Airbus Helicopters H145 vs Airbus Helicopters H160 vs Airbus Helicopters H175 vs Airbus Helicopters H215 vs Bell 525 Relentless
Airbus’s H145 is the light-twin option, typically used for short to medium missions. It generally offers the shortest range in this group and a smaller cabin, carrying about 6–9 passengers in a typical corporate/offshore layout (higher in dense seating). The H160 sits in the medium twin class with more speed and range than the H145 and usually accommodates roughly 8–12 passengers depending on fit. The H175 is a super-medium twin aimed at offshore and SAR work, with longer range than the H160 in many configurations and a larger cabin commonly arranged for about 12–16 passengers. The H215 (AS332 L1e) is a heavy twin with the largest lift and volume among the Airbus models listed, often configured for around 16–19 passengers and suited to longer, higher-payload missions, though its design is older. Bell’s 525 Relentless is a modern super-medium competing most directly with the H175, generally offering long range and a spacious cabin commonly planned around 12–16 passengers, emphasizing contemporary avionics and efficiency.
| Spec | AIRBUS H145 | AIRBUS H160 | AIRBUS H175 | AIRBUS H215 | Bell 525 Relentless |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 9.31 | — | $ 13.53 | $ 19.07 | — |
| Min Crew | 1 | 2 | 2 | 2 | 2 |
| Total Seats | 10 | 14 | 18 | 21 | 18 |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Bell |
| Aircraft Name | H145 | H160 | H175 | H215 | 525 Relentless |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 460 | 573 | 468 | 580 |
| DOC / nm / Seat | $ 0.93 | — | $ 0.75 | $ 0.91 | — |
| Max Cabin Seats | 9 | 12 | 18 | 22 | 16 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 4200 | 3992 | 6797 | 8903 | 6675 |
| Standard Cabin Seats | 8 | 12 | 16 | 19 | 16 |
| Direct Operating Cost | $ 1,210 | — | $ 2,016 | $ 2,708 | — |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS | EFIS | Garmin G5000H |
| Max Cruise Speed (ktas) | 130 | 155 | 149 | 142 | 160 |
| Base Aircraft Price (USD) | $10,200,000 | $14,000,000 | $17,900,000 | $27,500,000 | $15,000,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 2 | 2 | 2 |
| Total Seats | 10 | 14 | 18 | 21 | 18 |
| Configuration | Green Interior | Green Interior | — | — | — |
| Max Cabin Seats | 9 | 12 | 18 | 22 | 16 |
| Standard Cabin Seats | 8 | 12 | 16 | 19 | 16 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Dual-Channel |
| Model | Arriel 2E | HE Arrano | PT6A-67E | Makila 1A1 | CT7-2F1 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 | 3500 | 3000 | 4000 |
| Horsepower | 894 | — | 1775 | 1820 | 1800 |
| No. of Engines | 2 | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | — | — | — | 540 | 641 |
| Dimensions | |||||
| Length (ft) | 44.8 | 39.4 | 59.2 | 61.4 | 61.58 |
| Overall Height (ft) | 13 | 13.1 | 17.5 | 16.2 | 18.18 |
| Rotor Diameter (ft) | 36.1 | 45.2 | 48.5 | 51.2 | 54.5 |
| Cabin Volume (cu. ft) | 166 | — | 423.8 | 473.9 | — |
| Baggage Volume Ext. (cu. ft) | 46.8 | — | 81.9 | — | 128 |
| Width (ft) | — | — | — | — | 25.77 |
| Cabin Width (ft) | — | — | — | — | 7.58 |
| Cabin Height (ft) | — | — | — | — | 4.5 |
| Cabin Length (ft) | — | — | — | — | 15.5 |