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Note.— Guidance on the content of an application form for the issue of an Export Certificate of Airworthiness is given in Appendix C to this Chapter.
3.4.3  Exceptions
If it has any specific certification or operational requirements in place in addition to those adopted or required by the exporting State, the importing State will make these known to the exporting State and either agree that these may be listed as exceptions on the Export Certificate of Airworthiness or require compliance with the additional requirements before agreeing to accept the Export Certificate of Airworthiness. Exceptions therefore are a matter of agreement between the States concerned. When an aircraft is removed from storage immediately prior to its export, required maintenance inspections or Airworthiness Directives may not have been accomplished. For the purpose of the delivery flight, these non-compliances may be accepted by the importing State but again will be listed as agreed exceptions on the Export Certificate of Airworthiness.
3.4.4 Export certificate of airworthiness status
It is very important to understand that an export certificate of airworthiness is not a Certificate of Airworthiness as defined by Article 31 of the Convention and therefore does not confer the right of international flight and cannot be validated in accordance with Annex 8, Part II, Chapter 3, 3.2.4. To fly internationally, an aircraft having an Export Certificate of Airworthiness will require a valid Certificate of Airworthiness issued by the State of Registry, or some equivalent document mutually acceptable to the exporting and importing States and accepted by any State over which the aircraft will fly on its delivery flight.
3.4.5  Export certification of products other than a complete aircraft
Some States may have adopted more detailed export airworthiness approval procedures, covering not only the issue of an Export Certificate of Airworthiness for a complete aircraft but also encompassing the issue of export certifications for engines, propellers and other component parts. For the purpose of such procedures, the item being exported may be placed within a particular “Class”, for example:
a) Class I product – a complete aircraft, engine or propeller which has been type certificated
in accordance with the appropriate airworthiness requirements and for which the
necessary type certificate data sheets or equivalent have been issued.
b) Class II product – a major component of a Class I product such as a wing, fuselage,
empennage surface, etc. the failure of which would jeopardize the safety of a Class I
product or any part, material or system thereof.
c)  Class III product – any part or component which is not a Class I or Class II  product or a standard part.
For products other than a Class I product, the export airworthiness certification may be issued in the form of certificates or identification tags, which will confirm that the product in question meets the approved design data, is in a condition for safe operation and complies with any special requirements as notified by the importing State.
Note.— A sample export certificate of airworthiness for Class 1 products is shown in Appendix D to this Chapter.
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APPENDIX A.— APPLICATION FOR ISSUE OF A
CERTIFICATE OF AIRWORTHINESS – CONTENT

An applicant for the issue of a Certificate of Airworthiness (See Section 3.2.2 of Part III) will be required to provide sufficient detail concerning the aircraft, its engines and, if applicable, its propellers in order to enable the CAA to make an initial judgment concerning the aircraft’s immediate history, current status, equipment fit, modifications embodied and potential certification status.
The form to be completed in support of the application is therefore intended to provide basic details. Subsequent surveys of the aircraft, its logbooks and other supporting documentation by staff of the CAA’s AID or by its delegated representatives will allow detailed consideration concerning whether the aircraft conforms with the requirements of the State for the issue of a Certificate of Airworthiness. An application form therefore needs to require sufficient information to be provided for the initial assessment to be made but not to seek the essential but very detailed information which is readily obtainable later in the process.
　
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