Airbus Helicopters H225 vs Gulfstream G700 vs Md Helicopters (mcdonnell Douglas) 902 Explorer
The Airbus H225 and the MD Helicopters (McDonnell Douglas) 902 Explorer are twin‑engine helicopters, while the Gulfstream G700 is a long‑range business jet. In category terms, the H225 is a heavy, long‑range utility/transport helicopter commonly used for offshore, search and rescue, and VIP roles; the 902 Explorer is a lighter twin helicopter aimed at corporate, law‑enforcement, and medical/utility missions; and the G700 is an ultra‑long‑range private jet optimized for high‑speed intercontinental travel. For range, the G700 is in a different class, capable of roughly 7,500+ nautical miles depending on configuration and conditions, enabling nonstop city pairs across oceans. The H225 typically offers helicopter-range on the order of a few hundred nautical miles (often around 500–700 nm with reserves depending on load and tanks), suited to offshore legs rather than transoceanic routes. The 902 Explorer is shorter‑legged still, commonly around the 300–400 nm range depending on payload. Passenger capacity also differs: the G700 typically seats about 13–19 in executive layouts, the H225 can carry around 16–24 depending on fit, and the 902 Explorer generally carries about 8–10.
| Spec | AIRBUS H225 | Gulfstream G700 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 3 |
| DOC / nm | $ 20.87 | — |
| Min Crew | 2 | 4 |
| Total Seats | 21 | 16 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Gulfstream |
| Aircraft Name | H225 | G700 |
| Certification | FAA / EASA | In Development |
| Max Range (nm) | 454 | 7500 |
| DOC / nm / Seat | $ 0.99 | — |
| Max Cabin Seats | 28 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — |
| Standard Cabin Seats | 19 | 12 |
| Direct Operating Cost | $ 2,963 | — |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 4 |
| Total Seats | 21 | 16 |
| Max Cabin Seats | 28 | 19 |
| Standard Cabin Seats | 19 | 12 |
| Crew Rest | — | Optional |
| Jump Seat | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD / AFT |
| Engine | ||
| FADEC | Yes | — |
| Model | Makila 2A1 | Pearl 700 |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | On Condition |
| Horsepower | 2100 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Thrust (lbs) | — | 18250 |
| Dimensions | ||
| Length (ft) | 63.4 | 109.9 |
| Overall Height (ft) | 16.3 | 25.4 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | — |
| Wingspan (ft) | — | 103 |
| Aisle Step (ft) | — | Flat Floor |
| Cabin Width (ft) | — | 8.2 |
| Cabin Height (ft) | — | 6.25 |
| Cabin Length (ft) | — | 56.9 |
| Baggage Volume Int. (cu. ft) | — | 195 |