Bell 525 Relentless vs Cessna Citation Xls vs Pilatus Pc 24 vs Robinson R66
The Bell 525 Relentless and Robinson R66 are helicopters, while the Cessna Citation XLS+ and Pilatus PC-24 are fixed‑wing business jets. In category, the Bell 525 is a large, long‑range corporate helicopter aimed at offshore and executive missions, whereas the Robinson R66 is a light, single‑engine turbine helicopter typically used for short regional trips and utility flying. The Citation XLS+ is a midsize business jet optimized for comfortable, efficient point‑to‑point travel between paved airports, while the PC-24 is a light jet designed for versatility, including operations from shorter and more rugged runways than most business jets. For range, the two jets generally offer substantially longer nonstop capability than the helicopters, with the Citation XLS+ and PC-24 suited to multi‑hour intercity legs; the Bell 525 is the longer‑range option among the helicopters, while the R66 is best for comparatively short hops. For passenger capacity, the business jets commonly seat around eight to ten passengers in typical executive layouts. The Bell 525 is also configured around the high single digits to low teens depending on interior, while the R66 is usually limited to four passengers plus a pilot.
| Spec | Bell 525 Relentless | Cessna Citation XLS+ | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 10 | 6 |
| Flight Rules | IFR | — | — |
| Manufacturer | Bell | Cessna Citation | Pilatus |
| Aircraft Name | 525 Relentless | XLS+ | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1906 | 2076 |
| Max Cabin Seats | 16 | 9 | 10 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6675 | 7540 | 6680 |
| Standard Cabin Seats | 16 | 8 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 430 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $15,500,000 | $11,800,000 |
| DOC / nm | — | $ 5.34 | $ 3.71 |
| DOC / nm / Seat | — | $ 0.67 | $ 0.62 |
| Direct Operating Cost | — | $ 2,303 | $ 1,619 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 10 | 6 |
| Max Cabin Seats | 16 | 9 | 10 |
| Standard Cabin Seats | 16 | 8 | 6 |
| Lavatory | — | 1 Enclosed Belted Flushing | 1 Enclosed Flushing |
| Crew Rest | — | No | No |
| Jump Seat | — | No | No |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | AFT | FWD |
| Cabin Pressure (psi) | — | 9.3 | 9.3 |
| Galley / Refreshment | — | Galley | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 25230 | 23500 |
| Cargo Door | — | — | Yes |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | PW545C | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 5000 | 5000 |
| Horsepower | 1800 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 10 | ISA + 23 |
| Thrust (lbs) | — | 4119 | 3435 |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 52.5 | 52.2 |
| Cabin Width (ft) | 7.58 | 5.5 | 5.6 |
| Cabin Height (ft) | 4.5 | 5.7 | 5.1 |
| Cabin Length (ft) | 15.5 | 18.5 | 23 |
| Overall Height (ft) | 18.18 | 17.2 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 80 | — |
| Wingspan (ft) | — | 56.3 | 55.8 |
| Aisle Step (ft) | — | 0.7 | Flat Floor |
| Cabin Width - Floor (ft) | — | 3.9 | 3.8 |
| Cabin Length - Seating (ft) | — | 14.3 | 17 |
| Baggage Volume Int. (cu. ft) | — | 10 | 90 |