Beechcraft King Air 260 vs Beechcraft Kingair Denali vs Cessna Citation M2 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx"
The Beechcraft King Air 260 is a twin‑turboprop optimized for short‑to‑medium missions, typically offering roughly 1,500–1,700 nm of range and seating commonly around 6–9 passengers depending on layout. The Beechcraft King Air Denali (in development) is a larger, faster single‑engine turboprop intended to compete at the top of the utility/owner‑flown segment, targeting about 1,600 nm range with seating typically in the 6–9 passenger class. The Cessna Citation M2 is a light twin‑jet aimed at faster, higher‑altitude trips, generally around 1,300–1,550 nm range and usually 5–7 passenger seating. The Piaggio Avanti EVO is a high‑speed twin‑turboprop with jet‑like cruise, typically about 1,700–1,900 nm of range and commonly 6–7 passengers in an executive cabin. The Pilatus PC‑12 NGX is a versatile single‑engine turboprop emphasizing payload and rough‑field capability, generally around 1,700–1,800 nm of range with typical seating of 6–9 (and higher-density configurations possible).
| Spec | Beechcraft King Air 260 | Beechcraft KingAir Denali | Cessna Citation M2 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 4.08 | $ 3.45 | — |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 11 | 8 | 8 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Beechcraft | GE® Aerospace | Cessna Citation | Piaggio |
| Aircraft Name | KingAir 250 | KingAir Denali | M2 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 1600 | 1400 | 1530 |
| DOC / nm / Seat | $ 0.72 | $ 0.68 | $ 0.58 | — |
| Max Cabin Seats | 8 | 9 | 7 | 7 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 3760 | 3280 | 3810 | 3775 |
| Standard Cabin Seats | 6 | 7 | 6 | 6 |
| Direct Operating Cost | $ 1,333 | $ 1,111 | $ 1,395 | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Garmin G3000 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 310 | 285 | 404 | 400 |
| Base Aircraft Price (USD) | $6,450,000 | $4,150,000 | $5,150,000 | $ 7,695,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | 1 Flushing | 1 Enclosed Belted Flushing | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 11 | 8 | 8 |
| Max Cabin Seats | 8 | 9 | 7 | 7 |
| Lavatory Location | AFT | AFT | AFT | — |
| Cabin Pressure (psi) | 6.5 | 5 | 8.5 | 9 |
| Galley / Refreshment | No | No | No | No |
| Standard Cabin Seats | 6 | 7 | 6 | 6 |
| SL Cabin Altitude (ft) | 15293 | 11065 | 22027 | 24000 |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| FADEC | Yes | — | Yes | Yes |
| Model | PT6A-52 | Catalyst™ | FJ44-1AP-21 | PT6A–66B |
| TBO (hrs) | 3600 | — | 3500 | 3600 |
| Horsepower | 850 | — | — | 850 |
| Flat Rating | ISA + 37 | — | ISA + 7 | ISA + 28 |
| No. of Engines | 1 | 1 | 2 | 2 |
| Fuel Capacity (gal) | 544 | — | 492 | — |
| Thrust (lbs) | — | — | 1965 | — |
| Fuel Burn (lbph) | — | — | 516 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 43.8 | 14.86 | 42.6 | 47.3 |
| Wingspan (ft) | 57.9 | 54.3 | 47.3 | 47.1 |
| Cabin Width (ft) | 4.5 | 4.5 | 4.8 | 6.1 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.8 | 5.8 |
| Cabin Length (ft) | 16.7 | 12.6 | 11 | 14.9 |
| Overall Height (ft) | 14.8 | 4.65 | 14 | 13.1 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | 3.1 | 3.5 |
| Cabin Length - Seating (ft) | 16.7 | 12.6 | 8.8 | — |
| Baggage Volume Int. (cu. ft) | 55 | 48 | — | 35.2 |
| Aisle Step (ft) | — | — | 0.4 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 46 | — |