Airbus Helicopters H225 vs Daher Tbm 960 vs Piaggio Avanti Evo vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large twin‑engine helicopters, typically used for offshore transport and utility missions, with practical ranges on the order of roughly 450–550 nautical miles depending on payload and reserves. They generally seat around 16–19 passengers in typical transport layouts, though exact counts vary by configuration. The H225 is often selected where high payload and hot‑and‑high performance matter, while the S‑92 is widely used for offshore and SAR with strong dispatch reliability. The Daher TBM 960 is a single‑engine turboprop airplane in the high‑performance owner‑flown/light business category. It trades cabin volume for speed and efficiency, carrying about 4–6 passengers with a range around 1,400–1,700 nautical miles. The Piaggio Avanti EVO is a twin‑turboprop business aircraft with a larger, more comfortable cabin than the TBM and faster cruise than many turboprops, typically carrying about 6–9 passengers with a range around 1,400–1,800 nautical miles.
| Spec | AIRBUS H225 | Daher TBM 960 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | — | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 21 | 6 | 8 | 21 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Piaggio | Sikorsky |
| Aircraft Name | H225 | TBM 960 | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 1530 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | — | $ 0.94 |
| Max Cabin Seats | 28 | — | 7 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 | 3775 | 7417 |
| Standard Cabin Seats | 19 | 4 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | $ 744 | — | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 330 | 400 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $ 7,695,000 | $30,650,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 21 | 6 | 8 | 21 |
| Max Cabin Seats | 28 | — | 7 | 19 |
| Standard Cabin Seats | 19 | 4 | 6 | 19 |
| Lavatory | — | No | No | — |
| Galley Location | — | MID | — | — |
| Cabin Pressure (psi) | — | 6.2 | 9 | — |
| SL Cabin Altitude (ft) | — | 14390 | 24000 | — |
| Galley / Refreshment | — | — | No | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | PT6A–66B | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | 3500 | 3600 | 4000 |
| Horsepower | 2100 | 850 | 850 | 2520 |
| No. of Engines | 2 | — | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 49 | ISA + 28 | — |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 47.3 | — |
| Overall Height (ft) | 16.3 | — | 13.1 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | — | 775 |
| Wingspan (ft) | — | 42.1 | 47.1 | — |
| Cabin Width (ft) | — | 4 | 6.1 | — |
| Cabin Height (ft) | — | 4.1 | 5.8 | — |
| Cabin Length (ft) | — | 13.4 | 14.9 | — |
| Cabin Width - Floor (ft) | — | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |