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b)  the issue of a Certificate of Airworthiness with a non-expiring period of validity, continuing airworthiness being determined through a system of inspection approved by the State. (Refer to 3.2.5 below for further information on the system of inspection.)
3.2.3.3 Regardless of the period of validity shown on it, failure to comply with any of the following will invalidate the Certificate of Airworthiness:
a)  the aircraft remains in conformity with the type design approved by the State of Registry:
1)  modifications or repairs completed in accordance with procedures and methods approved by the State of Registry (Part III, Chapter 5 and Part IV, Chapter 3 refers);
2)  replacement components, parts, equipment or material are in accordance with the design requirements and installed in accordance with any prescribed procedures;
3)  all markings and placards included in the approval of the type design by the State of Registry are present;
4)  in addition to the information specified in Annex 8, the flight manual includes any changes made mandatory by the State of Registry as required by Annex 6, Part I,
11.1 or Part III, Section II, 9.1, as applicable;
5)  if the aircraft has been released to service with any airworthiness significant systems, components or equipment unserviceable, this is in compliance with a minimum equipment list or similar document approved by the State of Registry;
6)  if the aircraft has been released to service with any structural parts missing, this is in compliance with procedures approved by the State of Registry; and
Note.— Information of this nature is sometimes included as a configuration deviation list in the flight manual.
7)  unrepaired damage is within limits acceptable to the State of Registry (reference should be made to the structural repair manual for the aircraft type concerned to determine acceptable limits);
b) The aircraft has been correctly maintained in an airworthy condition, including:
Note.— Annex 6, Part I, 8.3 requires operators of commercially operated aeroplanes to
provide an aeroplane maintenance programme, approved by the State of Registry, containing
maintenance tasks and intervals at which these tasks are to be performed.
1) it is in compliance with a maintenance programme acceptable to the State of Registry;
2)  if the aircraft is the subject of a reliability programme, including in particular engine trend monitoring, corrective action has been instituted to rectify any adverse trends;
3)  it complies with any certification maintenance requirements at the prescribed intervals;
4)  it complies with all modifications or inspections declared mandatory by the State of Registry (commonly referred to as Airworthiness Directives).
Note.— The responsibilities of States of Registry in relation to continuing airworthiness requirements of this nature are contained in Annex 8, Part II, Chapter 4 (For more information, refer to Part III, Chapter 4, Section 4.4 of this manual).
5)  that those parts of the aircraft that have an ultimate service life limit declared by the organization responsible for the type design or the State of Registry have not exceeded their approved lives;
Note.— Aircraft maintenance manuals prepared in the format required by the Air Transport Association of America Specification Number 2200 (ATA 2200), formerly Specification 100 (ATA 100) contain this information in Chapter 5. For some older aircraft types, this information may sometimes be published in the flight manual or Type Certificate Data Sheet.
6)  conformity of the aircraft mass and balance data with the requirements of the State of Registry, including re-weighing if appropriate and/or compliance with a system for recording progressive mass and balance change; and
7)  conformity of the aircraft records with the requirements of the State of Registry, which must at a minimum meet the requirements of Annex 6, Part I, 8.4, Part II, 8.2.1 or Part III, Section II, 6.4 as applicable.
　
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