Cessna Citation Xls vs Daher Tbm 960 vs Piaggio Avanti Evo vs Sikorsky S 92
The Cessna Citation XLS+ is a midsize business jet aimed at short-to-midrange corporate missions. It typically carries about 7–9 passengers in a pressurized stand-up cabin and offers roughly 2,000 nautical miles of range, making it well suited to city-pair flying with jet speed and comfort. The Daher TBM 960 is a high-performance single-engine turboprop, best viewed as an owner-operator or small executive aircraft. It usually seats 4–6 passengers and has around 1,500–1,700 nautical miles of range, trading cabin volume for efficiency, speed for its class, and access to shorter runways. The Piaggio Avanti EVO is a twin-turboprop business aircraft with a distinctive design and a surprisingly spacious cabin for its footprint. It commonly carries 6–8 passengers and offers about 1,700–1,800 nautical miles of range, positioning it between the TBM and light/midsize jets in comfort and performance. The Sikorsky S-92 is a large twin-engine helicopter used for offshore transport, VIP, and SAR roles. It typically carries about 12–19 passengers, with range commonly in the 500–700 nautical mile class depending on configuration, emphasizing vertical lift and mission flexibility over cruise range.
| Spec | Cessna Citation XLS+ | Daher TBM 960 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 2.25 | — | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 10 | 6 | 8 | 21 |
| Manufacturer | Cessna Citation | Daher TBM | Piaggio | Sikorsky |
| Aircraft Name | XLS+ | TBM 960 | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 1730 | 1530 | 439 |
| DOC / nm / Seat | $ 0.67 | $ 0.56 | — | $ 0.94 |
| Max Cabin Seats | 9 | — | 7 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 7540 | 2908 | 3775 | 7417 |
| Standard Cabin Seats | 8 | 4 | 6 | 19 |
| Direct Operating Cost | $ 2,303 | $ 744 | — | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G3000 | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 430 | 330 | 400 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $4,450,000 | $ 7,695,000 | $30,650,000 |
| Flight Rules | — | IFR | IFR | IFR |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | No | — |
| Min Crew | 2 | 1 | 1 | 2 |
| Crew Rest | No | — | — | — |
| Jump Seat | No | — | — | — |
| Total Seats | 10 | 6 | 8 | 21 |
| Galley Location | FWD | MID | — | — |
| Max Cabin Seats | 9 | — | 7 | 19 |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 9.3 | 6.2 | 9 | — |
| Galley / Refreshment | Galley | — | No | — |
| Standard Cabin Seats | 8 | 4 | 6 | 19 |
| SL Cabin Altitude (ft) | 25230 | 14390 | 24000 | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW545C | TBM 960 | PT6A–66B | CT7-8A |
| TBO (hrs) | 5000 | 3500 | 3600 | 4000 |
| Flat Rating | ISA + 10 | ISA + 49 | ISA + 28 | — |
| Thrust (lbs) | 4119 | — | — | — |
| No. of Engines | 2 | — | 2 | 1 |
| Horsepower | — | 850 | 850 | 2520 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Type | — | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 52.5 | 35.3 | 47.3 | — |
| Wingspan (ft) | 56.3 | 42.1 | 47.1 | — |
| Aisle Step (ft) | 0.7 | — | — | — |
| Cabin Width (ft) | 5.5 | 4 | 6.1 | — |
| Cabin Height (ft) | 5.7 | 4.1 | 5.8 | — |
| Cabin Length (ft) | 18.5 | 13.4 | 14.9 | — |
| Overall Height (ft) | 17.2 | — | 13.1 | 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 | — |
| Cabin Volume (cu. ft) | — | 123 | — | 775 |