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MD Explorer

MD Explorer

Multi-Purpose. Affordable. Dependable. High-Performance.

  • Product Introduction
  • Technical Specification
  • Photo Gallery

  • Multi-Purpose. Affordable. Dependable. High-Performance.

    An international helicopter industry advisory board guided the design and development of the MD Explorer® with an objective to produce a multipurpose twin-engine helicopter that would set new standards in performance, affordability, dependability and safety.

    The MD Explorer® was initially certified under FAA Part 27 in December 1994, and is currently certified by FAA and JAA for day/night VFR and single pilot IFR with full Category A design standards to JAR-OPS 3 performance Class I.

    Powered by two Pratt and Whitney Canada PW207E engines, the MD Explorer® features a fully articulated main rotor system, bearingless composite flexbeams and rotor hub. Anti-torque control is provided by the patented NOTAR™ system that reduces pilot workload and external noise levels, and significantly improves safety in confined areas and on offshore platforms.

    The six-place MD Explorer® cabin is the largest in the light twin class and is accessed through two 52 inch (1.32m) sliding cabin doors and a large baggage compartment. Energy absorbing, stroking cabin seats meet stringent FAR Part 27.562 requirements up to 30g at 30 feet per second. The large cabin makes the MD Explorer® ideally suited for rapid role change from an Offshore/Onshore six-place passenger transport to Emergency Medical Services or Law Enforcement missions. Large selections of optional equipment have been fully qualified to meet various operational requirements. A heavy-duty cargo hook permits 3,000-pound (1360-KG) external load operations.

    MD Explorer® safety and maintainability are enhanced by built-in HIRF and lightning strike protection, built-in maintenance steps and platforms, and a composite airframe that is resistant to corrosion in a hostile marine environment.




  • MD Explorer


    Engine
    PW207E (2)
    MTOW
    2948 kg
    Standard Payload
    1418 kg
    ExternalPayload
    1600 kg
    HIGE
    3246①②m
    HOGE
    2676② m
    Max Cruise Speed
    244 km/hr
    Range
    607③④km
    Max Operating Altitude
    6097 m
    Seating
    2+6


    ①有地效悬停作业目前受制于起飞和着陆1524米密度高度的限制
    ②标准大气,白天
    ③ 主+副油箱:总燃油容量1308 磅,无储备
    ④1524 米,标准大气

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