Beechcraft King Air 360 Er vs Leonardo Aw189 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Pilatus Pc 24
The Beechcraft King Air 360ER is a pressurized twin‑turboprop airplane suited to short and medium regional missions, typically carrying about 6–9 passengers in executive layouts, with long legs for its class (roughly 1,500–2,000 nautical miles depending on payload and reserves). The Pilatus PC‑24 is a twin‑jet light business aircraft, generally seating about 6–10 passengers, optimized for faster point‑to‑point travel and often offering similar or greater practical range than the King Air (commonly around 1,800–2,000 nautical miles), depending on configuration. The Leonardo AW189 is a large twin‑engine helicopter aimed at offshore, SAR, and utility roles, usually configured for around 12–16 passengers with a typical range on the order of 450–500 nautical miles. The MD Helicopters 902 Explorer is a light twin helicopter used for EMS, law enforcement, and corporate missions, commonly carrying about 5–7 passengers with a shorter typical range around 250–350 nautical miles. Overall, the fixed‑wing aircraft dominate range and speed, while the helicopters trade range for vertical access and hover capability.
| Spec | AGUSTA / LEONARDO AW189 | Pilatus PC-24 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 15.57 | $ 3.71 |
| Min Crew | 1 | 1 |
| Total Seats | 21 | 6 |
| Flight Rules | IFR | — |
| Manufacturer | Leonardo | Pilatus |
| Aircraft Name | AW189 | PC-24 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 2076 |
| DOC / nm / Seat | $ 0.74 | $ 0.62 |
| Max Cabin Seats | 19 | 10 |
| OEM Verification | Un-Verified | VERIFIED |
| Standard Cabin Seats | 19 | 6 |
| Direct Operating Cost | $ 2,413 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 155 | 440 |
| Base Aircraft Price (USD) | $2,413,000 | $11,800,000 |
| Useful Load (lbs) | — | 6680 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 21 | 6 |
| Max Cabin Seats | 19 | 10 |
| Standard Cabin Seats | 19 | 6 |
| Lavatory | — | 1 Enclosed Flushing |
| Crew Rest | — | No |
| Jump Seat | — | No |
| Cargo Door | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD |
| Cabin Pressure (psi) | — | 9.3 |
| Galley / Refreshment | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 23500 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | CT7-2E1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 4000 | 5000 |
| Horsepower | 1983 | — |
| No. of Engines | 2 | 2 |
| Flat Rating | — | ISA + 23 |
| Thrust (lbs) | — | 3435 |
| Dimensions | ||
| Length (ft) | 57.8 | 52.2 |
| Overall Height (ft) | 16.6 | 17.4 |
| Rotor Diameter (ft) | 48 | — |
| Cabin Volume (cu. ft) | 395 | — |
| Baggage Volume Ext. (cu. ft) | 85 | — |
| Wingspan (ft) | — | 55.8 |
| Aisle Step (ft) | — | Flat Floor |
| Cabin Width (ft) | — | 5.6 |
| Cabin Height (ft) | — | 5.1 |
| Cabin Length (ft) | — | 23 |
| Cabin Width - Floor (ft) | — | 3.8 |
| Cabin Length - Seating (ft) | — | 17 |
| Baggage Volume Int. (cu. ft) | — | 90 |