Md Helicopters Md 500e vs Pilatus Pc 12 Ngx
The MD Helicopters MD 500E and the Pilatus PC-12 NGX sit in very different aircraft categories. The MD 500E is a light single‑engine helicopter designed for low‑altitude, short‑to‑medium missions such as utility work, law enforcement, training, and observation, with the ability to operate from confined areas and land without runways. The PC‑12 NGX is a single‑engine turboprop airplane built for efficient, pressurized, fixed‑wing transport, typically used for regional business travel, air ambulance, and cargo, requiring runways but offering higher cruise speed and altitude capability. In range, the MD 500E is generally suited to shorter legs, typically on the order of a few hundred nautical miles depending on payload and reserves, whereas the PC‑12 NGX is optimized for long regional sectors, commonly around 1,500 nautical miles class, again depending on configuration and conditions. Passenger capacity also differs sharply: the MD 500E typically carries a pilot plus up to four passengers in standard seating, while the PC‑12 NGX commonly accommodates a pilot or two plus about six to nine passengers in an executive layout, with flexible options for cargo or medical interiors.
| 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 |