Airworthiness directives › 98-11-08
AD 98-11-08 Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
Models named: A300, A310, A300-600 series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model A300, A310, and A300-600 series airplanes; on which Airbus Modification 8928 or 6094 has not been installed; certificated in any category. Note 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been otherwise modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.
Compliance
Required as indicated, unless accomplished previously. To prevent sticking of non-return valves located in the fuel system, which could result in fuel spillage overboard and consequent insufficient fuel for the airplane to reach its flight destination, accomplish the following: (a) Within 18 months after the effective date of this AD, accomplish paragraphs (a)(1) and (a)(2) of this AD, as applicable. (1) For airplanes on which Airbus Modification 8928 has not been installed: Replace the non-return valves located in the engine fuel feed lines on the outer fuel tank with new non-return valves, in accordance with Airbus Service Bulletin A300-28-0063, Revision 01 (for Model A300 series airplanes); Airbus Service Bulletin A310-28- 2053, Revision 01 (for Model A310 series airplanes); or Airbus Service Bulletin A300-28-6031, Revision 01 (for Model A300-600 series airplanes); all dated January 15, 1997; as applicable. (2) For extended range twin-engine operations (ETOPS) airplanes, or airplanes equipped with auxiliary tanks; on which Airbus Modification 6094 has not been installed: Replace the inner tank booster pump canisters with modified canisters, in accordance with Airbus Service Bulletin A300-28-0071 (for Model A300 series airplanes); A310-28-2124 (for Model A310 series airplanes); or A300- 28-6054 (for Model A300-600 series airplanes); all dated January 15, 1997; as applicable. (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, International Branch, ANM-116. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the International Branch, ANM-116. (c) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (d) The actions shall be done in accordance with the following Airbus Service Bulletins, as applicable: A300-28-0063, Revision 01, dated January 15, 1997; A310-28-2053, Revision 01, dated January 15, 1997; A300-28-6031, Revision 01, dated January 15, 1997; A300-28-0071, dated January 15, 1997; A310-28-2124, dated January 15, 1997; and A300-28-6054, dated January 15, 1997. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Airbus Industrie, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Note 3: The subject of this AD is addressed in French airworthiness directive 97-082-215(B), dated March 12, 1997. (e) This amendment becomes effective on June 24, 1998. Issued in Renton, Washington, on May 13, 1998. John J. Hickey, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 98-13292 Filed 5-19-98; 8:45 am] BILLING CODE 4910-13-U
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1