Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Bombardier Global 7500 vs Daher Tbm 960
The Airbus H225 is a heavy twin‑engine helicopter designed for offshore, SAR, and utility missions. It typically carries around 19 passengers in high‑density layouts (fewer in VIP) and offers a practical range on the order of roughly 500–600 nautical miles, trading speed and altitude for vertical access and hover capability. The Beechcraft King Air 360ER is a twin‑turboprop business/utility aircraft. It generally seats about 8–11 passengers and is optimized for regional and remote-field operations, with long‑leg capability roughly around 1,500–1,800 nautical miles depending on payload and reserves. The Bombardier Global 7500 is an ultra‑long‑range business jet built for intercontinental travel. Typical configurations seat about 14–19 passengers, and its headline range is about 7,700 nautical miles, enabling nonstop missions such as North America to Asia or deep transoceanic routes. The Daher TBM 960 is a high‑performance single‑engine turboprop, usually configured for about 4–6 passengers plus a pilot, with a range roughly around 1,000–1,700 nautical miles depending on power settings and load, emphasizing speed and efficiency for owner‑operators.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Daher TBM 960 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 2.25 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Daher TBM |
| Aircraft Name | H225 | Global 7500 | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1730 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.56 |
| Max Cabin Seats | 28 | 19 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 2908 |
| Standard Cabin Seats | 19 | 12 | 4 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 744 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 516 | 330 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $4,450,000 |
| Aircraft Type | — | Business Jet | Turbo Prop |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 6 |
| Max Cabin Seats | 28 | 19 | — |
| Standard Cabin Seats | 19 | 12 | 4 |
| Lavatory | — | 2 Enclosed Flushing | No |
| Crew Rest | — | Yes | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | FWD / AFT | — |
| Galley / Refreshment | — | Galley | — |
| Max Cabin Altitude (ft) | — | 4500 | — |
| Cabin Pressure (psi) | — | — | 6.2 |
| SL Cabin Altitude (ft) | — | — | 14390 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | TBM 960 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 3500 |
| Horsepower | 2100 | — | 850 |
| No. of Engines | 2 | 2 | — |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 15 | ISA + 49 |
| Thrust (lbs) | — | 18920 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 111 | 35.3 |
| Overall Height (ft) | 16.3 | 27 | — |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 |
| Wingspan (ft) | — | 104 | 42.1 |
| Cabin Width (ft) | — | 8 | 4 |
| Cabin Height (ft) | — | 6.2 | 4.1 |
| Cabin Length (ft) | — | 54.5 | 13.4 |