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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