Airbus Helicopters H225 vs Gulfstream G700 vs Robinson R66
The Airbus H225 is a heavy, twin‑engine helicopter built for offshore transport, search and rescue, and utility missions. It typically carries around 19 passengers in a high‑density configuration (fewer in VIP), and offers medium helicopter range—roughly in the 400–500 nautical mile class depending on load, reserves, and mission equipment. The Gulfstream G700 is an ultra‑long‑range business jet optimized for high‑speed intercontinental travel. It generally seats 12–19 passengers in executive layouts, and its range is about 7,500 nautical miles, enabling nonstop city pairs that helicopters and light rotorcraft cannot approach. The Robinson R66 is a light, single‑engine helicopter aimed at private, training, and light utility use. It seats up to 5 (including the pilot) and has short‑to‑moderate range for its class—roughly around 300 nautical miles, varying with payload and conditions. In summary, the G700 dominates range and cruise speed, the H225 leads helicopter lift and cabin capacity, and the R66 is the smallest and most economical but with the most limited capacity and range.
| 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 |