Chapter 9 Export Airworthiness Documentation
Article 66
Export airworthiness approvals must be applied through the CAA for export of aviation products, appliances and parts.
Article 67
An aircraft owner, operator, or the holder of the production certificate is entitled to apply for an export airworthiness approval when exporting aircraft or change aircraft registration to other country.
An engine or propeller manufacturer, owner, operator or repair station as well as the manufacturer of the TSO articles or PMA parts are entitled to apply for an export authorized release certificate.
Article 68
An applicant is entitled to an export certificate of airworthiness when it meets the following requirements:
1) Conform to the airworthiness requirement under Article 38.
2) Conform to special requirement set by importing country.
When exporting of an unassembled aircraft which has not been flight-tested or does not meet previous section’s requirements shall submit approved documents from the airworthiness authority of the importing country.
When applying for an export certificate of airworthiness the applicant should return the aircraft's certificate of airworthiness to the CAA.
The valid period of an Export Certificate of Airworthiness, is 90 days starting from the date of issue.
Article 69
An applicant is entitled to an export authorized release certificate for engines, propellers, TSO articles or PMA parts if that applicant conforms to the requirements of Attachment 17.
Article 70
An applicant is entitled to an export authorized release certificate for aviation products, appliances and parts when:
1) Providing documents and information to imported country airworthiness authorities containing the necessary information for safe operation the product.
2) Exporting an unassembled aircraft which has not been flight-tested, provide instructions for assembly and a flight test checklist to the country of airworthiness authority.
3) When temporary installations are incorporated in an aircraft for the purpose of export delivery, the installation will be removed and the aircraft restored to the approved configuration upon completion of the delivery flight.