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Commission Regulation (EU) No 748/2012 of 3 August 2012 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations (recast) (Text with EEA relevance)
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Version Superseded: 31/12/2020
Point in time view as at 03/08/2012.
There are currently no known outstanding effects by UK legislation for Commission Regulation (EU) No 748/2012, Appendix VIII.
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Enter name of the State of manufacture.
The competent authority under which authority the Statement of Conformity is issued.
A unique serial number should be pre-printed in this block for statement control and traceability purposes. Except that in the case of a computer generated document the number need not be pre-printed where the computer is programmed to produce and print a unique number.
The full name and location address of the organisation issuing the statement. This block may be pre-printed. Logos etc. are permitted if the logo can be contained within the block.
The aircraft type in full as defined in the type-certificate and its associated data sheet.
The type-certificate reference numbers and issue for the subject aircraft.
If the aircraft is registered then this mark will be the registration mark. If the aircraft is not registered then this will be such a mark that is accepted by the competent authority of the Member State and, if applicable, by the competent authority of a third country.
The identification number assigned by the manufacturer for control and traceability and product support. This is sometimes referred to as a Manufacturers Serial No or Constructors No.
The engine and propeller type(s) in full as defined in the relevant type-certificate and its associated data sheet. Their manufacturer identification No and associated location should also be shown.
Approved design changes to the aircraft definition.
A listing of all applicable airworthiness directives (or equivalent) and a declaration of compliance, together with a description of the method of compliance on the subject individual aircraft including products and installed parts, appliances and equipment. Any future compliance requirement time should be shown.
Approved unintentional deviation to the approved type design sometimes referred to as concessions, divergences, or non-conformances.
Only agreed exemptions, waivers or derogations may be included here.
Remarks. Any statement, information, particular data or limitation which may affect the airworthiness of the aircraft. If there is no such information or data, state; ‘NONE’.
Enter ‘Certificate of Airworthiness’, or ‘Restricted Certificate of Airworthiness’, or for the Certificate of Airworthiness requested.
Additional requirements such as those notified by an importing country should be noted in this block.
Validity of the Statement of Conformity is dependent on full completion of all blocks on the form. A copy of the flight test report together with any recorded defects and rectification details should be kept on file by the POA holder. The report should be signed as satisfactory by the appropriate certifying staff and a flight crew member, e.g. test pilot or flight test engineer. The flight tests performed are those defined under the control of the quality system, as established by point 21.A.139 in particular 21.A.139(b)(1)(vi), to ensure that the aircraft conforms with the applicable design data and is in condition for safe operation.
The listing of items provided (or made available) to satisfy the safe operation aspects of this statement should be kept on file by the POA holder.
The Statement of Conformity may be signed by the person authorised to do so by the production approval holder in accordance with point 21.A.145(d). A rubber stamp signature should not be used.
The name of the person signing the certificate should be typed or printed in a legible form.
The date the Statement of Conformity is signed should be given.
The competent authority approval reference should be quoted.
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