Airbus Helicopters H145 vs Md Helicopters Md 500e
The Airbus Helicopters H145 and the MD Helicopters MD 500E sit in different light-helicopter categories and are typically chosen for different mission profiles. The H145 is a twin‑engine light utility helicopter designed for higher payload, redundancy, and all‑weather public service roles such as HEMS, law enforcement, and offshore support. The MD 500E is a single‑engine light helicopter in the “500” family, optimized for agility, lower operating cost, and missions such as training, patrol, observation, and light utility work. In range, the H145 generally offers a longer practical reach than the MD 500E, helped by its larger fuel capacity and efficient cruise in typical utility configurations, while the MD 500E’s range is more modest and more sensitive to payload and reserve requirements. Passenger capacity also differs. The H145 typically carries one or two pilots plus a larger cabin load, commonly up to about eight to nine passengers depending on configuration. The MD 500E is usually configured for one pilot plus four passengers, with limited cabin volume compared with the H145.
| Spec | AIRBUS H145 | MD Helicopters MD 500E |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 9.31 | $ 2.95 |
| Min Crew | 1 | 1 |
| Total Seats | 10 | 4 |
| Flight Rules | IFR | VFR |
| Manufacturer | Airbus Helicopters | MD Helicotpers |
| Aircraft Name | H145 | MD 500E |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 258 |
| DOC / nm / Seat | $ 0.93 | $ 0.74 |
| Max Cabin Seats | 9 | 3 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 1483 |
| Standard Cabin Seats | 8 | 2 |
| Direct Operating Cost | $ 1,210 | $ 398 |
| Flight Deck (Base Spec) | EFIS | Gyro / Analog |
| Max Cruise Speed (ktas) | 130 | 135 |
| Base Aircraft Price (USD) | $10,200,000 | $ 2,750,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 10 | 4 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 9 | 3 |
| Standard Cabin Seats | 8 | 2 |
| Engine | ||
| FADEC | Yes | No |
| Model | Arriel 2E | 250-C20B |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3500 |
| Horsepower | 894 | 420 |
| No. of Engines | 2 | 1 |
| Fuel Burn (gph) | — | 35 |
| Fuel Capacity (gal) | — | 64 |
| Dimensions | ||
| Length (ft) | 44.8 | 30.9 |
| Overall Height (ft) | 13 | 8.7 |
| Rotor Diameter (ft) | 36.1 | 26.4 |
| Cabin Volume (cu. ft) | 166 | — |
| Baggage Volume Ext. (cu. ft) | 46.8 | — |