Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Cessna Citation Xls vs Dassault Falcon 8x
The Airbus H225 is a heavy twin‑engine helicopter rather than a fixed‑wing aircraft. It typically carries around 16–19 passengers in an offshore or transport configuration and is optimized for vertical access and short‑to‑medium missions; practical range is roughly 450–700 nm depending on payload and reserves. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft, usually seating 9–14 passengers, suited to short‑haul regional flying with a typical range around 900–1,000 nm. The Cessna Citation XLS+ is a midsize business jet, commonly arranged for about 8–9 passengers, offering higher speed and a typical range near 1,900–2,100 nm. The Dassault Falcon 8X is an ultra‑long‑range large‑cabin business jet, generally configured for about 12–16 passengers, and built for intercontinental missions with a range around 6,400–6,800 nm. Overall, capability steps up from vertical‑lift access (H225), to rugged short‑haul utility (Caravan), to faster midrange executive travel (XLS+), and finally to long‑range global premium transport (8X).
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Dassault Falcon 8X |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 7.66 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 10 | 17 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Cessna Citation | Dassault Falcon |
| Aircraft Name | H225 | XLS+ | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.64 |
| Max Cabin Seats | 28 | 9 | 16 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | 36900 |
| Standard Cabin Seats | 19 | 8 | 14 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 430 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $ 62,500,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 3 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 10 | 17 |
| Max Cabin Seats | 28 | 9 | 16 |
| Standard Cabin Seats | 19 | 8 | 14 |
| Lavatory | — | 1 Enclosed Belted Flushing | 2 Enclosed Flushing |
| Crew Rest | — | No | No |
| Jump Seat | — | No | Yes |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | 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 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 5000 | On-Condition |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 3 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 10 | ISA + 17 |
| Thrust (lbs) | — | 4119 | 6722 |
| Dimensions | |||
| Length (ft) | 63.4 | 52.5 | 80.2 |
| Overall Height (ft) | 16.3 | 17.2 | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 |
| Wingspan (ft) | — | 56.3 | 86.3 |
| Aisle Step (ft) | — | 0.7 | — |
| Cabin Width (ft) | — | 5.5 | 7.7 |
| Cabin Height (ft) | — | 5.7 | 6.2 |
| Cabin Length (ft) | — | 18.5 | 42.7 |
| 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 |