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master's thesis
Sustav vođenja plovidbenosti helikoptera Eurocopter EC 135 prema zahtjevima PART-a M
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2020. urn:nbn:hr:119:497054
Vlaović, Amalija
University of Zagreb
Faculty of Transport and Traffic Sciences
Division of Transport
Department of Air Transport

Institutional repository: Faculty of Transport and Traffic Sciences

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Vlaović, A. (2020). Sustav vođenja plovidbenosti helikoptera Eurocopter EC 135 prema zahtjevima PART-a M (Master's thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:497054

Vlaović, Amalija. "Sustav vođenja plovidbenosti helikoptera Eurocopter EC 135 prema zahtjevima PART-a M." Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2020. https://urn.nsk.hr/urn:nbn:hr:119:497054

Vlaović, Amalija. "Sustav vođenja plovidbenosti helikoptera Eurocopter EC 135 prema zahtjevima PART-a M." Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2020. https://urn.nsk.hr/urn:nbn:hr:119:497054

Vlaović, A. (2020). 'Sustav vođenja plovidbenosti helikoptera Eurocopter EC 135 prema zahtjevima PART-a M', Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 04 October 2024, https://urn.nsk.hr/urn:nbn:hr:119:497054

Vlaović A. Sustav vođenja plovidbenosti helikoptera Eurocopter EC 135 prema zahtjevima PART-a M [Master's thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2020 [cited 2024 October 04] Available at: https://urn.nsk.hr/urn:nbn:hr:119:497054

A. Vlaović, "Sustav vođenja plovidbenosti helikoptera Eurocopter EC 135 prema zahtjevima PART-a M", Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2020. Available at: https://urn.nsk.hr/urn:nbn:hr:119:497054

Metadata
TitleSustav vođenja plovidbenosti helikoptera Eurocopter EC 135 prema zahtjevima PART-a M
Title (english)Eurocopter EC 135 Airworthiness Management System According to PART M Requirements
AuthorAmalija Vlaović
MentorAnita Domitrović (mentor)
Committee memberErnest Bazijanac (predsjednik povjerenstva)
Committee memberMatija Bračić (član povjerenstva)
Committee memberAndrija Vidović (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Transport)
(Department of Air Transport)
Zagreb
Defense date and country2020-09-01, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Plovidbenost zrakoplova može se definirati kao sposobnost zrakoplova za sigurnu zračnu plovidbu. Može se podijeliti na inicijalnu i kontinuiranu plovidbenost. Inicijalna plovidbenost označava opremljenost zrakoplova svim potrebnim i ispravnim uređajima, a kontinuirana neprekidno nadziranje stanja zrakoplova i održavanje istog na propisan način. EASA zrakoplovni propis koji se odnosi na kontinuiranu plovidbenost je Part-M. Kako bi mogao letjeti, svaki zrakoplov pa tako i helikopter, mora biti plovidben. Nakon što je helikopteru utvrđena inicijalna plovidbenost izdana od nadležnog tijela, potrebno je voditi i održavati kontinuiranu plovidbenost. U ovom diplomskom radu obrađeni su zahtjevi i odgovornosti za kontinuiranu plovidbenost i održavanje helikoptera. Opisane su tehničko-eksploatacijske karakteristike helikoptera EC135 te su analizirani postupci od izdavanja inicijalne do vođenja i produljenja kontinuirane plovidbenosti tijekom eksploatacije.
Abstract (english)
Airworthiness of an aircraft can be defined as the ability of an aircraft to operate safely. It can be divided into initial and continuing airworthiness. Initial airworthiness means equipping the aircraft with all necessary and working devices, and continuing includes condition monitoring and maintenance of the aircraft in the prescribed manner. EASA regulation related to continuing airworthiness is Part M. In order to be able to fly, every aircraft, including a helicopter, must be airworthy. After the initial airworthiness of the helicopter has been issued by the competent authorities, it is necessary to manage and maintain continuing airworthiness. This final thesis deals with the requirements and responsibilities for continuing airworthiness and maintenance of helicopters. The technical-operational characteristics of the EC135 helicopter are described, and the procedures from issuance of initial airworthiness to management and extension of continuous airworthiness during operation are analyzed.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:497054
Study programmeTitle: Traffic and Transport; specializations in: Road Traffic and Transport, Railway Traffic and Transport, Water Traffic and Transport, Air Traffic and Transport, Postal Traffic, Information and Communication Traffic, Urban Traffic and Transport
Course: Road Traffic and Transport
Study programme type: university
Study level: graduate
Academic / professional title: magistar/magistra inženjer/inženjerka prometa (magistar/magistra inženjer/inženjerka prometa)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2020-10-13 09:46:03