Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Gulfstream G700 vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are both large twin‑engine helicopters aimed at offshore energy, search and rescue, and VIP/utility missions. Their range is broadly in the mid‑400 to roughly 550 nautical mile class depending on payload and tanking, and typical seating is around 16–19 passengers in transport layouts (with higher-density options possible for specific roles). The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility airplane optimized for short, unimproved strips and regional hauling; it has a much longer fixed‑wing range than the helicopters—often around 900–1,200 nautical miles—and commonly carries about 9 passengers (or equivalent cargo) in commuter configuration. The Gulfstream G700 is a long‑range business jet in a different league: it is designed for intercontinental travel with roughly 7,000+ nautical miles of range, and while it can be certified for more, it typically carries about 10–19 passengers in luxury business layouts. Overall, the helicopters prioritize vertical access and mission flexibility, the Caravan prioritizes rugged simplicity and payload-to-cost, and the G700 prioritizes speed, range, and cabin comfort.
| 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 |