Airbus Helicopters H225 vs Daher Tbm 960 vs Gulfstream G700 vs Robinson R66
The Airbus H225 and Robinson R66 are helicopters, while the Daher TBM 960 and Gulfstream G700 are fixed‑wing airplanes. The H225 is a large, twin‑engine utility helicopter used for offshore transport, SAR, and government missions; it typically carries around 16–19 passengers (higher in dense seating) and has a range on the order of roughly 450–650 nautical miles depending on configuration and reserves. The Robinson R66 is a light, single‑engine helicopter mainly for private, training, and light utility roles; it generally carries 4–5 people including the pilot and has an approximate range of about 300–350 nautical miles. Among airplanes, the TBM 960 is a high‑performance single‑engine turboprop optimized for fast owner‑operation; it usually seats 4–6 passengers (up to about 6 plus pilot) and offers roughly 1,400–1,700 nautical miles of range depending on payload and conditions. The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet for intercontinental travel; it typically accommodates 10–19 passengers in executive layouts and can fly about 7,500 nautical miles.
| 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 |