Beechcraft King Air 260 vs Cessna Citation Cj4 vs Embraer Phenom 300e vs Md Helicopters Md 600n vs Md Helicopters Md 902 Exlplorer vs Pilatus Pc 12 Ngx
The Beechcraft King Air 260 and Pilatus PC-12 NGX are pressurized turboprops suited to short and mid-range missions, generally offering around 1,500–1,800 nautical miles of range with typical seating for about 6–9 passengers, with the PC-12 often optimized for flexible cabin layouts and single-pilot-style utility while the King Air emphasizes twin‑engine redundancy. The Cessna Citation CJ4 and Embraer Phenom 300E are light business jets, faster and typically longer-legged than the turboprops, commonly around 1,900–2,200 nautical miles, and usually configured for roughly 6–10 passengers depending on cabin and amenities. The Phenom 300E is often positioned as the higher-performing light jet in speed and efficiency, while the CJ4 is known for a slightly roomier cabin feel in its class. The MD Helicopters MD 600N and MD 902 Explorer are turbine helicopters for short-range point-to-point access, typically a few hundred nautical miles, carrying about 5–8 passengers; the MD 902’s NOTAR anti-torque system reduces tail-rotor hazards and can lower noise signatures.
| Spec | Beechcraft King Air 260 | Cessna Citation CJ4 | Embraer Phenom 300E | MD Helicopters MD 600N | MD Helicopters MD 902 Exlplorer | Pilatus PC-12 NGX |
|---|---|---|---|---|---|---|
| Summary | ||||||
| Cockpit | 2 | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 4.37 | $ 3.88 | $ 4.06 | $ 7.54 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 9 | 10 | 6 | 8 | 8 |
| Flight Rules | IFR | — | — | VFR | VFR | IFR |
| Manufacturer | Beechcraft | Cessna Citation | Embraer | MD Helicotpers | MD Helicotpers | Pilatus |
| Aircraft Name | KingAir 250 | CJ4 | Phenom 300E | MD 600N | MD 902 Exlplorer | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 2170 | 2,010 | 341 | 317 | 1803 |
| DOC / nm / Seat | $ 0.72 | $ 0.62 | $ 0.55 | $ 0.68 | $ 0.94 | $ 0.46 |
| Max Cabin Seats | 8 | 8 | 10 | 5 | 6 | 9 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3760 | 6914 | 6914 | 2000 | 3125 | — |
| Standard Cabin Seats | 6 | 7 | 6 | 5 | 6 | 6 |
| Direct Operating Cost | $ 1,333 | $ 1,970 | $ 1,758 | $ 545 | $ 988 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line 21 | Prodigy Touch (G3000) | Gyro / Analog | Garmin G500H | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 310 | 440 | 464 | 134 | 131 | 290 |
| Base Aircraft Price (USD) | $6,450,000 | $11,290,000 | $9,650,000 | $3,400,000 | $7,250,000 | $5,350,000 |
| Cabin | ||||||
| Cockpit | 2 | 2 | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | 1 Enclosed Belted Flushing | 1 Enclosed Flushing | — | — | Optional |
| Min Crew | 1 | 1 | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 9 | 9 | 6 | 8 | 8 |
| Max Cabin Seats | 8 | 8 | 9 | 5 | 6 | 9 |
| Lavatory Location | AFT | AFT | AFT | — | — | FWD |
| Cabin Pressure (psi) | 6.5 | 9 | 9.4 | — | — | 5.8 |
| Galley / Refreshment | No | Galley | Galley | — | — | No |
| Standard Cabin Seats | 6 | 7 | 7 | 5 | 6 | 6 |
| SL Cabin Altitude (ft) | 15293 | 24005 | 25560 | — | — | 13100 |
| Crew Rest | — | No | No | — | — | — |
| Jump Seat | — | No | No | — | — | — |
| Galley Location | — | FWD | FWD | — | — | — |
| Cargo Door | — | — | — | — | — | Yes |
| Engine | ||||||
| FADEC | Yes | Yes | Yes | No | No | Yes |
| Model | PT6A-52 | FJ44-4A | Canada PW535E1 | 250-C47 | PW207E | PT6E-67XP |
| TBO (hrs) | 3600 | 5000 | 5000 | 2000 | 4000 | 5000 |
| Horsepower | 850 | — | — | 715 | 710 | 1200 |
| Flat Rating | ISA + 37 | ISA + 11 | ISA + 15 | — | — | ISA + 35 |
| No. of Engines | 1 | 2 | 2 | 1 | 2 | 1 |
| Fuel Capacity (gal) | 544 | 870 | — | 118 | 159 | — |
| Thrust (lbs) | — | 3621 | 3360 | — | — | — |
| Fuel Burn (lbph) | — | 757 | 757 | — | — | — |
| Fuel Type | — | — | — | JetFuel | JetFuel | — |
| Fuel Burn (gph) | — | — | — | 41 | 65 | — |
| Usable Fuel (gal) | — | — | — | — | — | 402 |
| Dimensions | ||||||
| Length (ft) | 43.8 | 53.4 | 51.2 | 36.9 | 40.6 | 47.25 |
| Wingspan (ft) | 57.9 | 50 | 52.16 | — | — | 53.33 |
| Cabin Width (ft) | 4.5 | 4.8 | 5.1 | — | — | 5 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.9 | — | — | 4.9 |
| Cabin Length (ft) | 16.7 | 17.2 | 17.2 | — | — | 16.9 |
| Overall Height (ft) | 14.8 | 15.5 | 16.75 | 9.7 | 12 | 14 |
| Cabin Width - Floor (ft) | 4.1 | 3.1 | 3.6 | — | — | 4.25 |
| Cabin Length - Seating (ft) | 16.7 | 14.8 | 14.8 | — | — | — |
| Baggage Volume Int. (cu. ft) | 55 | 7 | 10 | — | — | 40 |
| Aisle Step (ft) | — | 0.4 | 0.3 | — | — | — |
| Baggage Volume Ext. (cu. ft) | — | 70 | 74 | — | — | — |
| Rotor Diameter (ft) | — | — | — | 27.5 | 33.9 | — |