Beechcraft King Air 360er vs Beechcraft Kingair Denali vs Cessna Grand Caravan Ex vs Cessna Skycourier
The Beechcraft King Air 360ER and the Beechcraft King Air Denali are both pressurized twin‑engine turboprops positioned as higher‑end business/utility aircraft, while the Cessna Grand Caravan EX and the Cessna SkyCourier are primarily utility/regional turboprops optimized for simple operations and cargo flexibility. In category terms, the 360ER is an in‑service twin‑turboprop with a proven corporate and special‑missions footprint; the Denali is a newer‑generation, single‑engine turboprop in the upscale “large single” class. For range, the King Air 360ER is typically the longest‑leg option among these, suited to extended missions; the Denali is also designed for strong range for a single, generally ahead of the Caravan class but typically below the 360ER. The Grand Caravan EX offers solid regional range for short to mid sectors, while the SkyCourier is oriented to shorter regional legs with payload and cycle efficiency emphasized. Passenger capacity generally runs highest on the SkyCourier (commuter configurations commonly around the high‑teens), followed by the Grand Caravan EX (typically up to the low‑teens), while the King Air 360ER and Denali are usually configured for fewer passengers in more spacious executive layouts.
| Spec | Beechcraft King Air 360ER | Beechcraft KingAir Denali | Cessna Grand Caravan EX | Cessna SkyCourier |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.37 | $ 4.08 | $ 3.15 | — |
| Min Crew | 1 | 1 | 1 | 2 |
| Total Seats | 10 | 11 | 10 | 21 |
| Flight Rules | IFR | IFR | VFR | IFR |
| Manufacturer | Beechcraft | GE® Aerospace | Cessna | Cessna |
| Aircraft Name | KingAir 350ER | KingAir Denali | Grand Caravan EX | SkyCourier |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 2338 | 1600 | 964 | 900 |
| DOC / nm / Seat | $ 0.55 | $ 0.68 | $ 0.39 | — |
| Max Cabin Seats | 9 | 9 | 12 | 19 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6585 | 3280 | 3332 | — |
| Standard Cabin Seats | 8 | 7 | 8 | 19 |
| Direct Operating Cost | $ 1,324 | $ 1,111 | $ 614 | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi | Gyro / Analog |
| Max Cruise Speed (ktas) | 303 | 285 | 195 | 200 |
| Base Aircraft Price (USD) | $8,750,000 | $4,150,000 | $2,695,000 | $7,375,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Yes (Belted Optional) | 1 Flushing | No | No |
| Min Crew | 1 | 1 | 1 | 2 |
| Cargo Door | Optional | — | Yes | Yes |
| Total Seats | 10 | 11 | 10 | 21 |
| Galley Location | FWD | — | — | — |
| Max Cabin Seats | 9 | 9 | 12 | 19 |
| Lavatory Location | AFT | AFT | — | — |
| Cabin Pressure (psi) | 6.5 | 5 | Un-Pressurized | Un-Pressurized |
| Galley / Refreshment | Refreshment Center | No | No | No |
| Standard Cabin Seats | 8 | 7 | 8 | 19 |
| SL Cabin Altitude (ft) | — | 11065 | — | — |
| Engine | ||||
| FADEC | Yes | — | Yes | Yes |
| Model | PT6A-60A | Catalyst™ | PT6A-140 | PT6A-65SC |
| TBO (hrs) | 3600 | — | 4000 | 6000 |
| Horsepower | 1050 | — | 867 | 1100 |
| Flat Rating | ISA + 10 | — | ISA + 24 | — |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 775 | — | 335 | — |
| Dimensions | ||||
| Length (ft) | 46.7 | 14.86 | 41.6 | 54.9 |
| Wingspan (ft) | 57.9 | 54.3 | 52.1 | 72 |
| Cabin Width (ft) | 4.5 | 4.5 | 5.4 | — |
| Cabin Height (ft) | 4.8 | 4.8 | 4.5 | — |
| Cabin Length (ft) | 19.5 | 12.6 | 16.8 | — |
| Overall Height (ft) | 14.4 | 4.65 | 15.1 | 19.8 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | — | — |
| Cabin Length - Seating (ft) | 19.5 | 12.6 | — | — |
| Baggage Volume Int. (cu. ft) | 71 | 48 | 32 | — |