Cessna Citation Xls vs Leonardo Aw189 vs Piper M600 Sls vs Sikorsky S 92
The Cessna Citation XLS+ is a midsize business jet built for fast point‑to‑point travel. It typically offers roughly 1,800–2,100 nautical miles of range depending on load and reserves, and is commonly configured for about 7–9 passengers. The Piper M600 SLS is a single‑engine turboprop airplane in the personal/light business category; it prioritizes efficiency over speed, with about 1,200–1,500 nautical miles of range and seating usually around 4–6 passengers in comfort (up to 6 seats total). The Agusta/Leonardo AW189 is a super‑medium twin helicopter aimed at offshore and utility missions. Its range is generally on the order of 450–500+ nautical miles (mission‑dependent) and it can carry around 16–19 passengers in a transport layout. The Sikorsky S‑92 is a heavy twin helicopter used heavily for offshore transport and SAR; it has broadly similar mission range, often around 500+ nautical miles with reserves depending on configuration, and typically seats about 19 passengers, with higher capacity possible in dense layouts.
| Spec | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 15.57 | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 10 | 21 | 6 | 21 |
| Manufacturer | Cessna Citation | Leonardo | Piper | Sikorsky |
| Aircraft Name | XLS+ | AW189 | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 651 | 1406 | 439 |
| DOC / nm / Seat | $ 0.67 | $ 0.74 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 9 | 19 | — | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 7540 | — | 2200 | 7417 |
| Standard Cabin Seats | 8 | 19 | 4 | 19 |
| Direct Operating Cost | $ 2,303 | $ 2,413 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | EFIS | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 430 | 155 | 274 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $2,413,000 | $3,081,400 | $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 | 5 | 21 |
| Galley Location | FWD | — | MID | — |
| Max Cabin Seats | 9 | 19 | — | 19 |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 9.3 | — | 5.6 | — |
| Galley / Refreshment | Galley | — | Refreshment Centre | — |
| Standard Cabin Seats | 8 | 19 | 4 | 19 |
| SL Cabin Altitude (ft) | 25230 | — | 12600 | — |
| Max Cabin Altitude (ft) | — | — | 8644 | — |
| Engine | ||||
| FADEC | Yes | Yes | No | Yes |
| Model | PW545C | CT7-2E1 | PT6A-42A | CT7-8A |
| TBO (hrs) | 5000 | 4000 | 3600 | 4000 |
| Flat Rating | ISA + 10 | — | ISA + 55 | — |
| Thrust (lbs) | 4119 | — | — | — |
| No. of Engines | 2 | 2 | 1 | 1 |
| Fuel Type | — | JetFuel | — | JetFuel |
| Horsepower | — | 1983 | 600 | 2520 |
| Fuel Capacity (gal) | — | — | 260 | 760 |
| Dimensions | ||||
| Length (ft) | 52.5 | 57.8 | 29.7 | — |
| Wingspan (ft) | 56.3 | — | 43.2 | — |
| Aisle Step (ft) | 0.7 | — | — | — |
| Cabin Width (ft) | 5.5 | — | 4.1 | — |
| Cabin Height (ft) | 5.7 | — | 4 | — |
| Cabin Length (ft) | 18.5 | — | 12.3 | — |
| Overall Height (ft) | 17.2 | 16.6 | 11.3 | 17.8 |
| Cabin Width - Floor (ft) | 3.9 | — | — | — |
| Cabin Length - Seating (ft) | 14.3 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | 85 | — | 140 |
| Baggage Volume Int. (cu. ft) | 10 | — | 20 | — |
| Rotor Diameter (ft) | — | 48 | — | — |
| Cabin Volume (cu. ft) | — | 395 | 165 | 775 |