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Airworthiness directives › 2004-15-08

AD 2004-15-08 Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Series Airplanes

Superseded. This directive was replaced by AD 2012-22-15. Work to the current one.
2004-08-31
2004-07-27
39-13742
2002-NM-280-AD
Airframe
2012-22-15

Models named: F.28 Mark 0070, 0100 series. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

All Model F.28 Mark 0070 and 0100 series airplanes, certificated in any category.

Compliance

Required as indicated, unless accomplished previously. To ensure that fatigue cracking of certain structural elements is detected and corrected, and to ensure the structural integrity of affected airplanes, accomplish the following: Requirements of AD 2001-21-04 Airworthiness Limitations Revision (a) Within 30 days after December 4, 2001 (the effective date of AD 2001-21-04, amendment 39-12475), revise the Airworthiness Limitations section (ALS) of the Instructions for Continued Airworthiness by incorporating Report SE-623, “Fokker 70/100 Airworthiness Limitations Items and Safe Life Items,” of Appendix 1 of Fokker 70/100 Maintenance Review Board (MRB) document, dated June 1, 2000. (b) Except as provided by paragraph (c) this AD: After the actions specified in paragraph (a) of this AD have been accomplished, no alternative inspections or inspection intervals may be approved for the structural elements specified in the documents listed in paragraph (a) of this AD. New Requirements of This AD New Airworthiness Limitations Revision (c) Within 6 months after the effective date of this AD, revise the Airworthiness Limitations section (ALS) of the Instructions for Continued Airworthiness by incorporating Fokker Services B.V. Report SE-623, “Fokker 70/100 Airworthiness Limitations Items and Safe Life Items,” Issue 2, dated September 1, 2001; and Fokker Services B.V. Report SE-473, “Fokker 70/100 Certification Maintenance Requirements,” Issue 5, dated July 16, 2001; into Section 6 of the Fokker 70/100 MRB document. (These reports are already incorporated into Fokker 70/100 MRB document, Revision 10, dated October 1, 2001.) Once the actions required by this paragraph have been accomplished, the original issue of Fokker Services B.V. Report SE-623, “Fokker 70/100 Airworthiness Limitations Items and Safe Life Items,” dated June 1, 2000, may be removed from the ALS of the Instructions for Continued Airworthiness. (d) If the requirements of paragraph (c) of this AD are accomplished within the compliance time specified in paragraph (a) of this AD, it is not necessary to accomplish the requirements of paragraph (a) of this AD. (e) After the actions specified in paragraph (c) of this AD have been accomplished, no alternative inspections or inspection intervals may be approved for the structural elements specified in the documents listed in paragraph (c) of this AD. Alternative Methods of Compliance (f) In accordance with 14 CFR 39.19, the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, is authorized to approve alternative methods of compliance for this AD. Incorporation by Reference (g) The actions shall be done in accordance with Fokker Services B.V. Report SE-623, “Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,” dated June 1, 2000; Fokker Services B.V. Report SE-623, “Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,” Issue 2, dated September 1, 2001; and Fokker Services B.V. Report SE-473, “Fokker 70/100 Certification Maintenance Requirements,” Issue 5, dated July 16, 2001. (1) The incorporation by reference of Fokker Services B.V. Report SE-623, “Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,” Issue 2, dated September 1, 2001; and Fokker Services B.V. Report SE-473, “Fokker 70/100 Certification Maintenance Requirements,” Issue 5, dated July 16, 2001; is approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. (2) The incorporation by reference of Fokker Services B.V. Report SE-623, “Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,” dated June 1, 2000, was approved by the Director of the Federal Register as of December 4, 2001 (66 FR 54656, October 30, 2001). (3) Copies may be obtained from Fokker Services B.V., P.O. Box 231, 2150 AE Nieuw-Vennep, the Netherlands. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html . Note 1: The subject of this AD is addressed in Dutch airworthiness directive 2002-062, dated May 31, 2002. Effective Date (h) This amendment becomes effective on August 31, 2004. Issued in Renton, Washington, on July 9, 2004. Kevin M. Mullin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04-16677 Filed 7-26-04; 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