Airbus Helicopters H215 vs Bell 525 Relentless
The Airbus Helicopters H215 and Bell 525 Relentless sit in different parts of the civil helicopter market. The H215 is a proven, medium-class helicopter derived from the Super Puma family and is commonly positioned for utility work such as offshore transport, search and rescue, and government missions. The Bell 525 is a newer, “super-medium” helicopter aimed at higher-speed, longer-range offshore and executive transport with more modern avionics and fly-by-wire flight controls. On range, the 525 is generally marketed with a longer mission radius and higher cruise efficiency than the H215, reflecting its newer airframe and performance targets, though real-world range varies with payload, reserves, and operating conditions. On passenger capacity, both can be configured to carry roughly around the high teens in typical offshore layouts, but the H215 is often cited around 19 passengers, while the 525 is commonly cited around 16 to 19 depending on configuration. Overall, the H215 emphasizes established capability and lift, while the 525 emphasizes modern systems and range-speed performance.
| 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 |