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MD Explorer
MD Explorer
Multi-Purpose. Affordable. Dependable. High-Performance.
- Product Introduction
- Technical Specification
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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