Airbus Helicopters H145 vs Airbus Helicopters H175 vs Bell 412epi vs Leonardo Aw139 vs Sikorsky S 76d
All five are twin‑engine civil helicopters, but they span light to medium classes with different typical missions. The Airbus H145 is a light twin aimed at EMS, police, and utility work, offering roughly 350–400 nm of range and typically 8–10 passengers (about 1–2 pilots plus up to 9 in high‑density layouts). The Sikorsky S‑76D is also a light twin but optimized for corporate/offshore transport, with broadly similar range around 400 nm and usually 8–12 passengers depending on interior. Moving up, the Bell 412EPi is a medium twin utility helicopter emphasizing hot‑and‑high and lifting capability; it commonly carries about 10–13 passengers and reaches roughly 350–400 nm. The Leonardo AW139 is a fast, modern medium twin widely used offshore and for SAR, typically seating about 12–15 passengers with around 500–600 nm range. At the larger end here, the Airbus H175 is a super‑medium twin designed heavily around offshore and SAR, generally carrying about 16–18 passengers with range commonly around 550–650 nm. Actual figures vary with fuel, payload, and cabin configuration.
| Spec | AIRBUS H145 | AIRBUS H175 | Bell 412EPi | AGUSTA / LEONARDO AW139 | Sikorsky S-76D |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 9.31 | $ 13.53 | $ 12.09 | $ 11.69 | $ 11.49 |
| Min Crew | 1 | 2 | 1 | 2 | 2 |
| Total Seats | 10 | 18 | 14 | 17 | 12 |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Bell | Leonardo | Sikorsky |
| Aircraft Name | H145 | H175 | 412EPi | AW139 | S-76D |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 573 | 361 | 573 | 441 |
| DOC / nm / Seat | $ 0.93 | $ 0.75 | $ 0.86 | $ 0.69 | $ 0.96 |
| Max Cabin Seats | 9 | 18 | 13 | 15 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 6797 | 4829 | 4701 | — |
| Standard Cabin Seats | 8 | 16 | 13 | 15 | 10 |
| Direct Operating Cost | $ 1,210 | $ 2,016 | $ 1,487 | $ 1,929 | $ 1,781 |
| Flight Deck (Base Spec) | EFIS | EFIS | Bell BasiX-Pro | EFIS | Thales TopDeck |
| Max Cruise Speed (ktas) | 130 | 149 | 123 | 165 | 155 |
| Base Aircraft Price (USD) | $10,200,000 | $17,900,000 | $ 12,500,000 | $15,900,000 | $14,900,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 1 | 2 | 2 |
| Total Seats | 10 | 18 | 14 | 17 | 12 |
| Configuration | Green Interior | — | — | — | — |
| Max Cabin Seats | 9 | 18 | 13 | 15 | 10 |
| Standard Cabin Seats | 8 | 16 | 13 | 15 | 10 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | Arriel 2E | PT6A-67E | PT6T-9 | PT6C-67C | PW210S |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3500 | 4000 | 5000 | 4000 |
| Horsepower | 894 | 1775 | 1370 | 1679 | 1077 |
| No. of Engines | 2 | 2 | 2 | 2 | 1 |
| Fuel Burn (gph) | — | — | 113 | — | — |
| Fuel Capacity (gal) | — | — | 330.5 | 414 | 296 |
| Dimensions | |||||
| Length (ft) | 44.8 | 59.2 | 52.1 | 54.7 | 52.5 |
| Overall Height (ft) | 13 | 17.5 | 11.5 | 16.4 | 14.5 |
| Rotor Diameter (ft) | 36.1 | 48.5 | 46 | 54.7 | 44 |
| Cabin Volume (cu. ft) | 166 | 423.8 | 220 | 282 | — |
| Baggage Volume Ext. (cu. ft) | 46.8 | 81.9 | 28 | 120 | — |
| Width (ft) | — | — | 33 | — | — |