Airbus Helicopters H160 vs Airbus Helicopters H225 vs Md Helicopters Md 530f vs Sikorsky S 76d vs Sikorsky S 92
The Airbus H160 and Sikorsky S-76D sit in the medium twin category, typically optimized for corporate, EMS, and offshore support. Both usually offer mid-range endurance; the H160 is commonly positioned with a slightly longer usable range than many S-76D missions, while passenger capacity is broadly similar, generally around a dozen or fewer depending on interior and mission equipment. The Airbus H225 and Sikorsky S-92 are heavy twin helicopters aimed at high-demand offshore transport and SAR; they generally carry more passengers than the H160/S-76D class and are designed for longer offshore legs with higher payload, with typical seating often in the high teens and sometimes more in high-density layouts. The MD Helicopters MD 530F is a light single, best suited to utility, training, patrol, and light lift; it carries far fewer passengers (typically a small crew plus a few passengers) and has a notably shorter range than the twin-engine offshore-capable types. Overall, MD 530F is smallest/shortest-range, H160 and S-76D are mid-class and versatile, and H225 and S-92 are largest with the highest passenger capacity and offshore-oriented range.
| Spec | AIRBUS H160 | AIRBUS H225 | MD Helicopters MD 530F | Sikorsky S-76D | Sikorsky S-92 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 | 2 |
| Total Seats | 14 | 21 | 4 | 12 | 21 |
| Flight Rules | IFR | IFR | VFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | MD Helicotpers | Sikorsky | Sikorsky |
| Aircraft Name | H160 | H225 | MD 530F | S-76D | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 460 | 454 | 216 | 441 | 439 |
| Max Cabin Seats | 12 | 28 | 3 | 10 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3992 | 11929 | 1509 | — | 7417 |
| Standard Cabin Seats | 12 | 19 | 2 | 10 | 19 |
| Flight Deck (Base Spec) | EFIS | EFIS | Garmin G500H | Thales TopDeck | EFIS |
| Max Cruise Speed (ktas) | 155 | 142 | 134 | 155 | 155 |
| Base Aircraft Price (USD) | $14,000,000 | $ 29,500,000 | $ 3,400,000 | $14,900,000 | $30,650,000 |
| DOC / nm | — | $ 20.87 | $ 3.59 | $ 11.49 | $ 19.79 |
| DOC / nm / Seat | — | $ 0.99 | $ 0.90 | $ 0.96 | $ 0.94 |
| Direct Operating Cost | — | $ 2,963 | $ 480 | $ 1,781 | $ 3,068 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 | 2 |
| Total Seats | 14 | 21 | 4 | 12 | 21 |
| Configuration | Green Interior | — | — | — | — |
| Max Cabin Seats | 12 | 28 | 3 | 10 | 19 |
| Standard Cabin Seats | 12 | 19 | 2 | 10 | 19 |
| Engine | |||||
| FADEC | Yes | Yes | No | Yes | Yes |
| Model | HE Arrano | Makila 2A1 | 250-C30 | PW210S | CT7-8A |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3500 | 2000 | 4000 | 4000 |
| No. of Engines | 2 | 2 | 1 | 1 | 1 |
| Horsepower | — | 2100 | 650 | 1077 | 2520 |
| Fuel Capacity (gal) | — | 684 | 64 | 296 | 760 |
| Fuel Burn (gph) | — | — | 35 | — | — |
| Dimensions | |||||
| Length (ft) | 39.4 | 63.4 | 32.2 | 52.5 | — |
| Overall Height (ft) | 13.1 | 16.3 | 8.7 | 14.5 | 17.8 |
| Rotor Diameter (ft) | 45.2 | 53.2 | 27.5 | 44 | — |
| Cabin Volume (cu. ft) | — | 547 | — | — | 775 |
| Baggage Volume Ext. (cu. ft) | — | — | — | — | 140 |