Airworthiness directives › 2005-10-02
AD 2005-10-02 Airworthiness Directives; Dornier Model 328-300 Series Airplanes
Models named: 328-300 series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Dornier Model 328-300 series airplanes, certificated in any category.
Compliance
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Installation (f) Within 90 days after the effective date of this AD, install an additional mounting angle at rib 9 in the leading edge area of the left- and right-hand wings in accordance with the Accomplishment Instructions of Dornier Service Bulletin SB-328J-30-190, dated July 16, 2003. Alternative Methods of Compliance (AMOCs) (g) The Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. Related Information (h) German airworthiness directive D-2004-049, dated February 1, 2004, also addresses the subject of this AD. Material Incorporated by Reference (i) You must use Dornier Service Bulletin SB-328J-30-190, dated July 16, 2003, to perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approves the incorporation by reference of this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. To get copies of the service information, contact AvCraft Aerospace GmbH, P.O. Box 1103, D-82230 Wessling, Germany. To view the AD docket, go to the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., room PL-401, Nassif Building, Washington, DC. To review copies of the service information, contact the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html. Issued in Renton, Washington, on April 29, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05-9197 Filed 5-10-05; 8:45 am] BILLING CODE 4910-13-P
Unsafe condition
This AD was prompted by chafed de-icing lines in the wing leading edge area. We are issuing this AD to prevent chafing of the de-icing lines, which could result in a reduction in functionality of the anti-ice system, and possibly reduced controllability and performance of the airplane in icing conditions.
Read the original on the Federal Register →
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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