Beechcraft King Air 260 vs Beechcraft King Air 360 vs Cessna Caravan
The Beechcraft King Air 260 and King Air 360 are twin‑engine pressurized turboprops in the light business/utility category, while the Cessna Caravan is a single‑engine turboprop commonly used for regional utility, cargo, and short‑field operations. In range terms, the King Air 260 is typically suited to mid‑range missions, roughly around the 1,500–1,700 nautical mile class depending on load and conditions, and the King Air 360 generally stretches farther, often around the 1,700–1,800+ nautical mile class, again mission‑dependent. The Caravan’s range varies widely with configuration, but it is generally shorter for passenger missions than the King Airs, commonly around the ~900–1,200 nautical mile class. Passenger capacity also differs: King Air 260 and 360 interiors are commonly configured for about 6–9 passengers in executive layouts (with maximum seating higher in commuter arrangements), whereas the Caravan typically carries about 9 passengers in standard commuter seating, with flexibility to trade seats for cargo.
| Spec | Beechcraft King Air 260 | Beechcraft King Air 360 | Cessna Caravan |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 4.20 | $ 3.07 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 8 | 10 | 10 |
| Flight Rules | IFR | IFR | VFR |
| Manufacturer | Beechcraft | Beechcraft | Cessna |
| Aircraft Name | KingAir 250 | KingAir 350i | Caravan |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 1560 | 1070 |
| DOC / nm / Seat | $ 0.72 | $ 0.53 | $ 0.38 |
| Max Cabin Seats | 8 | 9 | 9 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3760 | 5145 | 3305 |
| Standard Cabin Seats | 6 | 8 | 8 |
| Direct Operating Cost | $ 1,333 | $ 1,311 | $ 571 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 310 | 312 | 186 |
| Base Aircraft Price (USD) | $6,450,000 | $7,650,000 | $2,355,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Flushing | Optional | No |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 8 | 10 | 10 |
| Max Cabin Seats | 8 | 9 | 9 |
| Lavatory Location | AFT | AFT | — |
| Cabin Pressure (psi) | 6.5 | 6.5 | Un-Pressurized |
| Galley / Refreshment | No | Optional | No |
| Standard Cabin Seats | 6 | 8 | 8 |
| SL Cabin Altitude (ft) | 15293 | — | — |
| Galley Location | — | FWD | — |
| Cargo Door | — | — | Yes |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PT6A-52 | PT6A-60A | PT6A-114A |
| TBO (hrs) | 3600 | 3600 | 3600 |
| Horsepower | 850 | 1050 | 675 |
| Flat Rating | ISA + 37 | ISA + 10 | ISA + 31 |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 544 | 539 | — |
| Dimensions | |||
| Length (ft) | 43.8 | 46.7 | 37.6 |
| Wingspan (ft) | 57.9 | 57.9 | 52.1 |
| Cabin Width (ft) | 4.5 | 4.5 | 5.4 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.5 |
| Cabin Length (ft) | 16.7 | 19.5 | 12.8 |
| Overall Height (ft) | 14.8 | 14.4 | 15 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | — |
| Cabin Length - Seating (ft) | 16.7 | 19.5 | — |
| Baggage Volume Int. (cu. ft) | 55 | 71 | 32 |