Common use of Conformity Certifications During Design Approval Clause in Contracts

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon the country in which a supplier is located, may request prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriate. (b) Only FAA to AA/EASA or EASA/AA to FAA requests are permissible and neither shall respond to a conformity certification request made directly by the manufacturer or supplier. Conformity certifications shall be conducted only after consultations and agreement to perform the work. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they cannot be inspected by the manufacturer or its regulatory authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement based on the complexity of the requested certifications. Conformity certifications may be delegated to authorized designees or approved organizations. (c) AA/EASA requests for conformity certifications shall be sent in writing. FAA requests for conformity certifications shall be sent on FAA Form 8120-10, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA requests shall be sent to the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location of the part or appliance. FAA requests shall be sent to the appropriate AA office. FAA and EASA offices are listed in Appendix A. (d) Upon completion of all conformity inspections conducted on each other's behalf, the FAA or EASA/AA shall complete and return all documentation as notified. The FAA or EASA/AA, depending upon the country in which the supplier is located, shall note all deviations from the requirements notified by the FAA or EASA on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA for evaluation and disposition as to its effect on safety and the validity of the test under consideration. The FAA or EASA should receive a report stating the disposition of each deviation before an FAA Form 8130-3 or EASA Form 1 is issued.

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon airworthiness authority of the country in which a design approval applicant is located may request conformity certifications from the airworthiness authority in the country in which the design approval applicant’s supplier is located, may request located for prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall authorities will not respond to a conformity certification request made directly by from the manufacturer or supplier. Conformity certifications shall Certifications will be conducted only after consultations between the two airworthiness authorities on the specific work to be performed, and agreement to perform has been obtained from the workairworthiness authority in the country in which the supplier is located. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they canare not be inspected inspectable by the manufacturer or its regulatory airworthiness authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized designees or approved delegated organizations. (c) AA/EASA The CAAI requests for conformity certifications shall will be sent in writingto the appropriate FAA Office. FAA requests for For conformity certifications shall associated with a current CAAI or FAA validation program, the requests should be sent on to the FAA Form 8120-10Aircraft Certification Office responsible for the U.S. applicant. For conformity certifications associated with an Israeli certification program only, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA requests shall should be sent to the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location of State in which the part or applianceconformity certification will take place. FAA Offices are listed in Appendix A. CAAI’s requests will be sent on a completed CAAI Form 8120-10, Request for Conformity. FAA requests shall for conformity certifications will be sent on a completed FAA Form 8120-10, Request for Conformity, to the appropriate AA office. FAA and EASA offices are CAAI address, as listed in Appendix A. (d) Upon completion of all conformity inspections conducted on each other's behalfbehalf of the requesting authority, the FAA or EASA/AA shall CAAI will complete and return all documentation to the requesting authority, as notified. The FAA or EASA/AA, depending upon airworthiness authority of the country in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s airworthiness authority on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA CAAI for evaluation and disposition as to its effect on safety and the validity of the test under considerationdisposition. The FAA or EASA CAAI should receive a report stating the disposition of required on each deviation before an FAA Form 8130-3 or EASA CAAI Form 1 8130-3 is issued. (e) Neither conformity certification on prototype parts, nor inspections on production parts, should be construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the responsibility of the design/production approval holder and the airworthiness authority of the country in which the holder is located.

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon civil aviation authority of the country state in which a design approval applicant is located may request conformity certifications from the civil aviation authority in the state in which the design approval applicant’s supplier is located, may request located for prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall authorities will not respond to a conformity certification request made directly by from the manufacturer or supplier. Conformity certifications shall Certifications will be conducted only after consultations between the two civil aviation authorities on the specific work to be performed, and agreement to perform has been obtained from the workcivil aviation authority in the state in which the supplier is located. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they cannot be inspected by the manufacturer or its regulatory civil aviation authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized designees or approved organizations. (c) AA/EASA The DGCA’s requests for conformity certifications shall be sent in writing. FAA requests for conformity certifications shall be sent on FAA Form 8120-10, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA requests shall will be sent to the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location state in which the conformity certification will take place. The DGCA’s requests will be sent by a letter of the part or appliance. request for conformity inspections to FAA Offices which are listed in Appendix A. FAA requests shall for conformity certifications will be sent on a completed FAA Form 8120-10 to the appropriate AA office. FAA and EASA offices are DGCA address, as listed in Appendix A. (d) Upon completion of all conformity inspections conducted on each other's behalfbehalf of the requesting authority, the FAA or EASA/AA shall the DGCA will complete and return all documentation to the requesting authority, as notified. The FAA or EASA/AA, depending upon civil aviation authority of the country state in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s civil aviation authority on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA the DGCA for evaluation and disposition as to its effect on safety and the validity of the test under considerationdisposition. The FAA or EASA the DGCA should receive a report stating the disposition of required on each deviation before an FAA Form 8130-3 or EASA DGCA CA Form 1 is issued. (e) Neither conformity certification on prototype parts, nor inspections on production parts, should be construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the responsibility of the design or production approval holder and the civil aviation authority of the state in which the holder is located.

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon airworthiness authority of the country in which a design approval applicant is located may request conformity certifications from the airworthiness authority in the country in which the design approval applicant’s supplier is located, may request prototype part conformity certifications, conformity of test setlocated for specified prototype/pre-ups, and conformity of test articles from the other as appropriateproduction parts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall no authority is obliged to respond to a conformity certification request made directly by the manufacturer from a manufacturer, supplier or supplierdesignee. Conformity certifications shall Certifications will be conducted only after consultations and agreement between the two airworthiness authorities on the specific work to perform the workbe performed. Requests for conformity certifications should be limited to test specimens or prototype prototype/pre-production parts that are of such complexity that they canare not be inspected inspectable by the product manufacturer or its regulatory airworthiness authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized designees or approved organizations. (c) AA/EASA TCCA requests for conformity certifications shall will be sent to the appropriate FAA geographic-accountable Directorate Manufacturing Inspection Office, as listed in writing. Appendix A. FAA requests for conformity certifications shall will be sent on FAA Form 8120-10, Request for Conformity, directly to TCCA’s Maintenance and described in the Special Instructions section of the form. AA/EASA requests shall be sent to the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location of the part or appliance. FAA requests shall be sent to the appropriate AA office. FAA and EASA offices are Branch as listed in Appendix A. (d) Upon completion The airworthiness authority of all conformity inspections conducted on each other's behalf, the FAA or EASA/AA shall complete and return all documentation as notified. The FAA or EASA/AA, depending upon the country in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s airworthiness authority on the conformity certification for the particular part. Any nonconformity described as a deviation . (e) Neither conformity certification on prototype/pre-production parts, nor inspections on production parts should be brought to construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the attention responsibility of the FAA or EASA for evaluation design/production approval holder and disposition as to its effect on safety and the validity of the test under consideration. The FAA or EASA should receive a report stating the disposition of each deviation before an FAA Form 8130-3 or EASA Form 1 is issuedairworthiness authority.

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon airworthiness authority of the country in which a design approval applicant is located may request conformity certifications from the airworthiness authority in the country in which the design approval applicant’s supplier is located, may request located for prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall authorities will not respond to a conformity certification request made directly by from the manufacturer or supplier. Conformity certifications shall All requests will be in writing. Certifications will be conducted only after consultations between the two airworthiness authorities on the specific work to be performed, and agreement to perform has been obtained from the workairworthiness authority in the country in which the supplier is located. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they cannot be inspected by the manufacturer or its regulatory airworthiness authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized designees or approved organizations. (c) AA/EASA The CAA requests for conformity certifications shall should be sent in writingwriting to the appropriate FAA Office. For conformity certifications associated with a current CAA certification or FAA validation program, the requests should be sent to the FAA Aircraft Certification Office responsible for the U.S. applicant. For conformity certifications associated with a New Zealand certification program only, the requests should be sent to the FAA Directorate Manufacturing Inspection Office that has geographic responsibility for the U.S. State in which the conformity certification will take place. FAA Offices are listed in Appendix A. FAA requests for conformity certifications shall will be sent on a completed FAA Form 8120-10, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA requests shall be sent to the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for CAA Aircraft Certification Unit at the location of the part or appliance. FAA requests shall be sent to the appropriate AA office. FAA and EASA offices are address listed in Appendix A.B. (d) Upon completion of all conformity inspections conducted on each other's behalfbehalf of the requesting authority, the FAA or EASA/AA shall CAA will complete and return all documentation to the requesting authority, as notified. The FAA or EASA/AA, depending upon airworthiness authority of the country in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s airworthiness authority on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA CAA for evaluation and disposition as to its effect on safety and the validity of the test under considerationdisposition. The FAA or EASA CAA should receive a report stating the disposition of required on each deviation before an FAA Form 8130-3 or EASA CAA Form 1 One is issued. (e) Neither conformity certification on prototype parts, nor inspections on production parts, should be construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the responsibility of the design/production approval holder and the airworthiness authority of the country in which the holder is located.

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon airworthiness authority of the country in which a design approval applicant is located may request conformity certifications from the airworthiness authority in the country in which the design approval applicant’s supplier is located, may request located for prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall authorities will not respond to a conformity certification request made directly by from the manufacturer or supplier. Conformity certifications shall Certifications will be conducted only after consultations between the two airworthiness authorities on the specific work to be performed, and agreement to perform has been obtained from the workairworthiness authority in the country in which the supplier is located. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they canare not be inspected inspectable by the manufacturer or its regulatory airworthiness authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized designees or approved organizations. (c) AA/EASA UKCAA requests for conformity certifications shall will be sent in writing. FAA requests for conformity certifications shall will be sent on FAA Form 8120-10, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA UKCAA or FAA requests shall will be sent to the UKCAA office or the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location of the part or appliance. FAA requests shall be sent to the appropriate AA office. FAA and EASA UKCAA offices are listed in Appendix A.Appendices A and B. (d) Upon completion of all conformity inspections conducted on each other's behalfbehalf of the requesting authority, the FAA or EASA/AA shall UKCAA will complete and return all documentation to the requesting authority, as notified. The FAA or EASA/AA, depending upon airworthiness authority of the country in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s airworthiness authority on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA UKCAA for evaluation and disposition as to its effect on safety and the validity of the test under consideration. The FAA or EASA UKCAA should receive a report stating the disposition of required on each deviation before an FAA Form 8130-3 or EASA JAA Form 1 One is issued. (e) Neither conformity certification on prototype parts, nor inspections on production parts, should be construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the responsibility of the design holder and/or manufacturer and their airworthiness authority.

Conformity Certifications During Design Approval. ‌ (a) The FAA or EASA, depending upon civil aviation authority of the country state in which a design approval applicant is located may request conformity certifications from the civil aviation authority in the state in which the design approval applicant’s supplier is located, may request located for prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall authorities will not respond to a conformity certification request made directly by from the manufacturer or supplier. Conformity certifications shall Certifications will be conducted only after consultations between the two civil aviation authorities on the specific work to be performed, and agreement to perform has been obtained from the workcivil aviation authority in the state in which the supplier is located. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they cannot be inspected by the manufacturer or its regulatory civil aviation authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized designees or approved organizations. (c) AA/EASA DGAC requests for conformity certifications shall be sent in writing. FAA requests for conformity certifications shall be sent on FAA Form 8120-10, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA requests shall will be sent to the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location State in which the conformity certification will take place. DGAC requests will be sent by a letter of the part or appliance. request for conformity inspections to FAA Offices which are listed in Appendix A. FAA requests shall for conformity certifications will be sent on a completed DGAC 8120-10, Request for Conformity, to the appropriate AA office. FAA and EASA offices are DGAC address, as listed in Appendix A. (d) Upon completion of all conformity inspections conducted on each other's behalfbehalf of the requesting authority, the FAA or EASA/AA shall DGAC will complete and return all documentation to the requesting authority, as notified. The FAA or EASA/AA, depending upon civil aviation authority of the country state in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s civil aviation authority on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA DGAC for evaluation and disposition as to its effect on safety and the validity of the test under considerationdisposition. The FAA or EASA DGAC should receive a report stating the disposition of required on each deviation before an FAA Form FAA/DGAC 8130-3 or EASA Form 1 is issued. (e) Neither conformity certification on prototype parts, nor inspections on production parts, should be construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the responsibility of the design or production approval holder and the civil aviation authority of the state in which the holder is located.

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon airworthiness authority of the country in which a design approval applicant is located may request conformity certifications from the airworthiness authority in the country in which the design approval applicant’s supplier is located, may request located for prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall authorities will not respond to a conformity certification request made directly by from the manufacturer or supplier. Conformity certifications shall Certifications will be conducted only after consultations between the two airworthiness authorities on the specific work to be performed, and agreement to perform has been obtained from the workairworthiness authority in the country in which the supplier is located. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they canare not be inspected inspectable by the manufacturer or its regulatory airworthiness authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized designees or approved organizations. (c) AA/EASA ENAC requests for conformity certifications shall will be sent in writing. FAA requests for conformity certifications shall will be sent on FAA Form 8120-10, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA ENAC or FAA requests shall will be sent to the appropriate ENAC regional office (with a copy to the Production and Maintenance Service) or the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location of the part or appliance. FAA requests shall be sent to the appropriate AA office. FAA and EASA ENAC offices are listed in Appendix A.Appendices A and B. (d) Upon completion of all conformity inspections conducted on each other's behalfbehalf of the requesting authority, the FAA or EASA/AA shall ENAC will complete and return all documentation to the requesting authority, as notified. The FAA or EASA/AA, depending upon airworthiness authority of the country in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s airworthiness authority on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA ENAC for evaluation and disposition as to its effect on safety and the validity of the test under consideration. The FAA or EASA ENAC should receive a report stating the disposition of required on each deviation before an FAA Form 8130-3 or EASA JAA Form 1 One is issued. (e) Neither conformity certification on prototype parts, nor inspections on production parts, should be construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the responsibility of the design holder and/or manufacturer and their airworthiness authority.

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon airworthiness authority of the country in which a design approval applicant is located may request conformity certifications from the airworthiness authority in the country in which the design approval applicant’s supplier is located, may request located for prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall authorities will not respond to a conformity certification request made directly by from the manufacturer or supplier. Conformity certifications shall Certifications will be conducted only after consultations between the two airworthiness authorities on the specific work to be performed, and agreement to perform has been obtained from the workairworthiness authority in the country in which the supplier is located. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they canare not be inspected inspectable by the manufacturer or its regulatory airworthiness authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized designees or approved organizations. (c) AA/EASA DGAC requests for conformity certifications shall will be sent in writing. FAA requests for conformity certifications shall will be sent on FAA Form 8120-10, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA DGAC or FAA requests shall will be sent to the DGAC office or the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location of the part or appliance. FAA requests shall be sent to the appropriate AA office. FAA and EASA DGAC offices are listed in Appendix A.Appendices A and B. (d) Upon completion of all conformity inspections conducted on each other's behalfbehalf of the requesting authority, the FAA or EASA/AA shall DGAC will complete and return all documentation to the requesting authority, as notified. The FAA or EASA/AA, depending upon airworthiness authority of the country in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s airworthiness authority on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA DGAC for evaluation and disposition as to its effect on safety and the validity of the test under consideration. The FAA or EASA DGAC should receive a report stating the disposition of required on each deviation before an FAA Form 8130-3 or EASA JAA Form 1 One is issued. (e) Neither conformity certification on prototype parts, nor inspections on production parts, should be construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the responsibility of the design holder and/or manufacturer and their airworthiness authority.

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon airworthiness authority of the country in which a design approval applicant is located may request conformity certifications from the airworthiness authority in the country in which the design approval applicant’s supplier is located, may request located for specified prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall authorties will not respond to a conformity certification request made directly by from the manufacturer or supplier. Conformity certifications shall Certifications will be conducted only after consultations between the two airworthiness authorities on the specific work to be performed, and agreement to perform has been obtained from the workairworthiness authority in the country in which the suppplier is located. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they canare not be inspected inspectable by the manufacturer or its regulatory airworthiness authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized designees or approved delegated organizations. (c) AA/EASA The DCA requests for conformity certifications shall will be sent in writingto the appropriate FAA Office. FAA requests for For conformity certifications shall associated with a current DCA or FAA validation program, the requests should be sent on to the FAA Form 8120-10Aircraft Certification Office responsible for the U.S. applicant. For conformity certifications associated with a Malaysian certification program only, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA requests shall should be sent to the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location of State in which the part or applianceconformity certification will take place. FAA Offices are listed in Appendix A. FAA requests shall for conformity certifications will be sent on a completed FAA Form 8120-10, Request for Conformity, to the appropriate AA office. FAA and EASA offices are DCA address listed in Appendix A. (d) Upon completion of all conformity inspections conducted on each other's behalfbehalf of the requesting authority, the FAA or EASA/AA shall DCA will complete and return all documentation to the requesting authority, as notified. The FAA or EASA/AA, depending upon airworthiness authority of the country in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s airworthiness authority on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA DCA for evaluation and disposition as to its effect on safety and the validity of the test under considerationdisposition. The FAA or EASA DCA should receive a report stating the disposition of required on each deviation before an FAA Form 8130-3 or EASA DCA Form 1 ARC/AAT is issued. (e) Neither conformity certification on prototype parts, nor inspections on production parts, should be construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the responsibility of the design/production approval holder and the airworthiness authority of the country in which the holder is located

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon airworthiness authority of the country in which a design approval applicant is located may request conformity certifications from the airworthiness authority in the country in which the design approval applicant’s supplier is located, may request located for prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall authorities will not respond to a conformity certification request made directly by from the manufacturer or supplier. Conformity certifications shall Certifications will be conducted only after consultations between the two airworthiness authorities on the specific work to be performed, and agreement to perform has been obtained from the workairworthiness authority in the country in which the supplier is located. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they canare not be inspected inspectable by the manufacturer or its regulatory airworthiness authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized designees or approved organizations. (c) AA/EASA RCAA requests for conformity certifications shall will be sent in writingto the appropriate FAA Office. For conformity inspections associated with a current RCAA or FAA validation program, the requests should be sent to the FAA Aircraft Certification Office responsible for the U.S. applicant. For conformity certifications shall be sent on FAA Form 8120-10associated with a Romanian certification program only, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA requests shall should be sent to the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location of State in which the part or applianceconformity certification will take place. FAA requests shall be sent to the appropriate AA office. FAA and EASA offices Offices are listed in Appendix A.A. RCAA requests for conformity will be sent by letter to the FAA. FAA requests for conformity certifications will be sent on FAA Form 8120-10, Request for Conformity, to the RCAA Headquarters. (d) Upon completion of all conformity inspections conducted on each other's behalfbehalf of the requesting authority, the FAA or EASA/AA shall RCAA will complete and return all documentation to the requesting authority, as notified. The FAA or EASA/AA, depending upon airworthiness authority of the country in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s airworthiness authority on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA RCAA for evaluation and disposition as to its effect on safety and the validity of the test under considerationdisposition. The FAA or EASA RCAA should receive a report stating the disposition of required on each deviation before an FAA Form 8130-3 or EASA JAA Form 1 One is issued. (e) Neither conformity certifications on prototype parts, nor inspections on production parts, should be construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the responsibility of the design holder and/or manufacturer and their airworthiness authority.

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon airworthiness authority of the country in which a design approval applicant is located may request conformity certifications from the airworthiness authority in the country in which the design approval applicant’s supplier is located, may request located for prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall authorities will not respond to a conformity certification request made directly by from the manufacturer or supplier. Conformity certifications shall Certifications will be conducted only after consultations between the two airworthiness authorities on the specific work to be performed, and agreement to perform has been obtained from the workairworthiness authority in the country in which the supplier is located. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they canare not be inspected inspectable by the manufacturer or its regulatory airworthiness authority prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized authorised designees or approved organizations. (c) AA/EASA LFV requests for conformity certifications shall will be sent in writing. FAA requests for conformity certifications shall will be sent on FAA Form 8120-10, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA LFV or FAA requests shall will be sent to the LFV office or the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location of the part or appliance. FAA requests shall be sent to the appropriate AA office. FAA and EASA LFV offices are listed in Appendix A.Appendices A and B. (d) Upon completion of all conformity inspections conducted on each other's behalfbehalf of the requesting authority, the FAA or EASA/AA shall LFV will complete and return all documentation to the requesting authority, as notified. The FAA or EASA/AA, depending upon airworthiness authority of the country in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s airworthiness authority on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA LFV for evaluation and disposition as to its effect on safety and the validity of the test under consideration. The FAA or EASA LFV should receive a report stating the disposition of required on each deviation before an FAA Form 8130-3 or EASA JAA Form 1 One is issued. (e) Neither conformity certification on prototype parts, nor inspections on production parts, should be construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the responsibility of the design holder and/or manufacturer and their airworthiness authority.

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon airworthiness authority of the country state in which a design approval applicant is located may request conformity certifications from the airworthiness authority in the state in which the design approval applicant's supplier is located, may request located for specified prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA requests are permissible and neither shall respond to The applicant's airworthiness authority, not the design approval applicant nor a designee, makes the written request for conformity certification request made directly by the manufacturer or supplier. Conformity certifications shall be conducted only after consultations and agreement to perform the workcertifications. Requests for conformity such certifications should would be limited considered, following consultations between the two airworthiness authorities on the specific work to test specimens or prototype parts that are of such complexity that they cannot be inspected by the manufacturer or its regulatory authority prior to installation in the final productperformed. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity certifications may be delegated to authorized designees or approved organizations. (c) AA/EASA IAC requests for conformity certifications shall associated with an IAC validation program and conformity certifications associated with Russian certification program will be sent in writingto the CAAC Headquarters. FAA CAAC requests for conformity certifications shall be sent on FAA Form 8120-10, Request for Conformity, associated with a CAAC validation program and described in the Special Instructions section of the form. AA/EASA requests shall conformity certifications associated with Chinese certification program will be sent to the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location of the part or appliance. FAA requests shall be sent to the appropriate AA office. FAA and EASA offices are listed in Appendix A.IAC. (d) Upon completion Requests for conformity certifications should be limited to prototype parts that are of all conformity inspections conducted on each other's behalf, such complexity that they are not inspectable by the FAA product manufacturer or EASA/AA shall complete and return all documentation as notifiedits airworthiness authority prior to installation in the product. The FAA or EASA/AA, depending upon airworthiness authority of the country state in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicants airworthiness authority on the conformity certification for the particular part. Any nonconformity described as a deviation . (e) Neither conformity certifications on prototype parts nor inspections on production parts should be brought to construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the attention responsibility of the FAA or EASA for evaluation and disposition as to its effect on safety design/production approval holder and the validity airworthiness authority of the test under consideration. The FAA or EASA should receive a report stating state in which the disposition of each deviation before an FAA Form 8130-3 or EASA Form 1 holder is issuedlocated.

Conformity Certifications During Design Approval. (a) The FAA or EASA, depending upon airworthiness authority of the country in which a design approval applicant is located may request conformity certifications from the airworthiness authority in the country in which the design approval applicant’s supplier is located, may request located for prototype part conformity certifications, conformity of test set-ups, and conformity of test articles from the other as appropriateparts produced by that supplier. (b) Only FAA to AA/EASA or EASA/AA to FAA authority-to-authority requests are permissible and neither shall authorities will not respond to a conformity certification request made directly by from the manufacturer or supplier. Conformity certifications shall Certifications will be conducted only after consultations between the two airworthiness authorities on the specific work to be performed, and agreement to perform has been obtained from the workairworthiness authority in the country in which the supplier is located. Requests for conformity certifications should be limited to test specimens or prototype parts that are of such complexity that they canare not be inspected inspectable by the manufacturer or its regulatory airworthiness authority after assembly but prior to installation in the final product. Conformity certifications may require the development of a working arrangement procedure based on the complexity of the requested certifications. Conformity At the discretion of the authority in receipt of such requests, conformity certifications may be delegated to authorized designees or approved delegated organizations. (c) AA/EASA The JCAB requests for conformity certifications shall will be sent in writingto the appropriate FAA Office. FAA requests for For conformity certifications shall associated with a current JCAB or FAA validation program, the requests should be sent on to the FAA Form 8120-10Aircraft Certification Office responsible for the U.S. applicant. For conformity certifications associated with an Japanese certification program only, Request for Conformity, and described in the Special Instructions section of the form. AA/EASA requests shall should be sent to the FAA Directorate Manufacturing Inspection Office which has geographic responsibility for the location of State in which the part or applianceconformity certification will take place. FAA Offices are listed in Appendix A. JCAB’s requests will be sent on a completed JCAB Form 1-309-1. FAA requests shall for conformity certifications will be sent on a completed FAA Form 8120-10, Request for Conformity, to the appropriate AA office. FAA and EASA offices are JCAB address, as listed in Appendix A. (d) Upon completion of all conformity inspections conducted on each other's behalfbehalf of the requesting authority, the FAA or EASA/AA shall JCAB will complete and return all documentation to the requesting authority, as notified. The FAA or EASA/AA, depending upon airworthiness authority of the country in which the supplier is located, shall located will note all deviations from the requirements notified by the FAA or EASA design approval applicant’s airworthiness authority on the conformity certification for the particular part. Any nonconformity described as a deviation should be brought to the attention of the FAA or EASA JCAB for evaluation and disposition as to its effect on safety and the validity of the test under considerationdisposition. The FAA or EASA JCAB should receive a report stating the disposition of required on each deviation before an FAA Form 8130-3 or EASA JCAB CAR Form 1 18 is issued. (e) Neither conformity certification on prototype parts, nor inspections on production parts, should be construed as being an export airworthiness approval, since a conformity certification does not constitute an airworthiness determination. Airworthiness determinations remain the responsibility of the design/production approval holder and the airworthiness authority of the country in which the holder is located.