Cessna Citation Xls vs Dassault Falcon 8x vs Leonardo Aw189 vs Piaggio Avanti Evo
The Cessna Citation XLS+ is a midsize business jet suited to regional and transcontinental missions, typically carrying about 8 to 9 passengers with a range around 2,000 nautical miles. The Dassault Falcon 8X is a long‑range, large‑cabin tri‑jet designed for intercontinental travel, commonly configured for roughly 12 to 16 passengers and offering about 6,400 nautical miles of range. The Leonardo (Agusta) AW189 is a super‑medium twin‑engine helicopter optimized for offshore, SAR, and utility/VIP roles; it can seat up to about 16 to 19 passengers depending on configuration, but its range is much shorter than jets, generally on the order of roughly 450 to 500 nautical miles. The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft positioned between turboprops and light/midsize jets; it typically carries 7 to 9 passengers and offers a range around 1,500 to 1,800 nautical miles, trading ultimate range for efficiency and strong short‑field performance.
| Spec | Cessna Citation XLS+ | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 7.66 | $ 15.57 | — |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 10 | 17 | 21 | 8 |
| Manufacturer | Cessna Citation | Dassault Falcon | Leonardo | Piaggio |
| Aircraft Name | XLS+ | 8X | AW189 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 6450 | 651 | 1530 |
| DOC / nm / Seat | $ 0.67 | $ 0.64 | $ 0.74 | — |
| Max Cabin Seats | 9 | 16 | 19 | 7 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 7540 | 36900 | — | 3775 |
| Standard Cabin Seats | 8 | 14 | 19 | 6 |
| Direct Operating Cost | $ 2,303 | $ 3,805 | $ 2,413 | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 430 | 516 | 155 | 400 |
| Base Aircraft Price (USD) | $15,500,000 | $ 62,500,000 | $2,413,000 | $ 7,695,000 |
| Flight Rules | — | — | IFR | IFR |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | 2 Enclosed Flushing | — | No |
| Min Crew | 2 | 2 | 1 | 1 |
| Crew Rest | No | No | — | — |
| Jump Seat | No | Yes | — | — |
| Total Seats | 10 | 17 | 21 | 8 |
| Galley Location | FWD | FWD | — | — |
| Max Cabin Seats | 9 | 16 | 19 | 7 |
| Lavatory Location | AFT | FWD / AFT | — | — |
| Cabin Pressure (psi) | 9.3 | 10.2 | — | 9 |
| Galley / Refreshment | Galley | Galley | — | No |
| Standard Cabin Seats | 8 | 14 | 19 | 6 |
| SL Cabin Altitude (ft) | 25230 | 29200 | — | 24000 |
| Max Cabin Altitude (ft) | — | 3900 | — | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW545C | PW307D | CT7-2E1 | PT6A–66B |
| TBO (hrs) | 5000 | On-Condition | 4000 | 3600 |
| Flat Rating | ISA + 10 | ISA + 17 | — | ISA + 28 |
| Thrust (lbs) | 4119 | 6722 | — | — |
| No. of Engines | 2 | 3 | 2 | 2 |
| Fuel Type | — | — | JetFuel | — |
| Horsepower | — | — | 1983 | 850 |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 52.5 | 80.2 | 57.8 | 47.3 |
| Wingspan (ft) | 56.3 | 86.3 | — | 47.1 |
| Aisle Step (ft) | 0.7 | — | — | — |
| Cabin Width (ft) | 5.5 | 7.7 | — | 6.1 |
| Cabin Height (ft) | 5.7 | 6.2 | — | 5.8 |
| Cabin Length (ft) | 18.5 | 42.7 | — | 14.9 |
| Overall Height (ft) | 17.2 | 26.1 | 16.6 | 13.1 |
| Cabin Width - Floor (ft) | 3.9 | 6.3 | — | 3.5 |
| Cabin Length - Seating (ft) | 14.3 | 29.2 | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | — | 85 | — |
| Baggage Volume Int. (cu. ft) | 10 | 140 | — | 35.2 |
| Cabin Volume (cu. ft) | — | 1695 | 395 | — |
| Rotor Diameter (ft) | — | — | 48 | — |