Md Helicopters Md 600n vs Sikorsky S 76d
The MD Helicopters MD 600N and Sikorsky S‑76D sit in different market categories. The MD 600N is a light single‑engine utility helicopter, typically used for roles like law enforcement, light passenger transport, and general utility work. The Sikorsky S‑76D is a medium twin‑engine helicopter positioned for higher-end corporate/VIP transport and offshore missions where twin-engine redundancy and greater performance margins are valued. In range, the S‑76D generally offers a longer practical mission radius and more fuel/reserve flexibility than the MD 600N, especially when configured for passenger transport at higher cruise speeds. The MD 600N’s range is suitable for shorter regional legs and local operations, but it is usually optimized more for simplicity and lower operating costs than maximum distance. Passenger capacity also separates them. The MD 600N is commonly configured for about five to six passengers (plus pilot), whereas the S‑76D typically carries a larger group, often around eight passengers in standard executive layouts (plus crew), with a larger cabin that better supports comfort and baggage.
| Spec | MD Helicopters MD 600N | Sikorsky S-76D |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.06 | $ 11.49 |
| Min Crew | 1 | 2 |
| Total Seats | 6 | 12 |
| Flight Rules | VFR | IFR |
| Manufacturer | MD Helicotpers | Sikorsky |
| Aircraft Name | MD 600N | S-76D |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 441 |
| DOC / nm / Seat | $ 0.68 | $ 0.96 |
| Max Cabin Seats | 5 | 10 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2000 | — |
| Standard Cabin Seats | 5 | 10 |
| Direct Operating Cost | $ 545 | $ 1,781 |
| Flight Deck (Base Spec) | Gyro / Analog | Thales TopDeck |
| Max Cruise Speed (ktas) | 134 | 155 |
| Base Aircraft Price (USD) | $3,400,000 | $14,900,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 2 |
| Total Seats | 6 | 12 |
| Max Cabin Seats | 5 | 10 |
| Standard Cabin Seats | 5 | 10 |
| Engine | ||
| FADEC | No | Yes |
| Model | 250-C47 | PW210S |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 2000 | 4000 |
| Horsepower | 715 | 1077 |
| No. of Engines | 1 | 1 |
| Fuel Burn (gph) | 41 | — |
| Fuel Capacity (gal) | 118 | 296 |
| Dimensions | ||
| Length (ft) | 36.9 | 52.5 |
| Overall Height (ft) | 9.7 | 14.5 |
| Rotor Diameter (ft) | 27.5 | 44 |