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Airworthiness directives › 2003-25-09

AD 2003-25-09 Airworthiness Directives; Airbus Model A300 B4-600 Series Airplanes, Model A300 B4-600R Series Airplanes, Model A300 C4-605R Variant F Airplanes, and Model A300 F4-605R Airplanes

2004-01-27
2003-12-23
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Airframe
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Models named: A300 B4-600 series, A300 B4-600R series, A300 C4-605R Variant F, A300 F4-605R. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

Model A300 B4-600 series airplanes, Model A300 B4-600R series airplanes, Model A300 C4-605R Variant F airplanes, and Model A300 F4-605R airplanes; as listed in Airbus Service Bulletin A300-28-6066, dated November 8, 2000; or Airbus Service Bulletin A300-28-6070, Revision 01, dated March 22, 2002; certificated in any category.

Compliance

Required as indicated, unless accomplished previously. To prevent short circuits between 115 Volts Alternating Current (VAC) wiring and certain fuel system electrical wire runs with subsequent overheating of the cadensicon sensor thermistor or fuel level sensor, which could be great enough to ignite fuel vapors in the fuel tank and cause an explosion, accomplish the following: Modification (a)Within 4,000 flight hours after the effective date of this AD, modify elements of the electrical wiring to separate the cadensicon wiring from the 115 VAC wiring, in accordance with Airbus Service Bulletin A300-28-6066, dated November 8, 2000. (b)Within 4,000 flight hours after the effective date of this AD, modify elements of the electrical wiring to separate the 115 VAC supply wiring of the fuel gauging system, in accordance with Airbus Service Bulletin A300-28-6070, Revision 01, dated March 22, 2002. Alternative Methods of Compliance (c) In accordance with 14 CFR 39.19, the Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate, is authorized to approve alternative methods of compliance for this AD. Incorporation by Reference (d) The actions shall be done in accordance with Airbus Service Bulletin A300-28-6066, dated November 8, 2000; and Airbus Service Bulletin A300-28-6070, Revision 01, dated March 22, 2002. 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 1: The subject of this AD is addressed in French airworthiness directives 2002-172(B) and 2002-171(B), both dated April 3, 2002. Effective Date (e) This amendment becomes effective on January 27, 2004. Issued in Renton, Washington, on December 11, 2003. Kevin M. Mullin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 03-31191 Filed 12-22-03; 8:45 am] BILLING CODE 4910-13-P

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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