Airbus Helicopters H160 vs Beechcraft King Air 360 vs Bell 525 Relentless vs Leonardo Aw139 vs Piaggio Avanti Evo
The Airbus Helicopters H160 and Leonardo AW139 are medium twin helicopters optimized for vertical access; the H160 is typically configured for about 6–12 passengers with roughly 450–500 nm range, while the AW139 commonly carries about 8–15 passengers with around 550–600 nm range depending on fit and reserves. The Bell 525 Relentless is a larger, long-range super-medium helicopter, generally aimed at about 12–16 passengers with roughly 600–700+ nm range, emphasizing offshore-style legs and higher cruise speed for a rotorcraft. The Beechcraft King Air 360 and Piaggio Avanti EVO are pressurized fixed‑wing turboprops designed for runway-to-runway efficiency and longer legs than most helicopters. The King Air 360 typically seats about 6–9 passengers with about 1,500+ nm range, prioritizing short-field capability and utility. The Avanti EVO usually carries about 7–9 passengers with roughly 1,300–1,700 nm range and stands out for higher cruise speed and cabin comfort relative to many turboprops. Actual figures vary by payload, reserves, and interior.
| Spec | AIRBUS H160 | Beechcraft King Air 360 | Bell 525 Relentless | AGUSTA / LEONARDO AW139 | Piaggio Avanti EVO |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 | 2 | 1 |
| Total Seats | 14 | 10 | 18 | 17 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Beechcraft | Bell | Leonardo | Piaggio |
| Aircraft Name | H160 | KingAir 350i | 525 Relentless | AW139 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 460 | 1560 | 580 | 573 | 1530 |
| Max Cabin Seats | 12 | 9 | 16 | 15 | 7 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3992 | 5145 | 6675 | 4701 | 3775 |
| Standard Cabin Seats | 12 | 8 | 16 | 15 | 6 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line Fusion | Garmin G5000H | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 155 | 312 | 160 | 165 | 400 |
| Base Aircraft Price (USD) | $14,000,000 | $7,650,000 | $15,000,000 | $15,900,000 | $ 7,695,000 |
| DOC / nm | — | $ 4.20 | — | $ 11.69 | — |
| DOC / nm / Seat | — | $ 0.53 | — | $ 0.69 | — |
| Direct Operating Cost | — | $ 1,311 | — | $ 1,929 | — |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 | 2 | 1 |
| Total Seats | 14 | 10 | 18 | 17 | 8 |
| Configuration | Green Interior | — | — | — | — |
| Max Cabin Seats | 12 | 9 | 16 | 15 | 7 |
| Standard Cabin Seats | 12 | 8 | 16 | 15 | 6 |
| Lavatory | — | Optional | — | — | No |
| Galley Location | — | FWD | — | — | — |
| Lavatory Location | — | AFT | — | — | — |
| Cabin Pressure (psi) | — | 6.5 | — | — | 9 |
| Galley / Refreshment | — | Optional | — | — | No |
| SL Cabin Altitude (ft) | — | — | — | — | 24000 |
| Max Cabin Altitude (ft) | — | — | — | — | 6600 |
| Engine | |||||
| FADEC | Yes | Yes | Dual-Channel | Yes | Yes |
| Model | HE Arrano | PT6A-60A | CT7-2F1 | PT6C-67C | PT6A–66B |
| Fuel Type | JetFuel | — | JetFuel | JetFuel | — |
| TBO (hrs) | 4000 | 3600 | 4000 | 5000 | 3600 |
| No. of Engines | 2 | 1 | 2 | 2 | 2 |
| Horsepower | — | 1050 | 1800 | 1679 | 850 |
| Flat Rating | — | ISA + 10 | — | — | ISA + 28 |
| Fuel Capacity (gal) | — | 539 | 641 | 414 | — |
| Fuel Burn (gph) | — | — | — | — | 100 |
| Dimensions | |||||
| Length (ft) | 39.4 | 46.7 | 61.58 | 54.7 | 47.3 |
| Overall Height (ft) | 13.1 | 14.4 | 18.18 | 16.4 | 13.1 |
| Rotor Diameter (ft) | 45.2 | — | 54.5 | 54.7 | — |
| Wingspan (ft) | — | 57.9 | — | — | 47.1 |
| Cabin Width (ft) | — | 4.5 | 7.58 | — | 6.1 |
| Cabin Height (ft) | — | 4.8 | 4.5 | — | 5.8 |
| Cabin Length (ft) | — | 19.5 | 15.5 | — | 14.9 |
| Cabin Width - Floor (ft) | — | 4.1 | — | — | 3.5 |
| Cabin Length - Seating (ft) | — | 19.5 | — | — | — |
| Baggage Volume Int. (cu. ft) | — | 71 | — | — | 35.2 |
| Width (ft) | — | — | 25.77 | — | — |
| Baggage Volume Ext. (cu. ft) | — | — | 128 | 120 | — |
| Cabin Volume (cu. ft) | — | — | — | 282 | — |