Airbus Helicopters H225 vs Daher Tbm 960 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Sikorsky S 92
The Daher TBM 960 is a single‑engine turboprop airplane in a different class from the three helicopters; it is optimized for fast point‑to‑point travel with a typical range around 1,400–1,700 nautical miles and usually carries about 4–6 passengers (up to 6 plus a pilot, depending on configuration). The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin helicopter suited to shorter missions, typically offering roughly 300–350 nautical miles of range and seating commonly around 6–8 passengers. The Airbus H225 is a heavy twin helicopter designed for offshore and utility roles, with an approximate range around 450–650 nautical miles and a typical passenger capacity in the high teens (often about 16–19, depending on layout). The Sikorsky S‑92 is also a heavy twin helicopter in a similar mission set to the H225, generally in the ~500–600 nautical mile range and commonly configured for about 16–19 passengers.
| 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 |