Airbus Helicopters H225 vs Gulfstream G700 vs Piaggio Avanti Evo vs Pilatus Pc 24
The Airbus H225 is a twin‑engine heavy helicopter rather than a fixed‑wing aircraft, optimized for vertical lift missions. Its range is typically around 500–700 nautical miles depending on load and reserves, and it commonly carries about 16–19 passengers in an offshore/utility layout (higher-density configurations are possible). The Gulfstream G700 is an ultra‑long‑range business jet focused on intercontinental travel. It offers roughly 7,500+ nautical miles of range and typically seats 12–19 passengers in executive cabin configurations, emphasizing comfort and productivity. The Piaggio Avanti EVO is a twin‑turboprop business aircraft positioned for efficient regional to midrange travel. Its range is about 1,400–1,800 nautical miles and it usually carries 6–8 passengers in an executive layout, with strong speed-for-fuel-burn efficiency in its class. The Pilatus PC‑24 is a “super versatile jet” combining business-jet performance with rough/short‑field access. Range is around 1,800–2,000 nautical miles with typical seating for 6–10 passengers (higher-density commuter layouts exist), making it a flexible option for smaller airports.
| Spec | AIRBUS H225 | Gulfstream G700 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 20.87 | — | — | $ 3.71 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 16 | 8 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Gulfstream | Piaggio | Pilatus |
| Aircraft Name | H225 | G700 | Avanti EVO | PC-24 |
| Certification | FAA / EASA | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7500 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.99 | — | — | $ 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 | 12 | 6 | 6 |
| Direct Operating Cost | $ 2,963 | — | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 400 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 | $ 7,695,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 16 | 8 | 6 |
| Max Cabin Seats | 28 | 19 | 7 | 10 |
| Standard Cabin Seats | 19 | 12 | 6 | 6 |
| Crew Rest | — | Optional | — | No |
| Jump Seat | — | Yes | — | No |
| Galley Location | — | FWD | — | FWD |
| Lavatory Location | — | FWD / AFT | — | FWD |
| 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 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | — | Yes | Yes |
| Model | Makila 2A1 | Pearl 700 | 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 | — | — | — |
| Thrust (lbs) | — | 18250 | — | 3435 |
| Flat Rating | — | — | ISA + 28 | ISA + 23 |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 109.9 | 47.3 | 52.2 |
| Overall Height (ft) | 16.3 | 25.4 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 103 | 47.1 | 55.8 |
| Aisle Step (ft) | — | Flat Floor | — | Flat Floor |
| Cabin Width (ft) | — | 8.2 | 6.1 | 5.6 |
| Cabin Height (ft) | — | 6.25 | 5.8 | 5.1 |
| Cabin Length (ft) | — | 56.9 | 14.9 | 23 |
| Baggage Volume Int. (cu. ft) | — | 195 | 35.2 | 90 |
| Cabin Width - Floor (ft) | — | — | 3.5 | 3.8 |
| Cabin Length - Seating (ft) | — | — | — | 17 |