Beechcraft King Air 260 vs Beechcraft Kingair Denali vs Cessna Caravan vs Cessna Grand Caravan Ex
The Beechcraft King Air 260 and the Beechcraft King Air Denali are pressurized, twin‑engine turboprops aimed at higher-speed business and utility missions, while the Cessna Caravan and Cessna Grand Caravan EX are single‑engine turboprops optimized for rugged, short-field, and lower-cost regional hauling. In category terms, the King Air 260 is an in-service light twin turboprop, the Denali is a newer-generation (still emerging) single‑engine turboprop positioned as a faster, more upscale alternative to utility singles, and both Caravans are proven utility singles. For range, the King Air 260 generally offers the longest legs in this group (roughly around 1,500–1,700 nm depending on configuration), the Denali is typically cited around the mid‑1,000 nm class, and the Caravan and Grand Caravan EX are usually around the ~900–1,200 nm class depending on payload and reserves. For passenger capacity, the King Air 260 commonly seats about 7–9, the Denali is typically around 8–10, the Caravan about 9–10, and the stretched Grand Caravan EX usually about 10–14 (operator layout dependent).
| Spec | Beechcraft King Air 260 | Beechcraft KingAir Denali | Cessna Caravan | Cessna Grand Caravan EX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 4.08 | $ 3.07 | $ 3.15 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 11 | 10 | 10 |
| Flight Rules | IFR | IFR | VFR | VFR |
| Manufacturer | Beechcraft | GE® Aerospace | Cessna | Cessna |
| Aircraft Name | KingAir 250 | KingAir Denali | Caravan | Grand Caravan EX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 1600 | 1070 | 964 |
| DOC / nm / Seat | $ 0.72 | $ 0.68 | $ 0.38 | $ 0.39 |
| Max Cabin Seats | 8 | 9 | 9 | 12 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3760 | 3280 | 3305 | 3332 |
| Standard Cabin Seats | 6 | 7 | 8 | 8 |
| Direct Operating Cost | $ 1,333 | $ 1,111 | $ 571 | $ 614 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 310 | 285 | 186 | 195 |
| Base Aircraft Price (USD) | $6,450,000 | $4,150,000 | $2,355,000 | $2,695,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | 1 Flushing | No | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 11 | 10 | 10 |
| Max Cabin Seats | 8 | 9 | 9 | 12 |
| Lavatory Location | AFT | AFT | — | — |
| Cabin Pressure (psi) | 6.5 | 5 | Un-Pressurized | Un-Pressurized |
| Galley / Refreshment | No | No | No | No |
| Standard Cabin Seats | 6 | 7 | 8 | 8 |
| SL Cabin Altitude (ft) | 15293 | 11065 | — | — |
| Cargo Door | — | — | Yes | Yes |
| Engine | ||||
| FADEC | Yes | — | Yes | Yes |
| Model | PT6A-52 | Catalyst™ | PT6A-114A | PT6A-140 |
| TBO (hrs) | 3600 | — | 3600 | 4000 |
| Horsepower | 850 | — | 675 | 867 |
| Flat Rating | ISA + 37 | — | ISA + 31 | ISA + 24 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 544 | — | — | 335 |
| Dimensions | ||||
| Length (ft) | 43.8 | 14.86 | 37.6 | 41.6 |
| Wingspan (ft) | 57.9 | 54.3 | 52.1 | 52.1 |
| Cabin Width (ft) | 4.5 | 4.5 | 5.4 | 5.4 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.5 | 4.5 |
| Cabin Length (ft) | 16.7 | 12.6 | 12.8 | 16.8 |
| Overall Height (ft) | 14.8 | 4.65 | 15 | 15.1 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | — | — |
| Cabin Length - Seating (ft) | 16.7 | 12.6 | — | — |
| Baggage Volume Int. (cu. ft) | 55 | 48 | 32 | 32 |