Airbus Helicopters H225 vs Daher Tbm 960 vs Dassault Falcon 8x vs Pilatus Pc 24
The Airbus H225 is a large twin‑engine helicopter suited to offshore, search‑and‑rescue, and utility missions. It trades speed and range for vertical lift and cabin volume, typically carrying around 19 passengers, with practical range on the order of roughly 450–700 nautical miles depending on fit and reserves. The Daher TBM 960 is a single‑engine turboprop airplane optimized for fast, efficient owner‑operation and short‑to‑medium trips. It generally seats 4–6 passengers and offers about 1,400–1,700 nautical miles of range. The Dassault Falcon 8X is a long‑range, large‑cabin tri‑jet business aircraft aimed at intercontinental travel. It commonly carries 8–14 passengers (with higher maximum layouts possible) and delivers roughly 6,000+ nautical miles of range. The Pilatus PC‑24 is a twin‑engine “super versatile jet” designed to operate from shorter and semi‑prepared runways while providing business‑jet speed. It typically seats 6–10 passengers and offers about 1,800–2,000 nautical miles of range.
| Spec | AIRBUS H225 | Daher TBM 960 | Dassault Falcon 8X | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 7.66 | $ 3.71 |
| Min Crew | 2 | 1 | 2 | 1 |
| Total Seats | 21 | 6 | 17 | 6 |
| Flight Rules | IFR | IFR | — | — |
| Manufacturer | Airbus Helicopters | Daher TBM | Dassault Falcon | Pilatus |
| Aircraft Name | H225 | TBM 960 | 8X | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 6450 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.64 | $ 0.62 |
| Max Cabin Seats | 28 | — | 16 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 2908 | 36900 | 6680 |
| Standard Cabin Seats | 19 | 4 | 14 | 6 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 3,805 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 330 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $ 62,500,000 | $11,800,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 1 | 2 | 1 |
| Total Seats | 21 | 6 | 17 | 6 |
| Max Cabin Seats | 28 | — | 16 | 10 |
| Standard Cabin Seats | 19 | 4 | 14 | 6 |
| Lavatory | — | No | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Galley Location | — | MID | FWD | FWD |
| Cabin Pressure (psi) | — | 6.2 | 10.2 | 9.3 |
| SL Cabin Altitude (ft) | — | 14390 | 29200 | 23500 |
| Crew Rest | — | — | No | No |
| Jump Seat | — | — | Yes | No |
| Lavatory Location | — | — | FWD / AFT | FWD |
| Galley / Refreshment | — | — | Galley | Optional Refreshment Center |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | PW307D | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 3500 | On-Condition | 5000 |
| Horsepower | 2100 | 850 | — | — |
| No. of Engines | 2 | — | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 49 | ISA + 17 | ISA + 23 |
| Thrust (lbs) | — | — | 6722 | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 80.2 | 52.2 |
| Overall Height (ft) | 16.3 | — | 26.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | 1695 | — |
| Wingspan (ft) | — | 42.1 | 86.3 | 55.8 |
| Cabin Width (ft) | — | 4 | 7.7 | 5.6 |
| Cabin Height (ft) | — | 4.1 | 6.2 | 5.1 |
| Cabin Length (ft) | — | 13.4 | 42.7 | 23 |
| Cabin Width - Floor (ft) | — | — | 6.3 | 3.8 |
| Cabin Length - Seating (ft) | — | — | 29.2 | 17 |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 90 |
| Aisle Step (ft) | — | — | — | Flat Floor |