Airbus Helicopters H225 vs Embraer Legacy 650 E vs Leonardo Aw189 vs Pilatus Pc 24
The Airbus H225 and Leonardo AW189 are large twin‑engine helicopters suited to offshore, SAR, and utility missions, while the Embraer Legacy 650E and Pilatus PC‑24 are fixed‑wing business jets aimed at executive and multi‑mission transport. In range, the Legacy 650E is longest‑legged at roughly 3,900 nm, enabling true intercontinental segments. The PC‑24 is a super‑versatile light jet with about 2,000 nm of range, trading absolute distance for short/rough‑field access and frequent regional-to-continental hops. The H225 and AW189 have helicopter ranges typically in the ~450–500 nm class (mission dependent), optimized for point-to-point access without runways rather than long-distance cruise. For passenger capacity, the Legacy 650E typically seats 13 in an executive layout, with higher-density options; the PC‑24 commonly seats 8–10 in executive configuration (up to about 11). The H225 can carry around 19 passengers in a transport setup, while the AW189 is typically around 16–19 depending on layout.
| Spec | AIRBUS H225 | AGUSTA / LEONARDO AW189 | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.57 | $ 3.71 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 21 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Leonardo | Pilatus |
| Aircraft Name | H225 | AW189 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 651 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.74 | $ 0.62 |
| Max Cabin Seats | 28 | 19 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | 6680 |
| Standard Cabin Seats | 19 | 19 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,413 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 155 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $2,413,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 21 | 6 |
| Max Cabin Seats | 28 | 19 | 10 |
| Standard Cabin Seats | 19 | 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 | Yes |
| Model | Makila 2A1 | CT7-2E1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 3500 | 4000 | 5000 |
| Horsepower | 2100 | 1983 | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | — | ISA + 23 |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Length (ft) | 63.4 | 57.8 | 52.2 |
| Overall Height (ft) | 16.3 | 16.6 | 17.4 |
| Rotor Diameter (ft) | 53.2 | 48 | — |
| Cabin Volume (cu. ft) | 547 | 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 |