Airbus Helicopters H225 vs Daher Tbm 960 vs Pilatus Pc 24 vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large, twin‑engine helicopters built for offshore transport and search‑and‑rescue–type missions. Their practical range is typically in the 450–550 nautical mile class depending on payload and reserves, and they generally seat around 18–19 passengers in high‑density configurations (often fewer for SAR or VIP layouts). The Daher TBM 960 is a single‑engine turboprop airplane aimed at fast personal and business travel; it has much longer range for its size (about 1,400–1,700 nautical miles with typical reserves) but carries far fewer people, usually 4–6 passengers plus a pilot. The Pilatus PC‑24 is a twin‑engine light business jet designed for flexible operations, including short or semi‑prepared runways; it typically ranges about 1,900–2,000 nautical miles and commonly carries 6–10 passengers (up to roughly 11 in high‑density seating). Overall, the helicopters prioritize vertical access and lift, while the TBM 960 and PC‑24 prioritize speed and point‑to‑point range.
| Spec | AIRBUS H225 | Daher TBM 960 | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 21 | 6 | 6 | 21 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Pilatus | Sikorsky |
| Aircraft Name | H225 | TBM 960 | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 2076 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 28 | — | 10 | 19 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 | 6680 | 7417 |
| Standard Cabin Seats | 19 | 4 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 142 | 330 | 440 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $11,800,000 | $30,650,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 21 | 6 | 6 | 21 |
| Max Cabin Seats | 28 | — | 10 | 19 |
| Standard Cabin Seats | 19 | 4 | 6 | 19 |
| Lavatory | — | No | 1 Enclosed Flushing | — |
| Galley Location | — | MID | FWD | — |
| Cabin Pressure (psi) | — | 6.2 | 9.3 | — |
| SL Cabin Altitude (ft) | — | 14390 | 23500 | — |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Cargo Door | — | — | Yes | — |
| Lavatory Location | — | — | FWD | — |
| Galley / Refreshment | — | — | Optional Refreshment Center | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | FJ44-4A-QPM | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | 3500 | 5000 | 4000 |
| Horsepower | 2100 | 850 | — | 2520 |
| No. of Engines | 2 | — | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 49 | ISA + 23 | — |
| Thrust (lbs) | — | — | 3435 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 52.2 | — |
| Overall Height (ft) | 16.3 | — | 17.4 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | — | 775 |
| Wingspan (ft) | — | 42.1 | 55.8 | — |
| Cabin Width (ft) | — | 4 | 5.6 | — |
| Cabin Height (ft) | — | 4.1 | 5.1 | — |
| Cabin Length (ft) | — | 13.4 | 23 | — |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Cabin Width - Floor (ft) | — | — | 3.8 | — |
| Cabin Length - Seating (ft) | — | — | 17 | — |
| Baggage Volume Int. (cu. ft) | — | — | 90 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |