With the design and development guided by the international helicopter industry advisory board, the objective of this multipurpose, twin-engine helicopter was to set a new standard in performance, affordability, dependability and safety.
Certified: FAA & JAA for day/night VFR, single pilot IFR
Engines: Two Pratt & Whitney Canada PW207E
Main Rotor: Fully articulated system
Anti-torque Control: NOTAR
Cruise Speed: 131 Knt (246 kph / 152 mph)
Useful Internal Load: 6,500 pounds
Maximum Altitude: 14,000 feet
Seats: 8
Separate Baggage Compartment: 52 cubic feet
These single-turbine engine helicopters provide high performance and increased capacity to give the customer greater versatility. All with dramatically low operating costs. It flies faster, hovers higher, and provides the agility and exceptional handling for which the MD 500® series is known.
Certified: FAA & JAA for single pilot VFR
Engine: Rolls Royce 250-C47
Main Rotor: Fully articulated 6 blade system
Anti-torque Control: NOTAR
Seats: 8Cruise Speed: 138 Knt (248 kph/ 154 mph)
Useful Internal Load: 2000 pounds / 907 kg max
Maximum Altitude: 20,000 feet
The "all purpose" MD 520N is a fast, agile, lightweight, turbine powered helicopter. Advanced technology has been used in the design and construction of the aircraft, resulting in excellent speed capabilities, high payload-to-empty-weight ratio, passenger/crew safety and handling and performance capabilities. This is one of the safest, quietest helicopters in the world.
Certified: FAA & JAA for single pilot VFR
Engines: Rolls Royce 250-C20R/2 turbine engine
Main Rotor: Fully articulated 5 blades system
Anti-torque Control: NOTAR
Cruise Speed: 123 Knt (229 kph / 142 mph)
Useful Internal Load: 1,764 pounds
Maximum Altitude: 20,000 feet
Seats: 5
Engineered to meet your requirements for hot-day, high-altitude operation - allows extra efficient operation in Hot Day Operation
The MD 530F's high altitude lift capability is achieved by main-rotor blades six inches longer than the MD 500E. The tailboom is extended eight inches and the tail rotor blades have been lengthened to provide increased thrust and directional control at high altitudes.
Certified: FAA & JAA for single pilot VFR
Engines: Rolls-Royce 250-C30
Main Rotor: Fully articulated 5 blades system
Anti-torque Control: NOTAR
Cruise Speed: 135 Knt (249 kph / 155 mph)
Useful Internal Load: 1,519 pounds
Maximum Altitude: 16,000 feet
Seats: 5
The MD 500E® helicopter delivers the highest speed, payload and productivity in its class. Rear seat passengers have greater headroom and visibility than earlier Model 500s. Refinements provide first class front and rear seating with ample legroom. The T-shaped instrument panel provides place for a full complement of modern avionics.
Certified: FAA & JAA for single pilot VFR
Engines: Rolls-Royce 250-C20B or C20R/2
Main Rotor: Fully articulated 5 blades system
Cruise Speed: 135 Knt (249 kph / 155 mph)
Useful Internal Load: 1,483 pounds
Maximum Altitude: 16,000 feet
Seats: 5
If you require more information on this aircraft please use the contact details below.
