Beechcraft King Air 360 Er vs Cessna Citation Xls vs Piper M600 Sls vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop business aircraft: it typically carries about 6 to 9 passengers and is optimized for shorter runways and efficient regional missions, with long‑range endurance on the order of roughly 1,500–1,800 nautical miles depending on load and reserves. The Cessna Citation XLS+ is a midsize business jet: it usually seats about 7 to 9 passengers and is faster than the turboprops, with a typical range around 1,700–2,100 nautical miles, making it well suited to city‑pair trips where speed matters. The Piper M600 SLS is a single‑engine turboprop (personal/light business): it commonly carries 4 to 6 passengers (up to 6 seats total) and offers solid cross‑country capability, roughly around 1,000–1,400 nautical miles depending on configuration. The Sikorsky S‑92 is a medium twin‑engine helicopter: it’s designed for offshore transport and utility/medevac roles, often configured for around 12 to 19 passengers, with a typical range roughly in the 400–600 nautical mile class depending on payload and reserves.
| Spec | Cessna Citation XLS+ | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 10 | 6 | 21 |
| Manufacturer | Cessna Citation | Piper | Sikorsky |
| Aircraft Name | XLS+ | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 1406 | 439 |
| DOC / nm / Seat | $ 0.67 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 9 | — | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 7540 | 2200 | 7417 |
| Standard Cabin Seats | 8 | 4 | 19 |
| Direct Operating Cost | $ 2,303 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 430 | 274 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $3,081,400 | $30,650,000 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | — |
| Min Crew | 2 | 1 | 2 |
| Crew Rest | No | — | — |
| Jump Seat | No | — | — |
| Total Seats | 10 | 5 | 21 |
| Galley Location | FWD | MID | — |
| Max Cabin Seats | 9 | — | 19 |
| Lavatory Location | AFT | — | — |
| Cabin Pressure (psi) | 9.3 | 5.6 | — |
| Galley / Refreshment | Galley | Refreshment Centre | — |
| Standard Cabin Seats | 8 | 4 | 19 |
| SL Cabin Altitude (ft) | 25230 | 12600 | — |
| Max Cabin Altitude (ft) | — | 8644 | — |
| Engine | |||
| FADEC | Yes | No | Yes |
| Model | PW545C | PT6A-42A | CT7-8A |
| TBO (hrs) | 5000 | 3600 | 4000 |
| Flat Rating | ISA + 10 | ISA + 55 | — |
| Thrust (lbs) | 4119 | — | — |
| No. of Engines | 2 | 1 | 1 |
| Horsepower | — | 600 | 2520 |
| Fuel Capacity (gal) | — | 260 | 760 |
| Fuel Type | — | — | JetFuel |
| Dimensions | |||
| Length (ft) | 52.5 | 29.7 | — |
| Wingspan (ft) | 56.3 | 43.2 | — |
| Aisle Step (ft) | 0.7 | — | — |
| Cabin Width (ft) | 5.5 | 4.1 | — |
| Cabin Height (ft) | 5.7 | 4 | — |
| Cabin Length (ft) | 18.5 | 12.3 | — |
| Overall Height (ft) | 17.2 | 11.3 | 17.8 |
| Cabin Width - Floor (ft) | 3.9 | — | — |
| Cabin Length - Seating (ft) | 14.3 | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | — | 140 |
| Baggage Volume Int. (cu. ft) | 10 | 20 | — |
| Cabin Volume (cu. ft) | — | 165 | 775 |