Gulfstream G700 vs Sikorsky S 92
The Gulfstream G700 is a long‑range, large‑cabin business jet designed primarily for intercity and intercontinental travel at high speed and altitude, while the Sikorsky S‑92 is a medium/heavy twin‑engine helicopter built for vertical lift missions such as offshore transport, search and rescue, and VIP shuttle where runway access is limited. In range, the G700 is optimized for global point‑to‑point flights, with published capability around 7,500 nautical miles depending on configuration and conditions, whereas the S‑92’s range is much shorter, typically a few hundred nautical miles (often roughly 500 nm class, mission‑dependent) because it trades endurance and speed for hover and VTOL capability. For passenger capacity, the G700 is commonly configured for about 13 to 19 passengers in executive layouts, emphasizing space and amenities, while the S‑92 can carry more people in high‑density seating—often up to around 19 passengers in typical offshore configurations—though VIP interiors may seat fewer to prioritize comfort and baggage.
| Spec | Gulfstream G700 | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 3 | 2 |
| Min Crew | 4 | 2 |
| Total Seats | 16 | 21 |
| Manufacturer | Gulfstream | Sikorsky |
| Aircraft Name | G700 | S-92 |
| Certification | In Development | FAA / EASA |
| Max Range (nm) | 7500 | 439 |
| Max Cabin Seats | 19 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Standard Cabin Seats | 12 | 19 |
| Flight Deck (Base Spec) | Gulfstream Symmetry Flight Deck | EFIS |
| Max Cruise Speed (ktas) | 516 | 155 |
| Base Aircraft Price (USD) | $78,000,000 | $30,650,000 |
| DOC / nm | — | $ 19.79 |
| Flight Rules | — | IFR |
| DOC / nm / Seat | — | $ 0.94 |
| Useful Load (lbs) | — | 7417 |
| Direct Operating Cost | — | $ 3,068 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 4 | 2 |
| Crew Rest | Optional | — |
| Jump Seat | Yes | — |
| Total Seats | 16 | 21 |
| Galley Location | FWD | — |
| Max Cabin Seats | 19 | 19 |
| Lavatory Location | FWD / AFT | — |
| Standard Cabin Seats | 12 | 19 |
| Engine | ||
| Model | Pearl 700 | CT7-8A |
| TBO (hrs) | On Condition | 4000 |
| Thrust (lbs) | 18250 | — |
| No. of Engines | 2 | 1 |
| FADEC | — | Yes |
| Fuel Type | — | JetFuel |
| Horsepower | — | 2520 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 109.9 | — |
| Wingspan (ft) | 103 | — |
| Aisle Step (ft) | Flat Floor | — |
| Cabin Width (ft) | 8.2 | — |
| Cabin Height (ft) | 6.25 | — |
| Cabin Length (ft) | 56.9 | — |
| Overall Height (ft) | 25.4 | 17.8 |
| Baggage Volume Int. (cu. ft) | 195 | — |
| Cabin Volume (cu. ft) | — | 775 |
| Baggage Volume Ext. (cu. ft) | — | 140 |