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5.5.4   Continuing airworthiness
Annex 8, Part II, Chapter 4, prescribes the activities and corresponding responsibilities of a State of Design, the States of Registry, and the modification approval holder in ensuring the continued airworthiness of an aircraft during its entire operational or service life. Service experiences involving faults, malfunctions, defects and other occurrences that may affect the continuing airworthiness of the aircraft are required to be recorded, reported, and assessed under Annex 8, Part II, Section 4.2. This information is used to determine if an unsafe or potentially unsafe condition exists in an aircraft. The State of Design, States of Registry, and the modification approval holder all play important roles in deciding if and when airworthiness action is needed to either correct an unsafe, or avoid a potentially unsafe, condition. See guidance in Chapter 4, Continuing Airworthiness of Aircraft, of this manual.
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APPENDIX A.— FLOW CHART OF PROCESS FOR DETERMINING
AIRWORTHINESS STANDARDS  FOR A MODIFIED PRODUCT

APPENDIX B.— EXAMPLE OF A SUPPLEMENTAL TYPE CERTIFICATE

Contracting State
Civil Aviation Authority

Supplemental Type Certificate No. ___
Pursuant to Civil Aviation Regulations Number ________of Contracting State,  this Supplemental Type Certificate is issued to:
Name of Holder
Complete Address of Holder

For the following Description of design change:
Affected Type Certificate Number__________ Product make and model__________________
Limitations and conditions of approval (See Continuation Sheet):
Date of application:
Conditions: This approval is only applicable to the type/model of aeronautical product specified therein. Prior to incorporating this modification, the installer shall establish that the interrelationship between this change and any other modification(s)
Issuing
incorporated will not adversely affect the airworthiness of the modified product.
Agency
Seal  or  Logo

Authorized Person – Civil Aviation Authority Date of Issue
Contracting State
Civil Aviation Authority

Supplemental Type Certificate No. ___
(Continuation Sheet)
Certification Basis:
Based on Part XX, and the Contracting State policy for major design changes, the certification basis for the Aircraft Model _____, as modified is as follows:
a.  
The type certification basis for Aircraft Model _____ series aiplane is shown on Type Certiicate Data sheet _____ for parts or areas not affected or changed by the modification.

b.  
The certification basis for parts affected or changed by the modification since the date of application (mm/dd/yy) is based upon Part XX, as amended by Amendment XX-98. The certification basis for this modification was determined to be:

Regulations at the latest amendment XX-0 through XX-98
XX.1 – XX.31, XX.301-XX.307, XX.561-XX.563, XX.601-XX.625
Regulations at an intermediate amendment
XX.574 Amendment XX-54
XX.629 Amendment XX-26
Appendix X  Amendment XX-58

Regulations at the amendment level in TCDS ______
XX.25, XX.321-XX.373, XX.471-XX.519

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CHAPTER 6.— REPAIRS TO APPROVED TYPE DESIGN
6.1 General
6.1.1 A Certificate of Airworthiness issued under Annex 8 is based on satisfactory evidence that an aircraft complies with a type design approved or accepted by a State of Registry. For aircraft engaged in international civil aviation, the recognition and acceptance of a Certificate of Airworthiness is facilitated through Article 33 of the Convention on International Civil Aviation. A State of Registry claiming such recognition, however, must ensure that there exists a national requirement for ensuring the continued airworthiness of an aircraft during its service life. This national requirement involves the aircraft owner or operator and the CAA in ensuring that the aircraft continues to conform to its approved type design after a modification, repair, and installation of a replacement part. For further details on continuing validity of the Certificate of Airworthiness, refer to Annex 8 Part II, Chapter 4, Continuing Airworthiness of Aircraft and in this guidance material Part III, Chapter 3.
　
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