Cessna Citation Xls vs Dassault Falcon 8x vs Piaggio Avanti Evo vs Sikorsky S 92
The Cessna Citation XLS+ is a midsize business jet aimed at efficient short-to-medium missions, with a typical range around 2,000 nautical miles and seating commonly configured for about 7 to 9 passengers. The Dassault Falcon 8X is a long‑range large‑cabin tri‑jet designed for intercontinental travel, offering roughly 6,400 nautical miles of range and typically accommodating about 12 to 16 passengers in executive layouts. The Piaggio Avanti EVO is a high‑speed turboprop business aircraft, generally positioned between light jets and midsize aircraft for cost‑efficient regional trips, with about 1,700 to 1,900 nautical miles of range and usually seating around 6 to 8 passengers. The Sikorsky S‑92 is a large twin‑engine helicopter used for offshore, VIP, and utility transport; its range is typically on the order of 500 to 600 nautical miles (mission dependent) and it can carry roughly 12 to 19 passengers depending on configuration. Overall, the Falcon 8X leads on range and cabin size, the XLS+ balances speed and access, the Avanti EVO emphasizes efficiency, and the S‑92 trades speed and range for vertical‑lift capability.
| Spec | Cessna Citation XLS+ | Dassault Falcon 8X | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 7.66 | — | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 10 | 17 | 8 | 21 |
| Manufacturer | Cessna Citation | Dassault Falcon | Piaggio | Sikorsky |
| Aircraft Name | XLS+ | 8X | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 6450 | 1530 | 439 |
| DOC / nm / Seat | $ 0.67 | $ 0.64 | — | $ 0.94 |
| Max Cabin Seats | 9 | 16 | 7 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 7540 | 36900 | 3775 | 7417 |
| Standard Cabin Seats | 8 | 14 | 6 | 19 |
| Direct Operating Cost | $ 2,303 | $ 3,805 | — | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 430 | 516 | 400 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $ 62,500,000 | $ 7,695,000 | $30,650,000 |
| Flight Rules | — | — | IFR | IFR |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | 2 Enclosed Flushing | No | — |
| Min Crew | 2 | 2 | 1 | 2 |
| Crew Rest | No | No | — | — |
| Jump Seat | No | Yes | — | — |
| Total Seats | 10 | 17 | 8 | 21 |
| Galley Location | FWD | FWD | — | — |
| Max Cabin Seats | 9 | 16 | 7 | 19 |
| Lavatory Location | AFT | FWD / AFT | — | — |
| Cabin Pressure (psi) | 9.3 | 10.2 | 9 | — |
| Galley / Refreshment | Galley | Galley | No | — |
| Standard Cabin Seats | 8 | 14 | 6 | 19 |
| SL Cabin Altitude (ft) | 25230 | 29200 | 24000 | — |
| Max Cabin Altitude (ft) | — | 3900 | 6600 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW545C | PW307D | PT6A–66B | CT7-8A |
| TBO (hrs) | 5000 | On-Condition | 3600 | 4000 |
| Flat Rating | ISA + 10 | ISA + 17 | ISA + 28 | — |
| Thrust (lbs) | 4119 | 6722 | — | — |
| No. of Engines | 2 | 3 | 2 | 1 |
| Horsepower | — | — | 850 | 2520 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Type | — | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 52.5 | 80.2 | 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 | 13.1 | 17.8 |
| Cabin Width - Floor (ft) | 3.9 | 6.3 | 3.5 | — |
| Cabin Length - Seating (ft) | 14.3 | 29.2 | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | — | — | 140 |
| Baggage Volume Int. (cu. ft) | 10 | 140 | 35.2 | — |
| Cabin Volume (cu. ft) | — | 1695 | — | 775 |