For the type certification of the Euro-ENAER Eaglet, compliance with airworthiness requirements must be proved. The Eaglet is to be used as a trainer and must fulfil the requirements of the JAR 23 utility category. One part of the JAR 23 is the flight performance requirements. These requirements comprehend all flight manoeuvres for which certification is requested. In general, performance data of the aircraft must be determined for all flight situations described in the requirements for a broad range of atmospheric conditions. These data have to be presented in the aircraft flight manual as information for the pilot. The numerous performance data can be determined partly by flight tests and partly by calculations, inter- and extrapolating flight test data to all required circumstances. For these calculations, a correct understanding of all aircraft characteristics is necessary. The characteristics are partly provided by manufacturers of various aircraft parts (engine, propeller) and lacking information has to be obtained from flight test data or theoretical derivations. This has been done for take-off, climb, cruise and glide.
Calculation Methods for the Performance Certification of the Euro-ENAER Eaglet
1998
96 pages
Report
No indication
English
Aeronautics , Human Factors Engineering , Air Transportation , Flight tests , Pilot performance , Certification , Calculation methods , Manual control , Flight maneuvers , Compliance , Flight operations , Flight management systems , Aircraft engines , Airworthiness , Requirements , Nomenclature , Flight control systems , Flight simulators , Atomspheric entry , Europe , Foreign technology
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