Beechcraft King Air 360 Er vs Bell 525 Relentless vs Piaggio Avanti Evo vs Piper M600 Sls
The Beechcraft King Air 360ER and Piaggio Avanti EVO are both pressurized, twin‑engine turboprop fixed‑wing aircraft aimed at efficient regional travel, while the Piper M600 SLS is a simpler, pressurized single‑engine turboprop for shorter, lighter missions. The Bell 525 Relentless is in a different category entirely: a large, long‑range twin‑engine helicopter optimized for point‑to‑point access where runways are impractical. On range, the King Air 360ER is typically the longest‑legged of these fixed‑wing options, designed specifically for extended endurance. The Avanti EVO also offers long range for a turboprop and is often chosen for speed‑and‑efficiency over regional to mid‑range trips. The M600 SLS generally has the shortest range of the group, suited to personal and small‑business missions rather than maximum legs. The Bell 525’s range is strong for a helicopter, but it usually trails comparable fixed‑wing turboprops on distance efficiency. For passenger capacity, the King Air 360ER commonly seats the most among the airplanes (often up to about 9), the Avanti EVO is typically configured around 7–9, the M600 SLS around 5–6, and the Bell 525 is commonly arranged for roughly 12–16 depending on layout.
| Spec | Bell 525 Relentless | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 18 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Bell | Piaggio | Piper |
| Aircraft Name | 525 Relentless | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1530 | 1406 |
| Max Cabin Seats | 16 | 7 | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6675 | 3775 | 2200 |
| Standard Cabin Seats | 16 | 6 | 4 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 160 | 400 | 274 |
| Base Aircraft Price (USD) | $15,000,000 | $ 7,695,000 | $3,081,400 |
| DOC / nm | — | — | $ 2.19 |
| DOC / nm / Seat | — | — | $ 0.55 |
| Direct Operating Cost | — | — | $ 603 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 18 | 8 | 5 |
| Max Cabin Seats | 16 | 7 | — |
| Standard Cabin Seats | 16 | 6 | 4 |
| Lavatory | — | No | No |
| Cabin Pressure (psi) | — | 9 | 5.6 |
| Galley / Refreshment | — | No | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 24000 | 12600 |
| Max Cabin Altitude (ft) | — | 6600 | 8644 |
| Galley Location | — | — | MID |
| Engine | |||
| FADEC | Dual-Channel | Yes | No |
| Model | CT7-2F1 | PT6A–66B | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 3600 | 3600 |
| Horsepower | 1800 | 850 | 600 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | 260 |
| Flat Rating | — | ISA + 28 | ISA + 55 |
| Fuel Burn (gph) | — | 100 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 47.3 | 29.7 |
| Cabin Width (ft) | 7.58 | 6.1 | 4.1 |
| Cabin Height (ft) | 4.5 | 5.8 | 4 |
| Cabin Length (ft) | 15.5 | 14.9 | 12.3 |
| Overall Height (ft) | 18.18 | 13.1 | 11.3 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — |
| Wingspan (ft) | — | 47.1 | 43.2 |
| Cabin Width - Floor (ft) | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 20 |
| Cabin Volume (cu. ft) | — | — | 165 |