Airbus Helicopters H225 vs Gulfstream G700 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter focused on vertical lift and offshore or rescue missions rather than long cruise legs; its range is roughly 450–550 nautical miles depending on fit, and it typically carries about 19 passengers (higher in dense seating). The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin helicopter aimed at law enforcement, EMS, and utility work; it has a shorter range around 300–400 nautical miles and usually seats 6–8 passengers. The Gulfstream G700 is an ultra‑long‑range business jet designed for intercontinental travel; it can fly about 7,500 nautical miles and generally accommodates 12–19 passengers in a luxury cabin (with higher-density layouts possible). The Piaggio Avanti EVO is a fast twin‑turboprop business aircraft optimized for efficient regional and transcontinental trips; its range is roughly 1,500–1,800 nautical miles and it typically seats 6–9 passengers. Overall, the helicopters prioritize point‑to‑point access without runways and carry fewer people over shorter distances, while the fixed‑wing aircraft prioritize speed, altitude, and longer range, with the G700 leading by a wide margin.
| Spec | AIRBUS H225 | Gulfstream G700 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | — | — |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 8 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Gulfstream | Piaggio |
| Aircraft Name | H225 | G700 | Avanti EVO |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 7500 | 1530 |
| DOC / nm / Seat | $ 0.99 | — | — |
| Max Cabin Seats | 28 | 19 | 7 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — | 3775 |
| Standard Cabin Seats | 19 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | — | — |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 516 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 | $ 7,695,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 8 |
| Max Cabin Seats | 28 | 19 | 7 |
| Standard Cabin Seats | 19 | 12 | 6 |
| Crew Rest | — | Optional | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD / AFT | — |
| Lavatory | — | — | No |
| Cabin Pressure (psi) | — | — | 9 |
| Galley / Refreshment | — | — | No |
| SL Cabin Altitude (ft) | — | — | 24000 |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| FADEC | Yes | — | Yes |
| Model | Makila 2A1 | Pearl 700 | PT6A–66B |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On Condition | 3600 |
| Horsepower | 2100 | — | 850 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Thrust (lbs) | — | 18250 | — |
| Flat Rating | — | — | ISA + 28 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 63.4 | 109.9 | 47.3 |
| Overall Height (ft) | 16.3 | 25.4 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Wingspan (ft) | — | 103 | 47.1 |
| Aisle Step (ft) | — | Flat Floor | — |
| Cabin Width (ft) | — | 8.2 | 6.1 |
| Cabin Height (ft) | — | 6.25 | 5.8 |
| Cabin Length (ft) | — | 56.9 | 14.9 |
| Baggage Volume Int. (cu. ft) | — | 195 | 35.2 |
| Cabin Width - Floor (ft) | — | — | 3.5 |