Airbus Helicopters H225 vs Daher Tbm 960 vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter aimed at offshore, SAR, and utility missions. It trades speed and altitude for vertical lift and cabin volume, typically carrying around 16–19 passengers in a transport layout, with range generally on the order of roughly 450–600 nautical miles depending on payload and tanks. The Daher TBM 960 is a single‑engine turboprop airplane optimized for fast owner‑pilot or small business travel. It is a long‑range, high‑speed point‑to‑point aircraft with typical seating for 4–6 passengers (up to about 6–7 seats including crew), and range roughly around 1,400–1,700 nautical miles depending on reserves and conditions. The Pilatus PC‑24 is a twin‑engine light business jet designed for flexibility, including operation from shorter or semi‑prepared runways. It sits between the TBM and larger midsize jets, commonly configured for about 6–10 passengers, with range typically around 1,800–2,000 nautical miles.
| Spec | AIRBUS H225 | Daher TBM 960 | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 3.71 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Daher TBM | Pilatus |
| Aircraft Name | H225 | TBM 960 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.62 |
| Max Cabin Seats | 28 | — | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 2908 | 6680 |
| Standard Cabin Seats | 19 | 4 | 6 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 330 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $11,800,000 |
| Aircraft Type | — | Turbo Prop | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 6 |
| Max Cabin Seats | 28 | — | 10 |
| Standard Cabin Seats | 19 | 4 | 6 |
| 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 |
| Model | Makila 2A1 | TBM 960 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 3500 | 5000 |
| Horsepower | 2100 | 850 | — |
| No. of Engines | 2 | — | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| 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 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | — |
| 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 |