Airbus Helicopters H225 vs Enstrom 480b vs Gulfstream G700 vs Sikorsky S 92
The Airbus H225, Enstrom 480B, and Sikorsky S-92 are helicopters, while the Gulfstream G700 is a long‑range business jet. For range, the G700 is in a different class, spanning roughly 7,500 nautical miles, enabling nonstop intercontinental missions. The H225 and S-92 are long‑range, medium/heavy transport helicopters typically suited to offshore and utility work, with practical ranges generally in the 450–550 nautical mile neighborhood depending on payload, reserves, and configuration. The Enstrom 480B is a light single‑engine piston helicopter with a much shorter reach, commonly around 200–300 nautical miles. Passenger capacity follows a similar pattern: the G700 typically seats a private-jet cabin load (often about 10–19 depending on layout), the H225 and S-92 usually carry larger groups for helicopter operations (often around 16–19 in offshore-style seating, with higher limits in some configurations), and the Enstrom 480B is much smaller, usually accommodating about 4–5 people including the pilot.
| Spec | AIRBUS H225 | Gulfstream G700 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | — | $ 19.79 |
| Min Crew | 2 | 4 | 2 |
| Total Seats | 21 | 16 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Gulfstream | Sikorsky |
| Aircraft Name | H225 | G700 | S-92 |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 7500 | 439 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.94 |
| Max Cabin Seats | 28 | 19 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — | 7417 |
| Standard Cabin Seats | 19 | 12 | 19 |
| Direct Operating Cost | $ 2,963 | — | $ 3,068 |
| 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 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 |
| 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 | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | On Condition | 4000 |
| Horsepower | 2100 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Thrust (lbs) | — | 18250 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 109.9 | — |
| Overall Height (ft) | 16.3 | 25.4 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 775 |
| 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) | — | — | 140 |