Bell 525 Relentless vs Pilatus Pc 24
The Bell 525 Relentless and Pilatus PC-24 sit in different aircraft categories and are optimized for different missions. The Bell 525 is a fly-by-wire, twin‑engine civilian helicopter aimed at point-to-point access where runways are limited or nonexistent, such as offshore, medical, or downtown landing sites. The Pilatus PC‑24 is a twin‑engine light business jet designed for fast, long-range travel between airports, including many shorter or less‑prepared runways than typical jets can use. On range, the PC‑24 generally offers substantially greater nonstop distance than the Bell 525, reflecting the efficiency of fixed‑wing cruise at altitude and its role in regional-to-transcontinental business travel. The Bell 525’s range is more modest but paired with vertical takeoff and landing flexibility that can reduce total trip time when door-to-door access matters more than cruise distance. For passenger capacity, both can be configured in the high single digits to low teens depending on layout. The PC‑24 commonly seats around 8–10 passengers in executive configuration, while the Bell 525 is often configured around 12–16 seats, though mission equipment can reduce seating.
| Spec | Bell 525 Relentless | Pilatus PC-24 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 18 | 6 |
| Flight Rules | IFR | — |
| Manufacturer | Bell | Pilatus |
| Aircraft Name | 525 Relentless | PC-24 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 2076 |
| Max Cabin Seats | 16 | 10 |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6675 | 6680 |
| Standard Cabin Seats | 16 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $11,800,000 |
| DOC / nm | — | $ 3.71 |
| DOC / nm / Seat | — | $ 0.62 |
| Direct Operating Cost | — | $ 1,619 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 18 | 6 |
| Max Cabin Seats | 16 | 10 |
| Standard Cabin Seats | 16 | 6 |
| Lavatory | — | 1 Enclosed Flushing |
| Crew Rest | — | No |
| Jump Seat | — | No |
| Cargo Door | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD |
| Cabin Pressure (psi) | — | 9.3 |
| Galley / Refreshment | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 23500 |
| Engine | ||
| FADEC | Dual-Channel | Yes |
| Model | CT7-2F1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 4000 | 5000 |
| Horsepower | 1800 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 641 | — |
| Flat Rating | — | ISA + 23 |
| Thrust (lbs) | — | 3435 |
| Dimensions | ||
| Width (ft) | 25.77 | — |
| Length (ft) | 61.58 | 52.2 |
| Cabin Width (ft) | 7.58 | 5.6 |
| Cabin Height (ft) | 4.5 | 5.1 |
| Cabin Length (ft) | 15.5 | 23 |
| Overall Height (ft) | 18.18 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — |
| Baggage Volume Ext. (cu. ft) | 128 | — |
| Wingspan (ft) | — | 55.8 |
| Aisle Step (ft) | — | Flat Floor |
| Cabin Width - Floor (ft) | — | 3.8 |
| Cabin Length - Seating (ft) | — | 17 |
| Baggage Volume Int. (cu. ft) | — | 90 |