Airbus Helicopters H225 vs Pilatus Pc 24 vs Piper M600 Sls
The Airbus H225 is a large twin‑engine helicopter typically used for offshore transport and heavy utility missions. It carries the most people of the three, commonly around 16–19 passengers (with higher-density seating possible), but its point‑to‑point range is generally shorter than the jets and turboprop, often on the order of roughly 400–600 nautical miles depending on payload and reserves. The Pilatus PC‑24 is a light business jet designed for fast regional travel and access to shorter or less‑prepared runways than many jets. In typical executive configuration it carries about 6–10 passengers and offers the longest practical range here, roughly around 2,000 nautical miles. The Piper M600 SLS is a single‑engine turboprop positioned as a high‑end personal or owner‑flown aircraft. It usually seats about 4–6 passengers in comfort (up to 6 total seats) and provides a mid‑to‑long range for its class, roughly around 1,200–1,500 nautical miles, trading jet speed and cabin volume for lower operating complexity and cost.
| Spec | AIRBUS H225 | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 3.71 | $ 2.19 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Pilatus | Piper |
| Aircraft Name | H225 | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 28 | 10 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6680 | 2200 |
| Standard Cabin Seats | 19 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 440 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $11,800,000 | $3,081,400 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 5 |
| Max Cabin Seats | 28 | 10 | — |
| Standard Cabin Seats | 19 | 6 | 4 |
| Lavatory | — | 1 Enclosed Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Cargo Door | — | Yes | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | FWD | — |
| Cabin Pressure (psi) | — | 9.3 | 5.6 |
| Galley / Refreshment | — | Optional Refreshment Center | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 23500 | 12600 |
| Max Cabin Altitude (ft) | — | — | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | Makila 2A1 | FJ44-4A-QPM | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 5000 | 3600 |
| Horsepower | 2100 | — | 600 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 |
| Flat Rating | — | ISA + 23 | ISA + 55 |
| Thrust (lbs) | — | 3435 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 52.2 | 29.7 |
| Overall Height (ft) | 16.3 | 17.4 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 |
| Wingspan (ft) | — | 55.8 | 43.2 |
| Aisle Step (ft) | — | Flat Floor | — |
| Cabin Width (ft) | — | 5.6 | 4.1 |
| Cabin Height (ft) | — | 5.1 | 4 |
| Cabin Length (ft) | — | 23 | 12.3 |
| Cabin Width - Floor (ft) | — | 3.8 | — |
| Cabin Length - Seating (ft) | — | 17 | — |
| Baggage Volume Int. (cu. ft) | — | 90 | 20 |