Airbus Helicopters H225 vs Embraer Legacy 650 E vs Gulfstream G700 vs Leonardo Aw189
The Airbus H225 and Leonardo AW189 are large twin‑engine helicopters, while the Embraer Legacy 650E and Gulfstream G700 are long‑range business jets. In category terms, the H225 is a heavy‑class rotorcraft designed for offshore transport, SAR, and utility missions; the AW189 is a super‑medium helicopter optimized for similar roles with slightly smaller overall capacity. The Legacy 650E is a large‑cabin, long‑range jet suited to intercontinental business travel, and the G700 is an ultra‑long‑range flagship jet aimed at the longest nonstop missions. For range, the helicopters are typically in the few‑hundred‑nautical‑mile class depending on payload and reserves, with the H225 generally offering longer endurance than the AW189 in comparable configurations. The Legacy 650E is roughly in the 3,900–4,000 nm range, enabling many transoceanic routes, while the G700 extends to about 7,500 nm, reaching true global city pairs. Passenger capacity also differs: the H225 can carry around 19 passengers in high‑density layouts, the AW189 commonly seats about 16–19, the Legacy 650E typically seats 13–14, and the G700 is usually configured for about 13–19 depending on cabin layout.
| Spec | AIRBUS H225 | Gulfstream G700 | AGUSTA / LEONARDO AW189 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | — | $ 15.57 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Gulfstream | Leonardo |
| Aircraft Name | H225 | G700 | AW189 |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 7500 | 651 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.74 |
| Max Cabin Seats | 28 | 19 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — | — |
| Standard Cabin Seats | 19 | 12 | 19 |
| Direct Operating Cost | $ 2,963 | — | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 | $2,413,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 21 |
| Max Cabin Seats | 28 | 19 | 19 |
| Standard Cabin Seats | 19 | 12 | 19 |
| Crew Rest | — | Optional | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD / AFT | — |
| Engine | |||
| FADEC | Yes | — | Yes |
| Model | Makila 2A1 | Pearl 700 | CT7-2E1 |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | On Condition | 4000 |
| Horsepower | 2100 | — | 1983 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Thrust (lbs) | — | 18250 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 109.9 | 57.8 |
| Overall Height (ft) | 16.3 | 25.4 | 16.6 |
| Rotor Diameter (ft) | 53.2 | — | 48 |
| Cabin Volume (cu. ft) | 547 | — | 395 |
| 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 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 85 |