Beechcraft King Air 360 Er vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo vs Pilatus Pc 24
The Beechcraft King Air 360ER is a pressurized twin‑turboprop airplane aimed at efficient regional and remote operations; it typically carries about 6–9 passengers and, with its extended‑range configuration, can fly roughly 1,500–1,800 nautical miles depending on load and conditions. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin helicopter optimized for short‑range missions such as utility, EMS, and law enforcement; it generally seats around 6–8 people including crew and has a range on the order of 250–350 nautical miles. The Piaggio Avanti EVO is a fast twin‑turboprop business aircraft that emphasizes speed and cabin comfort; it commonly carries 6–8 passengers and can cover about 1,500–1,800 nautical miles. The Pilatus PC‑24 is a light business jet with strong short/rough‑field capability; it typically seats 6–10 passengers and offers about 1,700–2,000 nautical miles of range, making it the longest‑legged and most “jet”‑like option among these, while the 902 is the only rotorcraft and thus the most flexible for point‑to‑point landings but with the shortest range.
| Spec | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 6 |
| Flight Rules | IFR | — |
| Manufacturer | Piaggio | Pilatus |
| Aircraft Name | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 2076 |
| Max Cabin Seats | 7 | 10 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3775 | 6680 |
| Standard Cabin Seats | 6 | 6 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 400 | 440 |
| Base Aircraft Price (USD) | $ 7,695,000 | $11,800,000 |
| DOC / nm | — | $ 3.71 |
| DOC / nm / Seat | — | $ 0.62 |
| Direct Operating Cost | — | $ 1,619 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | 1 Enclosed Flushing |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 6 |
| Max Cabin Seats | 7 | 10 |
| Cabin Pressure (psi) | 9 | 9.3 |
| Galley / Refreshment | No | Optional Refreshment Center |
| Standard Cabin Seats | 6 | 6 |
| SL Cabin Altitude (ft) | 24000 | 23500 |
| Max Cabin Altitude (ft) | 6600 | — |
| Crew Rest | — | No |
| Jump Seat | — | No |
| Cargo Door | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A–66B | FJ44-4A-QPM |
| TBO (hrs) | 3600 | 5000 |
| Horsepower | 850 | — |
| Flat Rating | ISA + 28 | ISA + 23 |
| No. of Engines | 2 | 2 |
| Fuel Burn (gph) | 100 | — |
| Thrust (lbs) | — | 3435 |
| Dimensions | ||
| Length (ft) | 47.3 | 52.2 |
| Wingspan (ft) | 47.1 | 55.8 |
| Cabin Width (ft) | 6.1 | 5.6 |
| Cabin Height (ft) | 5.8 | 5.1 |
| Cabin Length (ft) | 14.9 | 23 |
| Overall Height (ft) | 13.1 | 17.4 |
| Cabin Width - Floor (ft) | 3.5 | 3.8 |
| Baggage Volume Int. (cu. ft) | 35.2 | 90 |
| Aisle Step (ft) | — | Flat Floor |
| Cabin Length - Seating (ft) | — | 17 |