Airbus Helicopters H225 vs Daher Tbm 960 vs Gulfstream G700
The Airbus H225 is a heavy, twin‑engine helicopter used for offshore transport, search and rescue, and utility missions. It typically carries around 16–19 passengers in a transport layout and is best suited to shorter point‑to‑point legs, with an approximate range on the order of 450–500 nautical miles depending on payload, configuration, and reserves. The Daher TBM 960 is a high‑performance single‑engine turboprop airplane in the personal and owner‑flown/business category. It is optimized for efficient regional travel, generally seating 4–6 passengers plus a pilot, and offers a much longer range than the helicopter, roughly about 1,400–1,700 nautical miles depending on power setting and payload. The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet designed for intercontinental missions. It typically accommodates about 10–19 passengers in executive cabin layouts (with higher maximums possible) and provides the greatest reach by far, around 7,000+ nautical miles, enabling nonstop flights such as New York to Dubai under favorable conditions.
| 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 |