Bell 525 Relentless vs Dassault Falcon 8x vs Leonardo Aw189 vs Sikorsky S 92
The Bell 525 Relentless and Sikorsky S-92 are large, long-range helicopters aimed at offshore, SAR, and VIP missions, while the Leonardo AW189 is a slightly smaller “super-medium” helicopter optimized for similar roles with lower typical operating footprint. In contrast, the Dassault Falcon 8X is an ultra-long-range business jet built primarily for intercontinental executive travel rather than vertical-lift utility. On range, the Falcon 8X is in a different class, capable of true long-haul nonstop flights (roughly 6,000+ nautical miles depending on payload and conditions). The helicopters are far shorter-legged by comparison: the Bell 525 and S-92 are generally in the ~500–600 nm class, with the AW189 typically around the ~450–500 nm class, all varying with reserves, passenger load, and mission equipment. On passenger capacity, the Falcon 8X typically carries about 12–16 in executive layouts. The AW189 commonly seats around 16–19, the Bell 525 around 16–20, and the S-92 often about 19, with higher-density configurations possible for all three helicopters.
| Spec | Bell 525 Relentless | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 18 | 17 | 21 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Bell | Dassault Falcon | Leonardo | Sikorsky |
| Aircraft Name | 525 Relentless | 8X | AW189 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6450 | 651 | 439 |
| Max Cabin Seats | 16 | 16 | 19 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6675 | 36900 | — | 7417 |
| Standard Cabin Seats | 16 | 14 | 19 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell Primus EASy II | EFIS | EFIS |
| Max Cruise Speed (ktas) | 160 | 516 | 155 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $ 62,500,000 | $2,413,000 | $30,650,000 |
| DOC / nm | — | $ 7.66 | $ 15.57 | $ 19.79 |
| DOC / nm / Seat | — | $ 0.64 | $ 0.74 | $ 0.94 |
| Direct Operating Cost | — | $ 3,805 | $ 2,413 | $ 3,068 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 18 | 17 | 21 | 21 |
| Max Cabin Seats | 16 | 16 | 19 | 19 |
| Standard Cabin Seats | 16 | 14 | 19 | 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 | Yes |
| Model | CT7-2F1 | PW307D | CT7-2E1 | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel | JetFuel |
| TBO (hrs) | 4000 | On-Condition | 4000 | 4000 |
| Horsepower | 1800 | — | 1983 | 2520 |
| No. of Engines | 2 | 3 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | — | 760 |
| 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 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 85 | 140 |
| Wingspan (ft) | — | 86.3 | — | — |
| Cabin Volume (cu. ft) | — | 1695 | 395 | 775 |
| Cabin Width - Floor (ft) | — | 6.3 | — | — |
| Cabin Length - Seating (ft) | — | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | — | 140 | — | — |