Code: 21LDA2-E Aircraft 2
Lecturer: Max Chopart MSc. Weekly load: 2P+1C Completion: A, EX
Department: 16121 Credits: 4 Semester: W
Description:
Manufacturers responsibility, responsibilities of operator and professional supervising. Legislation in area of airworthiness. International and national standards. Static solidity of aircraft structures. Aeroelasticity. Inherent and operational reliability of aircraft structure. Fatigue strength. Aircraft structure lifetime presumption.
Recommended literature:
Beňo, L.: Lietadlá, vysokoškolská učebnice, Bratislava, Praha, Alfa + SNTL 1988
Schindler, J.: Letová způsobilost a spolehlivost, script, Praha, CVUT 1982
Regulations: Part 21, Part 26

Keywords:
airworthiness, certiffication process, load factor, manoeuvring envelope, gust loading envelope, ground cases of aircraft loading, aeroelasticity, operational reliability, fatigue issues

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