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Airworthiness directives › 2007-25-06

AD 2007-25-06 Airworthiness Directives; Airbus Model A300 Series Airplanes, Model A300-600 Series Airplanes, and Model A310 Series Airplanes

2008-01-14
2007-12-10
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Airframe
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Models named: A300 series, A310 series, A300-600 series. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to the following airplanes, certificated in any category: (1) Model A300 series airplanes, manufacturer serial numbers 0202, 0205, 0225, 0299, and 0302, in forward facing crew cockpit configuration, except airplanes which have received in service application of Airbus Service Bulletin A300-21-0132. (2) Model A310 series airplanes, all certified models, all serial numbers, except airplanes which have received in service application of Airbus Service Bulletin A310-21-2062. (3) Model A300-600 series airplanes, all certified models, all serial numbers, on which Airbus Modification 03881 is embodied, except airplanes which have received either incorporation of Airbus Modification 12942 during production, or application of Airbus Service Bulletin A300-21-6049 in service.

Compliance

Unless already done, do the following actions. (1) Within 18 months after the effective date of this AD: Install an automatic opening logic either for the forward and aft OFV (outflow valve) or for the single depress valve, as applicable, by introducing the use of discrete spoiler signals, driving one (Model A300 airplanes) or two (Model A310 airplanes and Model A300-600 series airplanes) time delay relays, in accordance with the instructions of Airbus Service Bulletin A300-21-0132, dated July 28, 2006; A310-21-2062, dated July 20, 2006; or A300-21-6049, Revision 02, dated April 16, 2007; as applicable. (2) Actions done before the effective date of this AD in accordance with Airbus Service Bulletin A300-21-6049, dated August 31, 2005; or Revision 01, dated September 15, 2006, are acceptable for compliance with the corresponding requirements of this AD. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Tom Stafford, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington, 98057-3356; telephone (425) 227-1622; fax (425) 227-1149. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (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. Related Information (h) Refer to MCAI European Aviation Safety Agency Airworthiness Directive 2007-0005, dated January 8, 2007; and Airbus Service Bulletins A300-21-0132, dated July 28, 2006; A300-21-6049, Revision 02, dated April 16, 2007; and A310-21-2062, dated July 20, 2006; for related information. Material Incorporated by Reference (i) You must use the applicable Airbus service information specified in Table 1 of this AD 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 . Table 1.—Material Incorporated by Reference Airbus Service Bulletin Revision Date A300-21-0132 Original July 28, 2006. A300-21-6049 02 April 16, 2007. A310-21-2062 Original July 20, 2006. Issued in Renton, Washington, on November 23, 2007. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-23462 Filed 12-7-07; 8:45 am] BILLING CODE 4910-13-P

Required actions

Unless already done, do the following actions. (1) Within 18 months after the effective date of this AD: Install an automatic opening logic either for the forward and aft OFV (outflow valve) or for the single depress valve, as applicable, by introducing the use of discrete spoiler signals, driving one (Model A300 airplanes) or two (Model A310 airplanes and Model A300-600 series airplanes) time delay relays, in accordance with the instructions of Airbus Service Bulletin A300-21-0132, dated July 28, 2006; A310-21-2062, dated July 20, 2006; or A300-21-6049, Revision 02, dated April 16, 2007; as applicable. (2) Actions done before the effective date of this AD in accordance with Airbus Service Bulletin A300-21-6049, dated August 31, 2005; or Revision 01, dated September 15, 2006, are acceptable for compliance with the corresponding requirements of this AD. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Tom Stafford, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington, 98057-3356; telephone (425) 227-1622; fax (425) 227-1149. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (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. Related Information (h) Refer to MCAI European Aviation Safety Agency Airworthiness Directive 2007-0005, dated January 8, 2007; and Airbus Service Bulletins A300-21-0132, dated July 28, 2006; A300-21-6049, Revision 02, dated April 16, 2007; and A310-21-2062, dated July 20, 2006; for related information. Material Incorporated by Reference (i) You must use the applicable Airbus service information specified in Table 1 of this AD 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 . Table 1.—Material Incorporated by Reference Airbus Service Bulletin Revision Date A300-21-0132 Original July 28, 2006. A300-21-6049 02 April 16, 2007. A310-21-2062 Original July 20, 2006. Issued in Renton, Washington, on November 23, 2007. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-23462 Filed 12-7-07; 8:45 am] BILLING CODE 4910-13-P

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