Airbus Helicopters H225 vs Leonardo Aw189 vs Piaggio Avanti Evo vs Pilatus Pc 24
The Airbus H225 and Leonardo AW189 are large twin‑engine helicopters suited to offshore, SAR, and utility missions. Both typically seat around 16–19 passengers, but their range is generally shorter than fixed‑wing aircraft; depending on fit and reserves they are commonly used in the roughly 400–500+ nautical mile class, with the H225 often cited with a slight edge in endurance/payload for heavy offshore work. The Piaggio Avanti EVO is a pressurized twin‑turboprop airplane aimed at fast executive transport. It typically carries 6–8 passengers in a quiet, high‑speed cabin and offers substantially longer legs than the helicopters, commonly around 1,300–1,700 nautical miles depending on payload and conditions. The Pilatus PC‑24 is a light business jet designed for versatile operations, including shorter and semi‑prepared runways. It typically accommodates about 6–10 passengers (higher in dense layouts) and delivers jet speeds with range often around 1,800–2,000+ nautical miles, generally the longest of this group.
| Spec | AIRBUS H225 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.57 | — | $ 3.71 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 21 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Leonardo | Piaggio | Pilatus |
| Aircraft Name | H225 | AW189 | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 651 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.74 | — | $ 0.62 |
| Max Cabin Seats | 28 | 19 | 7 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | 3775 | 6680 |
| Standard Cabin Seats | 19 | 19 | 6 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,413 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 155 | 400 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $2,413,000 | $ 7,695,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 21 | 8 | 6 |
| Max Cabin Seats | 28 | 19 | 7 | 10 |
| Standard Cabin Seats | 19 | 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 | Yes |
| Model | Makila 2A1 | CT7-2E1 | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | JetFuel | — | — |
| TBO (hrs) | 3500 | 4000 | 3600 | 5000 |
| Horsepower | 2100 | 1983 | 850 | — |
| No. of Engines | 2 | 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 | 57.8 | 47.3 | 52.2 |
| Overall Height (ft) | 16.3 | 16.6 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | 48 | — | — |
| Cabin Volume (cu. ft) | 547 | 395 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — | — |
| 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 |