Airbus Helicopters H145 vs Bell 525 Relentless
The Airbus Helicopters H145 and the Bell 525 Relentless sit in different helicopter categories and are typically chosen for different mission profiles. The H145 is a light twin-engine helicopter widely used for HEMS/EMS, law enforcement, utility work, and short-to-medium corporate or regional transport. The Bell 525 is a larger, super-midsize twin designed more for longer-range offshore, executive transport, and higher-capacity missions where speed, payload, and cabin volume matter most. In range terms, the H145 generally supports shorter legs and regional operations, while the 525 is aimed at substantially longer missions, especially over water, with greater fuel and payload flexibility. Passenger capacity also reflects the class difference: the H145 commonly carries a small group of passengers (often configured around six to nine depending on interior and mission equipment), whereas the 525 is intended to carry a larger group (typically in the low-to-mid teens in passenger layouts) with more cabin space and comfort. Overall, the H145 emphasizes versatility and lower operating footprint; the 525 emphasizes capacity and long-range capability.
| Spec | AIRBUS H145 | Bell 525 Relentless |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 9.31 | — |
| Min Crew | 1 | 2 |
| Total Seats | 10 | 18 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bell |
| Aircraft Name | H145 | 525 Relentless |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 580 |
| DOC / nm / Seat | $ 0.93 | — |
| Max Cabin Seats | 9 | 16 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 4200 | 6675 |
| Standard Cabin Seats | 8 | 16 |
| Direct Operating Cost | $ 1,210 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H |
| Max Cruise Speed (ktas) | 130 | 160 |
| Base Aircraft Price (USD) | $10,200,000 | $15,000,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 2 |
| Total Seats | 10 | 18 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 9 | 16 |
| Standard Cabin Seats | 8 | 16 |
| Engine | ||
| FADEC | Yes | Dual-Channel |
| Model | Arriel 2E | CT7-2F1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 |
| Horsepower | 894 | 1800 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | — | 641 |
| Dimensions | ||
| Length (ft) | 44.8 | 61.58 |
| Overall Height (ft) | 13 | 18.18 |
| Rotor Diameter (ft) | 36.1 | 54.5 |
| Cabin Volume (cu. ft) | 166 | — |
| Baggage Volume Ext. (cu. ft) | 46.8 | 128 |
| Width (ft) | — | 25.77 |
| Cabin Width (ft) | — | 7.58 |
| Cabin Height (ft) | — | 4.5 |
| Cabin Length (ft) | — | 15.5 |