Airbus Helicopters H225 vs Enstrom 480b vs Pilatus Pc 24 vs Piper M600 Sls
The Airbus H225 and Enstrom 480B are helicopters, while the Pilatus PC-24 and Piper M600 SLS are fixed‑wing aircraft, so their strengths differ. The H225 is a heavy, long‑range, twin‑engine helicopter optimized for offshore transport and SAR-style missions; it typically carries the most people of this group, commonly around 19 passengers in high‑density layouts, with a range on the order of roughly 450–500 nautical miles depending on configuration. The Enstrom 480B is a light, single‑engine helicopter aimed at utility, training, and personal use; passenger capacity is usually 4–5, and range is comparatively short, roughly a few hundred nautical miles. The Pilatus PC-24 is a twin‑engine business jet designed for fast point‑to‑point travel and short/rough-field capability; it typically seats about 6–10 passengers and has transcontinental-class range around 2,000 nautical miles. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft; it generally seats 5–6 passengers with range around 1,200–1,500 nautical miles, trading jet speed for lower operating complexity.
| 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 |