Airworthiness directives › 2001-13-17
AD 2001-13-17 Airworthiness Directives; Airbus Model A300 B2 and A300 B4; A300 B4-600, B4-600R, and F4-600R (Collectively Called A300-600); and A310 Series Airplanes
Applicability*9
All Model A300 B2 and A300 B4; A300 B4-600, B4-600R, and F4-600R (collectively called A300-600); and A310 series airplanes; certificated in any category.
Compliance
Required as indicated, unless accomplished previously. To prevent inadvertent excursions outside the normal flight envelope in the event of lost or erroneous airspeed indications, accomplish the following: Revision to Airplane Flight Manual (AFM) (a) For Model A300 B2-1A series airplanes equipped with General Electric CF6-50A engines, and for Model A300 B4-600 series airplanes equipped with Pratt & Whitney JT9D-7R4H1 engines: Within 10 days after the effective date of this AD, revise the “Procedures Following Failure” Section of the FAA-approved AFM, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA. (b) For all airplanes not identified in paragraph (a) of this AD: Within 10 days after the effective date of this AD, revise the “Procedures Following Failure” Section of the applicable AFM by inserting into the AFM a copy of the applicable Temporary Revision (TR) listed in the following table: Table 1.—Temporary Revisions Model/series Engine TR No. Date A300 GE CF6-50C 4.02.00/08 April 25, 2001. A300 GE CF6-50C2/C2R 4.02.00/09 April 26, 2001. A300-600 GE CF6-80C2 4.02.00/11 March 21, 2000. A300-600 PW 4000 4.02.00/13 March 28, 2000. A310 GE CF6-80A3 4.02.00/11 March 21, 2000. A310 GE CF6-80C2 4.02.00/12 March 22, 2000. A310 PW JT9D-7R4 4.02.00/13 March 23, 2000. A310 PW 4000 4.02.00/14 March 24, 2000. (c) When the information in the applicable TR listed in Table 1 of this AD has been incorporated into the FAA-approved general revisions of the AFM, the general revisions may be incorporated into the AFM, and the TR may be removed from the AFM. 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. 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, ANM-116. Note 1: 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 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 (f) The AFM revision required by paragraph (b) of this AD shall be done in accordance with A300 Flight Manual Temporary Revision 4.02.00/08, dated April 25, 2001; A300 Flight Manual Temporary Revision 4.02.00/09, dated April 26, 2001; A300-600 Flight Manual Temporary Revision 4.02.00/11, dated March 21, 2000; A300-600 Flight Manual Temporary Revision 4.02.00/13, dated March 28, 2000; A310 Flight Manual Temporary Revision 4.02.00/11, dated March 21, 2000; A310 Flight Manual Temporary Revision 4.02.00/12, dated March 22, 2000; A310 Flight Manual Temporary Revision 4.02.00/13, dated March 23, 2000; and A310 Flight Manual Temporary Revision 4.02.00/14, dated March 24, 2000; as applicable. (Only page 2 of each Temporary Revision contains the document date; no other page of these documents contains this information.) 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 2: The subject of this AD is addressed in French airworthiness directive 2001-129(B), dated April 4, 2001. Effective Date (g) This amendment becomes effective on July 17, 2001. Issued in Renton, Washington, on June 21, 2001. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 01-16199 Filed 6-29-01; 8:45 am] BILLING CODE 4910-13-P
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