Compare Beechcraft King Air 360ER vs Daher TBM 960 vs Leonardo AW139 vs Pilatus PC-12 NGX vs Sikorsky S-76D
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| Manufacturer | Beechcraft | Daher TBM | Leonardo | Pilatus | Sikorsky |
| Aircraft Type | KingAir 350ER | TBM 960 | AW139 | PC-12 NGX | S-76D |
| Base Aircraft Price (USD) | $8,750,000 | $4,450,000 | $15,900,000 | $5,350,000 | $14,900,000 |
| Direct Operating Cost | $ 1,324 | $ 744 | $ 1,929 | $ 793 | $ 1,781 |
| DOC / nm | $ 4.37 | $ 2.25 | $ 11.69 | $ 2.78 | $ 11.49 |
| DOC / nm / Seat | $ 0.55 | $ 0.56 | $ 0.69 | $ 0.46 | $ 0.96 |
| Max Cruise Speed (ktas) | 303 | 330 | 165 | 290 | 155 |
| Max Range (nm) | 2338 | 1730 | 573 | 1866 | 441 |
| Useful Load (lbs) | 6585 | 2601 | 4701 | 3692 | - |
| Total Seats | 10 | 6 | 17 | 8 | 12 |
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 4 | 15 | 6 | 10 |
| Max Cabin Seats | 9 | - | 15 | 9 | 10 |
| Min Crew | 1 | 1 | 2 | 1 | 2 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | EFIS | Honeywell Primus Apex | Thales TopDeck |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Weights | |||||
| MRAMP (lbs) | 16600 | 7430 | - | 10495 | - |
| MTOW (lbs) | 16500 | 7394 | 15430 | 10450 | 11700 |
| MLW (lbs) | 15675 | 7024 | - | 9921 | - |
| MZFW (lbs) | 13000 | 6032 | - | 9039 | - |
| BOW (lbs) | 10215 | 4629 | 9409 | 6803 | - |
| BEW (lbs) | 9915 | - | 7985 | 6758 | - |
| Useful Load (lbs) | 6585 | 2601 | 4701 | 3692 | - |
| Max Payload (lbs) | 2785 | 1403 | - | 2235 | - |
| Fuel Capacity (lbs) | 5192 | 2017 | 3276 | 2704 | 296 |
| Useful Load Max Fuel (lbs) | - | - | 1937 | - | - |
| Payload Max Fuel (lbs) | 1193 | 891 | - | 988 | - |
| Max Baggage Weight (lbs) | 1150 | 507 | - | - | - |
| Dimensions | |||||
| Wingspan (ft) | 57.9 | 42.1 | - | 53.33 | - |
| Rotor Diameter (ft) | - | - | 54.7 | - | 44 |
| Overall Height (ft) | 14.4 | - | 16.4 | 14 | 14.5 |
| Length (ft) | 46.7 | 35.3 | 54.7 | 47.25 | 52.5 |
| Cabin Height (ft) | 4.8 | 4.1 | - | 4.9 | - |
| Cabin Width (ft) | 4.5 | 4 | - | 5 | - |
| Cabin Width - Floor (ft) | 4.1 | - | - | 4.25 | - |
| Cabin Length (ft) | 19.5 | 13.4 | - | 16.9 | - |
| Cabin Length - Seating (ft) | 19.5 | - | - | - | - |
| Cabin Volume (cu. ft) | - | 123 | 282 | - | - |
| Baggage Volume Int. (cu. ft) | 71 | - | - | 40 | - |
| Baggage Volume Ext. (cu. ft) | - | - | 120 | - | - |
| Engine | |||||
| No. of Engines | 1 | - | 2 | 1 | 1 |
| Manufacturer | Beechcraft | Daher TBM | Leonardo | Pilatus | Sikorsky |
| Model | PT6A-60A | TBM 960 | PT6C-67C | PT6E-67XP | PW210S |
| Horsepower | 1050 | 850 | 1679 | 1200 | 1077 |
| Flat Rating | ISA + 10 | ISA + 49 | - | ISA + 35 | - |
| FADEC | Yes | Yes | Yes | Yes | Yes |
| TBO (hrs) | 3600 | 3500 | 5000 | 5000 | 4000 |
| Fuel Type | - | - | JetFuel | - | JetFuel |
| Fuel Capacity (gal) | 775 | - | 414 | - | 296 |
| Usable Fuel (gal) | - | - | - | 402 | - |
| Avionics | |||||
| Flight Deck | Rockwell Collins Pro Line Fusion | Garmin G3000 | EFIS | Honeywell Primus Apex | Thales TopDeck |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| FMS | 2 | - | 2 | 1 | 1 |
| Autopilot | 1 | 1 | 2 | 1 | 1 |
| PFD | 2 | 2 | - | 2 | 2 |
| MFD | 1 | 1 | - | 1 | 2 |
| GPS | 1 | 1 | 1 | 1 | 1 |
| AHRS | 1 | - | - | 1 | - |
| Transponder | 1 | 1 | 1 | 1 | 1 |
| VHF Com | 2 | 2 | 1 | 2 | 1 |
| VHF NAV | 2 | 2 | 1 | 2 | 1 |
| Cabin | |||||
| Total Seats | 10 | 6 | 17 | 8 | 12 |
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 4 | 15 | 6 | 10 |
| Max Cabin Seats | 9 | - | 15 | 9 | 10 |
| Min Crew | 1 | 1 | 2 | 1 | 2 |
| Cargo Door | Optional | - | - | Yes | - |
| Lavatory | Yes (Belted Optional) | No | - | Optional | - |
| Lavatory Location | AFT | - | - | FWD | - |
| Galley / Refreshment | Refreshment Center | - | - | No | - |
| Galley Location | FWD | MID | - | - | - |
| SL Cabin Altitude (ft) | - | 14390 | - | 13100 | - |
| Cabin Pressure (psi) | 6.5 | 6.2 | - | 5.8 | - |
| Other | |||||
| Prop Manufacturer | Hartzell | - | - | Hartzell | - |
| Prop Description | 4-Blade Constant Feathering Reverse | - | - | 5-Blade Comp | - |
| Gear Type | Retractable | Retractable | Retractable Wheels | Retractable | High Skids |
| Rotorhead | - | - | 5-Blade Articulated | - | 4-Blade Articulated |
| Tail Rotor | - | - | 4-Blade | - | 4-Blade |
| Performance | |||||
| Max Cruise Speed (Mach) | 0.58 | - | - | - | - |
| Max Cruise Speed (ktas) | 303 | 330 | 165 | 290 | 155 |
| Long Range Cruise (ktas) | 238 | 252 | 140 | 225 | 155 |
| Vref (kias) | 104 | - | - | - | - |
| Max Speed (Vne) | - | - | 167 | - | - |
| Stall Speed - Clean (kias) | 82 | - | - | - | - |
| Stall Speed - Flaps (kias) | - | - | - | 67 | - |
| Max Range (nm) | 2338 | 1730 | 573 | 1866 | 441 |
| Range @ 85% (nm) | - | 1440 | - | - | - |
| Range @ 75% | - | 1594 | - | - | - |
| Range Seats Full (nm) | - | - | 302 | - | 441 |
| Max Range Crew + 4 (nm) | 2271 | - | - | 1803 | - |
| Max Range Crew + 6 (nm) | - | - | - | 1568 | - |
| Max Range Crew + 8 (nm) | - | - | - | 1057 | - |
| Take-off FL (ft) | 4057 | - | - | - | - |
| Take-Off >50ft Obst. (ft) | - | 2380 | - | 2602 | - |
| Take-Off (5000 / ISA + 10) | 7675 | 3475 | - | 4270 | - |
| Landing >50ft Obst. (ft) | 2728 | 2430 | - | 2170 | - |
| Max Climb Rate (fpm) | 2400 | - | 2140 | 1920 | - |
| Service Ceiling (ft) | 35000 | 31000 | 20000 | 30000 | - |
| Hover IGE (ft) | - | - | 15360 | - | - |
| Hover OGE (ft) | - | - | 8130 | - | - |