Airbus Helicopters H225 vs Dassault Falcon 8x vs Enstrom 480b vs Gulfstream G700
The Airbus H225 is a heavy twin‑engine helicopter, optimized for vertical lift missions rather than long cruise. Its practical range is typically a few hundred nautical miles (often around 500–600 nm depending on payload and reserves), and passenger capacity is commonly in the low‑to‑mid teens in an executive or utility layout. The Dassault Falcon 8X is a long‑range large‑cabin business jet designed for intercontinental travel. It offers roughly 6,400 nm of range and usually seats about 12–16 passengers in typical corporate configurations, with more possible depending on layout. The Enstrom 480B is a light single‑engine helicopter, suited to short‑range travel, training, and utility work. Range is generally a few hundred nautical miles (around 300–400 nm), and it typically carries 4–5 people including the pilot. The Gulfstream G700 is an ultra‑long‑range, ultra‑large‑cabin business jet aimed at premium nonstop missions. It is rated around 7,500 nm of range and commonly accommodates about 13–19 passengers, with high flexibility for luxury cabin zones.
| 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 |