Airbus Helicopters H225 vs Daher Tbm 960 vs Gulfstream G700 vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter optimized for vertical lift missions rather than point‑to‑point speed. It typically carries around 16–19 passengers in an air-transport configuration and offers a practical range on the order of roughly 400–500 nautical miles, varying with payload and reserves. The Daher TBM 960 is a high‑performance single‑engine turboprop, best suited to fast regional trips for an owner‑pilot or small team. It generally seats up to about 6 passengers (plus pilot) and has a range commonly around 1,400–1,700 nautical miles depending on power settings and payload. The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet designed for intercontinental travel. Typical passenger loads are about 10–19 (with higher-density options), and published range is roughly 7,500 nautical miles. The Piaggio Avanti EVO is a twin‑engine turboprop with a distinctive, efficient design, positioned between the TBM class and light jets for cabin comfort and speed. It typically carries 6–7 passengers and offers about 1,500–1,800 nautical miles of range.
| Spec | AIRBUS H225 | Daher TBM 960 | Gulfstream G700 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | — | — |
| Min Crew | 2 | 1 | 4 | 1 |
| Total Seats | 21 | 6 | 16 | 8 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Gulfstream | Piaggio |
| Aircraft Name | H225 | TBM 960 | G700 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 7500 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | — | — |
| Max Cabin Seats | 28 | — | 19 | 7 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 | — | 3775 |
| Standard Cabin Seats | 19 | 4 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | $ 744 | — | — |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 330 | 516 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $78,000,000 | $ 7,695,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 4 | 1 |
| Total Seats | 21 | 6 | 16 | 8 |
| Max Cabin Seats | 28 | — | 19 | 7 |
| Standard Cabin Seats | 19 | 4 | 12 | 6 |
| Lavatory | — | No | — | No |
| Galley Location | — | MID | FWD | — |
| Cabin Pressure (psi) | — | 6.2 | — | 9 |
| SL Cabin Altitude (ft) | — | 14390 | — | 24000 |
| Crew Rest | — | — | Optional | — |
| Jump Seat | — | — | Yes | — |
| Lavatory Location | — | — | FWD / AFT | — |
| Galley / Refreshment | — | — | — | No |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | — | Yes |
| Model | Makila 2A1 | TBM 960 | Pearl 700 | PT6A–66B |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 3500 | On Condition | 3600 |
| Horsepower | 2100 | 850 | — | 850 |
| No. of Engines | 2 | — | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 49 | — | ISA + 28 |
| Thrust (lbs) | — | — | 18250 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 109.9 | 47.3 |
| Overall Height (ft) | 16.3 | — | 25.4 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | — | — |
| Wingspan (ft) | — | 42.1 | 103 | 47.1 |
| Cabin Width (ft) | — | 4 | 8.2 | 6.1 |
| Cabin Height (ft) | — | 4.1 | 6.25 | 5.8 |
| Cabin Length (ft) | — | 13.4 | 56.9 | 14.9 |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Baggage Volume Int. (cu. ft) | — | — | 195 | 35.2 |
| Cabin Width - Floor (ft) | — | — | — | 3.5 |