Cessna Citation Xls vs Piaggio Avanti Evo vs Piper M600 Sls vs Sikorsky S 92
The Cessna Citation XLS+ is a midsize business jet suited to fast point‑to‑point travel, typically offering around 1,900–2,100 nautical miles of range and seating for about 7–9 passengers in a pressurized cabin. The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft, generally a bit shorter in range than the XLS+ at roughly 1,700–1,900 nautical miles, with similar practical seating of about 7–9, emphasizing efficiency and a roomy cabin for its class. The Piper M600 SLS is a single‑engine turboprop (personal/light business aircraft) with substantially shorter range, about 1,200–1,500 nautical miles depending on configuration, and typically carries 4–6 passengers plus a pilot, favoring owner‑operators and shorter missions. The Sikorsky S‑92 is a large twin‑engine helicopter used for offshore, SAR, and VIP transport; its range is typically around 500–600 nautical miles, but it can carry far more people—commonly 12–19 passengers (and higher in some layouts)—trading speed and range for vertical‑lift capability.
| Spec | Cessna Citation XLS+ | Piaggio Avanti EVO | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | — | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 10 | 8 | 6 | 21 |
| Manufacturer | Cessna Citation | Piaggio | Piper | Sikorsky |
| Aircraft Name | XLS+ | Avanti EVO | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 1530 | 1406 | 439 |
| DOC / nm / Seat | $ 0.67 | — | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 9 | 7 | — | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 7540 | 3775 | 2200 | 7417 |
| Standard Cabin Seats | 8 | 6 | 4 | 19 |
| Direct Operating Cost | $ 2,303 | — | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 430 | 400 | 274 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $ 7,695,000 | $3,081,400 | $30,650,000 |
| Flight Rules | — | IFR | IFR | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | No | — |
| Min Crew | 2 | 1 | 1 | 2 |
| Crew Rest | No | — | — | — |
| Jump Seat | No | — | — | — |
| Total Seats | 10 | 8 | 5 | 21 |
| Galley Location | FWD | — | MID | — |
| Max Cabin Seats | 9 | 7 | — | 19 |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 9.3 | 9 | 5.6 | — |
| Galley / Refreshment | Galley | No | Refreshment Centre | — |
| Standard Cabin Seats | 8 | 6 | 4 | 19 |
| SL Cabin Altitude (ft) | 25230 | 24000 | 12600 | — |
| Max Cabin Altitude (ft) | — | 6600 | 8644 | — |
| Engine | ||||
| FADEC | Yes | Yes | No | Yes |
| Model | PW545C | PT6A–66B | PT6A-42A | CT7-8A |
| TBO (hrs) | 5000 | 3600 | 3600 | 4000 |
| Flat Rating | ISA + 10 | ISA + 28 | ISA + 55 | — |
| Thrust (lbs) | 4119 | — | — | — |
| No. of Engines | 2 | 2 | 1 | 1 |
| Horsepower | — | 850 | 600 | 2520 |
| Fuel Burn (gph) | — | 100 | — | — |
| Fuel Capacity (gal) | — | — | 260 | 760 |
| Fuel Type | — | — | — | JetFuel |
| Dimensions | ||||
| Length (ft) | 52.5 | 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 | 13.1 | 11.3 | 17.8 |
| Cabin Width - Floor (ft) | 3.9 | 3.5 | — | — |
| Cabin Length - Seating (ft) | 14.3 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | — | — | 140 |
| Baggage Volume Int. (cu. ft) | 10 | 35.2 | 20 | — |
| Cabin Volume (cu. ft) | — | — | 165 | 775 |