Airbus Helicopters H225 vs Bombardier Global 7500 vs Leonardo Aw189 vs Piaggio Avanti Evo
The Airbus H225 and Leonardo AW189 are large twin‑engine helicopters suited to offshore, search‑and‑rescue, and utility roles, while the Bombardier Global 7500 and Piaggio Avanti EVO are fixed‑wing business aircraft optimized for point‑to‑point travel. In range, the Global 7500 is in a different class, offering intercontinental capability at roughly 7,700 nautical miles, whereas the Avanti EVO is typically around 1,700–1,800 nautical miles. Helicopter range is far shorter: the H225 is roughly 450–500 nautical miles depending on configuration, and the AW189 is commonly around 450 nautical miles. For passenger capacity, the Global 7500 usually seats about 14–19 in executive layouts, while the Avanti EVO is generally 6–9. The H225 can carry the most people in high‑density transport configurations, often up to around 19 passengers, while the AW189 commonly carries up to about 16–19 depending on fit. Overall, the Global 7500 maximizes range and cabin comfort, the Avanti EVO targets efficient regional business travel, and the H225/AW189 trade speed and range for vertical access and mission flexibility.
| Spec | AIRBUS H225 | Bombardier Global 7500 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 15.57 | — |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 21 | 8 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Leonardo | Piaggio |
| Aircraft Name | H225 | Global 7500 | AW189 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 651 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.74 | — |
| Max Cabin Seats | 28 | 19 | 19 | 7 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — | — | 3775 |
| Standard Cabin Seats | 19 | 12 | 19 | 6 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 2,413 | — |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 516 | 155 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $2,413,000 | $ 7,695,000 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 21 | 8 |
| Max Cabin Seats | 28 | 19 | 19 | 7 |
| Standard Cabin Seats | 19 | 12 | 19 | 6 |
| Lavatory | — | 2 Enclosed Flushing | — | No |
| Crew Rest | — | Yes | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | — | — |
| Lavatory Location | — | FWD / AFT | — | — |
| Galley / Refreshment | — | Galley | — | No |
| Max Cabin Altitude (ft) | — | 4500 | — | 6600 |
| Cabin Pressure (psi) | — | — | — | 9 |
| SL Cabin Altitude (ft) | — | — | — | 24000 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | CT7-2E1 | PT6A–66B |
| Fuel Type | JetFuel | — | JetFuel | — |
| TBO (hrs) | 3500 | On-Condition | 4000 | 3600 |
| Horsepower | 2100 | — | 1983 | 850 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | — | ISA + 28 |
| Thrust (lbs) | — | 18920 | — | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 57.8 | 47.3 |
| Overall Height (ft) | 16.3 | 27 | 16.6 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | 48 | — |
| Cabin Volume (cu. ft) | 547 | — | 395 | — |
| Wingspan (ft) | — | 104 | — | 47.1 |
| Cabin Width (ft) | — | 8 | — | 6.1 |
| Cabin Height (ft) | — | 6.2 | — | 5.8 |
| Cabin Length (ft) | — | 54.5 | — | 14.9 |
| Baggage Volume Ext. (cu. ft) | — | — | 85 | — |
| Cabin Width - Floor (ft) | — | — | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | — | — | 35.2 |