Airbus Helicopters H225 vs Daher Tbm 960 vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are both large, twin‑engine transport helicopters, typically used for offshore energy support, search and rescue, and government/VIP missions, while the Daher TBM 960 is a single‑engine, pressurized turboprop airplane optimized for fast point‑to‑point business and personal travel. In range terms, the TBM 960 generally offers the longest reach for nonstop trips, commonly around 1,400–1,700 nautical miles depending on cruise profile and payload. The H225 and S-92, as helicopters, trade cruise speed and range for vertical lift and access to unprepared sites; their typical operational ranges are generally in the several-hundred‑nautical‑mile class, often roughly 450–600 nautical miles depending on configuration and reserves. For passenger capacity, the TBM 960 usually seats a pilot plus up to five or six passengers in an executive cabin. The H225 and S-92 carry far more, commonly around 16–19 passengers in high-density transport layouts, with lower counts in VIP or mission-equipped configurations.
| Spec | AIRBUS H225 | Daher TBM 960 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 6 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Sikorsky |
| Aircraft Name | H225 | TBM 960 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.94 |
| Max Cabin Seats | 28 | — | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 | 7417 |
| Standard Cabin Seats | 19 | 4 | 19 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 142 | 330 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $30,650,000 |
| Aircraft Type | — | Turbo Prop | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 6 | 21 |
| Max Cabin Seats | 28 | — | 19 |
| Standard Cabin Seats | 19 | 4 | 19 |
| Lavatory | — | No | — |
| Galley Location | — | MID | — |
| Cabin Pressure (psi) | — | 6.2 | — |
| SL Cabin Altitude (ft) | — | 14390 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 3500 | 4000 |
| Horsepower | 2100 | 850 | 2520 |
| No. of Engines | 2 | — | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Flat Rating | — | ISA + 49 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 35.3 | — |
| Overall Height (ft) | 16.3 | — | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | 775 |
| Wingspan (ft) | — | 42.1 | — |
| Cabin Width (ft) | — | 4 | — |
| Cabin Height (ft) | — | 4.1 | — |
| Cabin Length (ft) | — | 13.4 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |