Beechcraft King Air 360 Er vs Embraer Legacy 650 E vs Piper M600 Sls vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop airplane positioned between high‑end personal/corporate flying and utility missions. It offers a long-range profile for its class at roughly 1,800–2,000 nautical miles and typically carries about 6–9 passengers depending on cabin layout and fuel/weight tradeoffs. The Embraer Legacy 650E is a large‑cabin business jet aimed at intercontinental corporate travel, with about 3,800–3,900 nautical miles of range and seating commonly around 10–13 passengers, trading higher speed and cabin volume for higher operating cost. The Piper M600 SLS is a single‑engine turboprop designed primarily for owner‑pilots, with a typical range around 1,400–1,600 nautical miles and usually 5–6 passenger seats (plus the pilot), emphasizing simplicity and lower costs versus larger twins. The Sikorsky S‑92 is a medium twin‑engine helicopter used for offshore energy, search and rescue, and VIP transport; its range is roughly 500–600 nautical miles and it can be configured for about 12–19 passengers, excelling in vertical access rather than speed or long range.
| Spec | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 2.19 | $ 19.79 |
| Min Crew | 1 | 2 |
| Total Seats | 6 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Piper | Sikorsky |
| Aircraft Name | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1406 | 439 |
| DOC / nm / Seat | $ 0.55 | $ 0.94 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2200 | 7417 |
| Standard Cabin Seats | 4 | 19 |
| Direct Operating Cost | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 274 | 155 |
| Base Aircraft Price (USD) | $3,081,400 | $30,650,000 |
| Max Cabin Seats | — | 19 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | — |
| Min Crew | 1 | 2 |
| Total Seats | 5 | 21 |
| Galley Location | MID | — |
| Cabin Pressure (psi) | 5.6 | — |
| Galley / Refreshment | Refreshment Centre | — |
| Standard Cabin Seats | 4 | 19 |
| SL Cabin Altitude (ft) | 12600 | — |
| Max Cabin Altitude (ft) | 8644 | — |
| Max Cabin Seats | — | 19 |
| Engine | ||
| FADEC | No | Yes |
| Model | PT6A-42A | CT7-8A |
| TBO (hrs) | 3600 | 4000 |
| Horsepower | 600 | 2520 |
| Flat Rating | ISA + 55 | — |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 260 | 760 |
| Fuel Type | — | JetFuel |
| Dimensions | ||
| Length (ft) | 29.7 | — |
| Wingspan (ft) | 43.2 | — |
| Cabin Width (ft) | 4.1 | — |
| Cabin Height (ft) | 4 | — |
| Cabin Length (ft) | 12.3 | — |
| Overall Height (ft) | 11.3 | 17.8 |
| Cabin Volume (cu. ft) | 165 | 775 |
| Baggage Volume Int. (cu. ft) | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | 140 |