Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Cessna 208b Grand Caravan Ex vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter suited to offshore and utility work rather than point‑to‑point fixed‑wing travel. It typically carries around 16–19 passengers in transport layouts and offers roughly 500–600 nautical miles of range depending on payload and reserves. The Beechcraft King Air 360ER is a pressurized twin‑turboprop business/utility aircraft. It’s commonly configured for about 8–11 passengers and emphasizes endurance, with an extended range on the order of 1,500–1,800 nautical miles, varying with load and conditions. The Cessna 208B Grand Caravan EX is a rugged single‑engine turboprop optimized for short, unimproved strips and cargo/commuter missions. It usually seats up to 9 passengers and has a typical range around 900–1,000 nautical miles, mission‑dependent. The Piaggio Avanti EVO is a high‑speed, pressurized twin‑turboprop positioned as a business aircraft. It generally seats 7–9 passengers and delivers roughly 1,400–1,700 nautical miles of range, with cruise speed notably higher than most turboprops.
| Spec | AIRBUS H225 | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | — |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 8 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Piaggio |
| Aircraft Name | H225 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 |
| DOC / nm / Seat | $ 0.99 | — |
| Max Cabin Seats | 28 | 7 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 3775 |
| Standard Cabin Seats | 19 | 6 |
| Direct Operating Cost | $ 2,963 | — |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 8 |
| Max Cabin Seats | 28 | 7 |
| Standard Cabin Seats | 19 | 6 |
| Lavatory | — | No |
| Cabin Pressure (psi) | — | 9 |
| Galley / Refreshment | — | No |
| SL Cabin Altitude (ft) | — | 24000 |
| Max Cabin Altitude (ft) | — | 6600 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | PT6A–66B |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 3600 |
| Horsepower | 2100 | 850 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 28 |
| Fuel Burn (gph) | — | 100 |
| Dimensions | ||
| Length (ft) | 63.4 | 47.3 |
| Overall Height (ft) | 16.3 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | — |
| Wingspan (ft) | — | 47.1 |
| Cabin Width (ft) | — | 6.1 |
| Cabin Height (ft) | — | 5.8 |
| Cabin Length (ft) | — | 14.9 |
| Cabin Width - Floor (ft) | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | 35.2 |