Airbus Helicopters H160 vs Airbus Helicopters H215 vs Bell 525 Relentless vs Sikorsky S 92
In category, the Airbus H160 is a modern medium twin aimed at offshore, EMS, and corporate/VIP missions with strong emphasis on efficiency and low noise. The Airbus H215 and Sikorsky S-92 sit in the heavy twin class for higher-lift offshore transport and utility roles, while the Bell 525 Relentless is a super-medium twin positioned between traditional medium and heavy types, targeting high-speed offshore and executive transport. For range, the H160 and Bell 525 generally lead the group in typical long-range configurations for their class, often offering greater reach than older medium/heavy designs on comparable payloads. The H215’s range is competitive but is typically optimized around robust lifting capability and mission flexibility rather than maximum distance. The S-92 is designed around offshore mission profiles with solid range and reserves, usually competitive with the H215 and often dependent on cabin fit and fuel options. For passenger capacity, the H160 typically carries fewer passengers than the other three, reflecting its medium footprint. The Bell 525 usually carries more than the H160 and can approach lower-end heavy-mission seating. The H215 and S-92 generally offer the highest passenger capacity, commonly configured for larger offshore loads.
| Spec | AIRBUS H160 | AIRBUS H215 | Bell 525 Relentless | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 14 | 21 | 18 | 21 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Bell | Sikorsky |
| Aircraft Name | H160 | H215 | 525 Relentless | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 460 | 468 | 580 | 439 |
| Max Cabin Seats | 12 | 22 | 16 | 19 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 3992 | 8903 | 6675 | 7417 |
| Standard Cabin Seats | 12 | 19 | 16 | 19 |
| Flight Deck (Base Spec) | EFIS | EFIS | Garmin G5000H | EFIS |
| Max Cruise Speed (ktas) | 155 | 142 | 160 | 155 |
| Base Aircraft Price (USD) | $14,000,000 | $27,500,000 | $15,000,000 | $30,650,000 |
| DOC / nm | — | $ 19.07 | — | $ 19.79 |
| DOC / nm / Seat | — | $ 0.91 | — | $ 0.94 |
| Direct Operating Cost | — | $ 2,708 | — | $ 3,068 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 14 | 21 | 18 | 21 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 12 | 22 | 16 | 19 |
| Standard Cabin Seats | 12 | 19 | 16 | 19 |
| Engine | ||||
| FADEC | Yes | Yes | Dual-Channel | Yes |
| Model | HE Arrano | Makila 1A1 | CT7-2F1 | CT7-8A |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3000 | 4000 | 4000 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Horsepower | — | 1820 | 1800 | 2520 |
| Fuel Capacity (gal) | — | 540 | 641 | 760 |
| Dimensions | ||||
| Length (ft) | 39.4 | 61.4 | 61.58 | — |
| Overall Height (ft) | 13.1 | 16.2 | 18.18 | 17.8 |
| Rotor Diameter (ft) | 45.2 | 51.2 | 54.5 | — |
| Cabin Volume (cu. ft) | — | 473.9 | — | 775 |
| 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 | 140 |