Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 2788

b) to any other Contracting State upon request. Note 1.— In 4.3, the term “mandatory continuing airworthiness information” is intended to include mandatory requirements for modification, replacement of parts or inspection of aircraft and amendment of operating limitations and procedures. Among such information is that issued by Contracting States in the form of airworthiness directives. Note 2.— Circular 95, The Continuing Airworthiness of Aircraft in Service, provides the necessary information to assist Contracting States in establishing contact with competent authorities of other Contracting States, for the purpose of maintaining continuing airworthiness of aircraft in service. 4.3.3 The State of Registry shall, upon receipt of mandatory continuing airworthiness information from the State of Design, adopt the mandatory information directly or assess the information received and take appropriate action. 4.3.4 Any Contracting State that has entered on its register an aircraft in respect of which that Contracting State is not the State of Design and for which it has issued or validated a Certificate of Airworthiness in accordance with 3.2 of this part shall ensure the transmission to the State of Design of all mandatory continuing airworthiness information which it, as the State of Registry, originated in respect of that aircraft. 4.3.5 The State of Registry shall ensure that in respect of aeroplanes of over 5 700 kg and helicopters over 3 180 kg maximum certificated take-off mass, there exists a system whereby information on faults, malfunctions, defects and other occurrences that cause or might cause adverse effects on the continuing airworthiness of the aircraft is transmitted to the organization responsible for the type design of that aircraft. Note.— Guidance on interpretation of “the organization responsible for the type design” is contained in Volume II, Part A, of the Airworthiness Manual (Doc 9760). 4.3.6 The State of Design shall ensure that in respect of aeroplanes over 5 700 kg and helicopters over 3 180 kg maximum certificated take-off mass, there exists a system for:

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