Airworthiness directives › 2000-08-18
AD 2000-08-18 Airworthiness Directives; McDonnell Douglas Model DC-9 Series Airplanes, and Model MD-88 and MD-90-30 Airplanes
Models named: DC-9 series, MD-88, MD-90-30. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model DC-9 series airplanes, and Model MD-88 airplanes, as listed in McDonnell Douglas Alert Service Bulletin DC9-25A357, Revision 02, dated May 28, 1998; and Model MD-90-30 airplanes, as listed in McDonnell Douglas Alert Service Bulletin MD90-25A019, dated February 11, 1997; certificated in any category. Note 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been 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 the improper deployment of the evacuation slide, which could delay or impede evacuation of passengers during an emergency, accomplish the following: Replacement (a) Within 180 days after the effective date of this AD, replace the lanyard assembly pins of the evacuation slides with solid corrosion-resistant pins, in accordance with McDonnell Douglas Alert Service Bulletin MD80-25A357, dated February 11, 1997, Revision 01, dated March 16, 1998, or Revision 02, dated May 28, 1998 (for Model DC-9 series airplanes and Model MD-88 airplanes); or McDonnell Douglas Alert Service Bulletin MD90-25A019, dated February 11, 1997 (for Model MD-90-30 airplanes); as applicable. Spares (b) As of the effective date of this AD, no lanyard assembly, part number (P/N) 3961899-1 or P/N 3956939-501, shall be installed on any airplane unless that assembly has been modified in accordance with the requirements of paragraph (a) 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, Los Angeles Aircraft Certification Office (ACO), 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, Los Angeles ACO. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Los Angeles ACO. 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 replacement shall be done in accordance with McDonnell Douglas Alert Service Bulletin MD80-25A357, dated February 11, 1997; McDonnell Douglas Alert Service Bulletin DC9-25A357, Revision 01, dated March 16, 1998; McDonnell Douglas Alert Service Bulletin DC9-25A357, Revision 02, dated May 28, 1998; or McDonnell Douglas Alert Service Bulletin MD90-25A019, dated February 11, 1997; 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 Boeing Commercial Aircraft Group, Long Beach Division, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Technical Publications Business Administration, Dept. C1-L51 (2-60). Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Transport Airplane Directorate, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (f) This amendment becomes effective on June 13, 2000. Issued in Renton, Washington, on April 19, 2000. Donald L. Riggin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 00-10288 Filed 5-8-00; 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