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Airworthiness directives › 2000-26-09

AD 2000-26-09 Airworthiness Directives; Dornier Model 328-100 Series Airplanes

2001-02-07
2001-04-25
39-12190
2001-NM-67-AD
Airframe
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Models named: 328-100 series. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

All Model 328-100 series airplanes, 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 ensure continued structural integrity of these airplanes, accomplish the following: Airworthiness Limitations Revision (a) Within 30 days after the effective date of this AD, revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness by incorporating Revision 13 of the Dornier 328 Airworthiness Limitations Document (ALD), TM-ALD-010693-ALL, dated July 25, 1997, and the Temporary Revision (TR) documents into the Airworthiness Limitations Section (ALS) listed in Table 1, as follows: Table 1.—Temporary Revisions TR No. Date of issue TR ALD-042 January 31, 1997. TR ALD-048 May 12, 1998. TR ALD-050 October 2, 1997. TR ALD-052 December 11, 1997. TR ALD-053 April 29, 1998. TR ALD-054 May 12, 1998. TR ALD-055 May 26, 1998. TR ALD-056 July 22, 1998. TR ALD-057 October 23, 1998. TR ALD-059 December 11, 1998. TR ALD-062 May 18, 1999. TR ALD-063 August 10, 1999. TR ALD-064 October 10, 1999. TR ALD-065 November 26, 1999. TR ALD-067 February 7, 2000. TR ALD-068 February 4, 2000. TR ALD-070 May 25, 2000. Note 2: When the TR documents have been incorporated into the latest issue of the general revisions of the ALD, the general revisions may be incorporated into the ALS, provided that the information contained in the general revisions is identical to that specified in the TR documents. (b) Except as provided in paragraph (c) of 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. 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 3: 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 actions shall be done in accordance with Revision 13 of the Dornier 328 Airworthiness Limitations Document, TM-ALD-010693-ALL, dated July 25, 1997; and the Dornier Temporary Revisions listed in Table 2, as follows: Table 2.—Temporary Revisions TR No. Date of issue TR ALD-042 January 31, 1997. TR ALD-048 May 12, 1998. TR ALD-050 October 2, 1997. TR ALD-052 December 11, 1997. TR ALD-053 April 29, 1998. TR ALD-054 May 12, 1998. TR ALD-055 May 26, 1998. TR ALD-056 July 22, 1998. TR ALD-057 October 23, 1998. TR ALD-059 December 11, 1998. TR ALD-062 May 18, 1999. TR ALD-063 August 10, 1999. TR ALD-064 October 10, 1999. TR ALD-065 November 26, 1999. TR ALD-067 February 7, 2000. TR ALD-068 February 4, 2000. TR ALD-070 May 25, 2000. Revision 13 of the Dornier Airworthiness Limitations Document TM-ALD-010693-ALL, contains the following list of effective pages: Page No. Revision level shown on page Date shown on page List of Effective Pages: Pages 1, 2 13 July 25, 1997. 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 Fairchild Dornier, Dornier Luftfahrt GmbH, P.O. Box 1103, D-82230 Wessling, Germany. 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. Effective Date (f) This amendment becomes effective on February 7, 2001. Issued in Renton, Washington, on April 16, 2001. Donald L. Riggin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 01-9877 Filed 4-24-01; 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