Airbus Helicopters H225 vs Daher Tbm 960 vs Embraer Legacy 650 E vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter best categorized for offshore transport, search and rescue, and utility missions rather than fixed‑wing business travel. Its range is typically around 500–700 nautical miles depending on payload and reserves, and it generally carries about 16–19 passengers (with higher-capacity seating possible in certain layouts). The Daher TBM 960 is a single‑engine turboprop in the high‑performance owner‑pilot/business category. It offers roughly 1,400–1,700 nautical miles of range and typically seats 4–6 passengers plus a pilot (up to about 6–7 seats total depending on configuration). The Embraer Legacy 650E is a large‑cabin business jet optimized for long, comfortable trips. It provides about 3,900 nautical miles of range and commonly carries 10–13 passengers in executive layouts (certified for more depending on seating). The Piaggio Avanti EVO is a twin‑engine turboprop known for speed and efficiency, fitting the light/midsize business category. Its range is about 1,500–1,800 nautical miles and it typically seats 6–7 passengers plus pilots.
| 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 |