14、)AN, GT, FTAC 23-1923.302 Canard or tandem wing configurations.AN, GT, FTAC 23-1923.303 Factor of safety. (3.172)AN, GTAC 23-1923.305 Strength and deformation. (3.173)AN, GTAC 23-19, PS-ACE100-2001-006, PS-ACE100-2004-1003023.307 Proof of structure. (3.174)AN, GTAC 23-19, ...
23.303 Factor of safety. (3.172) 23.305 Strength and deformation. (3.173) 23.307 Proof of structure. (3.174) FT FT AC 23-8B, PS-ACE100-2001-004, PS-ACE100-2002-008 AC 23-8B AN, GT, FT AN, GT, FT AN, GT AN, GT AN, GT AC 23-19 AC 23-19 AC 23-19 AC 23-19, PS-ACE...
According to a report by the National Transportation Safety Board (NTSB), pilot fatigue was the major factor in an accident of a commuter jet operated by Pinnacle Airlines in April 2007. With this finding, the Federal Aviation Administration (FAA) scheduled a symposium in June 2008 in Vienna ...
AN, GT, FT AC 23-19 23.303 Factor of safety. (3.172) AN, GT AC 23-19 23.305 Stre ngth and deformati on. (3.173) AN, GT AC 23-19, PS-ACE100-2001-006, PS-ACE100-2004-10030 23.307 Proof of structure. (3.174) AN, GT AC 23-19, PS-ACE100-2001-006, PS-ACE100-2004-10030 ...
and stability on water.25.231MISCELLANEOUS FLIGHT REQUIREMENTS25.251Vibration and buffeting.25.253 High-speed characteristics.25.255 Out-of-trim characteristics.Subpart C —StructureGENERAL25.30125.303 Factor of safety.25.305 Strength and deformation.25.307 Proof of structure.Loads.FLIGHT LOADS25.321General.FLIG...
Section25.1435of14CodeofFederalRegulations(CFR)part25,asamendedthroughAmendment25-104,andothersectionsrelatingtohydraulicinstallations.a.RelatedFederalAviationRegulations(FAR).Sectionswhichcontainrequirementsforthedesign,substantiationandcertificationofhydraulicsystemsinclude:§25.301Loads.§25.303Factorofsafety.§25.863...
But there are multiple pieces of the FAA’s NextGen program that use ADS-B surveillance data that are in jeopardy, according to NATCA’s Jim Ullmann, director of safety and technology. They aren’t nationwide, but he calls them “really big-ticket items.” ...
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The bin A. may have an open top if it is placed in front of the passengers and the cargo is secured by a cargo net. B. must withstand the load factor required of passenger seats, multiplied by 1.15, using the combined weight of the bin and the maximum weight of the cargo that may...
and to use a factor of safety of 2 ½ to 3; but…[with] R31, R36 and R80, the fins failed during their trial flights... [due to] these failures the factors of safety in the girders should be at least 3½ when assuming the above loading… Also, the loading of 2 lb per sq...