Beechcraft King Air 360 Er vs Cessna Citation Xls vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piper M600 Sls
The Beechcraft King Air 360ER is a twin‑turboprop airplane suited to short and medium regional missions, typically carrying about 6 to 9 passengers, with a long-range profile around 1,500 to 1,800 nautical miles depending on load and reserves. The Cessna Citation XLS+ is a light business jet focused on faster point‑to‑point travel, usually seating about 7 to 9 passengers, with a typical range around 1,800 to 2,100 nautical miles. The MD Helicopters (McDonnell Douglas) 902 Explorer is a twin‑engine helicopter aimed at vertical‑lift operations rather than runway-to-runway transport, commonly configured for about 6 to 8 passengers, with range roughly in the 300 to 400 nautical mile class. The Piper M600 SLS is a single‑engine turboprop airplane positioned as a high‑performance personal and owner‑operated aircraft, typically carrying about 4 to 6 passengers, with range commonly around 1,200 to 1,500 nautical miles. Overall, the Citation emphasizes speed, the King Air emphasizes versatility and payload, the 902 emphasizes access, and the M600 emphasizes efficient owner operation.
| Spec | Cessna Citation XLS+ | Piper M600 SLS |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 5.34 | $ 2.19 |
| Min Crew | 2 | 1 |
| Total Seats | 10 | 6 |
| Manufacturer | Cessna Citation | Piper |
| Aircraft Name | XLS+ | M600 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 1406 |
| DOC / nm / Seat | $ 0.67 | $ 0.55 |
| Max Cabin Seats | 9 | — |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 7540 | 2200 |
| Standard Cabin Seats | 8 | 4 |
| Direct Operating Cost | $ 2,303 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 430 | 274 |
| Base Aircraft Price (USD) | $15,500,000 | $3,081,400 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No |
| Min Crew | 2 | 1 |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Total Seats | 10 | 5 |
| Galley Location | FWD | MID |
| Max Cabin Seats | 9 | — |
| Lavatory Location | AFT | — |
| Cabin Pressure (psi) | 9.3 | 5.6 |
| Galley / Refreshment | Galley | Refreshment Centre |
| Standard Cabin Seats | 8 | 4 |
| SL Cabin Altitude (ft) | 25230 | 12600 |
| Max Cabin Altitude (ft) | — | 8644 |
| Engine | ||
| FADEC | Yes | No |
| Model | PW545C | PT6A-42A |
| TBO (hrs) | 5000 | 3600 |
| Flat Rating | ISA + 10 | ISA + 55 |
| Thrust (lbs) | 4119 | — |
| No. of Engines | 2 | 1 |
| Horsepower | — | 600 |
| Fuel Capacity (gal) | — | 260 |
| 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 |
| Cabin Width - Floor (ft) | 3.9 | — |
| Cabin Length - Seating (ft) | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | 80 | — |
| Baggage Volume Int. (cu. ft) | 10 | 20 |
| Cabin Volume (cu. ft) | — | 165 |