Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Piaggio Avanti Evo vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter rather than a fixed‑wing aircraft, optimized for vertical lift missions such as offshore transport and SAR. Its practical range is typically in the several-hundred‑nautical‑mile class (often around 500+ nm depending on payload and reserves), and it can carry roughly 19 passengers in high‑density seating, though real-world layouts vary. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility airplane built for short, rugged routes. It generally offers a similar several-hundred‑nautical‑mile range (often around 900 nm in favorable configurations) and typically seats 9 passengers in commuter/charter use. The Piaggio Avanti EVO is a high-speed twin turboprop in the business category. It usually carries about 7–9 passengers and offers longer legs than utility turboprops, commonly around 1,500–1,800 nm depending on load and conditions. The Pilatus PC‑24 is a light business jet designed for flexibility, including operations from shorter runways. It commonly accommodates about 6–10 passengers and provides roughly 2,000 nm class range, making it the longest‑leg option among these four.
| 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 |