The existing international standards and recommended practices for light propeller driven airplane noise as published in annex 16 to the Convention on International Civil Aviation are reviewed. These airplanes are defined as having a maximum certificated takeoff mass below 9000 kg. The determination of atmospheric attenuation rate and the establishment of a confidence level are discussed.
Propeller-Driven-Small Airplane Noise Certification
1990
31 pages
Report
No indication
English