Bell 525 Relentless vs Cessna Citation Xls vs Piaggio Avanti Evo vs Piper M600 Sls
The Bell 525 Relentless is a fly-by-wire, twin‑engine helicopter in the super‑medium class, oriented toward vertical-access missions rather than point‑to‑point runway travel. It typically offers roughly 500–600 nautical miles of range and is commonly configured for about 12–16 passengers depending on interior and mission equipment. The Cessna Citation XLS+ is a light jet designed for efficient short-to-medium business trips between airports. It provides about 1,800–2,100 nautical miles of range and usually seats 7–9 passengers in a standard executive layout. The Piaggio Avanti EVO is a high-speed twin turboprop (often described as a “fast turboprop” or “mini businessliner”) that trades jetlike cruise for turboprop efficiency. Its range is generally around 1,400–1,700 nautical miles, with typical seating for 6–8 passengers. The Piper M600 SLS is a single‑engine pressurized turboprop, positioned as an owner‑pilot-friendly personal/business aircraft. It commonly offers about 1,200–1,500 nautical miles of range and seats about 5–6 passengers.
| Spec | Bell 525 Relentless | Cessna Citation XLS+ | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 18 | 10 | 8 | 6 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Bell | Cessna Citation | Piaggio | Piper |
| Aircraft Name | 525 Relentless | XLS+ | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1906 | 1530 | 1406 |
| Max Cabin Seats | 16 | 9 | 7 | — |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6675 | 7540 | 3775 | 2200 |
| Standard Cabin Seats | 16 | 8 | 6 | 4 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 160 | 430 | 400 | 274 |
| Base Aircraft Price (USD) | $15,000,000 | $15,500,000 | $ 7,695,000 | $3,081,400 |
| DOC / nm | — | $ 5.34 | — | $ 2.19 |
| DOC / nm / Seat | — | $ 0.67 | — | $ 0.55 |
| Direct Operating Cost | — | $ 2,303 | — | $ 603 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 18 | 10 | 8 | 5 |
| Max Cabin Seats | 16 | 9 | 7 | — |
| Standard Cabin Seats | 16 | 8 | 6 | 4 |
| Lavatory | — | 1 Enclosed Belted Flushing | No | No |
| Crew Rest | — | No | — | — |
| Jump Seat | — | No | — | — |
| Galley Location | — | FWD | — | MID |
| Lavatory Location | — | AFT | — | — |
| Cabin Pressure (psi) | — | 9.3 | 9 | 5.6 |
| Galley / Refreshment | — | Galley | No | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 25230 | 24000 | 12600 |
| Max Cabin Altitude (ft) | — | — | 6600 | 8644 |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | No |
| Model | CT7-2F1 | PW545C | PT6A–66B | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | 5000 | 3600 | 3600 |
| Horsepower | 1800 | — | 850 | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | — | 260 |
| Flat Rating | — | ISA + 10 | ISA + 28 | ISA + 55 |
| Thrust (lbs) | — | 4119 | — | — |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 52.5 | 47.3 | 29.7 |
| Cabin Width (ft) | 7.58 | 5.5 | 6.1 | 4.1 |
| Cabin Height (ft) | 4.5 | 5.7 | 5.8 | 4 |
| Cabin Length (ft) | 15.5 | 18.5 | 14.9 | 12.3 |
| Overall Height (ft) | 18.18 | 17.2 | 13.1 | 11.3 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 80 | — | — |
| Wingspan (ft) | — | 56.3 | 47.1 | 43.2 |
| 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 | 20 |
| Cabin Volume (cu. ft) | — | — | — | 165 |