Beechcraft King Air 360 Er vs Leonardo Aw189 vs Pilatus Pc 24 vs Piper M600 Sls
The Beechcraft King Air 360ER is a pressurized twin‑turboprop business/utility airplane optimized for endurance and short/remote airfields. It typically offers roughly 1,500–1,800 nautical miles of range (depending on payload and reserves) and commonly carries 6–9 passengers in executive layouts, with higher seating possible in commuter/utility configurations. The Leonardo AW189 is a medium twin‑engine helicopter aimed at offshore, SAR, and utility/VIP missions. Its practical range is generally about 400–500 nautical miles, and it usually carries around 12–16 passengers in transport seating (fewer in VIP or missionized roles). The Pilatus PC‑24 is a light business jet designed to combine jet speed with rough‑field capability. Typical range is about 2,000 nautical miles, and passenger capacity is commonly 6–10, with up to 11 in some configurations. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft emphasizing simplicity and operating cost. Typical range is about 1,000–1,400 nautical miles, and it generally seats 4–6 passengers (up to 6 total seats).
| Spec | AGUSTA / LEONARDO AW189 | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 15.57 | $ 3.71 | $ 2.19 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 21 | 6 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Leonardo | Pilatus | Piper |
| Aircraft Name | AW189 | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.74 | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 19 | 10 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Standard Cabin Seats | 19 | 6 | 4 |
| Direct Operating Cost | $ 2,413 | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 155 | 440 | 274 |
| Base Aircraft Price (USD) | $2,413,000 | $11,800,000 | $3,081,400 |
| Useful Load (lbs) | — | 6680 | 2200 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 21 | 6 | 5 |
| Max Cabin Seats | 19 | 10 | — |
| Standard Cabin Seats | 19 | 6 | 4 |
| Lavatory | — | 1 Enclosed Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Cargo Door | — | Yes | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | FWD | — |
| Cabin Pressure (psi) | — | 9.3 | 5.6 |
| Galley / Refreshment | — | Optional Refreshment Center | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 23500 | 12600 |
| Max Cabin Altitude (ft) | — | — | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | CT7-2E1 | FJ44-4A-QPM | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 5000 | 3600 |
| Horsepower | 1983 | — | 600 |
| No. of Engines | 2 | 2 | 1 |
| Flat Rating | — | ISA + 23 | ISA + 55 |
| Thrust (lbs) | — | 3435 | — |
| Fuel Capacity (gal) | — | — | 260 |
| Dimensions | |||
| Length (ft) | 57.8 | 52.2 | 29.7 |
| Overall Height (ft) | 16.6 | 17.4 | 11.3 |
| Rotor Diameter (ft) | 48 | — | — |
| Cabin Volume (cu. ft) | 395 | — | 165 |
| Baggage Volume Ext. (cu. ft) | 85 | — | — |
| 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 |
| Cabin Width - Floor (ft) | — | 3.8 | — |
| Cabin Length - Seating (ft) | — | 17 | — |
| Baggage Volume Int. (cu. ft) | — | 90 | 20 |