Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Piaggio Avanti Evo vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter optimized for vertical lift missions rather than point‑to‑point speed. It typically carries around 19 passengers in high‑density seating (fewer in VIP/utility layouts) and offers roughly 500–650 nm of range depending on payload and reserves, making it strong for offshore and SAR where landing sites are constrained. The Beechcraft King Air 360ER is a long‑range turboprop business/utility aircraft, usually configured for about 8–11 passengers, with approximately 1,500–1,800 nm range, emphasizing efficiency and short/remote runway access. The Piaggio Avanti EVO is a fast, efficient twin turboprop in the business category, commonly seating 6–9 passengers, with about 1,400–1,800 nm range, favoring higher cruise speed than most turboprops. The Pilatus PC‑24 is a light jet designed for “rough‑field” capability, typically carrying 6–10 passengers, with roughly 1,700–2,000+ nm range depending on load, combining jet speed with access to shorter runways.
| Spec | AIRBUS H225 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 3.71 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 8 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Piaggio | Pilatus |
| Aircraft Name | H225 | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.62 |
| Max Cabin Seats | 28 | 7 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 3775 | 6680 |
| Standard Cabin Seats | 19 | 6 | 6 |
| Direct Operating Cost | $ 2,963 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 400 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 8 | 6 |
| Max Cabin Seats | 28 | 7 | 10 |
| Standard Cabin Seats | 19 | 6 | 6 |
| Lavatory | — | No | 1 Enclosed Flushing |
| Cabin Pressure (psi) | — | 9 | 9.3 |
| Galley / Refreshment | — | No | Optional Refreshment Center |
| 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 | Yes |
| Model | Makila 2A1 | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 3600 | 5000 |
| Horsepower | 2100 | 850 | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 28 | ISA + 23 |
| Fuel Burn (gph) | — | 100 | — |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Length (ft) | 63.4 | 47.3 | 52.2 |
| Overall Height (ft) | 16.3 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| 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 |
| 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 |