Airbus Helicopters H225 vs Daher Tbm 960
The Airbus H225 and the Daher TBM 960 sit in very different aircraft categories. The H225 is a large, twin‑engine helicopter designed for utility and transport missions such as offshore, search and rescue, and governmental or corporate lift. The TBM 960 is a high‑performance single‑engine turboprop airplane optimized for fast, efficient point‑to‑point travel using runways. In range terms, the TBM 960 generally offers longer cross‑country reach and higher cruise efficiency for overland trips, making it better suited to longer nonstop sectors between airports. The H225’s range is typically shorter and more mission‑dependent, but it excels where vertical lift is required—reaching ships, remote sites, or locations without prepared runways. Passenger capacity also differs. The TBM 960 is normally configured for one pilot and up to five passengers (with seating depending on layout), prioritizing comfort and speed for a small group. The H225 can carry a much larger cabin load, commonly accommodating well over a dozen passengers in transport configurations, prioritizing volume and lift over speed.
| Spec | AIRBUS H225 | Daher TBM 960 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM |
| Aircraft Name | H225 | TBM 960 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 |
| Max Cabin Seats | 28 | — |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 |
| Standard Cabin Seats | 19 | 4 |
| Direct Operating Cost | $ 2,963 | $ 744 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 330 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 |
| Aircraft Type | — | Turbo Prop |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Max Cabin Seats | 28 | — |
| Standard Cabin Seats | 19 | 4 |
| Lavatory | — | No |
| Galley Location | — | MID |
| Cabin Pressure (psi) | — | 6.2 |
| SL Cabin Altitude (ft) | — | 14390 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | TBM 960 |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 3500 |
| Horsepower | 2100 | 850 |
| No. of Engines | 2 | — |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 49 |
| Dimensions | ||
| Length (ft) | 63.4 | 35.3 |
| Overall Height (ft) | 16.3 | — |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | 123 |
| Wingspan (ft) | — | 42.1 |
| Cabin Width (ft) | — | 4 |
| Cabin Height (ft) | — | 4.1 |
| Cabin Length (ft) | — | 13.4 |