Md Helicopters Md 500e vs Pilatus Pc 12 Ngx
The MD Helicopters MD 500E is a light, single‑engine helicopter typically used for short‑range missions such as training, patrol, utility work, or aerial observation. It generally carries a pilot plus about four passengers (depending on configuration and weight), making it best suited to small groups and flexible point‑to‑point access where landing space is limited. Its practical range is comparatively modest—on the order of a few hundred miles—reflecting helicopter speed, fuel capacity, and mission profiles. The Pilatus PC‑12 NGX is a single‑engine turboprop fixed‑wing aircraft designed for longer‑distance regional and business travel. It operates in a different category, emphasizing cruise speed, cabin comfort, and efficiency over range. Typical seating is around six to nine passengers plus pilots (depending on layout and regulations), and its range is far greater—commonly well over 1,000 miles—making it better for city‑to‑city trips and multi‑leg itineraries. In short, the MD 500E prioritizes access and hover/vertical capability, while the PC‑12 NGX prioritizes distance, payload, and cruise performance.
| Spec | MD Helicopters MD 500E | Pilatus PC-12 NGX |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 2.95 | $ 2.78 |
| Min Crew | 1 | 1 |
| Total Seats | 4 | 8 |
| Flight Rules | VFR | IFR |
| Manufacturer | MD Helicotpers | Pilatus |
| Aircraft Name | MD 500E | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 258 | 1803 |
| DOC / nm / Seat | $ 0.74 | $ 0.46 |
| Max Cabin Seats | 3 | 9 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 1483 | — |
| Standard Cabin Seats | 2 | 6 |
| Direct Operating Cost | $ 398 | $ 793 |
| Flight Deck (Base Spec) | Gyro / Analog | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 135 | 290 |
| Base Aircraft Price (USD) | $ 2,750,000 | $5,350,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 4 | 8 |
| Max Cabin Seats | 3 | 9 |
| Standard Cabin Seats | 2 | 6 |
| Lavatory | — | Optional |
| Cargo Door | — | Yes |
| Lavatory Location | — | FWD |
| Cabin Pressure (psi) | — | 5.8 |
| Galley / Refreshment | — | No |
| SL Cabin Altitude (ft) | — | 13100 |
| Engine | ||
| FADEC | No | Yes |
| Model | 250-C20B | PT6E-67XP |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 5000 |
| Horsepower | 420 | 1200 |
| No. of Engines | 1 | 1 |
| Fuel Burn (gph) | 35 | — |
| Fuel Capacity (gal) | 64 | — |
| Flat Rating | — | ISA + 35 |
| Usable Fuel (gal) | — | 402 |
| Dimensions | ||
| Length (ft) | 30.9 | 47.25 |
| Overall Height (ft) | 8.7 | 14 |
| Rotor Diameter (ft) | 26.4 | — |
| Wingspan (ft) | — | 53.33 |
| Cabin Width (ft) | — | 5 |
| Cabin Height (ft) | — | 4.9 |
| Cabin Length (ft) | — | 16.9 |
| Cabin Width - Floor (ft) | — | 4.25 |
| Baggage Volume Int. (cu. ft) | — | 40 |