Cessna Citation Xls vs Daher Tbm 960 vs Leonardo Aw189 vs Piper M600 Sls
The Cessna Citation XLS+ is a light business jet aimed at fast, comfortable point‑to‑point travel in the midrange category, typically carrying about 7–9 passengers in an enclosed pressurized cabin and offering roughly 2,000 nautical miles of range depending on loading and conditions. The Daher TBM 960 is a high‑performance single‑engine turboprop, generally optimized for owner‑pilot or small executive missions; it usually seats 4–6 passengers (up to about 6 plus a pilot) and delivers long legs for its class at around 1,500–1,700 nautical miles. The Leonardo AW189 is a twin‑engine medium helicopter focused on offshore, SAR, and utility/VIP roles; it commonly carries around 12–16 passengers (higher in some configurations) but has much shorter fixed‑wing‑like range, typically on the order of a few hundred nautical miles, with strong vertical‑lift flexibility instead. The Piper M600 SLS is a pressurized single‑engine turboprop in the personal/owner‑flown category, usually seating 4–6 and offering roughly 1,200–1,500 nautical miles.
| Spec | Cessna Citation XLS+ | Daher TBM 960 | AGUSTA / LEONARDO AW189 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 2.25 | $ 15.57 | $ 2.19 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 10 | 6 | 21 | 6 |
| Manufacturer | Cessna Citation | Daher TBM | Leonardo | Piper |
| Aircraft Name | XLS+ | TBM 960 | AW189 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 1730 | 651 | 1406 |
| DOC / nm / Seat | $ 0.67 | $ 0.56 | $ 0.74 | $ 0.55 |
| Max Cabin Seats | 9 | — | 19 | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 7540 | 2908 | — | 2200 |
| Standard Cabin Seats | 8 | 4 | 19 | 4 |
| Direct Operating Cost | $ 2,303 | $ 744 | $ 2,413 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G3000 | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 430 | 330 | 155 | 274 |
| Base Aircraft Price (USD) | $15,500,000 | $4,450,000 | $2,413,000 | $3,081,400 |
| 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 | 1 |
| Crew Rest | No | — | — | — |
| Jump Seat | No | — | — | — |
| Total Seats | 10 | 6 | 21 | 5 |
| Galley Location | FWD | MID | — | MID |
| Max Cabin Seats | 9 | — | 19 | — |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 9.3 | 6.2 | — | 5.6 |
| Galley / Refreshment | Galley | — | — | Refreshment Centre |
| Standard Cabin Seats | 8 | 4 | 19 | 4 |
| SL Cabin Altitude (ft) | 25230 | 14390 | — | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PW545C | TBM 960 | CT7-2E1 | PT6A-42A |
| TBO (hrs) | 5000 | 3500 | 4000 | 3600 |
| Flat Rating | ISA + 10 | ISA + 49 | — | ISA + 55 |
| Thrust (lbs) | 4119 | — | — | — |
| No. of Engines | 2 | — | 2 | 1 |
| Horsepower | — | 850 | 1983 | 600 |
| Fuel Type | — | — | JetFuel | — |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 52.5 | 35.3 | 57.8 | 29.7 |
| Wingspan (ft) | 56.3 | 42.1 | — | 43.2 |
| Aisle Step (ft) | 0.7 | — | — | — |
| Cabin Width (ft) | 5.5 | 4 | — | 4.1 |
| Cabin Height (ft) | 5.7 | 4.1 | — | 4 |
| Cabin Length (ft) | 18.5 | 13.4 | — | 12.3 |
| Overall Height (ft) | 17.2 | — | 16.6 | 11.3 |
| Cabin Width - Floor (ft) | 3.9 | — | — | — |
| Cabin Length - Seating (ft) | 14.3 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | — | 85 | — |
| Baggage Volume Int. (cu. ft) | 10 | — | — | 20 |
| Cabin Volume (cu. ft) | — | 123 | 395 | 165 |
| Rotor Diameter (ft) | — | — | 48 | — |