Cessna Citation Xls vs Leonardo Aw189 vs Piaggio Avanti Evo vs Piper M600 Sls
The Cessna Citation XLS+ is a light business jet designed for fast, pressurized, higher‑altitude travel. It typically carries about 7–9 passengers and offers roughly 1,900–2,100 nautical miles of range, making it well suited to medium‑length city pairs with jet speed and comfort. The Agusta/Leonardo AW189 is a large, twin‑engine helicopter focused on vertical lift missions such as offshore transport and SAR. Depending on interior, it commonly seats around 16–19 passengers, but its point‑to‑point range is shorter than fixed‑wing aircraft, generally on the order of about 450–500 nautical miles (mission dependent). The Piaggio Avanti EVO is a high‑speed, pressurized turboprop aircraft that splits the difference between turboprops and light jets in cruise efficiency. It usually seats about 7–9 passengers and delivers approximately 1,400–1,700 nautical miles of range. The Piper M600 SLS is a single‑engine, pressurized turboprop aimed at owner‑pilots. It typically seats 5–6 passengers and provides about 1,300–1,500 nautical miles of range, favoring simplicity and operating economy over maximum payload.
| Spec | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 15.57 | — | $ 2.19 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 10 | 21 | 8 | 6 |
| Manufacturer | Cessna Citation | Leonardo | Piaggio | Piper |
| Aircraft Name | XLS+ | AW189 | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 651 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.67 | $ 0.74 | — | $ 0.55 |
| Max Cabin Seats | 9 | 19 | 7 | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 7540 | — | 3775 | 2200 |
| Standard Cabin Seats | 8 | 19 | 6 | 4 |
| Direct Operating Cost | $ 2,303 | $ 2,413 | — | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | EFIS | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 430 | 155 | 400 | 274 |
| Base Aircraft Price (USD) | $15,500,000 | $2,413,000 | $ 7,695,000 | $3,081,400 |
| Flight Rules | — | IFR | IFR | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | — | No | No |
| Min Crew | 2 | 1 | 1 | 1 |
| Crew Rest | No | — | — | — |
| Jump Seat | No | — | — | — |
| Total Seats | 10 | 21 | 8 | 5 |
| Galley Location | FWD | — | — | MID |
| Max Cabin Seats | 9 | 19 | 7 | — |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 9.3 | — | 9 | 5.6 |
| Galley / Refreshment | Galley | — | No | Refreshment Centre |
| Standard Cabin Seats | 8 | 19 | 6 | 4 |
| SL Cabin Altitude (ft) | 25230 | — | 24000 | 12600 |
| Max Cabin Altitude (ft) | — | — | 6600 | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PW545C | CT7-2E1 | PT6A–66B | PT6A-42A |
| TBO (hrs) | 5000 | 4000 | 3600 | 3600 |
| Flat Rating | ISA + 10 | — | ISA + 28 | ISA + 55 |
| Thrust (lbs) | 4119 | — | — | — |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Type | — | JetFuel | — | — |
| Horsepower | — | 1983 | 850 | 600 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 52.5 | 57.8 | 47.3 | 29.7 |
| Wingspan (ft) | 56.3 | — | 47.1 | 43.2 |
| Aisle Step (ft) | 0.7 | — | — | — |
| Cabin Width (ft) | 5.5 | — | 6.1 | 4.1 |
| Cabin Height (ft) | 5.7 | — | 5.8 | 4 |
| Cabin Length (ft) | 18.5 | — | 14.9 | 12.3 |
| Overall Height (ft) | 17.2 | 16.6 | 13.1 | 11.3 |
| Cabin Width - Floor (ft) | 3.9 | — | 3.5 | — |
| Cabin Length - Seating (ft) | 14.3 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | 85 | — | — |
| Baggage Volume Int. (cu. ft) | 10 | — | 35.2 | 20 |
| Rotor Diameter (ft) | — | 48 | — | — |
| Cabin Volume (cu. ft) | — | 395 | — | 165 |