Cessna Citation Xls vs Leonardo Aw189 vs Pilatus Pc 24 vs Piper M600 Sls
The Cessna Citation XLS+ and Pilatus PC-24 are light business jets, while the Piper M600 SLS is a single‑engine turboprop airplane and the Agusta/Leonardo AW189 is a twin‑engine helicopter. For range, the jets generally lead: the PC-24 is typically around the low‑to‑mid 2,000 nautical mile class, and the Citation XLS+ is roughly similar, enabling longer nonstop city pairs than the turboprop or helicopter. The Piper M600 SLS usually offers about 1,400 nautical miles, suitable for regional trips at lower operating cost but with slower cruise than the jets. The AW189’s range is typically in the 400–500 nautical mile class depending on payload and reserves, trading distance for vertical lift and point‑to‑point access without runways. For passenger capacity, the Citation XLS+ commonly seats about 8–9 in a business configuration, the PC-24 about 6–10 depending on layout, the M600 SLS typically 5–6 plus a pilot, and the AW189 usually carries a larger cabin load, often up to the mid‑teens (around 16–19) in high‑density configurations.
| Spec | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 15.57 | $ 3.71 | $ 2.19 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 10 | 21 | 6 | 6 |
| Manufacturer | Cessna Citation | Leonardo | Pilatus | Piper |
| Aircraft Name | XLS+ | AW189 | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 651 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.67 | $ 0.74 | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 9 | 19 | 10 | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 7540 | — | 6680 | 2200 |
| Standard Cabin Seats | 8 | 19 | 6 | 4 |
| Direct Operating Cost | $ 2,303 | $ 2,413 | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | EFIS | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 430 | 155 | 440 | 274 |
| Base Aircraft Price (USD) | $15,500,000 | $2,413,000 | $11,800,000 | $3,081,400 |
| Flight Rules | — | IFR | — | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | — | 1 Enclosed Flushing | No |
| Min Crew | 2 | 1 | 1 | 1 |
| Crew Rest | No | — | No | — |
| Jump Seat | No | — | No | — |
| Total Seats | 10 | 21 | 6 | 5 |
| Galley Location | FWD | — | FWD | MID |
| Max Cabin Seats | 9 | 19 | 10 | — |
| Lavatory Location | AFT | — | FWD | — |
| Cabin Pressure (psi) | 9.3 | — | 9.3 | 5.6 |
| Galley / Refreshment | Galley | — | Optional Refreshment Center | Refreshment Centre |
| Standard Cabin Seats | 8 | 19 | 6 | 4 |
| SL Cabin Altitude (ft) | 25230 | — | 23500 | 12600 |
| Cargo Door | — | — | Yes | — |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PW545C | CT7-2E1 | FJ44-4A-QPM | PT6A-42A |
| TBO (hrs) | 5000 | 4000 | 5000 | 3600 |
| Flat Rating | ISA + 10 | — | ISA + 23 | ISA + 55 |
| Thrust (lbs) | 4119 | — | 3435 | — |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Type | — | JetFuel | — | — |
| Horsepower | — | 1983 | — | 600 |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 52.5 | 57.8 | 52.2 | 29.7 |
| Wingspan (ft) | 56.3 | — | 55.8 | 43.2 |
| Aisle Step (ft) | 0.7 | — | Flat Floor | — |
| Cabin Width (ft) | 5.5 | — | 5.6 | 4.1 |
| Cabin Height (ft) | 5.7 | — | 5.1 | 4 |
| Cabin Length (ft) | 18.5 | — | 23 | 12.3 |
| Overall Height (ft) | 17.2 | 16.6 | 17.4 | 11.3 |
| Cabin Width - Floor (ft) | 3.9 | — | 3.8 | — |
| Cabin Length - Seating (ft) | 14.3 | — | 17 | — |
| Baggage Volume Ext. (cu. ft) | 80 | 85 | — | — |
| Baggage Volume Int. (cu. ft) | 10 | — | 90 | 20 |
| Rotor Diameter (ft) | — | 48 | — | — |
| Cabin Volume (cu. ft) | — | 395 | — | 165 |