Bell 525 Relentless vs Cessna 208b Grand Caravan Ex vs Pilatus Pc 24
The Bell 525 Relentless is a fly-by-wire, twin‑engine helicopter aimed at offshore, corporate, and utility missions where vertical takeoff and landing matters most. It typically carries around 16 passengers in a high-density layout (often fewer in executive configurations) and has a practical range on the order of roughly 500–600 nautical miles depending on load and reserves. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility airplane optimized for rugged, short-field regional flying. It commonly seats about 9–14 passengers (up to roughly 14 in commuter layouts), with range generally around 800–900 nautical miles, varying with payload. The Pilatus PC‑24 is a twin‑engine light business jet designed for fast, longer-range point-to-point travel, including operations from shorter or semi-prepared runways compared with many jets. It typically carries about 6–10 passengers in executive seating, with range around 2,000 nautical miles. Overall, the 525 prioritizes access over speed, the Caravan prioritizes simplicity and payload flexibility, and the PC‑24 prioritizes speed and range.
| 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 |