Airbus Helicopters H225 vs Bombardier Global 7500 vs Piaggio Avanti Evo vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter built for offshore, search‑and‑rescue, and utility missions rather than point‑to‑point business flying. Its practical range is roughly 450–650 nautical miles depending on payload and tanks, and it typically carries about 16–19 passengers in transport layouts. The Bombardier Global 7500 is an ultra‑long‑range business jet optimized for intercontinental travel, offering about 7,700 nautical miles of range and typically seating 14–19 passengers in executive configurations. The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft positioned between light jets and larger turboprops; it generally ranges around 1,400–1,800 nautical miles and commonly seats 6–9 passengers. The Pilatus PC‑24 is a light/medium business jet designed for versatility and short or semi‑prepared runway capability; it offers roughly 2,000 nautical miles of range and typically seats 6–10 passengers (with higher‑density commuter options possible). Overall, the Global 7500 leads on range, the H225 leads in rotorcraft utility, and the Avanti EVO and PC‑24 balance speed, access, and cabin size for regional missions.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | — | $ 3.71 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 8 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Bombardier | Piaggio | Pilatus |
| Aircraft Name | H225 | Global 7500 | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | — | $ 0.62 |
| Max Cabin Seats | 28 | 19 | 7 | 10 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | 3775 | 6680 |
| Standard Cabin Seats | 19 | 12 | 6 | 6 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 400 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $ 7,695,000 | $11,800,000 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 8 | 6 |
| Max Cabin Seats | 28 | 19 | 7 | 10 |
| Standard Cabin Seats | 19 | 12 | 6 | 6 |
| Lavatory | — | 2 Enclosed Flushing | No | 1 Enclosed Flushing |
| Crew Rest | — | Yes | — | No |
| Jump Seat | — | Yes | — | No |
| Galley Location | — | FWD | — | FWD |
| Lavatory Location | — | FWD / AFT | — | FWD |
| Galley / Refreshment | — | Galley | No | Optional Refreshment Center |
| Max Cabin Altitude (ft) | — | 4500 | 6600 | — |
| Cabin Pressure (psi) | — | — | 9 | 9.3 |
| SL Cabin Altitude (ft) | — | — | 24000 | 23500 |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 | 5000 |
| Horsepower | 2100 | — | 850 | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 28 | ISA + 23 |
| Thrust (lbs) | — | 18920 | — | 3435 |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 47.3 | 52.2 |
| Overall Height (ft) | 16.3 | 27 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 104 | 47.1 | 55.8 |
| Cabin Width (ft) | — | 8 | 6.1 | 5.6 |
| Cabin Height (ft) | — | 6.2 | 5.8 | 5.1 |
| Cabin Length (ft) | — | 54.5 | 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 |