Beechcraft King Air 360 Er vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Pilatus Pc 24 vs Piper M600 Sls
The Beechcraft King Air 360ER is a twin‑turboprop business aircraft optimized for efficiency and short‑field access, offering long endurance with a typical range around 1,500–1,800 nautical miles and usually seating about 6–9 passengers depending on layout. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin‑engine helicopter, best for point‑to‑point access into confined areas rather than long cruise legs; its typical range is roughly 300–400 nautical miles with seating commonly around 6–8 including the pilot(s), depending on configuration. The Pilatus PC‑24 is a light business jet designed for high speed and versatile operations, including many shorter or unimproved runways; it generally provides about 1,800–2,000 nautical miles of range and typically seats around 6–10 passengers. The Piper M600 SLS is a single‑engine turboprop positioned as an owner‑pilot-friendly personal/business aircraft, with a typical range near 1,200–1,500 nautical miles and seating up to 5–6. Overall, the PC‑24 leads on speed and jet capability, the King Air balances capacity and efficiency, the M600 emphasizes simplicity, and the 902 prioritizes vertical-access missions.
| Spec | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 3.71 | $ 2.19 |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 6 |
| Manufacturer | Pilatus | Piper |
| Aircraft Name | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2076 | 1406 |
| DOC / nm / Seat | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 10 | — |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6680 | 2200 |
| Standard Cabin Seats | 6 | 4 |
| Direct Operating Cost | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 440 | 274 |
| Base Aircraft Price (USD) | $11,800,000 | $3,081,400 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Flushing | No |
| Min Crew | 1 | 1 |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Cargo Door | Yes | — |
| Total Seats | 6 | 5 |
| Galley Location | FWD | MID |
| Max Cabin Seats | 10 | — |
| Lavatory Location | FWD | — |
| Cabin Pressure (psi) | 9.3 | 5.6 |
| Galley / Refreshment | Optional Refreshment Center | Refreshment Centre |
| Standard Cabin Seats | 6 | 4 |
| SL Cabin Altitude (ft) | 23500 | 12600 |
| Max Cabin Altitude (ft) | — | 8644 |
| Engine | ||
| FADEC | Yes | No |
| Model | FJ44-4A-QPM | PT6A-42A |
| TBO (hrs) | 5000 | 3600 |
| Flat Rating | ISA + 23 | ISA + 55 |
| Thrust (lbs) | 3435 | — |
| No. of Engines | 2 | 1 |
| Horsepower | — | 600 |
| Fuel Capacity (gal) | — | 260 |
| Dimensions | ||
| Length (ft) | 52.2 | 29.7 |
| 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 |
| Overall Height (ft) | 17.4 | 11.3 |
| Cabin Width - Floor (ft) | 3.8 | — |
| Cabin Length - Seating (ft) | 17 | — |
| Baggage Volume Int. (cu. ft) | 90 | 20 |
| Cabin Volume (cu. ft) | — | 165 |