Bell 525 Relentless vs Piaggio Avanti Evo vs Pilatus Pc 24 vs Robinson R66
The Bell 525 Relentless and Robinson R66 are helicopters, while the Piaggio Avanti EVO and Pilatus PC-24 are fixed‑wing airplanes. In category terms, the Bell 525 is a super‑medium, twin‑engine turbine helicopter aimed at offshore/utility and executive transport; the R66 is a light, single‑engine turbine helicopter typically used for private, training, and light utility missions. The Avanti EVO is a pressurized twin‑turboprop business aircraft optimized for efficient regional trips, and the PC‑24 is a twin‑engine light business jet designed for faster travel and strong short/rough‑field capability. Range generally favors the fixed‑wing aircraft: the PC‑24 typically offers the longest legs, followed by the Avanti EVO, while the Bell 525 and then the R66 tend to have shorter practical ranges due to helicopter efficiency limits. Passenger capacity also trends higher in the larger platforms: the Bell 525 and PC‑24 commonly seat around 8–10 passengers in executive layouts, the Avanti EVO typically carries about 7–9, and the R66 is usually configured for about 4 passengers plus a pilot (five seats total).
| Spec | Bell 525 Relentless | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 18 | 8 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Bell | Piaggio | Pilatus |
| Aircraft Name | 525 Relentless | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1530 | 2076 |
| Max Cabin Seats | 16 | 7 | 10 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6675 | 3775 | 6680 |
| Standard Cabin Seats | 16 | 6 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 400 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $ 7,695,000 | $11,800,000 |
| DOC / nm | — | — | $ 3.71 |
| DOC / nm / Seat | — | — | $ 0.62 |
| Direct Operating Cost | — | — | $ 1,619 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 18 | 8 | 6 |
| Max Cabin Seats | 16 | 7 | 10 |
| Standard Cabin Seats | 16 | 6 | 6 |
| Lavatory | — | No | 1 Enclosed Flushing |
| Cabin Pressure (psi) | — | 9 | 9.3 |
| Galley / Refreshment | — | No | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 24000 | 23500 |
| Max Cabin Altitude (ft) | — | 6600 | — |
| Crew Rest | — | — | No |
| Jump Seat | — | — | No |
| Cargo Door | — | — | Yes |
| Galley Location | — | — | FWD |
| Lavatory Location | — | — | FWD |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 3600 | 5000 |
| Horsepower | 1800 | 850 | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 28 | ISA + 23 |
| Fuel Burn (gph) | — | 100 | — |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 47.3 | 52.2 |
| Cabin Width (ft) | 7.58 | 6.1 | 5.6 |
| Cabin Height (ft) | 4.5 | 5.8 | 5.1 |
| Cabin Length (ft) | 15.5 | 14.9 | 23 |
| Overall Height (ft) | 18.18 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — |
| Wingspan (ft) | — | 47.1 | 55.8 |
| Cabin Width - Floor (ft) | — | 3.5 | 3.8 |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 90 |
| Aisle Step (ft) | — | — | Flat Floor |
| Cabin Length - Seating (ft) | — | — | 17 |