Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Pilatus Pc 24 vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter, typically used for offshore, SAR, and utility missions. It prioritizes vertical lift and hoist capability over speed and fixed‑wing efficiency, carrying roughly 16–19 passengers in high‑density transport layouts, with range in the several‑hundred‑nautical‑mile class depending on payload and reserves. The Beechcraft King Air 360ER is a twin‑turboprop fixed‑wing aircraft optimized for long endurance and short/remote runway access. It generally seats 6–9 passengers in executive configurations and offers the longest range of this group, around 2,000+ nautical miles depending on conditions and fit. The Pilatus PC‑24 is a light business jet aimed at combining jet speed with rough/short‑field capability. Typical seating is about 6–10 passengers, with range roughly in the 1,800–2,000 nautical mile class. The Piper M600 SLS is a single‑engine turboprop personal/owner‑flown aircraft. It usually carries about 4–6 passengers and has range around 1,200–1,500 nautical miles, emphasizing lower operating complexity and cost versus the larger twins and the jet.
| 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 |