Bell 525 Relentless vs Enstrom 480b vs Leonardo Aw189
The Bell 525 Relentless, Enstrom 480B, and Agusta/Leonardo AW189 sit in very different helicopter categories, so their capabilities don’t directly overlap. The Enstrom 480B is a light single‑engine utility helicopter aimed at short‑range missions and lower operating complexity; it typically carries about five passengers (plus a pilot) and is best suited to comparatively modest range and payload needs. The Bell 525 Relentless is a super‑medium, twin‑engine aircraft designed for higher utilization commercial roles, offering substantially greater range than light singles and a much larger cabin; typical passenger configurations are in the mid‑teens depending on interior and mission. The AW189 is also a super‑medium twin and broadly comparable in mission class to the 525, with long‑range capability and a large cabin commonly arranged for roughly 16–19 passengers in offshore-style layouts, again depending on configuration. In general, the Enstrom prioritizes simplicity and light utility, while the 525 and AW189 target offshore transport, SAR, and corporate/VIP missions where range, redundancy, and cabin volume are the key differentiators.
| Spec | Bell 525 Relentless | AGUSTA / LEONARDO AW189 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 18 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Bell | Leonardo |
| Aircraft Name | 525 Relentless | AW189 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 651 |
| Max Cabin Seats | 16 | 19 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | — |
| Standard Cabin Seats | 16 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | EFIS |
| Max Cruise Speed (ktas) | 160 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $2,413,000 |
| DOC / nm | — | $ 15.57 |
| DOC / nm / Seat | — | $ 0.74 |
| Direct Operating Cost | — | $ 2,413 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 18 | 21 |
| Max Cabin Seats | 16 | 19 |
| Standard Cabin Seats | 16 | 19 |
| Engine | ||
| FADEC | Dual-Channel | Yes |
| Model | CT7-2F1 | CT7-2E1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 |
| Horsepower | 1800 | 1983 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 641 | — |
| Dimensions | ||
| Width (ft) | 25.77 | — |
| Length (ft) | 61.58 | 57.8 |
| Cabin Width (ft) | 7.58 | — |
| Cabin Height (ft) | 4.5 | — |
| Cabin Length (ft) | 15.5 | — |
| Overall Height (ft) | 18.18 | 16.6 |
| Rotor Diameter (ft) | 54.5 | 48 |
| Baggage Volume Ext. (cu. ft) | 128 | 85 |
| Cabin Volume (cu. ft) | — | 395 |