Bell 525 Relentless vs Cessna Citation Xls vs Pilatus Pc 24
The Bell 525 Relentless is a fly-by-wire, twin‑engine commercial helicopter, while the Cessna Citation XLS+ and Pilatus PC‑24 are twin‑engine business jets. In category terms, the 525 emphasizes vertical access to helipads and confined sites, whereas the jets prioritize speed and high‑altitude efficiency from runways (with the PC‑24 also designed for more rugged, shorter-field operations than many light jets). On range, the Bell 525 is typically suited to medium-range missions on the order of roughly 500–600 nautical miles, depending on payload and reserves. The Citation XLS+ generally reaches about 2,000+ nautical miles class range, and the PC‑24 is in a similar bracket at roughly 2,000 nautical miles, varying with load and operating conditions. For passenger capacity, the Bell 525 commonly seats around 12–16 in typical offshore/VIP layouts. The Citation XLS+ is usually configured for about 8–9 passengers. The PC‑24 typically carries about 6–10 passengers, with flexibility for combinations of passengers, cargo, or medical evacuation.
| 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 |