Airbus Helicopters H225 vs Gulfstream G700
The Airbus H225 and the Gulfstream G700 serve very different missions. The H225 is a twin‑engine heavy helicopter designed for vertical lift operations such as offshore transport, search and rescue, and utility roles, making it valuable where runways are unavailable and point‑to‑point access is needed. The Gulfstream G700 is an ultra‑long‑range business jet optimized for high‑speed intercontinental travel between airports, prioritizing cabin comfort, altitude capability, and cruise efficiency. In range, the G700 is dramatically longer‑legged, with a published range of about 7,500 nautical miles, enabling nonstop flights like New York to Dubai under typical conditions. The H225’s range is much shorter, generally on the order of a few hundred nautical miles depending on payload and fuel configuration, reflecting the different physics and mission profile of helicopters. Passenger capacity also differs by configuration. An H225 can be outfitted to carry roughly 19 passengers in a high‑density transport layout, while the G700 typically carries fewer, commonly around 10 to 19 in executive seating, with the emphasis on space and amenities rather than maximum seats.
| 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 |