Bell 412epi vs Leonardo Aw139 vs Leonardo Aw189 vs Leonardo Sh09 vs Md Helicopters Md 500e
The Bell 412EPi and MD Helicopters MD 500E sit in lighter, utility-focused categories, while the Leonardo AW139 and AW189 are medium twins aimed at higher-capacity transport and offshore/EMS roles; the Leonardo SH09 (single‑engine) fits between light utility and light/intermediate passenger transport. In range, the MD 500E is typically shortest-range among these and is most often used for local missions. The Bell 412EPi generally offers moderate range for utility, EMS, and multi‑role work, usually exceeding light singles in practical mission radius. The SH09 is designed for efficient regional transport with a range broadly comparable to modern light/intermediate singles, typically below medium twins. The AW139 commonly provides longer range than the 412EPi/SH09 class and is a frequent choice where speed and legs between stops matter. The AW189 is the long‑leg, heavy‑lift option here, generally offering the greatest range and endurance. For passenger capacity, the MD 500E carries the fewest (often 4–5), the SH09 and Bell 412EPi are mid-pack (typically around 8–13 depending on fit), the AW139 is higher (often about 12–15), and the AW189 is highest (commonly up to around 16–19).
| Spec | Bell 412EPi | AGUSTA / LEONARDO AW139 | AGUSTA / LEONARDO AW189 | AGUSTA / LEONARDO SH09 | MD Helicopters MD 500E |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 12.09 | $ 11.69 | $ 15.57 | $4.48 | $ 2.95 |
| Min Crew | 1 | 2 | 1 | 1 | 1 |
| Total Seats | 14 | 17 | 21 | 8 | 4 |
| Flight Rules | IFR | IFR | IFR | VFR | VFR |
| Manufacturer | Bell | Leonardo | Leonardo | Leonardo | MD Helicotpers |
| Aircraft Name | 412EPi | AW139 | AW189 | SH09 | MD 500E |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In-Development | FAA / EASA |
| Max Range (nm) | 361 | 573 | 651 | 430 | 258 |
| DOC / nm / Seat | $ 0.86 | $ 0.69 | $ 0.74 | $0.56 | $ 0.74 |
| Max Cabin Seats | 13 | 15 | 19 | 6 | 3 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4829 | 4701 | — | — | 1483 |
| Standard Cabin Seats | 13 | 15 | 19 | 6 | 2 |
| Direct Operating Cost | $ 1,487 | $ 1,929 | $ 2,413 | $627 | $ 398 |
| Flight Deck (Base Spec) | Bell BasiX-Pro | EFIS | EFIS | EFIS | Gyro / Analog |
| Max Cruise Speed (ktas) | 123 | 165 | 155 | 140 | 135 |
| Base Aircraft Price (USD) | $ 12,500,000 | $15,900,000 | $2,413,000 | $3,500,000 | $ 2,750,000 |
| Max Passengers | — | — | — | 7 | — |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 1 | 1 | 1 |
| Total Seats | 14 | 17 | 21 | 8 | 4 |
| Max Cabin Seats | 13 | 15 | 19 | — | 3 |
| Standard Cabin Seats | 13 | 15 | 19 | 6 | 2 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | No |
| Model | PT6T-9 | PT6C-67C | CT7-2E1 | HTS 900 | 250-C20B |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 5000 | 4000 | 5500 | 3500 |
| Horsepower | 1370 | 1679 | 1983 | 1020 | 420 |
| No. of Engines | 2 | 2 | 2 | 1 | 1 |
| Fuel Burn (gph) | 113 | — | — | — | 35 |
| Fuel Capacity (gal) | 330.5 | 414 | — | — | 64 |
| Dimensions | |||||
| Width (ft) | 33 | — | — | — | — |
| Length (ft) | 52.1 | 54.7 | 57.8 | — | 30.9 |
| Overall Height (ft) | 11.5 | 16.4 | 16.6 | — | 8.7 |
| Rotor Diameter (ft) | 46 | 54.7 | 48 | — | 26.4 |
| Cabin Volume (cu. ft) | 220 | 282 | 395 | — | — |
| Baggage Volume Ext. (cu. ft) | 28 | 120 | 85 | — | — |