Airbus Helicopters H215 vs Bell 525 Relentless
| Spec | AIRBUS H215 | Bell 525 Relentless |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 19.07 | — |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 18 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bell |
| Aircraft Name | H215 | 525 Relentless |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 468 | 580 |
| DOC / nm / Seat | $ 0.91 | — |
| Max Cabin Seats | 22 | 16 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 8903 | 6675 |
| Standard Cabin Seats | 19 | 16 |
| Direct Operating Cost | $ 2,708 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H |
| Max Cruise Speed (ktas) | 142 | 160 |
| Base Aircraft Price (USD) | $27,500,000 | $15,000,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 18 |
| Max Cabin Seats | 22 | 16 |
| Standard Cabin Seats | 19 | 16 |
| Engine | ||
| FADEC | Yes | Dual-Channel |
| Model | Makila 1A1 | CT7-2F1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3000 | 4000 |
| Horsepower | 1820 | 1800 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 540 | 641 |
| Dimensions | ||
| Length (ft) | 61.4 | 61.58 |
| Overall Height (ft) | 16.2 | 18.18 |
| Rotor Diameter (ft) | 51.2 | 54.5 |
| Cabin Volume (cu. ft) | 473.9 | — |
| 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 |