Compare Beechcraft King Air 360 vs Bombardier Challenger 650 vs Cessna Citation Latitude vs Cessna Citation XLS+
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| Manufacturer | Beechcraft | Bombardier | Cessna Citation | Cessna Citation |
| Aircraft Type | KingAir 350i | Challenger 650 | Latitude | XLS+ |
| Base Aircraft Price (USD) | $7,650,000 | $32,400,000 | $19,305,000 | $15,500,000 |
| Direct Operating Cost | $ 1,311 | $ 3,365 | $ 2,936 | $ 2,303 |
| DOC / nm | $ 4.20 | $ 7.16 | $ 6.80 | $ 5.34 |
| DOC / nm / Seat | $ 0.53 | $ 0.80 | $ 0.85 | $ 0.67 |
| Max Cruise Speed (ktas) | 312 | 470 | 458 | 430 |
| Max Range (nm) | 1560 | 4085 | 2731 | 1906 |
| Useful Load (lbs) | 5145 | 21050 | 12394 | 7540 |
| Total Seats | 10 | 11 | 10 | 10 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 9 | 8 | 8 |
| Max Cabin Seats | 9 | 12 | 9 | 9 |
| Min Crew | 1 | 2 | 2 | 2 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line 21 Advanced | Garmin G5000 | Rockwell Collins Pro Line 21 |
| Flight Rules | IFR | - | - | - |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Weights | ||||
| MRAMP (lbs) | 15100 | 48300 | 31050 | 20400 |
| MTOW (lbs) | 15000 | 48200 | 30800 | 20200 |
| MLW (lbs) | 15000 | 38000 | 27575 | 18700 |
| MZFW (lbs) | 12500 | 32000 | 21200 | 16000 |
| BOW (lbs) | 9955 | 27250 | 18656 | 12860 |
| BEW (lbs) | 9855 | 27150 | 18406 | 12660 |
| Useful Load (lbs) | 5145 | 21050 | 12394 | 7540 |
| Max Payload (lbs) | 2545 | 3750 | 2544 | - |
| Fuel Capacity (lbs) | 3611 | 19852 | 11394 | 6740 |
| Useful Load Max Fuel (lbs) | - | - | 1000 | 2240 |
| Payload Max Fuel (lbs) | 1534 | 1198 | 1000 | 800 |
| Max Baggage Weight (lbs) | 1150 | 900 | 1245 | 800 |
| Dimensions | ||||
| Wingspan (ft) | 57.9 | 64.4 | 72.3 | 56.3 |
| Overall Height (ft) | 14.4 | 20.7 | 20.9 | 17.2 |
| Length (ft) | 46.7 | 68.4 | 62 | 52.5 |
| Cabin Height (ft) | 4.8 | 6 | 6 | 5.7 |
| Aisle Step (ft) | - | Flat Floor | Flat Floor | 0.7 |
| Cabin Width (ft) | 4.5 | 7.9 | 6.4 | 5.5 |
| Cabin Width - Floor (ft) | 4.1 | 6.9 | 4.4 | 3.9 |
| Cabin Length (ft) | 19.5 | 25.6 | 21.8 | 18.5 |
| Cabin Length - Seating (ft) | 19.5 | 15.4 | 15.9 | 14.3 |
| Baggage Volume Int. (cu. ft) | 71 | 112 | 27 | 10 |
| Baggage Volume Ext. (cu. ft) | - | - | 100 | 80 |
| Engine | ||||
| No. of Engines | 1 | 2 | 2 | 2 |
| Manufacturer | Beechcraft | Bombardier | Cessna Citation | Cessna Citation |
| Model | PT6A-60A | CF34-3B MTO | PW306D1 | PW545C |
| Horsepower | 1050 | - | - | - |
| Thrust (lbs) | - | 9220 | 5907 | 4119 |
| Flat Rating | ISA + 10 | ISA + 15 | ISA + 15 | ISA + 10 |
| FADEC | Yes | Yes | Yes | Yes |
| TBO (hrs) | 3600 | On-Condition | 6000 | 5000 |
| Fuel Capacity (gal) | 539 | - | 1700 | - |
| Fuel Burn (lbph) | - | - | 1114 | - |
| Avionics | ||||
| Flight Deck | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line 21 Advanced | Garmin G5000 | Rockwell Collins Pro Line 21 |
| Flight Rules | IFR | - | - | - |
| FMS | 2 | 2 | 1 | 1 |
| Autopilot | 1 | 1 | 1 | 1 |
| PFD | 2 | 2 | 2 | 2 |
| MFD | 1 | 2 | 1 | 2 |
| GPS | 1 | 2 | 1 | 1 |
| AHRS | 1 | 2 | 1 | 2 |
| ADC | - | 2 | - | 2 |
| Transponder | 1 | 2 | 1 | 1 |
| VHF Com | 2 | 2 | 1 | 1 |
| VHF NAV | 2 | 2 | 1 | 1 |
| Cabin | ||||
| Total Seats | 10 | 11 | 10 | 10 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 9 | 8 | 8 |
| Max Cabin Seats | 9 | 12 | 9 | 9 |
| Min Crew | 1 | 2 | 2 | 2 |
| Lavatory | Optional | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | 1 Enclosed Belted Flushing |
| Lavatory Location | AFT | FWD / AFT | AFT | AFT |
| Galley / Refreshment | Optional | Galley | Galley | Galley |
| Galley Location | FWD | FWD | FWD | FWD |
| Crew Rest | - | Yes | No | No |
| Jump Seat | - | Yes | No | No |
| Max Cabin Altitude (ft) | - | - | 5,950 | - |
| SL Cabin Altitude (ft) | - | 23000 | 26800 | 25230 |
| Cabin Pressure (psi) | 6.5 | 8.8 | 9.7 | 9.3 |
| Other | ||||
| Prop Manufacturer | Hartzell | - | - | - |
| Prop Description | 4-Blade Constant Feathering Reverse | - | - | - |
| APU Manufacturer | - | - | Honeywell | Honeywell |
| APU Model | - | - | RE100 | RE100 |
| APU TBO (hrs) | - | - | - | - |
| Gear Type | Retractable | - | - | - |
| Warranty | ||||
| Airframe (Yrs) | - | 3 | 3 | 3 |
| Airframe (Hrs) | - | 1000 | 1000 | 1000 |
| Engine (Yrs) | - | 2 | 2 | 2 |
| Engine (Hrs) | - | 1000 | 1000 | 1000 |
| APU (Hrs) | - | 2000 | 2000 | 2000 |
| Performance | ||||
| Max Cruise Speed (Mach) | 0.58 | 0.82 | 0.8 | 0.75 |
| Max Cruise Speed (ktas) | 312 | 470 | 458 | 430 |
| Long Range Cruise (Mach) | - | 0.8 | 0.71 | 0.71 |
| Long Range Cruise (ktas) | 235 | 458 | 404 | 404 |
| Vref (kias) | 100 | 117 | 115 | 106 |
| Stall Speed - Clean (kias) | 82 | - | - | - |
| Max Range (nm) | 1560 | 4085 | 2731 | 1906 |
| Max Range Crew + 4 (nm) | 1533 | 4011 | 2700 | 1841 |
| Max Range Crew + 6 (nm) | - | 4011 | 2583 | 1694 |
| Max Range Crew + 8 (nm) | - | - | 2451 | 1536 |
| Take-off FL (ft) | 3300 | 5640 | 3580 | 3560 |
| Take-Off (5000 / ISA + 10) | 5376 | - | 5070 | 5430 |
| Landing Roll (ft) | - | 2402 | 2480 | 2740 |
| Landing >50ft Obst. (ft) | 2692 | - | - | 3180 |
| Max Climb Rate (fpm) | 2731 | 4345 | 2313 | 3500 |
| Service Ceiling (ft) | 35000 | 41000 | 45000 | 45000 |