Beechcraft King Air 260 vs Cessna Citation M2 vs Embraer Phenom 100ev vs Piper M600 Sls
The Beechcraft King Air 260 is a twin‑turboprop business aircraft valued for short‑field capability and flexibility. It typically flies roughly 1,500–1,800 nautical miles and commonly carries about 6–9 passengers depending on layout. The Cessna Citation M2 is an entry‑level light jet aimed at fast point‑to‑point trips; it generally offers about 1,200–1,500 nautical miles of range and seats around 4–7 passengers, often configured for 4–5 plus one or two in the cockpit. The Embraer Phenom 100EV is also a very light jet, similar in mission but often a bit roomier in cabin feel; it typically delivers about 1,100–1,300 nautical miles of range and usually accommodates 4–7 passengers. The Piper M600 SLS is a single‑engine turboprop positioned for owner‑pilots, trading jet speeds for simplicity and operating efficiency; it commonly reaches about 1,200–1,500 nautical miles and carries about 4–6 passengers. Overall, the King Air emphasizes payload/runway versatility, the M2 and Phenom prioritize speed, and the M600 focuses on efficient owner operation.
| Spec | Beechcraft King Air 260 | Cessna Citation M2 | Embraer Phenom 100EV | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 3.45 | $ 2.84 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 8 | 7 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Beechcraft | Cessna Citation | Embraer | Piper |
| Aircraft Name | KingAir 250 | M2 | Phenom 100EV | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 1400 | 1,178 | 1406 |
| DOC / nm / Seat | $ 0.72 | $ 0.58 | $ 0.71 | $ 0.55 |
| Max Cabin Seats | 8 | 7 | 7 | — |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3760 | 3810 | 3451 | 2200 |
| Standard Cabin Seats | 6 | 6 | 5 | 4 |
| Direct Operating Cost | $ 1,333 | $ 1,395 | $ 1,152 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | Prodigy Touch (G3000) | Garmin G3000 |
| Max Cruise Speed (ktas) | 310 | 404 | 406 | 274 |
| Base Aircraft Price (USD) | $6,450,000 | $5,150,000 | $4,250,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | 1 Enclosed Belted Flushing | 1 Flushing | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 8 | 6 | 5 |
| Max Cabin Seats | 8 | 7 | 6 | — |
| Lavatory Location | AFT | AFT | AFT | — |
| Cabin Pressure (psi) | 6.5 | 8.5 | 8.3 | 5.6 |
| Galley / Refreshment | No | No | No | Refreshment Centre |
| Standard Cabin Seats | 6 | 6 | 4 | 4 |
| SL Cabin Altitude (ft) | 15293 | 22027 | 21280 | 12600 |
| Crew Rest | — | No | No | — |
| Jump Seat | — | No | No | — |
| Galley Location | — | — | — | MID |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PT6A-52 | FJ44-1AP-21 | PW617F1-E | PT6A-42A |
| TBO (hrs) | 3600 | 3500 | 3500 | 3600 |
| Horsepower | 850 | — | — | 600 |
| Flat Rating | ISA + 37 | ISA + 7 | ISA + 8 | ISA + 55 |
| No. of Engines | 1 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 544 | 492 | — | 260 |
| Thrust (lbs) | — | 1965 | 1730 | — |
| Fuel Burn (lbph) | — | 516 | 543 | — |
| Dimensions | ||||
| Length (ft) | 43.8 | 42.6 | 42.1 | 29.7 |
| Wingspan (ft) | 57.9 | 47.3 | 40.4 | 43.2 |
| Cabin Width (ft) | 4.5 | 4.8 | 5.1 | 4.1 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.9 | 4 |
| Cabin Length (ft) | 16.7 | 11 | 11 | 12.3 |
| Overall Height (ft) | 14.8 | 14 | 14.3 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | 3.1 | 3.6 | — |
| Cabin Length - Seating (ft) | 16.7 | 8.8 | 9 | — |
| Baggage Volume Int. (cu. ft) | 55 | — | 10 | 20 |
| Aisle Step (ft) | — | 0.4 | 0.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 46 | 60 | — |
| Cabin Volume (cu. ft) | — | — | — | 165 |