Bell 525 Relentless vs Cessna 208b Grand Caravan Ex vs Dassault Falcon 8x vs Leonardo Aw189
The Bell 525 Relentless and Leonardo AW189 are both large, modern twin‑engine helicopters aimed at offshore, SAR, and executive utility missions. In category terms they sit well above light twins, with the AW189 generally positioned as a proven super‑medium and the 525 as a newer “super‑medium” with fly‑by‑wire ambitions. Their ranges are broadly comparable for this class—typically a few hundred nautical miles depending on payload and reserves—while passenger capacity is usually in the mid‑teens, often around 16–19 in high‑density layouts. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft, not a helicopter, optimized for short/rough fields and simple logistics. It commonly carries roughly 9–14 passengers depending on configuration and tends to offer longer legs than the helicopters, often on the order of ~800–1,000+ nautical miles with appropriate payload. The Dassault Falcon 8X is a long‑range tri‑jet business aircraft in a different league for range and speed, routinely spanning intercontinental sectors (about 6,000+ nautical miles), with typical executive seating around 12–16 (and higher maximums in denser layouts).
| Spec | Bell 525 Relentless | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 17 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Dassault Falcon | Leonardo |
| Aircraft Name | 525 Relentless | 8X | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6450 | 651 |
| Max Cabin Seats | 16 | 16 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 36900 | — |
| Standard Cabin Seats | 16 | 14 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 160 | 516 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $ 62,500,000 | $2,413,000 |
| DOC / nm | — | $ 7.66 | $ 15.57 |
| DOC / nm / Seat | — | $ 0.64 | $ 0.74 |
| Direct Operating Cost | — | $ 3,805 | $ 2,413 |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 17 | 21 |
| Max Cabin Seats | 16 | 16 | 19 |
| Standard Cabin Seats | 16 | 14 | 19 |
| Lavatory | — | 2 Enclosed Flushing | — |
| Crew Rest | — | No | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD / AFT | — |
| Cabin Pressure (psi) | — | 10.2 | — |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 29200 | — |
| Max Cabin Altitude (ft) | — | 3900 | — |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | PW307D | CT7-2E1 |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | On-Condition | 4000 |
| Horsepower | 1800 | — | 1983 |
| No. of Engines | 2 | 3 | 2 |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 17 | — |
| Thrust (lbs) | — | 6722 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 80.2 | 57.8 |
| Cabin Width (ft) | 7.58 | 7.7 | — |
| Cabin Height (ft) | 4.5 | 6.2 | — |
| Cabin Length (ft) | 15.5 | 42.7 | — |
| Overall Height (ft) | 18.18 | 26.1 | 16.6 |
| Rotor Diameter (ft) | 54.5 | — | 48 |
| Baggage Volume Ext. (cu. ft) | 128 | — | 85 |
| Wingspan (ft) | — | 86.3 | — |
| Cabin Volume (cu. ft) | — | 1695 | 395 |
| Cabin Width - Floor (ft) | — | 6.3 | — |
| Cabin Length - Seating (ft) | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | 140 | — |