Beechcraft King Air 260 vs Piper M500
The Beechcraft King Air 260 and Piper M500 sit in different turboprop categories, which shapes their capabilities. The King Air 260 is a twin‑engine turboprop in the light/entry-level business twin class, aimed at higher redundancy, strong short-field utility, and flexible cabin use for corporate or special-mission flying. The Piper M500 is a single‑engine turboprop in the personal/business “M‑Class” category, optimized for owner-operators seeking simpler operation and lower operating complexity than a twin. In range terms, the King Air 260 is generally positioned for longer legs, with typical published maximum range around roughly 1,700 nautical miles depending on payload and conditions, while the M500 is usually quoted around roughly 1,000 nautical miles, again varying with reserves, speed, and loading. Passenger capacity also differs: a King Air 260 commonly carries six to nine passengers in addition to one or two pilots depending on configuration, whereas the M500 is typically arranged for one pilot plus up to five passengers, with four to five passengers being more typical when balancing comfort and baggage.
| Spec | Beechcraft King Air 260 | Piper M500 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.30 | $ 3.11 |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Beechcraft | Piper |
| Aircraft Name | KingAir 250 | M500 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 1000 |
| DOC / nm / Seat | $ 0.72 | $ 0.78 |
| Max Cabin Seats | 8 | — |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3760 | 1698 |
| Standard Cabin Seats | 6 | 4 |
| Direct Operating Cost | $ 1,333 | $ 579 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 310 | 260 |
| Base Aircraft Price (USD) | $6,450,000 | $2,122,600 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Flushing | No |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 5 |
| Max Cabin Seats | 8 | — |
| Lavatory Location | AFT | — |
| Cabin Pressure (psi) | 6.5 | 5.5 |
| Galley / Refreshment | No | Refreshment Centre |
| Standard Cabin Seats | 6 | 4 |
| SL Cabin Altitude (ft) | 15293 | 12600 |
| Galley Location | — | MID |
| Max Cabin Altitude (ft) | — | 8244 |
| Engine | ||
| FADEC | Yes | No |
| Model | PT6A-52 | PT6A-42A |
| TBO (hrs) | 3600 | 3600 |
| Horsepower | 850 | 500 |
| Flat Rating | ISA + 37 | ISA + 55 |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 544 | 170 |
| Dimensions | ||
| Length (ft) | 43.8 | 29.6 |
| Wingspan (ft) | 57.9 | 43.2 |
| Cabin Width (ft) | 4.5 | 4.1 |
| Cabin Height (ft) | 4.8 | 4 |
| Cabin Length (ft) | 16.7 | 12.3 |
| Overall Height (ft) | 14.8 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | — |
| Cabin Length - Seating (ft) | 16.7 | — |
| Baggage Volume Int. (cu. ft) | 55 | 20 |
| Cabin Volume (cu. ft) | — | 165 |