Airbus Helicopters H155 vs Airbus Helicopters H215 vs Bell 525 Relentless
Airbus Helicopters’ H155, H215, and Bell’s 525 Relentless sit in different parts of the civil/utility helicopter spectrum. The H155 is typically positioned as a medium, twin‑engine helicopter optimized for corporate and offshore passenger transport, with a comparatively modest range and a cabin sized for roughly a dozen passengers in high‑density layouts, often fewer in VIP configurations. The H215 is a heavier, twin‑engine “Super Puma” class aircraft aimed at utility and offshore lift, trading a larger airframe and higher payload capability for range that is generally in the medium-to-long bracket, and passenger capacity commonly around the high‑teens to low‑20s depending on seating and mission kit. The Bell 525 Relentless is a modern “super‑medium” twin designed for offshore and executive missions, typically offering long-range capability competitive with its class and a spacious cabin that usually seats around the mid‑teens in airline-style layouts, with flexible configurations. Exact range and seating vary significantly with fuel options, reserves, cabin fit, and payload.
| Spec | AIRBUS H155 | AIRBUS H215 | Bell 525 Relentless |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 11.06 | $ 19.07 | — |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 14 | 21 | 18 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Bell |
| Aircraft Name | H155 | H215 | 525 Relentless |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 423 | 468 | 580 |
| DOC / nm / Seat | $ 0.74 | $ 0.91 | — |
| Max Cabin Seats | 12 | 22 | 16 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 4012 | 8903 | 6675 |
| Standard Cabin Seats | 12 | 19 | 16 |
| Direct Operating Cost | $ 1,593 | $ 2,708 | — |
| Flight Deck (Base Spec) | EFIS | EFIS | Garmin G5000H |
| Max Cruise Speed (ktas) | 144 | 142 | 160 |
| Base Aircraft Price (USD) | $14,800,000 | $27,500,000 | $15,000,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 14 | 21 | 18 |
| Configuration | Green Interior | — | — |
| Max Cabin Seats | 12 | 22 | 16 |
| Standard Cabin Seats | 12 | 19 | 16 |
| Engine | |||
| FADEC | Yes | Yes | Dual-Channel |
| Model | Arriel 2C2 | Makila 1A1 | CT7-2F1 |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3000 | 4000 |
| Horsepower | 943 | 1820 | 1800 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 332 | 540 | 641 |
| Dimensions | |||
| Length (ft) | 46.9 | 61.4 | 61.58 |
| Overall Height (ft) | 14.3 | 16.2 | 18.18 |
| Rotor Diameter (ft) | 41.1 | 51.2 | 54.5 |
| Cabin Volume (cu. ft) | 235.2 | 473.9 | — |
| Baggage Volume Ext. (cu. ft) | 88.3 | — | 128 |
| Width (ft) | — | — | 25.77 |
| Cabin Width (ft) | — | — | 7.58 |
| Cabin Height (ft) | — | — | 4.5 |
| Cabin Length (ft) | — | — | 15.5 |