Beechcraft King Air 360 Er vs Gulfstream G700 vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop business aircraft suited to short and medium missions, typically offering roughly a 1,500–1,800 nautical mile range depending on payload and conditions and usually seating about 6–9 passengers in a corporate layout. The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet designed for intercontinental travel, with a published range around 7,500 nautical miles and typical seating configurations commonly in the low‑to‑mid teens (often about 13–19) while still allowing multiple living zones. The Sikorsky S‑92 is a medium twin‑engine helicopter used for offshore transport, search and rescue, and VIP missions; its practical range is much shorter than the fixed‑wing aircraft, generally on the order of a few hundred nautical miles (often roughly 400–600, mission‑dependent), and it can carry a larger headcount in transport roles, commonly around 12–19 passengers depending on configuration.
| 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 |