AD 2007-06-03 Airworthiness Directives; Airbus Model A330 Airplanes

Models named: A330. Read the applicability below — it usually turns on serial or part numbers too.

This AD applies to Airbus Model A330 airplanes, all certified models, certificated in any category, all serial numbers up to 755 included. Reason (d) The mandatory continuing airworthiness information (MCAI) states that one Model A330 operator discovered that the line connection to the discharge head could not be properly secured during engine fire bottle replacement, due to a missing retaining-ring. Inspections revealed that all four discharge-heads line connectors, two per engine, were missing the retaining-ring. It was confirmed later that it was a quality issue. The function of the retaining-ring is to secure a tight connection between the fire-extinguishing line and the discharge head. In absence of the retaining-ring, in case of activation of the fire extinguishing system, the pressure exerted by the agent on the pipe could compromise the tightness of the connection, leading to an incomplete discharge of the extinguishing agent in the fire zone. This situation if not corrected could lead, in the worst case, in combination with an engine fire, to a temporary uncontrolled engine fire which constitutes an unsafe condition. The MCAI requires a one-time detailed visual inspection for the presence of the retaining-ring on the discharge head assembly of engine fire extinguishing system, and repair if necessary.

Unless already done, do the following actions. Within 900 flight hours from the effective date of this AD: On both engine pylons (left hand and right hand), for all four engine fire extinguisher bottles, two per engine pylon, perform a one-time detailed visual inspection for the presence of the retaining ring on the discharge head of the bottles and apply all applicable corrective actions, in accordance with instructions defined in Airbus Service Bulletin A330-26A3037, dated July 26, 2006. Do all applicable corrective actions before further flight. Aircraft on which the four engine fire extinguishing bottles, 2 per engine pylon, have been removed and re-installed at the opportunity of hydrostatic test of engine fire extinguishing as per Airbus A330 Maintenance Review Board Report (MRBR) task 26.21.00/04, are not concerned by this AD. Other FAA AD Provisions (f) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, Attn: Todd Thompson, Aerospace Engineer, 1601 Lind Avenue, SW., Renton, Washington 98057-3356, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Before using any AMOC approved in accordance with § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Material Incorporated by Reference (g) You must use Airbus Service Bulletin A330-26A3037, excluding Appendix 01, dated July 26, 2006, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France. (3) You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Renton, Washington, on March 5, 2007. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-4380 Filed 3-14-07; 8:45 am] BILLING CODE 4910-13-P

Unless already done, do the following actions. Within 900 flight hours from the effective date of this AD: On both engine pylons (left hand and right hand), for all four engine fire extinguisher bottles, two per engine pylon, perform a one-time detailed visual inspection for the presence of the retaining ring on the discharge head of the bottles and apply all applicable corrective actions, in accordance with instructions defined in Airbus Service Bulletin A330-26A3037, dated July 26, 2006. Do all applicable corrective actions before further flight. Aircraft on which the four engine fire extinguishing bottles, 2 per engine pylon, have been removed and re-installed at the opportunity of hydrostatic test of engine fire extinguishing as per Airbus A330 Maintenance Review Board Report (MRBR) task 26.21.00/04, are not concerned by this AD. Other FAA AD Provisions (f) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, Attn: Todd Thompson, Aerospace Engineer, 1601 Lind Avenue, SW., Renton, Washington 98057-3356, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Before using any AMOC approved in accordance with § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Material Incorporated by Reference (g) You must use Airbus Service Bulletin A330-26A3037, excluding Appendix 01, dated July 26, 2006, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France. (3) You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Renton, Washington, on March 5, 2007. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-4380 Filed 3-14-07; 8:45 am] BILLING CODE 4910-13-P