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1.1 The following requirements apply for the manufacture of weight-shift-control aircraft. This practice includes the production acceptance test requirements for weight-shift-control aircraft. 1.2 This practice applies to aircraft seeking civil aviation authority approval, in...
1.1 The following requirements apply for the manufacture of weight-shift-control aircraft. This practice includes the production acceptance test requirements for weight-shift-control aircraft. 1.2 This practice applies to aircraft seeking civil aviation authority approval, in...
1.1 The following requirements apply for the manufacture of weight-shift-control aircraft. This practice includes the production acceptance test requirements for weight-shift-control aircraft. 1.2 This practice applies to aircraft seeking civil aviation authority approval, in...
1.1 The following requirements apply for the manufacture of weight-shift-control aircraft. This practice includes the production acceptance test requirements for weight-shift-control aircraft. 1.2 This practice applies to aircraft seeking civil aviation authority approval, in...
The following requirements apply for the manufacture of weight-shift-control aircraft. This practice includes the production acceptance test requirements for weight-shiftcontrol aircraft. This practice applies to aircraft seeking civil aviation authority approval, in the form...
1.1 This specification covers the minimum airworthiness standards a manufacturer shall meet in the designing, testing, and labeling of weight-shift-control aircraft. 1.2 This specification covers only weight-shift-control aircraft in which flight control systems do not use...
This specification covers the minimum airworthiness standards a manufacturer shall meet in the designing, testing, and labeling of weight-shift-control aircraft. This specification covers only weight-shift-control aircraft in which flight control systems do not use hinged...
1.1 This specification covers the minimum airworthiness standards a manufacturer shall meet in the designing, testing, and labeling of weight-shift-control aircraft. 1.2 This specification covers only weight-shift-control aircraft in which flight control systems do not use...
1.1 This specification covers the minimum airworthiness standards a manufacturer shall meet in the designing, testing, and labeling of weight-shift-control aircraft. 1.2 This specification covers only weight-shift-control aircraft in which flight control systems do not use...
1.1 This specification covers the minimum airworthiness standards a manufacturer shall meet in the designing, testing, and labeling of weight-shift-control aircraft. 1.2 This specification covers only weight-shift-control aircraft in which flight control systems do not use...
1.1 This specification covers the minimum airworthiness standards a manufacturer shall meet in the designing, testing, and labeling of weight-shift-control aircraft. 1.2 This specification covers only weight-shift-control aircraft in which flight control systems do not use...
1.1 This specification covers the minimum airworthiness standards a manufacturer shall meet in the designing, testing, and labeling of weight-shift-control aircraft. 1.2 This specification covers only weight-shift-control aircraft in which flight control systems do not use...
The weight for cabin equipment is an important topic in the aviation business. The cabin equipment weight has a direct impact on the payload of the aircraft, operation cost and revenue of the airlines. Due to the number of aircraft seats, seats are one of the major weight...
This European Standard specifies the required characteristics of a light weight coaxial cable, 50 Ω, type KX for use in aircraft electrical systems at operating temperature between − 55 °C and 200 °C and specially for high frequency up to 6 GHz. Nevertheless, if needed, − 65 °C is also...
This European Standard specifies the required characteristics of a light weight coaxial cable, 50 Ω, type KW for use in aircraft electrical systems at operating temperature between -55 °C and 180 °C and specially for high frequency up to 6 GHz. Nevertheless, if needed, -65 °C is also...
This European Standard specifies the required characteristics of a light weight coaxial cable, 50 Ω, type KX for use in aircraft electrical systems at operating temperature between − 55 °C and 200 °C and specially for high frequency up to 6 GHz. Nevertheless, if needed, − 65 °C is also...
1.1 This guide covers the manufacture of Weight Shift aircraft and their qualification for certification. 1.2 This guide applies to Weight Shift Control aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation....
1.1 This guide covers the manufacture of Weight Shift aircraft and their qualification for certification. 1.2 This guide applies to Weight Shift Control aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation....
1.1 This practice covers minimum requirements for a quality assurance program for weight-shift-control aircraft. 1.2 This practice applies to weight-shift-control aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like...
