Cessna Citation Xls vs Leonardo Aw189 vs Piaggio Avanti Evo vs Pilatus Pc 24
The Cessna Citation XLS+ and Pilatus PC-24 are light jets, while the Piaggio Avanti EVO is a twin‑turboprop business aircraft, and the Agusta/Leonardo AW189 is a medium twin‑engine helicopter. For range, the PC-24 is typically the longest-legged of the group at roughly about 2,000 nautical miles class, the Citation XLS+ is close behind in the high‑1,000s nautical miles, and the Avanti EVO is generally in a similar ballpark to the XLS+ but often slightly shorter depending on reserves and payload; the AW189’s practical range is substantially shorter, commonly in the few‑hundred‑nautical‑mile class (mission dependent). For passenger capacity, the XLS+ and PC-24 are usually configured around 6–8 passengers in executive layouts (with maximum seating higher in dense configurations), the Avanti EVO is also commonly 6–8, and the AW189 can carry more people overall, often around the mid‑teens in typical transport layouts, reflecting its rotorcraft cabin volume and mission focus.
| Spec | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 15.57 | — | $ 3.71 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 10 | 21 | 8 | 6 |
| Manufacturer | Cessna Citation | Leonardo | Piaggio | Pilatus |
| Aircraft Name | XLS+ | AW189 | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 651 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.67 | $ 0.74 | — | $ 0.62 |
| Max Cabin Seats | 9 | 19 | 7 | 10 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 7540 | — | 3775 | 6680 |
| Standard Cabin Seats | 8 | 19 | 6 | 6 |
| Direct Operating Cost | $ 2,303 | $ 2,413 | — | $ 1,619 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 430 | 155 | 400 | 440 |
| Base Aircraft Price (USD) | $15,500,000 | $2,413,000 | $ 7,695,000 | $11,800,000 |
| Flight Rules | — | IFR | IFR | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | — | No | 1 Enclosed Flushing |
| Min Crew | 2 | 1 | 1 | 1 |
| Crew Rest | No | — | — | No |
| Jump Seat | No | — | — | No |
| Total Seats | 10 | 21 | 8 | 6 |
| Galley Location | FWD | — | — | FWD |
| Max Cabin Seats | 9 | 19 | 7 | 10 |
| Lavatory Location | AFT | — | — | FWD |
| Cabin Pressure (psi) | 9.3 | — | 9 | 9.3 |
| Galley / Refreshment | Galley | — | No | Optional Refreshment Center |
| Standard Cabin Seats | 8 | 19 | 6 | 6 |
| SL Cabin Altitude (ft) | 25230 | — | 24000 | 23500 |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW545C | CT7-2E1 | PT6A–66B | FJ44-4A-QPM |
| TBO (hrs) | 5000 | 4000 | 3600 | 5000 |
| Flat Rating | ISA + 10 | — | ISA + 28 | ISA + 23 |
| Thrust (lbs) | 4119 | — | — | 3435 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Type | — | JetFuel | — | — |
| Horsepower | — | 1983 | 850 | — |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 52.5 | 57.8 | 47.3 | 52.2 |
| Wingspan (ft) | 56.3 | — | 47.1 | 55.8 |
| Aisle Step (ft) | 0.7 | — | — | Flat Floor |
| Cabin Width (ft) | 5.5 | — | 6.1 | 5.6 |
| Cabin Height (ft) | 5.7 | — | 5.8 | 5.1 |
| Cabin Length (ft) | 18.5 | — | 14.9 | 23 |
| Overall Height (ft) | 17.2 | 16.6 | 13.1 | 17.4 |
| Cabin Width - Floor (ft) | 3.9 | — | 3.5 | 3.8 |
| Cabin Length - Seating (ft) | 14.3 | — | — | 17 |
| Baggage Volume Ext. (cu. ft) | 80 | 85 | — | — |
| Baggage Volume Int. (cu. ft) | 10 | — | 35.2 | 90 |
| Rotor Diameter (ft) | — | 48 | — | — |
| Cabin Volume (cu. ft) | — | 395 | — | — |