Airbus Helicopters H225 vs Cessna Citation Xls vs Dassault Falcon 8x vs Gulfstream G700
The Airbus H225 is a twin‑engine helicopter rather than a fixed‑wing business jet, typically used for offshore, SAR, and utility missions. Its practical range is roughly a few hundred nautical miles (around 500–700 nm depending on fit and reserves) and it commonly carries around 19 passengers in high‑density seating (fewer in VIP layouts). The Cessna Citation XLS+ is a midsize business jet suited to regional and transcontinental missions, with about 2,000 nm of range and usually 7–9 passengers in typical executive configuration. The Dassault Falcon 8X is an ultra‑long‑range large‑cabin jet, generally offering about 6,450 nm of range and carrying roughly 12–16 passengers depending on layout. The Gulfstream G700 sits at the top end of large‑cabin, ultra‑long‑range business jets, with about 7,500 nm of range and typical seating around 13–19 passengers, emphasizing spacious multi‑zone cabins. Overall, the H225 prioritizes vertical lift and mission utility, the XLS+ targets efficient midsize jet travel, and the 8X and G700 dominate long‑haul range and cabin comfort, with the G700 generally leading on range and cabin volume.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Dassault Falcon 8X | Gulfstream G700 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 7.66 | — |
| Min Crew | 2 | 2 | 2 | 4 |
| Total Seats | 21 | 10 | 17 | 16 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Airbus Helicopters | Cessna Citation | Dassault Falcon | Gulfstream |
| Aircraft Name | H225 | XLS+ | 8X | G700 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 454 | 1906 | 6450 | 7500 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.64 | — |
| Max Cabin Seats | 28 | 9 | 16 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | 36900 | — |
| Standard Cabin Seats | 19 | 8 | 14 | 12 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 3,805 | — |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 430 | 516 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $ 62,500,000 | $78,000,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 2 | 4 |
| Total Seats | 21 | 10 | 17 | 16 |
| Max Cabin Seats | 28 | 9 | 16 | 19 |
| Standard Cabin Seats | 19 | 8 | 14 | 12 |
| Lavatory | — | 1 Enclosed Belted Flushing | 2 Enclosed Flushing | — |
| Crew Rest | — | No | No | Optional |
| Jump Seat | — | No | Yes | Yes |
| Galley Location | — | FWD | FWD | FWD |
| Lavatory Location | — | AFT | FWD / AFT | FWD / AFT |
| Cabin Pressure (psi) | — | 9.3 | 10.2 | — |
| Galley / Refreshment | — | Galley | Galley | — |
| SL Cabin Altitude (ft) | — | 25230 | 29200 | — |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | — |
| Model | Makila 2A1 | PW545C | PW307D | Pearl 700 |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 5000 | On-Condition | On Condition |
| Horsepower | 2100 | — | — | — |
| No. of Engines | 2 | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 10 | ISA + 17 | — |
| Thrust (lbs) | — | 4119 | 6722 | 18250 |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 80.2 | 109.9 |
| Overall Height (ft) | 16.3 | 17.2 | 26.1 | 25.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 | — |
| Wingspan (ft) | — | 56.3 | 86.3 | 103 |
| Aisle Step (ft) | — | 0.7 | — | Flat Floor |
| Cabin Width (ft) | — | 5.5 | 7.7 | 8.2 |
| Cabin Height (ft) | — | 5.7 | 6.2 | 6.25 |
| Cabin Length (ft) | — | 18.5 | 42.7 | 56.9 |
| Cabin Width - Floor (ft) | — | 3.9 | 6.3 | — |
| Cabin Length - Seating (ft) | — | 14.3 | 29.2 | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | — | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 140 | 195 |