Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Dassault Falcon 8x vs Gulfstream G700
The Airbus H225 is a heavy, twin‑engine helicopter, optimized for vertical lift missions rather than long cruise legs; its typical operational range is in the few‑hundred‑nautical‑mile class, and it generally carries a couple dozen passengers depending on configuration. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft; it offers short‑to‑medium regional range (also generally in the few‑hundred to roughly 1,000‑nautical‑mile class) and commonly seats around 9–14 passengers in commuter layouts. The Dassault Falcon 8X is an ultra‑long‑range business jet designed for intercontinental flying, with range roughly in the 6,000‑nautical‑mile class and typical executive seating around 12–16 passengers (higher in dense layouts). The Gulfstream G700 is a flagship large‑cabin business jet with similarly intercontinental capability, generally around the 7,000‑nautical‑mile class, and typical seating about 13–19. Overall, the H225 prioritizes access over distance, the Caravan prioritizes rugged regional utility, and the Falcon 8X and G700 dominate for long‑range, high‑comfort executive travel.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Gulfstream G700 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 3 |
| DOC / nm | $ 20.87 | $ 7.66 | — |
| Min Crew | 2 | 2 | 4 |
| Total Seats | 21 | 17 | 16 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Gulfstream |
| Aircraft Name | H225 | 8X | G700 |
| Certification | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 454 | 6450 | 7500 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | — |
| Max Cabin Seats | 28 | 16 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 36900 | — |
| Standard Cabin Seats | 19 | 14 | 12 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | — |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 516 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $78,000,000 |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 4 |
| Total Seats | 21 | 17 | 16 |
| Max Cabin Seats | 28 | 16 | 19 |
| Standard Cabin Seats | 19 | 14 | 12 |
| Lavatory | — | 2 Enclosed Flushing | — |
| Crew Rest | — | No | Optional |
| Jump Seat | — | Yes | Yes |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | FWD / AFT | FWD / AFT |
| Cabin Pressure (psi) | — | 10.2 | — |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 29200 | — |
| Max Cabin Altitude (ft) | — | 3900 | — |
| Engine | |||
| FADEC | Yes | Yes | — |
| Model | Makila 2A1 | PW307D | Pearl 700 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | On Condition |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 17 | — |
| Thrust (lbs) | — | 6722 | 18250 |
| Dimensions | |||
| Length (ft) | 63.4 | 80.2 | 109.9 |
| Overall Height (ft) | 16.3 | 26.1 | 25.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — |
| Wingspan (ft) | — | 86.3 | 103 |
| Cabin Width (ft) | — | 7.7 | 8.2 |
| Cabin Height (ft) | — | 6.2 | 6.25 |
| Cabin Length (ft) | — | 42.7 | 56.9 |
| Cabin Width - Floor (ft) | — | 6.3 | — |
| Cabin Length - Seating (ft) | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 195 |
| Aisle Step (ft) | — | — | Flat Floor |