Sikorskys92 vs Airbus Helicopters H175 vs Bell 525 Relentless
The Sikorsky S‑92 is typically positioned as a heavy, long-range offshore and utility helicopter, generally offering the greatest cabin volume and passenger capacity of the three, commonly configured around 18–19 passengers in offshore layouts (and more in high-density arrangements). Its range is strong for extended overwater missions and it is widely used for oil-and-gas transport and government roles. The Airbus H175 sits in the super‑medium class, optimized for offshore and SAR with a balance of payload, operating costs, and cabin comfort. Passenger capacity is commonly in the mid-to-high teens depending on configuration, and its range is competitive for typical offshore sectors, though usually not aimed at the same “heavy” lift bracket as the S‑92. The Bell 525 Relentless is a modern super‑medium emphasizing speed, advanced avionics, and efficient long-range capability. It generally targets similar passenger counts to the H175 (often mid-to-high teens) with a range intended to be highly competitive in the super‑medium category, bridging some of the gap toward heavy-class mission profiles without matching the S‑92’s maximum cabin and capacity focus.
| Spec | AIRBUS H175 | Bell 525 Relentless |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 13.53 | — |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 18 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bell |
| Aircraft Name | H175 | 525 Relentless |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 573 | 580 |
| DOC / nm / Seat | $ 0.75 | — |
| Max Cabin Seats | 18 | 16 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6797 | 6675 |
| Standard Cabin Seats | 16 | 16 |
| Direct Operating Cost | $ 2,016 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H |
| Max Cruise Speed (ktas) | 149 | 160 |
| Base Aircraft Price (USD) | $17,900,000 | $15,000,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 18 |
| Max Cabin Seats | 18 | 16 |
| Standard Cabin Seats | 16 | 16 |
| Engine | ||
| FADEC | Yes | Dual-Channel |
| Model | PT6A-67E | CT7-2F1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 4000 |
| Horsepower | 1775 | 1800 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | — | 641 |
| Dimensions | ||
| Length (ft) | 59.2 | 61.58 |
| Overall Height (ft) | 17.5 | 18.18 |
| Rotor Diameter (ft) | 48.5 | 54.5 |
| Cabin Volume (cu. ft) | 423.8 | — |
| Baggage Volume Ext. (cu. ft) | 81.9 | 128 |
| Width (ft) | — | 25.77 |
| Cabin Width (ft) | — | 7.58 |
| Cabin Height (ft) | — | 4.5 |
| Cabin Length (ft) | — | 15.5 |