Cessna Citation M2 vs Cessna Citation Xls vs Daher Tbm 960 vs Piper M350
The Cessna Citation M2 and Citation XLS+ are light jets, while the Daher TBM 960 and Piper M350 are pressurized single‑engine turboprops. The Citation M2 is typically a 6–7 passenger airplane (plus one or two pilots) with roughly 1,500 nautical miles of range, aimed at short to mid-length business trips. The Citation XLS+ is a larger light/midsize-class jet, commonly configured for about 8–9 passengers, with around 2,000–2,100 nautical miles of range, better suited to longer legs and a more spacious cabin. The TBM 960 is a high-performance single turboprop that usually carries about 4–6 passengers (plus a pilot) and offers roughly 1,400–1,700 nautical miles depending on mission profile, balancing speed and efficiency. The Piper M350 is a cabin-class piston single, typically seating about 4–5 passengers (plus a pilot) with around 1,000–1,300 nautical miles of range, optimized for owner-pilots and lower operating costs versus turboprops and jets.
| Spec | Cessna Citation M2 | Cessna Citation XLS+ | Daher TBM 960 | Piper M350 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 3.45 | $ 5.34 | $ 2.25 | $ 1.34 |
| Min Crew | 1 | 2 | 1 | — |
| Total Seats | 8 | 10 | 6 | 6 |
| Manufacturer | Cessna Citation | Cessna Citation | Daher TBM | Piper |
| Aircraft Name | M2 | XLS+ | TBM 960 | M350 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1400 | 1906 | 1730 | 1343 |
| DOC / nm / Seat | $ 0.58 | $ 0.67 | $ 0.56 | $ 0.22 |
| Max Cabin Seats | 7 | 9 | — | — |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3810 | 7540 | 2908 | 1308 |
| Standard Cabin Seats | 6 | 8 | 4 | 4 |
| Direct Operating Cost | $ 1,395 | $ 2,303 | $ 744 | $ 285 |
| Flight Deck (Base Spec) | Garmin G3000 | Rockwell Collins Pro Line 21 | Garmin G3000 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 404 | 430 | 330 | 213 |
| Base Aircraft Price (USD) | $5,150,000 | $15,500,000 | $4,450,000 | $1,195,000 |
| Flight Rules | — | — | IFR | VFR |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | 1 Enclosed Belted Flushing | No | — |
| Min Crew | 1 | 2 | 1 | — |
| Crew Rest | No | No | — | — |
| Jump Seat | No | No | — | — |
| Total Seats | 8 | 10 | 6 | 6 |
| Max Cabin Seats | 7 | 9 | — | — |
| Lavatory Location | AFT | AFT | — | — |
| Cabin Pressure (psi) | 8.5 | 9.3 | 6.2 | 5.6 |
| Galley / Refreshment | No | Galley | — | — |
| Standard Cabin Seats | 6 | 8 | 4 | 4 |
| SL Cabin Altitude (ft) | 22027 | 25230 | 14390 | — |
| Galley Location | — | FWD | MID | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | FJ44-1AP-21 | PW545C | TBM 960 | TIO-540-AE2A |
| TBO (hrs) | 3500 | 5000 | 3500 | 2000 |
| Flat Rating | ISA + 7 | ISA + 10 | ISA + 49 | — |
| Thrust (lbs) | 1965 | 4119 | — | — |
| No. of Engines | 2 | 2 | — | 1 |
| Fuel Burn (lbph) | 516 | — | — | — |
| Fuel Capacity (gal) | 492 | — | — | 120 |
| Horsepower | — | — | 850 | 350 |
| Fuel Type | — | — | — | AvGas |
| TBO (yrs) | — | — | — | 12 |
| Fuel Delivery | — | — | — | Fuel Injected |
| Dimensions | ||||
| Length (ft) | 42.6 | 52.5 | 35.3 | 29 |
| Wingspan (ft) | 47.3 | 56.3 | 42.1 | 43 |
| Aisle Step (ft) | 0.4 | 0.7 | — | — |
| Cabin Width (ft) | 4.8 | 5.5 | 4 | 4.1 |
| Cabin Height (ft) | 4.8 | 5.7 | 4.1 | 4 |
| Cabin Length (ft) | 11 | 18.5 | 13.4 | 12.3 |
| Overall Height (ft) | 14 | 17.2 | — | 11.4 |
| Cabin Width - Floor (ft) | 3.1 | 3.9 | — | — |
| Cabin Length - Seating (ft) | 8.8 | 14.3 | — | — |
| Baggage Volume Ext. (cu. ft) | 46 | 80 | — | 13 |
| Baggage Volume Int. (cu. ft) | — | 10 | — | 20 |
| Cabin Volume (cu. ft) | — | — | 123 | 165 |