With a five-blade main rotor and a choice of 420-shp Rolls-Royce 250-C20B or 450-shp Rolls-Royce 250-C20R turbine engine, the MD 500E offers unparalleled versatility for a wide range of customer-defined mission profiles.

The MD Helicopters MD 500 series is an American family of light utility civilian and military helicopters. The MD 500 was developed from the Hughes 500, a civilian version of the US Army's OH-6A Cayuse/Loach. The series currently includes the MD 500E, MD 520N, and MD 530F. The MD 500 was initially produced by Hughes Helicopters as the Hughes ...

With a five-blade main rotor and a Rolls-Royce M250-C20 turbine engine, the MD 500E is the best performing helicopter in its class. The MD 500E has a relatively small diameter main rotor system and a short tail with a high horizontal stabilizer with two tip plates to provide vertical, longitudinal, and lateral stability in forward flight.

2021年9月14日 · MD 500E Price and Operating Costs Specifications. The MD 500E, production in 1983 – to present, requires a one man crew and can be configured in 3 seats. Maximum operating altitude of 16,000′, a optimal cruise speed of 135 knots/156 …

With a five-blade main rotor and a choice of 420-shp Rolls-Royce 250-C20B or 450-shp Rolls-Royce 250-C20R turbine engine, the MD 500E ofers unparalleled versatility for a wide range of customer-defined mission profiles.

The MD 500E is a lightweight, twin engine helicopter that was manufactured in the United States. The aircraft was produced by McDonnell Douglas Helicopter Company and first flown on July 9th, 1968. It had a maximum gross weight of 3,600 pounds and an empty weight of 1,890 pounds.

The MD 500E light turbine helicopter allows easy configuration conversion from a five-place personnel transport to a utility helicopter. With a five-blade main rotor and either a 420-shp Rolls-Royce 250-C20B turbine engine or an optional 450-shp Rolls-Royce 250-C20R/2 turbine engine, the MD 500E is the best performing helicopter in its class.

The MD 500E helicopter is powered by a single Rolls-Royce turboshaft engine, both type 250-C20B 313kW (420shp) or 250-C20R 336kW (450shp), providing 280kW take-off power. MD 500E has a maximum cruising speed of 135 knots (249 kpj / 155 mph), operating altitude of 16,000 ft, and a range of 290 nm.

Powered by a Rolls-Royce 250-C20B turboshaft engine, the MD 500E offers a top cruise speed of approximately 136 knots (155 mph) and a maximum range of 300 nautical miles. It can carry up to five passengers, including the pilot, and has a maximum gross weight of 3,000 lbs.

The MD 500E helicopter is powered by a single Rolls-Royce turboshaft engine, either a type 250-C20B 313kW (420shp) or a 250-C20R 336kW (450shp), providing 280kW take-off power. The MD 530F is fitted with a Rolls-Royce 250-C30 485kW (650shp) turboshaft engine.