Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Piper M600 Sls vs Sikorsky S 92
The Airbus H225 and Sikorsky S‑92 are large twin‑engine helicopters designed for offshore transport and SAR-style missions, while the Beechcraft King Air 360ER and Piper M600 SLS are fixed‑wing turboprops aimed at business and utility travel. In range, the King Air 360ER is typically the longest‑leg option, offering roughly 1,800–2,000+ nautical miles depending on payload and reserves, whereas the Piper M600 SLS is a smaller single‑engine turboprop with around 1,400–1,500 nautical miles. The helicopters generally have shorter point‑to‑point range than the fixed‑wing aircraft: the H225 is commonly around the 450–550 nautical mile class, and the S‑92 is typically around 500–600 nautical miles, mission-fit dependent. For passenger capacity, the S‑92 and H225 can be configured for high-density seating, often carrying roughly 16–19 passengers (and more in maximum seating layouts), making them strongest for moving larger teams. The King Air 360ER usually seats about 8–11, while the M600 SLS is typically arranged for about 5–6 passengers plus a pilot.
| Spec | AIRBUS H225 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 6 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Piper | Sikorsky |
| Aircraft Name | H225 | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1406 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 28 | — | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 2200 | 7417 |
| Standard Cabin Seats | 19 | 4 | 19 |
| Direct Operating Cost | $ 2,963 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 142 | 274 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $3,081,400 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 5 | 21 |
| Max Cabin Seats | 28 | — | 19 |
| Standard Cabin Seats | 19 | 4 | 19 |
| Lavatory | — | No | — |
| Galley Location | — | MID | — |
| Cabin Pressure (psi) | — | 5.6 | — |
| Galley / Refreshment | — | Refreshment Centre | — |
| SL Cabin Altitude (ft) | — | 12600 | — |
| Max Cabin Altitude (ft) | — | 8644 | — |
| Engine | |||
| FADEC | Yes | No | Yes |
| Model | Makila 2A1 | PT6A-42A | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 3600 | 4000 |
| Horsepower | 2100 | 600 | 2520 |
| No. of Engines | 2 | 1 | 1 |
| Fuel Capacity (gal) | 684 | 260 | 760 |
| Flat Rating | — | ISA + 55 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 29.7 | — |
| Overall Height (ft) | 16.3 | 11.3 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 165 | 775 |
| Wingspan (ft) | — | 43.2 | — |
| Cabin Width (ft) | — | 4.1 | — |
| Cabin Height (ft) | — | 4 | — |
| Cabin Length (ft) | — | 12.3 | — |
| Baggage Volume Int. (cu. ft) | — | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |