Airbus Helicopters H225 vs Daher Tbm 960 vs Embraer Legacy 650 E vs Gulfstream G700
The Airbus H225 is a heavy twin‑engine helicopter typically used for offshore, SAR, and utility missions rather than point‑to‑point business travel. It carries a relatively large cabin load for a rotorcraft (often in the mid‑teens to around twenty seats depending on layout), but its range is generally shorter than business jets, roughly a few hundred nautical miles to around 500+ nm in many configurations. The Daher TBM 960 is a single‑engine turboprop, best categorized as a high‑performance personal/business aircraft. It typically seats about 4–6 passengers, with range around 1,000–1,700 nm depending on reserves and mission profile. The Embraer Legacy 650E is a large‑cabin business jet aimed at longer corporate missions, usually accommodating around 10–14 passengers, with intercontinental‑leaning range around 3,900–4,000 nm. The Gulfstream G700 is an ultra‑long‑range, large‑cabin flagship business jet, commonly configured for about 12–19 passengers, and offers true intercontinental reach of roughly 7,000+ nm, enabling nonstop city pairs the others cannot.
| Spec | AIRBUS H225 | Daher TBM 960 | Gulfstream G700 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 3 |
| DOC / nm | $ 20.87 | $ 2.25 | — |
| Min Crew | 2 | 1 | 4 |
| Total Seats | 21 | 6 | 16 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Daher TBM | Gulfstream |
| Aircraft Name | H225 | TBM 960 | G700 |
| Certification | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 454 | 1730 | 7500 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | — |
| Max Cabin Seats | 28 | — | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 | — |
| Standard Cabin Seats | 19 | 4 | 12 |
| Direct Operating Cost | $ 2,963 | $ 744 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 330 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $78,000,000 |
| Aircraft Type | — | Turbo Prop | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 4 |
| Total Seats | 21 | 6 | 16 |
| Max Cabin Seats | 28 | — | 19 |
| Standard Cabin Seats | 19 | 4 | 12 |
| Lavatory | — | No | — |
| Galley Location | — | MID | FWD |
| Cabin Pressure (psi) | — | 6.2 | — |
| SL Cabin Altitude (ft) | — | 14390 | — |
| Crew Rest | — | — | Optional |
| Jump Seat | — | — | Yes |
| Lavatory Location | — | — | FWD / AFT |
| Engine | |||
| FADEC | Yes | Yes | — |
| Model | Makila 2A1 | TBM 960 | Pearl 700 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 3500 | On Condition |
| Horsepower | 2100 | 850 | — |
| No. of Engines | 2 | — | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 49 | — |
| Thrust (lbs) | — | — | 18250 |
| Dimensions | |||
| Length (ft) | 63.4 | 35.3 | 109.9 |
| Overall Height (ft) | 16.3 | — | 25.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | — |
| Wingspan (ft) | — | 42.1 | 103 |
| Cabin Width (ft) | — | 4 | 8.2 |
| Cabin Height (ft) | — | 4.1 | 6.25 |
| Cabin Length (ft) | — | 13.4 | 56.9 |
| Aisle Step (ft) | — | — | Flat Floor |
| Baggage Volume Int. (cu. ft) | — | — | 195 |