Cessna Citation Xls vs Daher Tbm 960 vs Dassault Falcon 8x vs Leonardo Aw189
The Cessna Citation XLS+ is a midsize business jet suited to short-to-medium missions, offering roughly 2,000 nautical miles of range and typically seating about 7–9 passengers in a comfortable cabin. The Daher TBM 960 is a high-performance single‑engine turboprop in the “fast personal/business” category rather than a jet; it trades cabin size for efficiency, with about 1,400–1,700 nautical miles of range depending on reserves and payload and usually carrying 4–6 passengers in addition to the pilot. The Dassault Falcon 8X is an ultra‑long‑range large‑cabin business jet designed for intercontinental flying, with about 6,400 nautical miles of range and typical configurations around 12–16 passengers (higher in dense layouts). The Agusta/Leonardo AW189 is a large twin‑engine helicopter aimed at offshore, SAR, and utility/VIP roles; it has far shorter range than the jets (generally a few hundred nautical miles, mission‑dependent) but can carry a comparatively high passenger load for rotorcraft, commonly around 12–16 passengers in transport layouts.
| Spec | Cessna Citation XLS+ | Daher TBM 960 | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 2.25 | $ 7.66 | $ 15.57 |
| Min Crew | 2 | 1 | 2 | 1 |
| Total Seats | 10 | 6 | 17 | 21 |
| Manufacturer | Cessna Citation | Daher TBM | Dassault Falcon | Leonardo |
| Aircraft Name | XLS+ | TBM 960 | 8X | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 1730 | 6450 | 651 |
| DOC / nm / Seat | $ 0.67 | $ 0.56 | $ 0.64 | $ 0.74 |
| Max Cabin Seats | 9 | — | 16 | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 7540 | 2908 | 36900 | — |
| Standard Cabin Seats | 8 | 4 | 14 | 19 |
| Direct Operating Cost | $ 2,303 | $ 744 | $ 3,805 | $ 2,413 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G3000 | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 430 | 330 | 516 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $4,450,000 | $ 62,500,000 | $2,413,000 |
| Flight Rules | — | IFR | — | IFR |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | 2 Enclosed Flushing | — |
| Min Crew | 2 | 1 | 2 | 1 |
| Crew Rest | No | — | No | — |
| Jump Seat | No | — | Yes | — |
| Total Seats | 10 | 6 | 17 | 21 |
| Galley Location | FWD | MID | FWD | — |
| Max Cabin Seats | 9 | — | 16 | 19 |
| Lavatory Location | AFT | — | FWD / AFT | — |
| Cabin Pressure (psi) | 9.3 | 6.2 | 10.2 | — |
| Galley / Refreshment | Galley | — | Galley | — |
| Standard Cabin Seats | 8 | 4 | 14 | 19 |
| SL Cabin Altitude (ft) | 25230 | 14390 | 29200 | — |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW545C | TBM 960 | PW307D | CT7-2E1 |
| TBO (hrs) | 5000 | 3500 | On-Condition | 4000 |
| Flat Rating | ISA + 10 | ISA + 49 | ISA + 17 | — |
| Thrust (lbs) | 4119 | — | 6722 | — |
| No. of Engines | 2 | — | 3 | 2 |
| Horsepower | — | 850 | — | 1983 |
| Fuel Type | — | — | — | JetFuel |
| Dimensions | ||||
| Length (ft) | 52.5 | 35.3 | 80.2 | 57.8 |
| Wingspan (ft) | 56.3 | 42.1 | 86.3 | — |
| Aisle Step (ft) | 0.7 | — | — | — |
| Cabin Width (ft) | 5.5 | 4 | 7.7 | — |
| Cabin Height (ft) | 5.7 | 4.1 | 6.2 | — |
| Cabin Length (ft) | 18.5 | 13.4 | 42.7 | — |
| Overall Height (ft) | 17.2 | — | 26.1 | 16.6 |
| Cabin Width - Floor (ft) | 3.9 | — | 6.3 | — |
| Cabin Length - Seating (ft) | 14.3 | — | 29.2 | — |
| Baggage Volume Ext. (cu. ft) | 80 | — | — | 85 |
| Baggage Volume Int. (cu. ft) | 10 | — | 140 | — |
| Cabin Volume (cu. ft) | — | 123 | 1695 | 395 |
| Rotor Diameter (ft) | — | — | — | 48 |