Airbus Helicopters H225 vs Bell 525 Relentless vs Embraer Legacy 650 E
The Airbus H225 and Bell 525 Relentless are both large, twin‑engine helicopters designed for vertical lift missions, while the Embraer Legacy 650E is a long‑range business jet intended for fast, high‑altitude point‑to‑point travel. In range terms, the H225 typically offers a mission radius suited to offshore and SAR profiles, roughly on the order of 500–600 nautical miles depending on fuel, payload, and reserves, whereas the Bell 525 is in a similar bracket, often cited around 560 nautical miles, also highly dependent on configuration. The Legacy 650E operates in a different league for range, commonly quoted around 3,900 nautical miles, enabling intercontinental sectors that are impractical for helicopters. For passenger capacity, the H225 can be configured for high-density transport, commonly around 16–19 passengers (and in some layouts more), while the Bell 525 is generally positioned for about 16–20 passengers depending on interior. The Legacy 650E typically seats 13 passengers in a standard executive configuration, trading density for comfort, speed, and cabin amenities.
| Spec | AIRBUS H225 | Bell 525 Relentless |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | — |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 18 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bell |
| Aircraft Name | H225 | 525 Relentless |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 |
| DOC / nm / Seat | $ 0.99 | — |
| Max Cabin Seats | 28 | 16 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 |
| Standard Cabin Seats | 19 | 16 |
| Direct Operating Cost | $ 2,963 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H |
| Max Cruise Speed (ktas) | 142 | 160 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 18 |
| Max Cabin Seats | 28 | 16 |
| Standard Cabin Seats | 19 | 16 |
| Engine | ||
| FADEC | Yes | Dual-Channel |
| Model | Makila 2A1 | CT7-2F1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 4000 |
| Horsepower | 2100 | 1800 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | 641 |
| Dimensions | ||
| Length (ft) | 63.4 | 61.58 |
| Overall Height (ft) | 16.3 | 18.18 |
| Rotor Diameter (ft) | 53.2 | 54.5 |
| Cabin Volume (cu. ft) | 547 | — |
| Width (ft) | — | 25.77 |
| Cabin Width (ft) | — | 7.58 |
| Cabin Height (ft) | — | 4.5 |
| Cabin Length (ft) | — | 15.5 |
| Baggage Volume Ext. (cu. ft) | — | 128 |