Aircraft 2

The course is not on the list Without time-table

Code	Completion	Credits	Range	Language
16LLA2	Z,ZK	2	2P+1C	Czech

Garant předmětu:

Lecturer:

Tutor:

Supervisor:

Department of Vehicle Technology

Synopsis:

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.

Requirements:

16LLA1

Syllabus of lectures:

Syllabus of tutorials:

Study Objective:

Solving problems of airworthiness of an aeroplane when an executive point of view is demanded at civil air operator's environment. Knowledge required for managing technical handling and technical operation of an aircraft. The subject provides also basic orientation in the field of operational reliability and safe life of an airplane.

Study materials:

Beňo, L,: Lietadlá, Alfa Bratislava + SNTL Praha 1988, ISBN 063-562-88

Předpis L-7, Ministerstvo dopravy ČR v platném znění

Předpis L-8, Ministerstvo dopravy ČR v platném znění

Thomas Henry Gordon Megson: Aircraft Structures for Engineering Students, Butterworth-Heinemann 2017

Note:

Further information:

No time-table has been prepared for this course

The course is a part of the following study plans:

TUL bak.prez.22/23 (program TUL) (compulsory course in the program)