Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Daher Tbm 960 vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter built for offshore and utility missions rather than point‑to‑point business travel. It typically carries far more people than the others (often around 16–19 passengers depending on layout) but has a comparatively shorter practical range, generally in the few‑hundred‑nautical‑mile class, with endurance and payload varying strongly by mission equipment and reserves. The Beechcraft King Air 360ER is a pressurized twin‑turboprop optimized for long legs and flexibility. It usually seats about 6–9 passengers in executive layouts and offers long range around roughly 1,500–1,800 nautical miles, depending on payload and conditions. The Daher TBM 960 is a high‑performance single‑engine turboprop aimed at fast, efficient owner‑flown travel. Cabin capacity is typically 4–6 passengers plus pilot, with range commonly around 1,400–1,700 nautical miles. The Piaggio Avanti EVO is a twin‑turboprop designed for speed and cabin comfort. It generally carries about 6–8 passengers and offers range in the broad 1,400–1,700 nautical mile bracket, with cruise speeds often closer to light jets than typical turboprops.
| 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 |