Airworthiness directives › 2002-16-24
AD 2002-16-24 Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R (Collectively Called A300-600) Series Airplanes; and Model A310 Series Airplanes
Models named: A310 series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model A300 B4-600, B4-600R, and F4-600R (collectively called A300-600) series airplanes; and Model A310 series airplanes; certificated in any category; except those on which Airbus Service Bulletin A300-34-6132 or A310-34-2157, both dated May 17, 2001 (Airbus Industrie Modification 12100 or 12291), has been accomplished. 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 ensure that the flightcrew has adequate flight information by preventing temporary loss of data from the primary flight and navigation displays, accomplish the following: Replacement and Modification (a) Within 3 years after the effective date of this AD, replace all symbol generator units (SGUs), part number (P/N) 9612660319, in the electronic flight instrument system, with new, improved SGUs, P/N 9612660321, and modify associated equipment and wiring, according to Airbus Service Bulletin A300-34-6132 (for Model A300-600 series airplanes) or A310-34-2157 (for Model A310 series airplanes), both dated May 17, 2001, as applicable. Note 2: Airbus Service Bulletin A300-34-6132 or A310-34-2157, both dated May 17, 2001, references Thompson-CSF Sextant Service Bulletin 961266-34-038 as an additional source of service information for accomplishment of the modification. Alternative Methods of Compliance (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, Transport Airplane Directorate, FAA. 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 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the International Branch, ANM-116. Special Flight Permits (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. Incorporation by Reference (d) The actions shall be done in accordance with Airbus Service Bulletin A300-34-6132, dated May 17, 2001; or Airbus Service Bulletin A310-34-2157, dated May 17, 2001; as applicable. 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 4: The subject of this AD is addressed in French airworthiness directive 2001-467(B), dated October 3, 2001. Effective Date (e) This amendment becomes effective on September 23, 2002. Issued in Renton, Washington, on August 9, 2002. Vi Lipski, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 02-20708 Filed 8-16-02; 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