Beechcraft Kingair Denali vs Leonardo Aw139 vs Robinson Helicopters R66
The Beechcraft King Air Denali is a fixed‑wing, single‑engine turboprop airplane aimed at efficient regional travel between runways. It is expected to offer roughly 1,600 nautical miles of range (depending on configuration and reserves) and typically seats about 6 to 9 passengers in an executive layout. The Leonardo AW139 is a twin‑engine, medium helicopter designed for offshore transport, search and rescue, and corporate/VIP missions where vertical lift and cabin volume matter more than runway efficiency. Its practical range is commonly on the order of about 500 to 600 nautical miles, and it can carry up to around 15 passengers in high‑density seating, or fewer in VIP/mission configurations. The Robinson R66 is a light, single‑engine helicopter focused on lower operating costs and simpler missions such as utility work, training, and private transport. Typical range is roughly 300 to 350 nautical miles, and passenger capacity is 4 plus 1 pilot (five seats total).
| Spec | Beechcraft KingAir Denali | AGUSTA / LEONARDO AW139 | ROBINSON R66 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.08 | $ 11.69 | $ 3.49 |
| Min Crew | 1 | 2 | 1 |
| Total Seats | 11 | 17 | 5 |
| Flight Rules | IFR | IFR | VFR |
| Manufacturer | GE® Aerospace | Leonardo | Robinson Helicopters |
| Aircraft Name | KingAir Denali | AW139 | R66 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1600 | 573 | 350 |
| DOC / nm / Seat | $ 0.68 | $ 0.69 | $ 0.70 |
| Max Cabin Seats | 9 | 15 | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3280 | 4701 | 1355 |
| Standard Cabin Seats | 7 | 15 | 3 |
| Direct Operating Cost | $ 1,111 | $ 1,929 | $ 384 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | EFIS | Gyro / Analog |
| Max Cruise Speed (ktas) | 285 | 165 | 110 |
| Base Aircraft Price (USD) | $4,150,000 | $15,900,000 | $ 920,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Flushing | — | — |
| Min Crew | 1 | 2 | 1 |
| Total Seats | 11 | 17 | 5 |
| Max Cabin Seats | 9 | 15 | — |
| Lavatory Location | AFT | — | — |
| Cabin Pressure (psi) | 5 | — | — |
| Galley / Refreshment | No | — | — |
| Standard Cabin Seats | 7 | 15 | 3 |
| SL Cabin Altitude (ft) | 11065 | — | — |
| Engine | |||
| Model | Catalyst™ | PT6C-67C | RR300 |
| No. of Engines | 1 | 2 | 1 |
| FADEC | — | Yes | No |
| Fuel Type | — | JetFuel | JetFuel |
| TBO (hrs) | — | 5000 | 2000 |
| Horsepower | — | 1679 | 300 |
| Fuel Capacity (gal) | — | 414 | 73.6 |
| Dimensions | |||
| Length (ft) | 14.86 | 54.7 | 38.3 |
| Wingspan (ft) | 54.3 | — | — |
| Cabin Width (ft) | 4.5 | — | — |
| Cabin Height (ft) | 4.8 | — | — |
| Cabin Length (ft) | 12.6 | — | — |
| Overall Height (ft) | 4.65 | 16.4 | 11.4 |
| Cabin Width - Floor (ft) | 4.1 | — | — |
| Cabin Length - Seating (ft) | 12.6 | — | — |
| Baggage Volume Int. (cu. ft) | 48 | — | — |
| Rotor Diameter (ft) | — | 54.7 | 33 |
| Cabin Volume (cu. ft) | — | 282 | 50 |
| Baggage Volume Ext. (cu. ft) | — | 120 | 18 |