Compare Beechcraft King Air 260 vs Daher TBM 960 vs Piaggio Avanti EVO
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| Manufacturer | Beechcraft | Daher TBM | Piaggio |
| Aircraft Type | KingAir 250 | TBM 960 | Avanti EVO |
| Base Aircraft Price (USD) | $6,450,000 | $4,450,000 | $ 7,695,000 |
| Direct Operating Cost | $ 1,333 | $ 744 | - |
| DOC / nm | $ 4.30 | $ 2.25 | - |
| DOC / nm / Seat | $ 0.72 | $ 0.56 | - |
| Max Cruise Speed (ktas) | 310 | 330 | 400 |
| Max Range (nm) | 1420 | 1730 | 1530 |
| Useful Load (lbs) | 3760 | 2601 | 3775 |
| Total Seats | 8 | 6 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 6 | 4 | 6 |
| Max Cabin Seats | 8 | - | 7 |
| Min Crew | 1 | 1 | 1 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | Rockwell Collins Pro Line 21 |
| Flight Rules | IFR | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Weights | |||
| MRAMP (lbs) | 12590 | 7430 | 12150 |
| MTOW (lbs) | 12500 | 7394 | 12100 |
| MLW (lbs) | 12500 | 7024 | 11500 |
| MZFW (lbs) | 11000 | 6032 | 9800 |
| BOW (lbs) | 8830 | 4629 | 8375 |
| BEW (lbs) | 8740 | - | 8325 |
| Useful Load (lbs) | 3760 | 2601 | 3775 |
| Max Payload (lbs) | 2170 | 1403 | 1425 |
| Fuel Capacity (lbs) | 3645 | 2017 | 2802 |
| Payload Max Fuel (lbs) | 115 | 891 | 973 |
| Max Baggage Weight (lbs) | 550 | 507 | 350 |
| Dimensions | |||
| Wingspan (ft) | 57.9 | 42.1 | 47.1 |
| Overall Height (ft) | 14.8 | - | 13.1 |
| Length (ft) | 43.8 | 35.3 | 47.3 |
| Cabin Height (ft) | 4.8 | 4.1 | 5.8 |
| Cabin Width (ft) | 4.5 | 4 | 6.1 |
| Cabin Width - Floor (ft) | 4.1 | - | 3.5 |
| Cabin Length (ft) | 16.7 | 13.4 | 14.9 |
| Cabin Length - Seating (ft) | 16.7 | - | - |
| Cabin Volume (cu. ft) | - | 123 | - |
| Baggage Volume Int. (cu. ft) | 55 | - | 35.2 |
| Engine | |||
| No. of Engines | 1 | - | 2 |
| Manufacturer | Beechcraft | Daher TBM | Piaggio |
| Model | PT6A-52 | TBM 960 | PT6A–66B |
| Horsepower | 850 | 850 | 850 |
| Flat Rating | ISA + 37 | ISA + 49 | ISA + 28 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | 3600 | 3500 | 3600 |
| Fuel Capacity (gal) | 544 | - | - |
| Fuel Burn (gph) | - | - | 100 |
| Avionics | |||
| Flight Deck | Rockwell Collins Pro Line Fusion | Garmin G3000 | Rockwell Collins Pro Line 21 |
| Flight Rules | IFR | IFR | IFR |
| FMS | 1 | - | - |
| Autopilot | 1 | 1 | - |
| PFD | 2 | 2 | - |
| MFD | 1 | 1 | - |
| GPS | 1 | 1 | - |
| AHRS | 1 | - | - |
| Transponder | 1 | 1 | - |
| VHF Com | 2 | 2 | - |
| VHF NAV | 2 | 2 | - |
| Cabin | |||
| Total Seats | 8 | 6 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 6 | 4 | 6 |
| Max Cabin Seats | 8 | - | 7 |
| Min Crew | 1 | 1 | 1 |
| Lavatory | 1 Flushing | No | No |
| Lavatory Location | AFT | - | - |
| Galley / Refreshment | No | - | No |
| Galley Location | - | MID | - |
| Max Cabin Altitude (ft) | - | - | 6600 |
| SL Cabin Altitude (ft) | 15293 | 14390 | 24000 |
| Cabin Pressure (psi) | 6.5 | 6.2 | 9 |
| Other | |||
| Prop Manufacturer | Hartzell | - | Hartzell |
| Prop Description | 4-Blade Constant Feathering Reverse | - | Scimitar |
| Gear Type | Retractable | Retractable | Retractable |
| Performance | |||
| Max Cruise Speed (Mach) | - | - | 0.7 |
| Max Cruise Speed (ktas) | 310 | 330 | 400 |
| Long Range Cruise (ktas) | 256 | 252 | 318 |
| Stall Speed - Clean (kias) | 80 | - | - |
| Max Range (nm) | 1420 | 1730 | 1530 |
| Range @ 85% (nm) | - | 1440 | - |
| Range @ 75% | - | 1594 | - |
| Max Range Crew + 4 (nm) | 1038 | - | - |
| Take-off FL (ft) | 2111 | - | - |
| Take-off Roll (ft) | - | - | 3262 |
| Take-Off >50ft Obst. (ft) | - | 2380 | - |
| Take-Off (5000 / ISA + 10) | 3099 | 3475 | 4700 |
| Landing >50ft Obst. (ft) | 2845 | 2430 | 3282 |
| Max Climb Rate (fpm) | 2450 | - | 2770 |
| Service Ceiling (ft) | 35000 | 31000 | 41000 |