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AW101 airframe diagram. The AW101 follows a conventional design layout, but makes use of advanced technologies, such as the design of the rotor blades, avionics systems, and extensive use of composite materials. [38] The fuselage structure is modular and comprises an aluminium–lithium alloy, designed to be both light and damage-resistant. [39]
Data from Jane's All The World's Aircraft 1969–70 General characteristics Crew: 2 Capacity: up to 36 pax / 18 stretchers with 5 attendants / 5,000 kg (11,000 lb) payload Length: 20.19 m (66 ft 3 in) including tail-rotor Width: 4.64 m (15 ft 3 in) rotor blades folded Height: 6.56 m (21 ft 6 in) to top of rotor head Empty weight: 6,850 kg (15,102 lb) Gross weight: 12,400 kg (27,337 lb) Max ...
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The AgustaWestland CH-149 Cormorant is the Canadian Armed Forces designation for the AgustaWestland AW101 (formerly EH101), a helicopter used for air-sea rescue in Canada. Developed from AgustaWestland in Italy (now merged as part of Leonardo ), the CH-149 is a medium-lift helicopter for military applications.
AgustaWestland; Bell Helicopter (assembly) Variant of the AgustaWestland AW101 designed to replace the United States Marine Corps' Marine One presidential transport fleet. In January 2005, the US101 was selected for the VXX Presidential Helicopter Replacement Program, and was promptly re-designated as the VH-71. However, development was subject ...
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Pages in category "AgustaWestland aircraft" The following 17 pages are in this category, out of 17 total. ... AgustaWestland AW101; AgustaWestland AW109;
An AW101 undergoing VH-71 testing near the Lockheed facility in Owego, New York. Delays and engineering issues plagued the VH-71's development. [31] By 2007, the estimated cost of developing and modifying the aircraft had risen by 40% to $2.4 billion and had passed the $4.2 billion expected for the production of the fleet. [32]