Bell 525 Relentless vs Cessna 208b Grand Caravan Ex vs Pilatus Pc 24 vs Sikorsky S 92
The Bell 525 Relentless and Sikorsky S-92 are twin‑engine helicopters, while the Cessna 208B Grand Caravan EX is a single‑engine turboprop utility airplane and the Pilatus PC‑24 is a twin‑engine light business jet. In range, the PC‑24 generally leads among these, designed for longer point‑to‑point trips typical of business aviation; the Grand Caravan EX offers moderate range optimized for regional utility and short/rough-field operations; the Bell 525 provides helicopter-range suitable for intercity or offshore-style missions; and the larger S‑92 is commonly configured for extended helicopter missions with range varying significantly by payload and mission equipment. Passenger capacity differs by role: the PC‑24 typically carries around 6–10 passengers in executive seating; the Grand Caravan EX commonly seats about 9–14 in commuter configurations; the Bell 525 is usually arranged for roughly 12–16 passengers; and the S‑92 is often configured around 19 passengers, with higher-capacity layouts possible depending on certification and interior. Overall, PC‑24 prioritizes speed and runway-to-runway mobility, the Grand Caravan EX emphasizes utility access, and the helicopters trade speed for vertical lift and mission flexibility.
| Spec | Bell 525 Relentless | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 18 | 6 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Pilatus | Sikorsky |
| Aircraft Name | 525 Relentless | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 2076 | 439 |
| Max Cabin Seats | 16 | 10 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 6680 | 7417 |
| Standard Cabin Seats | 16 | 6 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 160 | 440 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $11,800,000 | $30,650,000 |
| DOC / nm | — | $ 3.71 | $ 19.79 |
| DOC / nm / Seat | — | $ 0.62 | $ 0.94 |
| Direct Operating Cost | — | $ 1,619 | $ 3,068 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 18 | 6 | 21 |
| Max Cabin Seats | 16 | 10 | 19 |
| Standard Cabin Seats | 16 | 6 | 19 |
| 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 | Yes |
| Model | CT7-2F1 | FJ44-4A-QPM | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | 5000 | 4000 |
| Horsepower | 1800 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | 760 |
| 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 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 140 |
| 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 | — |
| Cabin Volume (cu. ft) | — | — | 775 |