Compare Beechcraft King Air 360 vs Cessna Citation M2 vs Daher TBM 960
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| Manufacturer | Beechcraft | Cessna Citation | Daher TBM |
| Aircraft Type | KingAir 350i | M2 | TBM 960 |
| Base Aircraft Price (USD) | $7,650,000 | $5,150,000 | $4,450,000 |
| Direct Operating Cost | $ 1,311 | $ 1,395 | $ 744 |
| DOC / nm | $ 4.20 | $ 3.45 | $ 2.25 |
| DOC / nm / Seat | $ 0.53 | $ 0.58 | $ 0.56 |
| Max Cruise Speed (ktas) | 312 | 404 | 330 |
| Max Range (nm) | 1560 | 1400 | 1730 |
| Useful Load (lbs) | 5145 | 3810 | 2601 |
| Total Seats | 10 | 8 | 6 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 6 | 4 |
| Max Cabin Seats | 9 | 7 | - |
| Min Crew | 1 | 1 | 1 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | Garmin G3000 |
| Flight Rules | IFR | - | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Weights | |||
| MRAMP (lbs) | 15100 | 10800 | 7430 |
| MTOW (lbs) | 15000 | 10700 | 7394 |
| MLW (lbs) | 15000 | 9900 | 7024 |
| MZFW (lbs) | 12500 | 8400 | 6032 |
| BOW (lbs) | 9955 | 6990 | 4629 |
| BEW (lbs) | 9855 | 6890 | - |
| Useful Load (lbs) | 5145 | 3810 | 2601 |
| Max Payload (lbs) | 2545 | 1410 | 1403 |
| Fuel Capacity (lbs) | 3611 | 3296 | 2017 |
| Useful Load Max Fuel (lbs) | - | 514 | - |
| Payload Max Fuel (lbs) | 1534 | 514 | 891 |
| Max Baggage Weight (lbs) | 1150 | 725 | 507 |
| Dimensions | |||
| Wingspan (ft) | 57.9 | 47.3 | 42.1 |
| Overall Height (ft) | 14.4 | 14 | - |
| Length (ft) | 46.7 | 42.6 | 35.3 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.1 |
| Aisle Step (ft) | - | 0.4 | - |
| Cabin Width (ft) | 4.5 | 4.8 | 4 |
| Cabin Width - Floor (ft) | 4.1 | 3.1 | - |
| Cabin Length (ft) | 19.5 | 11 | 13.4 |
| Cabin Length - Seating (ft) | 19.5 | 8.8 | - |
| Cabin Volume (cu. ft) | - | - | 123 |
| Baggage Volume Int. (cu. ft) | 71 | - | - |
| Baggage Volume Ext. (cu. ft) | - | 46 | - |
| Engine | |||
| No. of Engines | 1 | 2 | - |
| Manufacturer | Beechcraft | Cessna Citation | Daher TBM |
| Model | PT6A-60A | FJ44-1AP-21 | TBM 960 |
| Horsepower | 1050 | - | 850 |
| Thrust (lbs) | - | 1965 | - |
| Flat Rating | ISA + 10 | ISA + 7 | ISA + 49 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | 3600 | 3500 | 3500 |
| Fuel Capacity (gal) | 539 | 492 | - |
| Fuel Burn (lbph) | - | 516 | - |
| Avionics | |||
| Flight Deck | Rockwell Collins Pro Line Fusion | Garmin G3000 | Garmin G3000 |
| Flight Rules | IFR | - | IFR |
| FMS | 2 | 1 | - |
| Autopilot | 1 | 1 | 1 |
| PFD | 2 | 2 | 2 |
| MFD | 1 | 1 | 1 |
| GPS | 1 | 2 | 1 |
| AHRS | 1 | 2 | - |
| ADC | - | 2 | - |
| Transponder | 1 | 1 | 1 |
| VHF Com | 2 | 1 | 2 |
| VHF NAV | 2 | 1 | 2 |
| Cabin | |||
| Total Seats | 10 | 8 | 6 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 6 | 4 |
| Max Cabin Seats | 9 | 7 | - |
| Min Crew | 1 | 1 | 1 |
| Lavatory | Optional | 1 Enclosed Belted Flushing | No |
| Lavatory Location | AFT | AFT | - |
| Galley / Refreshment | Optional | No | - |
| Galley Location | FWD | - | MID |
| Crew Rest | - | No | - |
| Jump Seat | - | No | - |
| SL Cabin Altitude (ft) | - | 22027 | 14390 |
| Cabin Pressure (psi) | 6.5 | 8.5 | 6.2 |
| Other | |||
| Prop Manufacturer | Hartzell | - | - |
| Prop Description | 4-Blade Constant Feathering Reverse | - | - |
| Gear Type | Retractable | - | Retractable |
| Warranty | |||
| Airframe (Yrs) | - | 3 | - |
| Airframe (Hrs) | - | 1000 | - |
| Engine (Yrs) | - | 2 | - |
| Engine (Hrs) | - | 1000 | - |
| APU (Hrs) | - | 2000 | - |
| Performance | |||
| Max Cruise Speed (Mach) | 0.58 | 0.71 | - |
| Max Cruise Speed (ktas) | 312 | 404 | 330 |
| Long Range Cruise (Mach) | - | 0.65 | - |
| Long Range Cruise (ktas) | 235 | 370 | 252 |
| Vref (kias) | 100 | 101 | - |
| Stall Speed - Clean (kias) | 82 | - | - |
| Max Range (nm) | 1560 | 1400 | 1730 |
| Range @ 85% (nm) | - | - | 1440 |
| Range @ 75% | - | - | 1594 |
| Range Seats Full (nm) | - | 819 | - |
| Max Range Crew + 4 (nm) | 1533 | 1062 | - |
| Max Range Crew + 6 (nm) | - | 819 | - |
| Take-off FL (ft) | 3300 | 3210 | - |
| Take-Off >50ft Obst. (ft) | - | - | 2380 |
| Take-Off (5000 / ISA + 10) | 5376 | 5580 | 3475 |
| Landing >50ft Obst. (ft) | 2692 | 2590 | 2430 |
| Max Climb Rate (fpm) | 2731 | 3698 | - |
| Service Ceiling (ft) | 35000 | 41000 | 31000 |