natgillin/translations-raw huggingface dataset:
In laying down measures for the implementation of common essential requirements in the field of airworthiness, the Commission must take care that they reflect the state of the art and the best practices, take into account worldwide aircraft experience and scientific and technical progress and allow for immediate reaction to established causes of accidents and serious incidents.
Pri določanju ukrepov za izvajanje skupnih bistvenih zahtev na področju plovnosti mora Komisija paziti, da odražajo stanje tehnike in najboljšo prakso, upoštevajo globalne letalske izkušnje ter znanstveni in tehnični napredek ter omogočajo takojšen odziv na ugotovljene vzroke nesreč in resnih incidentov.
The need to ensure uniformity in the application of common airworthiness and environmental requirements for aeronautical products, parts and appliances requires that common procedures be followed by the competent authorities of the Member States and, where applicable, the Agency to assess compliance with these requirements.
Potreba po zagotavljanju enotnosti pri uporabi skupnih zahtev glede plovnosti in okoljskih zahtev za letalske proizvode, dele in naprave zahteva, da pristojni organi držav članic in po potrebi agencija upoštevajo skupne postopke za ocenjevanje izpolnjevanja teh zahtev.
The Agency should develop certification specifications and guidance material to facilitate the necessary regulatory uniformity.
Agencija bi morala pripraviti certifikacijske specifikacije in smernice za lajšanje regulativne enotnosti.
It is necessary to recognise the continuing validity of certificates issued before the entry into force of Regulation (EC) No 1702/2003, in accordance with Article 69 of Regulation (EC) No 216/2008.
V skladu s členom 69 Uredbe (ES) št. 216/2008 je treba priznati stalno veljavnost potrdil, izdanih pred začetkom veljavnosti Uredbe (ES) št. 1702/2003.
In order to maintain a high uniform level of aviation safety in Europe, it is necessary to introduce changes to requirements and procedures for the certification of aircraft and related products, parts and appliances and of design and production organisations, in particular to elaborate the rules related to the demonstration of compliance with the type-certification basis and environmental protection requirements and to introduce the possibility to choose to comply with later standards for changes to type-certificates.
Da bi ohranili visoko enotno raven varnosti letalstva v Evropi, je treba spremeniti zahteve in postopke za certificiranje zrakoplovov in sorodnih proizvodov, delov in naprav ter potrjevanje projektivnih in proizvodnih organizacij, zlasti izpopolniti predpise o prikazu skladnosti z osnovo za certifikacijo tipa in zahtevami glede varstva okolja ter določiti, da je možno izpolnjevati poznejše standarde za spremembe certifikatov tipa.
The concept and complexity of auxiliary power units (APU) resembles that of aircraft engines and in some cases APU designs are even derived from engine designs.
Zasnova in kompleksnost pomožnih pogonskih enot (PPE) sta podobni zasnovi in kompleksnosti letalskih motorjev. V nekaterih primerih projekti za PPE celo temeljijo na motorskih projektih.
Changes to provisions for repairs to APU are therefore needed to restore consistency with repairs process to engines.
Spremeniti je treba določbe o popravilih PPE, da bi jih uskladili s postopkom popravila motorjev.
In order to subject non-complex motor-powered aircraft, recreational aircraft and related products, parts and appliances to measures that are proportionate to their simple design and type of operation, while maintaining a high uniform level of aviation safety in Europe, it is necessary to introduce changes to requirements and procedures for the certification of those aircraft and related products, parts and appliances and of design and production organisations and in particular, for the owners of European Light Aircraft below 2000 kg (ELA2) or below 1200 kg (ELA1), to introduce the possibility to accept certain not safety critical parts for installation without an EASA Form 1.
Da bi za nekompleksne zrakoplove na motorni pogon, rekreativna letala ter povezane proizvode, dele in naprave uvedli ukrepe, ki so sorazmerni z njihovo enostavno zasnovo in vrsto operacij, obenem pa ohranili visoko enotno raven varnosti letalstva v Evropi, je treba spremeniti zahteve in postopke za certificiranje zrakoplovov in sorodnih proizvodov, delov in naprav ter potrjevanje projektivnih in proizvodnih organizacij, zlasti da bi lastnikom evropskih lahkih zrakoplovov pod 2000 kg (European Light Aircraft – ELA2) ali pod 1200 kg (ELA1) omogočili, da brez obrazca EASA 1 sprejmejo za vgradnjo nekatere dele, ki niso kritični za varnost.
The Agency prepared draft implementing rules and submitted them as opinions No 01/2009 on ‘Possibility to deviate from airworthiness code in case of design changes’, No 02/2009 on ‘Repair and design changes to European Technical Standard Order’, No 01/2010 on ‘SubPart J DOA’ and Opinion No 01/2011 on ‘ELA Process and “standard changes and repairs” ’ to the Commission in accordance with Article 19(1) of Regulation (EC) No 216/2008.
Agencija je pripravila osnutek izvedbenih predpisov in ga predložila Komisiji v skladu s členom 19(1) Uredbe (ES) št. 216/2008 v obliki naslednjih mnenj: mnenje št. 01/2009 o možnosti odstopanja od plovnostne kode v primeru sprememb projektov (Possibility to deviate from airworthiness code in case of design changes), mnenje št. 02/2009 o spremembah popravil in projektov v dovoljenjih po odredbi o evropskem tehničnem standardu (Repair and design changes to European Technical Standard Order; European Technical Standard Order – ETSO), mnenje št. 01/2010 o poddelu J DOA (SubPart J DOA) in mnenje št. 01/2011 o postopku ELA ter „standardnih spremembah in popravilih“ELA Process and „standard changes and repairs“.
The measures provided for in this Regulation are in accordance with the opinion of the European Aviation Safety Agency Committee established by Article 65(1) of Regulation (EC) No 216/2008,
Ukrepi iz te uredbe so v skladu z mnenjem odbora Evropske agencije za varnost v letalstvu, ustanovljenim s členom 65(1) Uredbe (ES) št. 216/2008 –
This Regulation lays down, in accordance with Article 5(5) and Article 6(3) of Regulation (EC) No 216/2008, common technical requirements and administrative procedures for the airworthiness and environmental certification of products, parts and appliances specifying:
Ta uredba v skladu s členom 5(5) in členom 6(3) Uredbe (ES) št. 216/2008 določa skupne tehnične zahteve in upravne postopke za certificiranje proizvodov, delov in naprav glede plovnosti in okoljske ustreznosti ter opredeljuje:
the issue of type-certificates, restricted type-certificates, supplemental type-certificates and changes to those certificates;
izdajo certifikatov tipa, certifikatov tipa z omejitvami, dodatnih certifikatov tipa in spremembe teh certifikatov;
the issue of certificates of airworthiness, restricted certificates of airworthiness, permits to fly and authorised release certificates;
izdajo spričeval o plovnosti, spričeval o plovnosti z omejitvami, dovoljenj za letenje in dovoljenj za sprostitev v uporabo;
the issue of repair design approvals;
izdajo odobritev projektov popravil;
the showing of compliance with environmental protection requirements;
dokazovanje izpolnjevanja zahtev glede varstva okolja;
the issue of noise certificates;
izdajo spričeval o hrupu;
the identification of products, parts and appliances;
opredelitev proizvodov, delov in naprav;
the certification of certain parts and appliances;
certificiranje proizvodov, delov in naprav;
the certification of design and production organisations;
potrjevanje projektivnih in proizvodnih organizacij;
the issue of airworthiness directives.
izdajo plovnostnih zahtev.
‘JAA’ means the ‘Joint Aviation Authorities’;
„JAA“ pomeni „Joint Aviation Authorities“;
‘JAR’ means ‘Joint Aviation Requirements’;
„JAR“ pomeni „Joint Aviation Requirements“;
‘Part 21’ means the requirements and procedures for the certification of aircraft and related products, parts and appliances, and of design and production organisations laid down in Annex I to this Regulation;
„del 21“ pomeni zahteve in postopke za certificiranje zrakoplovov in sorodnih proizvodov, delov in naprav ter potrjevanje projektivnih in proizvodnih organizacij iz Priloge I k tej uredbi;
‘Part M’ means the applicable continuing airworthiness requirements adopted in pursuance of Regulation (EC) No 216/2008;
„del M“ pomeni ustrezne zahteve za stalno plovnost, sprejete v skladu z Uredbo (ES) št. 216/2008;
‘principal place of business’ means the head office or registered office of the undertaking within which the principal financial functions and operational control of the activities referred to in this Regulation are exercised;
„glavni sedež“ pomeni glavno upravo ali registrirani sedež podjetja, kjer se izvajajo glavne finančne naloge in operativni nadzor nad dejavnostmi, navedenimi v tej uredbi;
‘article’ means any part and appliance to be used on civil aircraft;
„artikel“ pomeni kateri koli del ali napravo, ki se uporablja v civilnem zrakoplovu;
‘ETSO’ means European Technical Standard Order.
„ETSO“ pomeni odredbo o evropskem tehničnem standardu.
The European Technical Standard Order is a detailed airworthiness specification issued by the European Aviation Safety Agency (the ‘Agency’) to ensure compliance with the requirements of this Regulation as a minimum performance standard for specified articles;
Odredba o evropskem tehničnem standardu je podrobna specifikacija plovnosti, ki jo zaradi zagotavljanja skladnosti z zahtevami iz te uredbe Evropska agencija za varnost v letalstvu (v nadaljnjem besedilu: agencija) izda kot minimalni standard zmogljivosti za določene artikle;
‘EPA’ means European Part Approval.
„EPA“ pomeni Evropsko odobritev delov.
European Part Approval of an article means the article has been produced in accordance with approved design data not belonging to the type-certificate holder of the related product, except for ETSO articles;
Evropska odobritev delov pomeni, da je bil artikel proizveden v skladu z odobrenimi projektnimi podatki, ki ne pripadajo nosilcu certifikata tipa za zadevni proizvod, razen artiklov ETSO;
‘ELA1 aircraft’ means the following manned European Light Aircraft:
„zrakoplov ELA1“ pomeni naslednje evropske lahke zrakoplove s posadko:
an aeroplane with a Maximum Take-off Mass (MTOM) of 1200 kg or less that is not classified as complex motor-powered aircraft;
zrakoplov z največjo vzletno maso (Maximum Take-off Mass – MTOM) 1200 kg ali manj, ki ni opredeljen kot kompleksni zrakoplov na motorni pogon;
a sailplane or powered sailplane of 1200 kg MTOM or less;
jadralno letalo ali jadralno letalo s pogonom z MTOM 1200 kg ali manj;
an airship designed for not more than 4 occupants and a maximum design lifting gas or hot air volume of not more than 3400 m3 for hot air airships and 1000 m3 for gas airships;
zračno ladjo, namenjeno največ štirim potnikom in z največjo deklarirano prostornino vzgonskega plina ali prostornino toplega zraka, ki ne presega 3400 m3 za toplozračne zračne ladje in 1000 m3 za plinske zračne ladje;
‘ELA2 aircraft’ means the following manned European Light Aircraft:
„zrakoplov ELA2“ pomeni naslednje evropske lahke zrakoplove s posadko:
an aeroplane with a Maximum Take-off Mass (MTOM) of 2000 kg or less that is not classified as complex motor-powered aircraft;
zrakoplov z MTOM 2000 kg ali manj, ki ni opredeljen kot kompleksni zrakoplov na motorni pogon;
a sailplane or powered sailplane of 2000 kg MTOM or less;
jadralno letalo ali jadralno letalo s pogonom z MTOM 2000 kg ali manj;
a hot air airship;
toplozračno zračno ladjo;
a gas airship complying with all of the following characteristics:
plinsko zračno ladjo z vsemi naslednjimi značilnostmi:
3 % maximum static heaviness,
3 % največje statične obteženosti,
Non-vectored thrust (except reverse thrust),
nevektorskim potiskom (razen povratnega potiska),
Conventional and simple design of: structure, control system and ballonet system,
konvencionalno in enostavno zasnovo strukture, nadzornega sistema in balonetnega sistema,
Non-power assisted controls;
komandami brez servo podpore;
a Very Light Rotorcraft.
zelo lahek rotoplan.
Products, parts and appliances shall be issued certificates as specified in Annex I (Part 21).
Certifikati za proizvode, dele in naprave se izdajo, kakor je opredeljeno v Prilogi I (delu 21).
By way of derogation from point 1, aircraft, including any installed product, part and appliance, which are not registered in a Member State shall be exempted from the provisions of Subparts H and I of Annex I (Part 21).
Z odstopanjem od točke 1 so zrakoplovi, vključno z vgrajenimi proizvodi, deli in napravami, ki niso registrirani v državi članici, izvzeti iz določb poddelov H in I Priloge I (dela 21).
They shall also be exempted from the provisions of Subpart P of Annex I (Part 21) except when aircraft identification marks are prescribed by a Member State.
Prav tako so izvzeti iz določb poddela P Priloge I (dela 21), razen kadar identifikacijske oznake zrakoplovov predpiše država članica.
Continued validity of type-certificates and related certificates of airworthiness
Nadaljevanje veljavnosti certifikatov tipa in povezanih spričeval o plovnosti
the product shall be deemed to have a type-certificate issued in accordance with this Regulation when:
šteje se, da je bil certifikat tipa za proizvod izdan v skladu s to uredbo, če:
the JAA type-certification basis, for products that have been certificated under JAA procedures, as defined in their JAA data sheet, or
osnova za certifikacijo tipa JAA za proizvode, ki so bili certificirani po postopkih JAA, kakor je opredeljeno v njihovi listi podatkov JAA, ali
a Member State, unless the Agency determines, taking into account, in particular, airworthiness codes used and service experience, that such type-certification basis does not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation, or
država članica, razen če agencija ugotovi, ob upoštevanju zlasti uporabljenih plovnostnih kod in obratovalnih izkušenj, da navedena osnova za izdajo certifikatov tipa ne zagotavlja ravni varnosti, enakovredne tisti, ki jo zahtevata Uredba (ES) št. 216/2008 in ta uredba, ali
a State with which a Member State had concluded a bilateral airworthiness agreement or similar arrangement under which such products have been certificated on the basis of the airworthiness codes of that State of design, unless the Agency determines that such airworthiness codes or service experience or the safety system of that State of design do not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation.
država, s katero je država članica sklenila dvostranski sporazum ali podoben dogovor, po katerem so bili ti proizvodi certificirani na osnovi plovnostnih kod navedene države projektiranja, razen če agencija ugotovi, da navedene plovnostne kode ali obratovalne izkušnje ali varnostni sistem navedene države projektiranja ne zagotavljajo ravni varnosti, enakovredne tisti, ki jo zahtevata Uredba (ES) št. 216/2008 in ta uredba.
the applicable airworthiness directives were those of the State of design;
se uporabljajo plovnostne zahteve države projektiranja;
the design of an individual aircraft, which was on the register of a Member State before 28 September 2003, shall be deemed to have been approved in accordance with this Regulation when:
šteje se, da je projekt posameznega zrakoplova, ki je bil vpisan v register države članice pred 28. septembrom 2003, odobren v skladu s to uredbo, če:
all changes to this basic type design, which were not under the responsibility of the type-certificate holder, had been approved; and
so bile vse spremembe tega osnovnega projekta tipa, za katere ne odgovarja nosilec certifikata tipa, odobrene, ter
points 21.A.15(a), (b) and (c) of Annex I (Part 21) shall not apply;
se točke 21.A.15(a), (b) in (c) Priloge I (dela 21) ne uporabljajo;
by way of derogation from point 21.A.17(a) of Annex I (Part 21), the type-certification basis shall be that established by the JAA or, where applicable, the Member State at the date of application for the approval;
z odstopanjem od točke 21.A.17(a) Priloge I (dela 21) osnovo za certifikacijo tipa določi JAA ali po potrebi država članica na dan vložitve vloge za odobritev;
compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with points 21.A.20(a) and (b) of Annex I (Part 21).
se za ugotovitve o skladnosti po postopkih JAA ali države članice šteje, da jih je opravila agencija zaradi izpolnjevanja točk 21.A.20(a) in (b) Priloge I (dela 21).
point 21.A.93 of Annex I (Part 21) shall not apply;
se točka 21.A.93 Priloge I (dela 21) ne uporablja;
compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with points 21.A.103(a)(2) and (b) of Annex I (Part 21).
se za ugotovitve o skladnosti po postopkih JAA ali države članice šteje, da jih je opravila agencija zaradi izpolnjevanja točk 21.A.103(a)(2) in (b) Priloge I (dela 21).
With regard to products that had a national type-certificate, or equivalent, and for which the approval process of a major repair design carried out by a Member State was not finalised at the time when the type-certificate had to be determined in accordance with this Regulation, compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with point 21.A.433(a) of Annex I (Part 21).
V zvezi s proizvodi, ki imajo nacionalen ali njemu enakovreden certifikat tipa in za katere v trenutku, ko je certifikat tipa moral biti določen v skladu s to uredbo, proces odobritve projekta velikega popravila, ki ga izvaja država članica, še ni bil končan, se za ugotovitve o skladnosti po postopkih JAA ali države članice šteje, da jih je opravila agencija zaradi izpolnjevanja točke 21.A.433(a) Priloge I (dela 21).
A certificate of airworthiness issued by a Member State attesting conformity with a type-certificate determined in accordance with point 1 shall be deemed to comply with this Regulation.
Šteje se, da je spričevalo o plovnosti, ki ga izda država članica in izkazuje skladnost s certifikatom tipa, določenim v skladu s točko 1, v skladu s to uredbo.
With regard to supplemental type-certificates issued by a Member State under JAA procedures or applicable national procedures and with regard to changes to products proposed by persons other than the type-certificate holder of the product, which were approved by a Member State under applicable national procedures, if the supplemental type-certificate, or change, was valid on 28 September 2003, the supplemental type-certificate, or change shall be deemed to have been issued under this Regulation.
Za dodatne certifikate tipa, ki so jih izdale države članice po postopkih JAA ali ustreznih nacionalnih postopkih, in za spremembe proizvodov, ki so jih predlagale osebe, ki niso nosilci certifikata tipa za proizvod, ki ga je odobrila država članica po ustreznih nacionalnih postopkih, se šteje, da je bil dodatni certifikat tipa ali sprememba izdan po tej uredbi, če je bil dodatni certifikat tipa ali sprememba v veljavi 28. septembra 2003.
point 21.A.113 (a) and (b) of Annex I (Part 21) shall not apply;
se točki 21.A.113(a) in (b) Priloge I (dela 21) ne uporabljata;
the compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with point 21.A.115(a) of Annex I (Part 21).
se za ugotovitve o skladnosti po postopkih JAA ali države članice šteje, da jih je opravila agencija zaradi izpolnjevanja točke 21.A.115(a) Priloge I (dela 21).
Continued operation of certain aircraft registered by Member States
Stalno obratovanje določenih zrakoplovov, ki so registrirani v državah članicah
With regard to an aircraft that cannot be deemed to have a type-certificate issued in accordance with Article 3(1)(a) of this Regulation, that has been issued a certificate of airworthiness by a Member State before Regulation (EC) No 1702/2003 became applicable in that Member State [4], was on its register on that date, and was still on the register of a Member State on 28 March 2007, the combination of the following shall be deemed to constitute the applicable specific airworthiness specifications issued in accordance with this Regulation:
Glede zrakoplova, za katerega se ne more šteti, da mu je bil certifikat tipa izdan v skladu s členom 3(1)(a) te uredbe, za katerega je država članica izdala spričevalo o plovnosti pred začetkom uporabe Uredbe (ES) št. 1702/2003 v tej državi članici [4], ki je bilo na ta dan v registru in je bilo še vedno v registru države članice 28. marca 2007, se šteje, da posebne plovnostne specifikacije, izdane v skladu s to uredbo, pomeni kombinacija:
the type-certificate data sheet and type-certificate data sheet for noise, or equivalent documents, of the State of design, provided that the State of design has concluded the appropriate working arrangement in accordance with Article 27(2) of Regulation (EC) No 216/2008 with the Agency covering the continued airworthiness of the design of such an aircraft;
podatkov o certifikatu tipa in podatkov o certifikatu tipa glede hrupa ali enakovredni dokumenti države projektiranja, pod pogojem, da je država projektiranja sklenila ustrezni delovni dogovor v skladu s členom 27(2) Uredbe (ES) št. 216/2008 z agencijo, ki pokriva stalno plovnost projekta takšnega zrakoplova;
the environmental protection requirements laid down in Annex 16 to the Chicago Convention, as applicable to that aircraft; and
zahtev glede varstva okolja, ki so določene v Prilogi 16 k Čikaški konvenciji, kakor veljajo za takšen zrakoplov, in
the mandatory continuing airworthiness information of the State of design.
obveznih informacij o stalni plovnosti države projektiranja.
point 21.A.603 of Annex I (Part 21) shall not apply;
se točka 21.A.603 Priloge I (dela 21) ne uporablja;
the applicable data requirements laid down in point 21.A.605 of Annex I (Part 21) shall be those established by the relevant Member State, at the date of application for the approval or authorisation;
so ustrezne zahteve glede podatkov iz točke 21.A.605 Priloge I (dela 21) tiste, ki jih določi ustrezna država članica na dan vložitve vloge za odobritev ali potrditev;
compliance findings made by the relevant Member State shall be deemed to have been made by the Agency for the purpose of complying with point 21.A.606(b) of Annex I (Part 21).
se za ugotovitve o skladnosti po postopkih ustrezne države članice šteje, da jih je opravila agencija zaradi izpolnjevanja točke 21.A.606(b) Priloge I (dela 21).
The conditions determined before 28 March 2007 by the Member States for permits to fly or other airworthiness certificate issued for aircraft which did not hold a certificate of airworthiness or restricted certificate of airworthiness issued under this Regulation, are deemed to have been determined in accordance with this Regulation, unless the Agency has determined before 28 March 2008 that such conditions do not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 or this Regulation.
Pogoji, določeni pred 28. marcem 2007 s strani držav članic glede dovoljenj za letenje ali drugih spričeval o plovnosti, ki so bila izdana za zrakoplov, za katerega niso bila izdana spričevala o plovnosti ali spričevala o plovnosti z omejitvami v skladu s to uredbo, štejejo kot pogoji, ki so bili določeni v skladu s to uredbo, razen če je agencija pred 28. marcem 2008 ugotovila, da takšni pogoji ne zagotavljajo enake stopnje varnosti, kot jo zagotavlja Uredba (ES) št. 216/2008 ali ta uredba.
Design organisations
Projektivne organizacije
An organisation responsible for the design of products, parts and appliances or for changes or repairs thereto shall demonstrate its capability in accordance with Annex I (Part 21).
Organizacija, pristojna za projektiranje proizvodov, delov in naprav ali za njihove spremembe ali popravila, dokazuje svojo sposobnost v skladu z (delom 21) Priloge I.