Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Gulfstream G700
The Airbus H225 is a heavy twin‑engine helicopter, best suited to missions that need vertical takeoff and landing, hoisting, or access to remote sites without runways. Its typical range is on the order of a few hundred nautical miles (often roughly 450–600 nm depending on payload and fuel fit), and passenger capacity is commonly in the mid‑teens up to around 19 in a standard transport layout, with higher counts possible in dense seating. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility airplane designed for short and unimproved runways and cost‑effective regional lift. It typically ranges about 900–1,200 nm depending on load and reserves, and usually seats up to 9 passengers (or carries comparable cargo). The Gulfstream G700 is an ultra‑long‑range business jet optimized for intercontinental travel at high speed and comfort. It offers about 7,500 nm of range and typically carries around 12–19 passengers in executive configurations, with higher maximum seating in airline‑style layouts.
| Spec | AIRBUS H225 | Gulfstream G700 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 3 |
| DOC / nm | $ 20.87 | — |
| Min Crew | 2 | 4 |
| Total Seats | 21 | 16 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Gulfstream |
| Aircraft Name | H225 | G700 |
| Certification | FAA / EASA | In Development |
| Max Range (nm) | 454 | 7500 |
| DOC / nm / Seat | $ 0.99 | — |
| Max Cabin Seats | 28 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — |
| Standard Cabin Seats | 19 | 12 |
| Direct Operating Cost | $ 2,963 | — |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 4 |
| Total Seats | 21 | 16 |
| Max Cabin Seats | 28 | 19 |
| Standard Cabin Seats | 19 | 12 |
| Crew Rest | — | Optional |
| Jump Seat | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD / AFT |
| Engine | ||
| FADEC | Yes | — |
| Model | Makila 2A1 | Pearl 700 |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | On Condition |
| Horsepower | 2100 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Thrust (lbs) | — | 18250 |
| Dimensions | ||
| Length (ft) | 63.4 | 109.9 |
| Overall Height (ft) | 16.3 | 25.4 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | — |
| 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 |