Airworthiness directives › 2000-04-11
AD 2000-04-11 Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes
Models named: A319, A320, A321 series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model A319, A320, and A321 series airplanes; certificated in any category; equipped with Rockwell Collins radio altimeter LRA 700 having part number (P/N) 622-4542-020; excluding those on which Airbus Modification 26017 (Airbus Service Bulletin A320-31-1106) has been installed. 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 (c) 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 erroneous display of decision height information to the flight crew during final approach, which could result in an increased risk of collision with the terrain, accomplish the following: Airplane Flight Manual (AFM) Revision (a) Within 10 days after the effective date of this AD, revise the Limitations and Normal Procedures Sections of the FAA-approved AFM by inserting a copy of Airbus Temporary Revision (TR) 2.05.00/43, dated September 16, 1999, into the AFM. Note 2: When the Temporary Revision required by paragraph (a) of this AD has been incorporated into the general revisions of the AFM, the general revisions may be inserted into the AFM, provided that the information contained in the general revisions is identical to that specified in the Temporary Revision. Optional Terminating Modification (b) In lieu of accomplishing the requirements of paragraph (a) of this AD, modify the flight warning computers, in accordance with Airbus Service Bulletin A320-31-1106, Revision 04, dated December 21, 1999. After accomplishment of the modification, the AFM temporary revision required by paragraph (a) of this AD may be removed from the AFM. Note 3: Accomplishment of the modification specified by paragraph (b) of the AD, prior to the effective date of this AD, in accordance with Airbus Service Bulletin A320-31-1106, Revision 01, dated April 16, 1997; Revision 02, dated January 20, 1998; or Revision 03, dated July 9, 1999; is considered acceptable for compliance with the applicable actions specified in paragraph (b) of this AD. Alternative Methods of Compliance (c) 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 4: 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 (d) 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 (e) The revision to the Airplane Flight Manual shall be done in accordance with Airbus Temporary Revision 2.05.00/43, dated September 16, 1999. 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 5: The subject of this AD is addressed in French airworthiness directive 2000-004-142(B), dated January 12, 2000. (f) This amendment becomes effective on March 10, 2000. Issued in Renton, Washington, on February 15, 2000. Donald L. Riggin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 00-4120 Filed 2-23-00; 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