Cessna Citation Xls vs Daher Tbm 960 vs Leonardo Aw189 vs Sikorsky S 92
The Cessna Citation XLS+ is a light/midsize business jet designed for fast, high-altitude point‑to‑point travel. It typically carries about 7–9 passengers and offers roughly 2,000 nautical miles of range, making it well suited to longer nonstop city pairs at jet speeds. The Daher TBM 960 is a high‑performance single‑engine turboprop in the personal/business aircraft category. It usually seats 4–6 passengers in practical use (up to about 6 plus pilot) and delivers about 1,700 nautical miles of range, trading some speed for efficiency and access to shorter runways. The Leonardo (Agusta) AW189 is a super‑medium twin helicopter aimed at offshore, SAR, and utility/VIP roles. Passenger capacity is commonly around 16–19 in a transport layout, with range on the order of 450–500 nautical miles depending on configuration. The Sikorsky S‑92 is a larger heavy helicopter used heavily for offshore transport and SAR. It typically carries about 19 passengers and has a similar medium‑range helicopter profile, roughly 500 nautical miles, prioritizing payload, cabin volume, and overwater capability over speed and long-range cruise.
| Spec | Cessna Citation XLS+ | Daher TBM 960 | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 2.25 | $ 15.57 | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 10 | 6 | 21 | 21 |
| Manufacturer | Cessna Citation | Daher TBM | Leonardo | Sikorsky |
| Aircraft Name | XLS+ | TBM 960 | AW189 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 1730 | 651 | 439 |
| DOC / nm / Seat | $ 0.67 | $ 0.56 | $ 0.74 | $ 0.94 |
| Max Cabin Seats | 9 | — | 19 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 7540 | 2908 | — | 7417 |
| Standard Cabin Seats | 8 | 4 | 19 | 19 |
| Direct Operating Cost | $ 2,303 | $ 744 | $ 2,413 | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G3000 | EFIS | EFIS |
| Max Cruise Speed (ktas) | 430 | 330 | 155 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $4,450,000 | $2,413,000 | $30,650,000 |
| Flight Rules | — | IFR | IFR | IFR |
| Aircraft Type | — | Turbo Prop | — | — |
| 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 | 6 | 21 | 21 |
| Galley Location | FWD | MID | — | — |
| Max Cabin Seats | 9 | — | 19 | 19 |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 9.3 | 6.2 | — | — |
| Galley / Refreshment | Galley | — | — | — |
| Standard Cabin Seats | 8 | 4 | 19 | 19 |
| SL Cabin Altitude (ft) | 25230 | 14390 | — | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW545C | TBM 960 | CT7-2E1 | CT7-8A |
| TBO (hrs) | 5000 | 3500 | 4000 | 4000 |
| Flat Rating | ISA + 10 | ISA + 49 | — | — |
| Thrust (lbs) | 4119 | — | — | — |
| No. of Engines | 2 | — | 2 | 1 |
| Horsepower | — | 850 | 1983 | 2520 |
| Fuel Type | — | — | JetFuel | JetFuel |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 52.5 | 35.3 | 57.8 | — |
| Wingspan (ft) | 56.3 | 42.1 | — | — |
| Aisle Step (ft) | 0.7 | — | — | — |
| Cabin Width (ft) | 5.5 | 4 | — | — |
| Cabin Height (ft) | 5.7 | 4.1 | — | — |
| Cabin Length (ft) | 18.5 | 13.4 | — | — |
| Overall Height (ft) | 17.2 | — | 16.6 | 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 | — | — | — |
| Cabin Volume (cu. ft) | — | 123 | 395 | 775 |
| Rotor Diameter (ft) | — | — | 48 | — |