Compare Beechcraft King Air 260 vs Beechcraft King Air 360 vs Beechcraft King Air 360ER vs Cessna SkyCourier vs Piaggio Avanti EVO
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| Manufacturer | Beechcraft | Beechcraft | Beechcraft | Cessna | Piaggio |
| Aircraft Type | KingAir 250 | KingAir 350i | KingAir 350ER | SkyCourier | Avanti EVO |
| Base Aircraft Price (USD) | $6,450,000 | $7,650,000 | $8,750,000 | $7,375,000 | $ 7,695,000 |
| Direct Operating Cost | $ 1,333 | $ 1,311 | $ 1,324 | - | - |
| DOC / nm | $ 4.30 | $ 4.20 | $ 4.37 | - | - |
| DOC / nm / Seat | $ 0.72 | $ 0.53 | $ 0.55 | - | - |
| Max Cruise Speed (ktas) | 310 | 312 | 303 | 200 | 400 |
| Max Range (nm) | 1420 | 1560 | 2338 | 900 | 1530 |
| Useful Load (lbs) | 3760 | 5145 | 6585 | - | 3775 |
| Total Seats | 8 | 10 | 10 | 21 | 8 |
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 6 | 8 | 8 | 19 | 6 |
| Max Cabin Seats | 8 | 9 | 9 | 19 | 7 |
| Min Crew | 1 | 1 | 1 | 2 | 1 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Gyro / Analog | Rockwell Collins Pro Line 21 |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Weights | |||||
| MRAMP (lbs) | 12590 | 15100 | 16600 | - | 12150 |
| MTOW (lbs) | 12500 | 15000 | 16500 | - | 12100 |
| MLW (lbs) | 12500 | 15000 | 15675 | - | 11500 |
| MZFW (lbs) | 11000 | 12500 | 13000 | - | 9800 |
| BOW (lbs) | 8830 | 9955 | 10215 | - | 8375 |
| BEW (lbs) | 8740 | 9855 | 9915 | - | 8325 |
| Useful Load (lbs) | 3760 | 5145 | 6585 | - | 3775 |
| Max Payload (lbs) | 2170 | 2545 | 2785 | 5000 | 1425 |
| Fuel Capacity (lbs) | 3645 | 3611 | 5192 | - | 2802 |
| Useful Load Max Fuel (lbs) | - | - | - | 3427 | - |
| Payload Max Fuel (lbs) | 115 | 1534 | 1193 | - | 973 |
| Max Baggage Weight (lbs) | 550 | 1150 | 1150 | - | 350 |
| Dimensions | |||||
| Wingspan (ft) | 57.9 | 57.9 | 57.9 | 72 | 47.1 |
| Overall Height (ft) | 14.8 | 14.4 | 14.4 | 19.8 | 13.1 |
| Length (ft) | 43.8 | 46.7 | 46.7 | 54.9 | 47.3 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.8 | - | 5.8 |
| Cabin Width (ft) | 4.5 | 4.5 | 4.5 | - | 6.1 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | 4.1 | - | 3.5 |
| Cabin Length (ft) | 16.7 | 19.5 | 19.5 | - | 14.9 |
| Cabin Length - Seating (ft) | 16.7 | 19.5 | 19.5 | - | - |
| Baggage Volume Int. (cu. ft) | 55 | 71 | 71 | - | 35.2 |
| Engine | |||||
| No. of Engines | 1 | 1 | 1 | 1 | 2 |
| Manufacturer | Beechcraft | Beechcraft | Beechcraft | Cessna | Piaggio |
| Model | PT6A-52 | PT6A-60A | PT6A-60A | PT6A-65SC | PT6A–66B |
| Horsepower | 850 | 1050 | 1050 | 1100 | 850 |
| Flat Rating | ISA + 37 | ISA + 10 | ISA + 10 | - | ISA + 28 |
| FADEC | Yes | Yes | Yes | Yes | Yes |
| TBO (hrs) | 3600 | 3600 | 3600 | 6000 | 3600 |
| Fuel Capacity (gal) | 544 | 539 | 775 | - | - |
| Fuel Burn (gph) | - | - | - | - | 100 |
| Avionics | |||||
| Flight Deck | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Gyro / Analog | Rockwell Collins Pro Line 21 |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| FMS | 1 | 2 | 2 | 1 | - |
| Autopilot | 1 | 1 | 1 | 1 | - |
| PFD | 2 | 2 | 2 | 2 | - |
| MFD | 1 | 1 | 1 | 1 | - |
| GPS | 1 | 1 | 1 | 1 | - |
| AHRS | 1 | 1 | 1 | - | - |
| Transponder | 1 | 1 | 1 | 1 | - |
| VHF Com | 2 | 2 | 2 | 2 | - |
| VHF NAV | 2 | 2 | 2 | 2 | - |
| Cabin | |||||
| Total Seats | 8 | 10 | 10 | 21 | 8 |
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 6 | 8 | 8 | 19 | 6 |
| Max Cabin Seats | 8 | 9 | 9 | 19 | 7 |
| Min Crew | 1 | 1 | 1 | 2 | 1 |
| Cargo Door | - | - | Optional | Yes | - |
| Lavatory | 1 Flushing | Optional | Yes (Belted Optional) | No | No |
| Lavatory Location | AFT | AFT | AFT | - | - |
| Galley / Refreshment | No | Optional | Refreshment Center | No | No |
| Galley Location | - | FWD | FWD | - | - |
| Max Cabin Altitude (ft) | - | - | - | - | 6600 |
| SL Cabin Altitude (ft) | 15293 | - | - | - | 24000 |
| Cabin Pressure (psi) | 6.5 | 6.5 | 6.5 | Un-Pressurized | 9 |
| Other | |||||
| Prop Manufacturer | Hartzell | Hartzell | Hartzell | McCauley | Hartzell |
| Prop Description | 4-Blade Constant Feathering Reverse | 4-Blade Constant Feathering Reverse | 4-Blade Constant Feathering Reverse | 4-Blade Alum Feathering Reverse | Scimitar |
| Gear Type | Retractable | Retractable | Retractable | Fixed Wheels | Retractable |
| Performance | |||||
| Max Cruise Speed (Mach) | - | 0.58 | 0.58 | - | 0.7 |
| Max Cruise Speed (ktas) | 310 | 312 | 303 | 200 | 400 |
| Long Range Cruise (ktas) | 256 | 235 | 238 | - | 318 |
| Vref (kias) | - | 100 | 104 | - | - |
| Stall Speed - Clean (kias) | 80 | 82 | 82 | - | - |
| Max Range (nm) | 1420 | 1560 | 2338 | 900 | 1530 |
| Range Seats Full (nm) | - | - | - | 400 | - |
| Max Range Crew + 4 (nm) | 1038 | 1533 | 2271 | - | - |
| Take-off FL (ft) | 2111 | 3300 | 4057 | 3300 | - |
| Take-off Roll (ft) | - | - | - | - | 3262 |
| Take-Off (5000 / ISA + 10) | 3099 | 5376 | 7675 | - | 4700 |
| Landing >50ft Obst. (ft) | 2845 | 2692 | 2728 | - | 3282 |
| Max Climb Rate (fpm) | 2450 | 2731 | 2400 | - | 2770 |
| Service Ceiling (ft) | 35000 | 35000 | 35000 | - | 41000 |