Beechcraft King Air 360 vs Bell 525 Relentless vs Leonardo Aw139 vs Piaggio Avanti Evo
The Beechcraft King Air 360 and Piaggio Avanti EVO are pressurized twin‑turboprop airplanes, while the Bell 525 Relentless and Leonardo AW139 are twin‑engine helicopters. For category and typical use, the King Air 360 is a versatile utility/business aircraft suited to short runways and regional missions; the Avanti EVO is a faster, more business‑oriented turboprop optimized for efficient point‑to‑point travel. The AW139 is a widely used intermediate helicopter for offshore, EMS, and corporate shuttle work, and the Bell 525 is a larger, fly‑by‑wire helicopter aimed at offshore and high‑end transport. On range, the airplanes generally fly farther and faster than the helicopters: King Air 360 and Avanti EVO typically offer roughly 1,000–1,800 nautical miles depending on payload and reserves, whereas AW139 and Bell 525 are commonly in the several‑hundred‑nautical‑mile class, with the 525 generally longer‑legged than the AW139. On passenger capacity, King Air 360 and Avanti EVO are commonly configured for about 6–9 passengers, while AW139 often carries around 8–12, and Bell 525 can be configured for roughly 12–16, depending on interior and mission.
| Spec | Beechcraft King Air 360 | Bell 525 Relentless | AGUSTA / LEONARDO AW139 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.20 | — | $ 11.69 | — |
| Min Crew | 1 | 2 | 2 | 1 |
| Total Seats | 10 | 18 | 17 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Bell | Leonardo | Piaggio |
| Aircraft Name | KingAir 350i | 525 Relentless | AW139 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1560 | 580 | 573 | 1530 |
| DOC / nm / Seat | $ 0.53 | — | $ 0.69 | — |
| Max Cabin Seats | 9 | 16 | 15 | 7 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 5145 | 6675 | 4701 | 3775 |
| Standard Cabin Seats | 8 | 16 | 15 | 6 |
| Direct Operating Cost | $ 1,311 | — | $ 1,929 | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G5000H | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 312 | 160 | 165 | 400 |
| Base Aircraft Price (USD) | $7,650,000 | $15,000,000 | $15,900,000 | $ 7,695,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Optional | — | — | No |
| Min Crew | 1 | 2 | 2 | 1 |
| Total Seats | 10 | 18 | 17 | 8 |
| Galley Location | FWD | — | — | — |
| Max Cabin Seats | 9 | 16 | 15 | 7 |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 6.5 | — | — | 9 |
| Galley / Refreshment | Optional | — | — | No |
| Standard Cabin Seats | 8 | 16 | 15 | 6 |
| SL Cabin Altitude (ft) | — | — | — | 24000 |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | Yes |
| Model | PT6A-60A | CT7-2F1 | PT6C-67C | PT6A–66B |
| TBO (hrs) | 3600 | 4000 | 5000 | 3600 |
| Horsepower | 1050 | 1800 | 1679 | 850 |
| Flat Rating | ISA + 10 | — | — | ISA + 28 |
| No. of Engines | 1 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 539 | 641 | 414 | — |
| Fuel Type | — | JetFuel | JetFuel | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 46.7 | 61.58 | 54.7 | 47.3 |
| 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 |
| Overall Height (ft) | 14.4 | 18.18 | 16.4 | 13.1 |
| 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 | — | — |
| Rotor Diameter (ft) | — | 54.5 | 54.7 | — |
| Baggage Volume Ext. (cu. ft) | — | 128 | 120 | — |
| Cabin Volume (cu. ft) | — | — | 282 | — |