Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Daher Tbm 960 vs Gulfstream G700
The Airbus H225 is a heavy, long‑range twin‑engine helicopter used for offshore, SAR, and utility missions. It typically carries around 19 passengers in standard seating, and its range is roughly in the 450–550 nautical mile class depending on configuration and reserves. The Beechcraft King Air 360ER is a twin‑turboprop business/utility airplane aimed at extended regional flying; it commonly seats 6–11 passengers in executive layouts and can reach about 1,500–1,800 nautical miles with long‑range equipment and payload tradeoffs. The Daher TBM 960 is a single‑engine turboprop designed for fast owner‑flown business travel, usually seating 4–6 passengers (up to about 6–7 including the pilot depending on layout) with a range around 1,300–1,700 nautical miles. The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet, typically configured for about 13–19 passengers, with a range on the order of 7,500 nautical miles, enabling intercontinental nonstop missions.
| 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 |