Cessna Citation Xls vs Leonardo Aw189 vs Piaggio Avanti Evo vs Sikorsky S 92
The Cessna Citation XLS+ is a midsize business jet suited to fast point‑to‑point travel. It typically carries about 7–9 passengers in a pressurized cabin and offers roughly 2,000 nautical miles of range, making it best for city pairs that would be inefficient by helicopter. The Leonardo AW189 is a super‑medium twin helicopter optimized for offshore and utility missions. It commonly seats around 16–19 passengers and has a typical range on the order of 450–500 nautical miles, trading speed and range for vertical access and mission flexibility. The Piaggio Avanti EVO is a high‑performance turboprop aircraft positioned between light jets and traditional turboprops. It usually carries 6–9 passengers and offers about 1,500–1,800 nautical miles of range, with strong short‑field capability and efficient cruise for its class. The Sikorsky S‑92 is a heavy twin helicopter widely used offshore and for government/VIP transport. It generally carries about 16–19 passengers and offers roughly 500–600 nautical miles of range, emphasizing payload and all‑weather capability over long-distance cruise.
| Spec | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 15.57 | — | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 10 | 21 | 8 | 21 |
| Manufacturer | Cessna Citation | Leonardo | Piaggio | Sikorsky |
| Aircraft Name | XLS+ | AW189 | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 651 | 1530 | 439 |
| DOC / nm / Seat | $ 0.67 | $ 0.74 | — | $ 0.94 |
| Max Cabin Seats | 9 | 19 | 7 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 7540 | — | 3775 | 7417 |
| Standard Cabin Seats | 8 | 19 | 6 | 19 |
| Direct Operating Cost | $ 2,303 | $ 2,413 | — | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | EFIS | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 430 | 155 | 400 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $2,413,000 | $ 7,695,000 | $30,650,000 |
| Flight Rules | — | IFR | IFR | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | — | No | — |
| Min Crew | 2 | 1 | 1 | 2 |
| Crew Rest | No | — | — | — |
| Jump Seat | No | — | — | — |
| Total Seats | 10 | 21 | 8 | 21 |
| Galley Location | FWD | — | — | — |
| Max Cabin Seats | 9 | 19 | 7 | 19 |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 9.3 | — | 9 | — |
| Galley / Refreshment | Galley | — | No | — |
| Standard Cabin Seats | 8 | 19 | 6 | 19 |
| SL Cabin Altitude (ft) | 25230 | — | 24000 | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW545C | CT7-2E1 | PT6A–66B | CT7-8A |
| TBO (hrs) | 5000 | 4000 | 3600 | 4000 |
| Flat Rating | ISA + 10 | — | ISA + 28 | — |
| Thrust (lbs) | 4119 | — | — | — |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Type | — | JetFuel | — | JetFuel |
| Horsepower | — | 1983 | 850 | 2520 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 52.5 | 57.8 | 47.3 | — |
| Wingspan (ft) | 56.3 | — | 47.1 | — |
| Aisle Step (ft) | 0.7 | — | — | — |
| Cabin Width (ft) | 5.5 | — | 6.1 | — |
| Cabin Height (ft) | 5.7 | — | 5.8 | — |
| Cabin Length (ft) | 18.5 | — | 14.9 | — |
| Overall Height (ft) | 17.2 | 16.6 | 13.1 | 17.8 |
| Cabin Width - Floor (ft) | 3.9 | — | 3.5 | — |
| Cabin Length - Seating (ft) | 14.3 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | 85 | — | 140 |
| Baggage Volume Int. (cu. ft) | 10 | — | 35.2 | — |
| Rotor Diameter (ft) | — | 48 | — | — |
| Cabin Volume (cu. ft) | — | 395 | — | 775 |