Cessna Citation Xls vs Dassault Falcon 8x vs Leonardo Aw189 vs Piper M600 Sls
The Cessna Citation XLS+ is a midsize business jet suited to regional and transcontinental trips, typically flying about 2,000 nautical miles and carrying around 7–9 passengers in a pressurized cabin. The Dassault Falcon 8X is an ultra-long-range large-cabin business jet designed for intercontinental missions, offering roughly 6,400–6,450 nautical miles of range and usually seating about 12–16 passengers depending on configuration. The Agusta/Leonardo AW189 is a twin‑engine medium helicopter aimed at offshore, SAR, and utility/VIP roles; it trades speed and range for vertical access, with typical range around 450–500 nautical miles (mission-dependent) and seating commonly 16–19 passengers (or fewer in VIP fit). The Piper M600 SLS is a single‑engine turboprop personal/business aircraft positioned below jets for cost and runway flexibility, with about 1,400–1,500 nautical miles of range and generally 4–6 passengers plus a pilot. Overall, the Falcon 8X leads on range and cabin size, the XLS+ balances comfort and efficiency, the M600 SLS emphasizes simplicity and operating economy, and the AW189 uniquely provides helicopter access where runways aren’t available.
| Spec | Cessna Citation XLS+ | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 7.66 | $ 15.57 | $ 2.19 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 10 | 17 | 21 | 6 |
| Manufacturer | Cessna Citation | Dassault Falcon | Leonardo | Piper |
| Aircraft Name | XLS+ | 8X | AW189 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 6450 | 651 | 1406 |
| DOC / nm / Seat | $ 0.67 | $ 0.64 | $ 0.74 | $ 0.55 |
| Max Cabin Seats | 9 | 16 | 19 | — |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 7540 | 36900 | — | 2200 |
| Standard Cabin Seats | 8 | 14 | 19 | 4 |
| Direct Operating Cost | $ 2,303 | $ 3,805 | $ 2,413 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 430 | 516 | 155 | 274 |
| Base Aircraft Price (USD) | $15,500,000 | $ 62,500,000 | $2,413,000 | $3,081,400 |
| 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 | 5 |
| Galley Location | FWD | FWD | — | MID |
| Max Cabin Seats | 9 | 16 | 19 | — |
| Lavatory Location | AFT | FWD / AFT | — | — |
| Cabin Pressure (psi) | 9.3 | 10.2 | — | 5.6 |
| Galley / Refreshment | Galley | Galley | — | Refreshment Centre |
| Standard Cabin Seats | 8 | 14 | 19 | 4 |
| SL Cabin Altitude (ft) | 25230 | 29200 | — | 12600 |
| Max Cabin Altitude (ft) | — | 3900 | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PW545C | PW307D | CT7-2E1 | PT6A-42A |
| TBO (hrs) | 5000 | On-Condition | 4000 | 3600 |
| Flat Rating | ISA + 10 | ISA + 17 | — | ISA + 55 |
| Thrust (lbs) | 4119 | 6722 | — | — |
| No. of Engines | 2 | 3 | 2 | 1 |
| Fuel Type | — | — | JetFuel | — |
| Horsepower | — | — | 1983 | 600 |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 52.5 | 80.2 | 57.8 | 29.7 |
| Wingspan (ft) | 56.3 | 86.3 | — | 43.2 |
| Aisle Step (ft) | 0.7 | — | — | — |
| Cabin Width (ft) | 5.5 | 7.7 | — | 4.1 |
| Cabin Height (ft) | 5.7 | 6.2 | — | 4 |
| Cabin Length (ft) | 18.5 | 42.7 | — | 12.3 |
| Overall Height (ft) | 17.2 | 26.1 | 16.6 | 11.3 |
| Cabin Width - Floor (ft) | 3.9 | 6.3 | — | — |
| Cabin Length - Seating (ft) | 14.3 | 29.2 | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | — | 85 | — |
| Baggage Volume Int. (cu. ft) | 10 | 140 | — | 20 |
| Cabin Volume (cu. ft) | — | 1695 | 395 | 165 |
| Rotor Diameter (ft) | — | — | 48 | — |