Common use of Unsafe Condition and Mandatory Continuing Airworthiness Actions Clause in Contracts

Unsafe Condition and Mandatory Continuing Airworthiness Actions. (a) The FAA (under 14 CFR Part 39) and LFV under BCL-M1.11 issue mandatory continuing airworthiness actions. The FAA and LFV agree to perform the following functions for the products, appliances, and parts for which it is the State of Design (exporting authority): (1) Issuing a mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product or appliance, and is likely to exist or develop on a type certificated product or appliance of the same design. This may include a product or appliance that has another product, part, or appliance installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, the following: (i) Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, and parts; (ii) Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, unapproved part); (iv) The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and (v) Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date. (2) Ensuring that the following information is provided to the other authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (i) The number of aircraft world-wide needing corrective action; (ii) A statement on the availability of parts; and (iii) An estimate of the number of labor hours and the cost of parts required for the corrective actions. (3) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (4) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c) above. Additionally, the exporting authority shall arrange for copies of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to be forwarded to the appropriate focal point in the product-responsible FAA Directorate and the Luftfartsverket. (5) In the case of emergency airworthiness action, the exporting authority should ensure special handling so that the importing authority is notified immediately. (6) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (7) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) On a yearly basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products exported to the country of import. (b) The FAA and LFV recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design prior to issuing its own airworthiness directive.

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Samples: Implementation Procedures

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Unsafe Condition and Mandatory Continuing Airworthiness Actions. (a) The FAA (under 14 CFR Part 39) and LFV under BCL-M1.11 UKCAA Airworthiness Notice No. 36 issue mandatory continuing airworthiness actions. The FAA and LFV UKCAA agree to perform the following functions for the products, appliances, and parts for which it is the State of Design (exporting authority): (1) Issuing a mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product or appliance, and is likely to exist or develop on a type certificated product or appliance of the same design. This may include a product or appliance that has another product, part, or appliance installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, the following: (i) Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, and parts; (ii) Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, unapproved part); (iv) The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and (v) Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date. (2) Ensuring that the following information is provided to the other authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (i) The number of aircraft world-wide needing corrective action; (ii) A statement on the availability of parts; and (iii) An estimate of the number of labor hours and the cost of parts required for the corrective actions. (3) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (4) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c) above. Additionally, the exporting authority shall arrange for copies of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to be forwarded to the appropriate focal point in the product-responsible FAA Directorate and the LuftfartsverketUKCAA Applications and Certifications Department, Safety Regulation Group. (5) In the case of emergency airworthiness action, the exporting authority should ensure special handling so that the importing authority is notified immediately. (6) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (7) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) On a yearly basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products exported to the country of import. (b) The FAA and LFV UKCAA recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design prior to issuing its own airworthiness directive. (c) The FAA and UKCAA, as importing authorities, agree to respond quickly to the issuance of a mandatory continuing airworthiness action by the exporting authority in making its own determination of the need for issuing its own similar mandatory continuing airworthiness action that addresses the unsafe condition on the affected product certified, approved or otherwise accepted by the importing authority.

Appears in 1 contract

Samples: Implementation Procedures

Unsafe Condition and Mandatory Continuing Airworthiness Actions. (a) The FAA (under 14 CFR Part 39) and LFV ENAC (under BCL-M1.11 Regolamento Tecnico, Primo/11/F and Procedura Operativa ASV-04) issue mandatory continuing airworthiness actions. The FAA and LFV ENAC agree to perform the following functions for the products, appliances, and parts for which it is the State of Design (exporting authority): (1) Issuing a mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product or appliance, appliance and is likely to exist or develop on a type certificated product or appliance of the same design. This may include a product or appliance that has another product, part, or appliance installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, the following: (i) Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, and parts; (ii) Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, unapproved part); (iv) The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and (v) Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date. (2) Ensuring that the following information is provided to the other authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (i) The number of aircraft world-wide needing corrective action; (ii) A statement on the availability of parts; and (iii) An estimate of the number of labor hours and the cost of parts required for the corrective actions. (3) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (4) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c) above. Additionally, the exporting authority shall arrange for copies of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to be forwarded to the appropriate focal point in the product-responsible FAA Directorate and the LuftfartsverketENAC’s Maintenance and Production Service. (5) In the case of emergency airworthiness action, the exporting authority should ensure special handling so that the importing authority is notified immediately. (6) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (7) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) On a yearly basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products exported to the country of import. (b) The FAA and LFV ENAC recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design prior to issuing its own airworthiness directive.

Appears in 1 contract

Samples: Implementation Procedures

Unsafe Condition and Mandatory Continuing Airworthiness Actions. (aReference Section III Par 3.3.0.2). (1) The Each country’s implementing authority, the FAA (under 14 CFR part 39) and CASA (under CASR Part 39) and LFV under BCL-M1.11 issue mandatory continuing airworthiness actions. The FAA and LFV agree to will perform the following functions for the products, appliances, and parts for which it is the State of Design (exporting authority): (1i) Issuing a Ensuring the mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product or appliance, and is likely to exist or develop on a type certificated product or appliance of the same design. This may include a product or appliance that has another product, part, or appliance installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, includes the following: (i) a. Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, and parts; (ii) b. Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) c. Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, unapproved part); (iv) d. The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and (v) e. Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date. (2ii) Ensuring that the following information is provided to the other implementing authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (i) The a. An estimate of the number of aircraft world-wide needing corrective action; (ii) b. A statement on the availability of parts; and (iii) c. An estimate of the number of labor hours and the cost of parts required for the corrective actions. (3iii) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (4iv) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c) aboveappropriate address. Additionally, the exporting authority shall for Australian products, CASA should arrange for copies of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to be forwarded to the appropriate focal point in the product-product- responsible FAA Directorate and as listed in Appendix A to the LuftfartsverketImplementation Procedures for Airworthiness. (5v) In the case of emergency airworthiness actioninformation, the exporting authority should ensure special handling so that the importing authority is notified immediately. (6vi) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (7vii) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) On a yearly basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products exported to the country of import. (b) The FAA and LFV recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design prior to issuing its own airworthiness directive.

Appears in 1 contract

Samples: Agreement on the Promotion of Aviation Safety

Unsafe Condition and Mandatory Continuing Airworthiness Actions. (a) The FAA (under 14 CFR Part 39) and LFV CAA-NL (under BCL-M1.11 Artikel 3.22 van de Luchtvaartwet) issue mandatory continuing airworthiness actions. The FAA and LFV CAA-NL agree to perform the following functions for the products, appliances, and parts for which it is the State of Design (exporting authority): (1) Issuing a mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product or appliance, and is likely to exist or develop on a type certificated product or appliance of the same design. This may include a product or appliance that has another product, part, or appliance installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, the following: (i) Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, and parts; (ii) Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, unapproved part); (iv) The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and (v) Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date. (2) Ensuring that the following information is provided to the other authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (i) The number of aircraft world-wide needing corrective action; (ii) A statement on the availability of parts; and (iii) An estimate of the number of labor hours and the cost of parts required for the corrective actions. (3) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (4) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c) above. Additionally, the exporting authority shall arrange for copies of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to be forwarded to the appropriate focal point in the product-responsible FAA Directorate and the LuftfartsverketCivil Aviation Authority Netherlands. (5) In the case of emergency airworthiness action, the exporting authority should ensure special handling so that the importing authority is notified immediately. (6) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (7) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) On a yearly basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products exported to the country of import. (b) The FAA and LFV recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design prior to issuing its own airworthiness directive.

Appears in 1 contract

Samples: Implementation Procedures

Unsafe Condition and Mandatory Continuing Airworthiness Actions. (a) The FAA (under 14 CFR Part 39) and LFV JCAB (under BCLJCAB Circular 3-M1.11 issue mandatory continuing airworthiness actions. The FAA and LFV 003, Management of Mandatory Continuing Airworthiness Actions) agree to perform the following functions for the products, appliances, and parts for which it is the State of Design (exporting authority): (1) Issuing a mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product or appliance, and is likely to exist or develop on a type certificated product or appliance of the same type design. This may include a product or appliance that has another product, part, or appliance installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, the following: (i) Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, and parts; (ii) Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, unapproved part); (iv) The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and (v) Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date. (2) Ensuring that the following information is provided to the other authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (i) The number of aircraft world-wide needing corrective action; (ii) A statement on the availability of parts; and (iii) An estimate of the number of labor hours and the cost of parts required for the corrective actions. (3) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (4) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c) above. Additionally, for Japanese products, the exporting authority shall JCAB should arrange for copies of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to be forwarded to the appropriate focal point in the product-responsible FAA Directorate and the LuftfartsverketDirectorate. (5) In the case of emergency airworthiness actioninformation, the exporting authority should ensure special handling so that the importing authority is notified immediately. (6) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (7) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) On a yearly basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products exported to the country of import. (b) The FAA and LFV JCAB recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design (exporting authority) prior to issuing its own airworthiness directive. If the State of Design agrees that mandatory action is needed, then they will issue the AD. If the State of Design disagrees with the proposed mandatory action, it will notify the importing authority with its justification in writing via email. The importing authority will hold a teleconference with appropriate management of both authorities to discuss the unilateral AD action and when it will commence. (c) The FAA and JCAB, as importing authorities, agree to respond quickly to the issuance of a mandatory continuing airworthiness action by the exporting authority in making its own determination of the need for issuing its own similar mandatory continuing airworthiness action that addresses all unsafe conditions on affected products or appliances certified, approved or otherwise accepted by the importing authority.

Appears in 1 contract

Samples: Implementation Procedures

Unsafe Condition and Mandatory Continuing Airworthiness Actions. (a) The FAA (under 14 CFR Part 39) and LFV ANAC (under BCL-M1.11 RBHA 39) issue mandatory continuing airworthiness actions. The FAA and LFV ANAC agree to perform the following functions for the products, appliances, parts and parts appliances for which it is the State of Design (exporting authority): (1) Issuing a mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product or appliance, and is likely to exist or develop on a type certificated product or appliance of the same type design. This may include a product or appliance that has another product, part, or appliance installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, the following: (i) Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, and parts; (ii) Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, unapproved part); (iv) The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and (v) Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date. (2) Ensuring that the following information is provided to the other authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (i) The number of aircraft world-wide worldwide needing corrective action; (ii) A statement on the availability of parts; and (iii) An estimate of the number of labor hours and the cost of parts required for the corrective actions. (For Brazil, this data is included in the applicable service bulletin.) (3) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (4) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c) above. Additionally, the exporting authority shall arrange for copies of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to be forwarded to the appropriate focal point in the product-responsible FAA Directorate and the LuftfartsverketANAC. (5) In the case of emergency airworthiness action, the exporting authority should ensure special handling so that the importing authority is notified immediately. (6) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (7) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) On a yearly quarterly basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products and appliances exported to the country of import. (b) The FAA and LFV ANAC recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design (exporting authority) prior to issuing its own airworthiness directive. (c) The FAA and ANAC, as importing authorities, agree to respond quickly to the issuance of a mandatory continuing airworthiness action by the exporting authority in making its own determination of the need for issuing its own similar mandatory continuing airworthiness action that addresses the unsafe condition on affected products or appliances certified, approved or otherwise accepted by the importing authority.

Appears in 1 contract

Samples: Implementation Procedures

Unsafe Condition and Mandatory Continuing Airworthiness Actions. (a) The FAA (under 14 CFR Part 39) and LFV LBA (under BCL-M1.11 LuftBO) issue mandatory continuing airworthiness actions. The FAA and LFV LBA agree to perform the following functions for the products, appliances, and parts for which it is the State of Design (exporting authority): (1) Issuing a mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product or appliance, and is likely to exist or develop on a type certificated product or appliance of the same design. This may include a product or appliance that has another product, part, or appliance installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, the following: (i) Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, and parts; (ii) Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, unapproved part); (iv) The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and (v) Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date. (2) Ensuring that the following information is provided to the other authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (i) The number of aircraft world-wide needing corrective action; (ii) A statement on the availability of parts; and (iii) An estimate of the number of labor hours and the cost of parts required for the corrective actions. (3) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (4) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c) above. Additionally, the exporting authority shall arrange for copies of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to be forwarded to the appropriate focal point in the product-responsible FAA Directorate and the LuftfartsverketLBA. For the LBA, this information is located on the LBA internet web site (xxx.xxx.xx). (5) In the case of emergency airworthiness action, the exporting authority should ensure special handling so that the importing authority is notified immediately. (6) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (7) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) On a yearly basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products exported to the country of import. (b) The FAA and LFV recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design prior to issuing its own airworthiness directive.

Appears in 1 contract

Samples: Implementation Procedures

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Unsafe Condition and Mandatory Continuing Airworthiness Actions. (a) The FAA (under 14 CFR Part 39) and LFV DGAC (under BCL-M1.11 Arrêté dated November 22, 1978) issue mandatory continuing airworthiness actions. The FAA and LFV DGAC agree to perform the following functions for the products, appliances, and parts for which it is the State of Design (exporting authority): (1) Issuing a mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product or appliance, and is likely to exist or develop on a type certificated product or appliance of the same design. This may include a product or appliance that has another product, part, or appliance installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, the following: (i) Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, and parts; (ii) Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, unapproved part); (iv) The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and (v) Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date. (2) Ensuring that the following information is provided to the other authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (i) The number of aircraft world-wide needing corrective action; (ii) A statement on the availability of parts; and (iii) An estimate of the number of labor hours and the cost of parts required for the corrective actions. (3) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (4) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c) above. Additionally, the exporting authority shall arrange for copies of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to be forwarded to the appropriate focal point in the product-responsible FAA Directorate and the Luftfartsverketor to Groupement pour la Sécurité de l’Aviation Civile (GSAC). (5) In the case of emergency airworthiness action, the exporting authority should ensure special handling so that the importing authority is notified immediately. (6) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (7) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) On a yearly basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products exported to the country of import. (b) The FAA and LFV recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design prior to issuing its own airworthiness directive.

Appears in 1 contract

Samples: Implementation Procedures

Unsafe Condition and Mandatory Continuing Airworthiness Actions. (a) The FAA (under subject to 14 CFR Part 39) and LFV under BCL-M1.11 issue mandatory continuing airworthiness actions. The FAA and LFV TCCA (subject to CAR 593) agree to perform the following functions for the products, appliances, and parts for which it is the State of Design (exporting authority):Design: (1) Issuing a mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product product, or appliance, and is likely to exist or develop on a type certificated product or appliance of the same type design. This may include a product or appliance that has another product, part, or appliance product installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, the following: (i) Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, and parts; (ii) Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, suspected unapproved part); (iv) The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and; (v) Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date.; (2) Ensuring that the following information is provided to the other authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (ivi) The number of aircraft world-wide needing corrective action; (iivii) A statement on the availability of parts; and (iiiviii) An estimate of the number of labor hours and the cost of parts required for the corrective actions. (For Canada this data is included in the applicable service bulletin.) (32) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (43) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c) above. AdditionallyAdditionally for Canadian products, the exporting authority shall arrange for copies a copy of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to should be forwarded to the appropriate focal point in the FAA product-responsible FAA Directorate and the LuftfartsverketDirectorate. (54) In the case of emergency airworthiness actioninformation, the exporting authority should ensure special handling so that notify the importing authority immediately. TCCA will ensure that the information is notified immediatelytransmitted by fax to AFS-610 in Oklahoma City and the New York ACO for a Canadian product.. The FAA will ensure that information is faxed to TCCA Headquarters Aircraft Certification from the responsible directorate and/or AFS-610 in Oklahoma City when emergency airworthiness information is issued on U.S. products. (65) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (76) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) 7) On a yearly quarterly basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products exported to the country of import. (b) The FAA and LFV TCCA recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design (exporting authority) prior to issuing its own airworthiness directive. The exporting authority will facilitate the type certificate holder’s providing sufficient information, e.g. service bulletins, to the importing authority in a timely manner for its use in issuing this unilateral airworthiness directive.

Appears in 1 contract

Samples: Implementation Procedures

Unsafe Condition and Mandatory Continuing Airworthiness Actions. (a) The FAA (under subject to 14 CFR Part 39) and LFV under BCL-M1.11 issue mandatory continuing airworthiness actions. The FAA and LFV AR (subject to AP-39) agree to perform the following functions for the products, appliances, and parts for which it is the State of Design (exporting authority):: (1) Issuing a mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product product, or appliance, and is likely to exist or develop on a type certificated product or appliance of the same type design. This may include a product or appliance that has another product, part, or appliance product installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, the following: (i) Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, product and parts; (ii) Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, suspected unapproved part); (iv) The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and; (v) Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date.; (2) Ensuring that the following information is provided to the other authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (ivi) The number of aircraft world-wide needing the corrective action; (iivii) A statement on the availability of parts; and (iiiviii) An estimate of the number of labor hours and the cost of parts required for the corrective actions. (32) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (43) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c3.4.0.1(c) above. Additionally, the exporting authority shall arrange for copies Russian aeronautical products, a copy of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to should be forwarded to the appropriate focal point in the product-responsible FAA Directorate and the LuftfartsverketDirectorate. (54) In the case of emergency airworthiness actioninformation, the exporting authority should ensure special handling so that the importing authority is notified immediately. (65) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (76) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) 7) On a yearly quarterly basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products exported to the country of import. (b) The FAA and LFV AR recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design (exporting authority) prior to issuing its own airworthiness directive. (c) The FAA and AR, as importing authorities, agree to respond quickly to the issuance of a mandatory continuing airworthiness action by the exporting authority in making its own determination of the need for issuing its own similar mandatory continuing airworthiness action that addresses all unsafe conditions on affected products certified, approved or otherwise accepted by the importing authority.

Appears in 1 contract

Samples: Implementation Procedures

Unsafe Condition and Mandatory Continuing Airworthiness Actions. (a) The FAA (under 14 CFR Part 39) and LFV RCAA (under BCL-M1.11 RACR 39) issue mandatory continuing airworthiness actions. The FAA and LFV RCAA agree to perform the following functions for the products, appliancesparts, and parts appliances for which it is the State of Design (exporting authority): (1) Issuing a mandatory continuing airworthiness action (Airworthiness Directive) whenever the authority determines that an unsafe condition exists in a type certificated product or appliance, and is likely to exist or develop on a type certificated product or appliance of the same design. This may include a product or appliance that has another product, part, or appliance installed on it and the installation causes the unsafe condition. The contents of such a mandatory continuing airworthiness action should include, but are not limited to, the following: (i) Make, model, and serial numbers of affected aircraft, aircraft engines, propellers, appliances, and parts; (ii) Description of the unsafe condition, reasons for the mandatory action, and its impact on the overall aircraft and continued operation; (iii) Description of the cause of the unsafe condition (e.g., stress corrosion, fatigue, design problem, quality control, unapproved part); (iv) The means by which the unsafe condition was detected and, if resulting from in-service experience, the number of occurrences; and (v) Corrective actions and corresponding compliance times, with a list of the relevant manufacturer’s service information including reference number, revision number and date.; (2) Ensuring that the following information is provided to the other authority as part of the mandatory continuing airworthiness action or directly from the approval holder: (i) The number of aircraft world-wide needing the corrective action; (ii) A statement on the availability of parts; and (iii) An estimate of the number of labor hours and the cost of parts required for the corrective actions. (3) Issuing a revised or superseding mandatory continuing airworthiness action whenever the exporting authority finds any previously issued mandatory continuing airworthiness action was incomplete or inadequate to fully correct the unsafe condition. (4) Notifying the importing authority of the unsafe condition and the necessary corrective actions by submitting a copy of the mandatory continuing airworthiness action at the time of publication to the address referenced in 3.3.0.1(c) above. Additionally, for Romanian products, the exporting authority shall RCAA should arrange for copies of all relevant service bulletins referenced in the mandatory action, as well as other supporting documentation, to be forwarded to the appropriate focal point in the product-responsible FAA Directorate and the LuftfartsverketSmall Airplane Directorate. (5) In the case of emergency airworthiness action, the exporting authority should ensure special handling so that the importing authority is notified immediately. (6) Advising and assisting the importing authority in defining the appropriate actions for the importing authority to take in the issuance of its own mandatory continuing airworthiness action. (7) Providing sufficient information to the importing authority for its use in making determinations as to the acceptability of alternative means of compliance to mandatory continuing airworthiness actions. (8) On a yearly annual basis, providing the importing authority a summary index list of mandatory continuing airworthiness actions issued by the exporting authority for products and appliances exported to the country of import. (b) The FAA and LFV RCAA recognize that they may disagree as to the finding of an unsafe condition. In that case, it is expected that the importing authority will normally consult with the authority of the State of Design (exporting authority) prior to issuing its own airworthiness directive. (c) The FAA and RCAA, as importing authorities, agree to respond quickly to the issuance of a mandatory continuing airworthiness action by the exporting authority in making its own determination of the need for issuing its own similar mandatory continuing airworthiness action that addresses the unsafe condition on the affected products or appliances certified, approved or otherwise accepted by the importing authority.

Appears in 1 contract

Samples: Implementation Procedures

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