Bell 525 Relentless vs Cessna Citation Xls vs Enstrom 480b vs Piaggio Avanti Evo
The Bell 525 Relentless and Enstrom 480B are helicopters, while the Cessna Citation XLS+ and Piaggio Avanti EVO are fixed‑wing business aircraft. In category terms, the Bell 525 is a modern “super‑medium” twin‑engine helicopter aimed at offshore and corporate transport, whereas the Enstrom 480B is a much smaller single‑engine utility/light turbine helicopter. The Citation XLS+ is a light jet optimized for short to mid‑range business trips, and the Avanti EVO is a high‑speed twin‑turboprop positioned between light jets and traditional turboprops. On range, the Enstrom 480B is the shortest‑legged (generally a few hundred nautical miles). The Bell 525 offers substantially more helicopter range, typically in the mid‑hundreds of nautical miles. Both fixed‑wing aircraft go notably farther; the Citation XLS+ and Avanti EVO are broadly comparable in mission reach, commonly around the 1,500–1,800 nautical mile class depending on payload and reserves. For passenger capacity, the Enstrom typically carries around 4–5 including the pilot. The Bell 525 is configured for roughly 12–16 seats depending on layout. The Citation XLS+ and Avanti EVO usually seat about 7–9 passengers in typical corporate configurations.
| Spec | Bell 525 Relentless | Cessna Citation XLS+ | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 10 | 8 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Cessna Citation | Piaggio |
| Aircraft Name | 525 Relentless | XLS+ | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1906 | 1530 |
| Max Cabin Seats | 16 | 9 | 7 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 7540 | 3775 |
| Standard Cabin Seats | 16 | 8 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 160 | 430 | 400 |
| Base Aircraft Price (USD) | $15,000,000 | $15,500,000 | $ 7,695,000 |
| DOC / nm | — | $ 5.34 | — |
| DOC / nm / Seat | — | $ 0.67 | — |
| Direct Operating Cost | — | $ 2,303 | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 10 | 8 |
| Max Cabin Seats | 16 | 9 | 7 |
| Standard Cabin Seats | 16 | 8 | 6 |
| Lavatory | — | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | AFT | — |
| Cabin Pressure (psi) | — | 9.3 | 9 |
| Galley / Refreshment | — | Galley | No |
| SL Cabin Altitude (ft) | — | 25230 | 24000 |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | PW545C | PT6A–66B |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 5000 | 3600 |
| Horsepower | 1800 | — | 850 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 10 | ISA + 28 |
| Thrust (lbs) | — | 4119 | — |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 52.5 | 47.3 |
| Cabin Width (ft) | 7.58 | 5.5 | 6.1 |
| Cabin Height (ft) | 4.5 | 5.7 | 5.8 |
| Cabin Length (ft) | 15.5 | 18.5 | 14.9 |
| Overall Height (ft) | 18.18 | 17.2 | 13.1 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 80 | — |
| Wingspan (ft) | — | 56.3 | 47.1 |
| Aisle Step (ft) | — | 0.7 | — |
| Cabin Width - Floor (ft) | — | 3.9 | 3.5 |
| Cabin Length - Seating (ft) | — | 14.3 | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 35.2 |