Structural Design. The Aircraft is a swept-wing monoplane with a pressurized cabin and is capable of accommodating a pilot, a co-pilot, a third crewmember and up to 19 passengers. The Aircraft structure, in general, is fabricated from aluminum alloy but also includes alloy steels, stainless steel, titanium and composites. Materials used are in accordance with standard U.S. aerospace industry specifications for aircraft quality materials. The Aircraft structure and systems are designed and installed to facilitate inspection, maintenance and permit ready removal of appropriate items. Parts and assemblies subject to ready removal from the Aircraft are interchangeable and/or replaceable from one BD-700-1A10 aircraft to another where Seller considers this practical. The Aircraft and its installed equipment is certified to operate at ground level ambient temperatures from -30ºC (-22ºF) to +45ºC (+113ºF). The Aircraft pressurization system is certificated for operations up to a maximum of pressure altitude of 51,000 ft.
Appears in 2 contracts
Sources: Aircraft Purchase Agreement (Williams Sonoma Inc), Aircraft Purchase Agreement (Williams Sonoma Inc)