Cessna Citation Xls vs Daher Tbm 960 vs Piaggio Avanti Evo vs Piper M600 Sls
By category, the Cessna Citation XLS+ is a super‑light business jet, while the Daher TBM 960 and Piper M600 SLS are high‑performance single‑engine turboprops, and the Piaggio Avanti EVO is a fast twin‑turboprop often described as a “turboprop with jetlike cruise.” In range, the XLS+ typically offers roughly about 2,000 nautical miles class capability depending on load and reserves, generally exceeding the M600 SLS (around the mid‑1,000‑nm class) and often comparable to or somewhat ahead of the TBM 960 (around the high‑1,000‑nm class). The Avanti EVO is also in the ~1,700–1,800 nm class, but real‑world range varies notably with speed selection. For passenger capacity, the XLS+ commonly seats 7–9 in an enclosed, stand‑up‑ish cabin for its class, making it the most comfortable for larger groups. The Avanti EVO typically seats about 7–9 as well, with a roomy cabin for a turboprop. The TBM 960 and M600 SLS are usually configured for about 4–6 passengers plus pilot, optimized for owner‑operators rather than larger parties.
| Spec | Cessna Citation XLS+ | Daher TBM 960 | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 2.25 | — | $ 2.19 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 10 | 6 | 8 | 6 |
| Manufacturer | Cessna Citation | Daher TBM | Piaggio | Piper |
| Aircraft Name | XLS+ | TBM 960 | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 1730 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.67 | $ 0.56 | — | $ 0.55 |
| Max Cabin Seats | 9 | — | 7 | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 7540 | 2908 | 3775 | 2200 |
| Standard Cabin Seats | 8 | 4 | 6 | 4 |
| Direct Operating Cost | $ 2,303 | $ 744 | — | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G3000 | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 430 | 330 | 400 | 274 |
| Base Aircraft Price (USD) | $15,500,000 | $4,450,000 | $ 7,695,000 | $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 | No |
| Min Crew | 2 | 1 | 1 | 1 |
| Crew Rest | No | — | — | — |
| Jump Seat | No | — | — | — |
| Total Seats | 10 | 6 | 8 | 5 |
| Galley Location | FWD | MID | — | MID |
| Max Cabin Seats | 9 | — | 7 | — |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 9.3 | 6.2 | 9 | 5.6 |
| Galley / Refreshment | Galley | — | No | Refreshment Centre |
| Standard Cabin Seats | 8 | 4 | 6 | 4 |
| SL Cabin Altitude (ft) | 25230 | 14390 | 24000 | 12600 |
| Max Cabin Altitude (ft) | — | — | 6600 | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PW545C | TBM 960 | PT6A–66B | PT6A-42A |
| TBO (hrs) | 5000 | 3500 | 3600 | 3600 |
| Flat Rating | ISA + 10 | ISA + 49 | ISA + 28 | ISA + 55 |
| Thrust (lbs) | 4119 | — | — | — |
| No. of Engines | 2 | — | 2 | 1 |
| Horsepower | — | 850 | 850 | 600 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 52.5 | 35.3 | 47.3 | 29.7 |
| Wingspan (ft) | 56.3 | 42.1 | 47.1 | 43.2 |
| Aisle Step (ft) | 0.7 | — | — | — |
| Cabin Width (ft) | 5.5 | 4 | 6.1 | 4.1 |
| Cabin Height (ft) | 5.7 | 4.1 | 5.8 | 4 |
| Cabin Length (ft) | 18.5 | 13.4 | 14.9 | 12.3 |
| Overall Height (ft) | 17.2 | — | 13.1 | 11.3 |
| Cabin Width - Floor (ft) | 3.9 | — | 3.5 | — |
| Cabin Length - Seating (ft) | 14.3 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | — | — | — |
| Baggage Volume Int. (cu. ft) | 10 | — | 35.2 | 20 |
| Cabin Volume (cu. ft) | — | 123 | — | 165 |