Airworthiness directives › 2001-09-05
AD 2001-09-05 Airworthiness Directives; Airbus Model A310-324, A310-325, and A300 B4-622R Series Airplanes Equipped with Pratt & Whitney PW4000 Series Engines
Models named: A310-324, A310-325, A300 B4-622R series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model A310-324, A310-325, and A300 B4-622R series airplanes; certificated in any category; equipped with Pratt & Whitney PW4000 series engines, except for airplanes fitted with current-production FB2C fan blades (Phase 3 fan blades) on both engines. Note 1: Airbus Modification 10925 installs Phase 3 engines, and these are equipped with FB2C (Phase 3) fan blades. Therefore, this AD is not applicable to airplanes with that modification.
Compliance
Required as indicated, unless accomplished previously. To prevent acceleration and climb performance less than that specified in the Airplane Flight Manual (AFM), which could result in runway overruns or impact with obstacles or terrain, accomplish the following: AFM Revision (a) For Model A310-324 and -325 series airplanes: Within 30 days after the effective date of this AD, revise the FAA-approved AFM to incorporate specified adjustments in performance by inserting the following Airbus A310 Flight Manual Temporary Revisions (TR), all dated January 22, 2001, as applicable, into the Performance section of the AFM: 5.03.00/01 (for Airbus Model A310-324 series airplanes); or 5.03.00/02 (for Airbus Model A310-325 series airplanes). (b) For Model A300 B4-622R series airplanes: Within 30 days after the effective date of this AD, revise the FAA-approved AFM to incorporate specified adjustments in performance by inserting the following A300-600 Flight Manual TR, dated January 22, 2001 into the Performance section of the AFM: 5.03.00/01 (for Airbus Model A300 B4-622R series airplanes). (c) When the information in the TR's specified in paragraphs (a) and (b) of this AD, has been incorporated into FAA-approved general revisions of the applicable AFM's, the general revisions may be incorporated in the applicable AFM, and the TR's may be removed from the AFM's. Alternative Methods of Compliance (d) 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 Operations Inspector, who may add comments and then send it to the Manager, International Branch. 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. Special Flight Permits (e) Special flight permits may be issued in accordance with §§ 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 (f) The actions shall be done in accordance with Airbus A310 Flight Manual Temporary Revision 5.03.00/01, dated January 22, 2001; Airbus A310 Flight Manual Temporary Revision 5.03.00/02, dated January 22, 2001; and Airbus A300-600 Flight Manual Temporary Revision 5.03.00/01, dated January 22, 2001; as applicable. (Note: Only the first page to each of these Temporary Revisions are date stamped; no other pages of the Temporary Revisions contain the revision date.) 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 2001-086(B), dated March 7, 2001. Effective Date (g) This amendment becomes effective on May 22, 2001. Issued in Renton, Washington, on April 23, 2001. Donald L. Riggin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 01-10591 Filed 5-4-01; 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