Sustav vođenja plovidbenosti helikoptera Eurocopter EC 135 prema zahtjevima PART-a M

master's thesis

• Title (english): Eurocopter EC 135 Airworthiness Management System According to PART M Requirements
• Author: Amalija Vlaović
• Mentor: Anita Domitrović (mentor)
• Committee member: Ernest Bazijanac (predsjednik povjerenstva)
• Committee member: Matija Bračić (član povjerenstva)
• Committee member: Andrija Vidović (član povjerenstva)
• Granter: University of Zagreb; Faculty of Transport and Traffic Sciences; (Division of Transport); (Department of Air Transport); Zagreb
• Defense date and country: 2020-09-01, 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: kontinuirana plovidbenost zrakoplova; zrakoplovni propisi; PART M; održavanje zrakoplova; helikopter; EC135
• Keywords (english): continuing airworthiness of an aircraft; aviation regulations; PART M; aircraft maintenance; helicopter; EC135
• Language: croatian
• URN:NBN: urn:nbn:hr:119:497054
• Study programme: Title: 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 resource: Text
• File origin: Born digital
• Access conditions: Open access
• Created on: 2020-10-13 09:46:03