Airbus Helicopters H225 vs Dassault Falcon 8x vs Pilatus Pc 24 vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter, best suited to offshore, SAR, and utility missions rather than point‑to‑point business travel. Its typical range is on the order of roughly 450–600 nautical miles depending on fuel and payload, and it can carry a large cabin load—often around 16–19 passengers in transport layouts (more in high‑density configurations, fewer in VIP). The Dassault Falcon 8X is an ultra‑long‑range tri‑jet business aircraft built for intercontinental nonstop travel, with range around 6,400 nautical miles and a typical executive cabin capacity of about 12–16 passengers (with higher maximums in denser layouts). The Pilatus PC‑24 is a light jet positioned for versatile regional missions, including operation from shorter or semi‑prepared runways. Range is roughly 2,000 nautical miles, and it typically seats about 6–10 passengers in executive use. The Piper M600 SLS is a single‑engine turboprop in the owner‑flown category, optimized for efficiency and shorter trips. Range is about 1,400 nautical miles, with seating commonly 4–6 passengers (up to 6 seats total).
| Spec | AIRBUS H225 | Dassault Falcon 8X | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | $ 3.71 | $ 2.19 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 17 | 6 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Pilatus | Piper |
| Aircraft Name | H225 | 8X | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 28 | 16 | 10 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 | 6680 | 2200 |
| Standard Cabin Seats | 19 | 14 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 516 | 440 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $11,800,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 17 | 6 | 5 |
| Max Cabin Seats | 28 | 16 | 10 | — |
| Standard Cabin Seats | 19 | 14 | 6 | 4 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Flushing | No |
| Crew Rest | — | No | No | — |
| Jump Seat | — | Yes | No | — |
| Galley Location | — | FWD | FWD | MID |
| Lavatory Location | — | FWD / AFT | FWD | — |
| Cabin Pressure (psi) | — | 10.2 | 9.3 | 5.6 |
| Galley / Refreshment | — | Galley | Optional Refreshment Center | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 29200 | 23500 | 12600 |
| Max Cabin Altitude (ft) | — | 3900 | — | 8644 |
| Cargo Door | — | — | Yes | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | PW307D | FJ44-4A-QPM | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 | 3600 |
| Horsepower | 2100 | — | — | 600 |
| No. of Engines | 2 | 3 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 17 | ISA + 23 | ISA + 55 |
| Thrust (lbs) | — | 6722 | 3435 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 80.2 | 52.2 | 29.7 |
| Overall Height (ft) | 16.3 | 26.1 | 17.4 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — | 165 |
| Wingspan (ft) | — | 86.3 | 55.8 | 43.2 |
| Cabin Width (ft) | — | 7.7 | 5.6 | 4.1 |
| Cabin Height (ft) | — | 6.2 | 5.1 | 4 |
| Cabin Length (ft) | — | 42.7 | 23 | 12.3 |
| Cabin Width - Floor (ft) | — | 6.3 | 3.8 | — |
| Cabin Length - Seating (ft) | — | 29.2 | 17 | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 90 | 20 |
| Aisle Step (ft) | — | — | Flat Floor | — |