2013-22-12: Engine Starting

Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new AD: 2013-22-12 DG Flugzeugbau GmbH: Amendment 39-17644; Docket No. FAA- 2013-0927; Directorate Identifier 2012-CE-036-AD. (a) Effective Date This airworthiness directive (AD) becomes effective November 18, 2013. (b) Affected ADs None. (c) Applicability This AD applies to DG Flugzeugbau GmbH DG-800A, DG-800B, and DG- 500MB gliders, all serial numbers, certificated in any category. (d) Subject Air Transport Association of America (ATA) Code 80: Engine Starting. (e) Reason This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a defective starter motor control, which could activate the starter motor without pressing the starter button. We are issuing this AD to prevent sudden propeller rotation, which could result in injury to the pilot and/or other persons. (f) Actions and Compliance Unless already done, do the actions in paragraphs (f)(1) and (f)(2) of this AD: (1) Within 10 days after November 18, 2013 (the effective date of this AD), inspect to determine if an unmodified starter control unit is installed. If an unmodified starter control unit is installed, remove the unit and replace it with a modified unit. Do the removal and replacement following the Instructions section of DG Flugzeugbau GmbH Technical note No. 800/42, 500/06 (co-published as one document), dated May 29, 2013. (2) As of November 18, 2013 (the effective date of this AD), do not install any starter motor control unit unless it has been modified and labeled with placard ``MS.'' (g) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Jim Rutherford, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4165; fax: (816) 329-4090; email: [email protected]. Before using any approved AMOC on any glider to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (h) Related Information Refer to MCAI European Aviation Safety Agency (EASA) AD No. 2013-0212, dated September 13, 2013, for related information. You may examine the MCAI on the Internet at http://www.regulations.gov by searching for and locating it in Docket No. FAA-2013-0927. For service information related to this AD, contact DG-Flugzeugbau GmbH, 76646 Bruchsal, Germany; telephone: +49 7251 3020 140; fax: +49 7251 3020 269; Internet: http://www.dg-flugzeugbau.de/index.php?id=1329; email: [email protected]. You may review copies of the referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. (i) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) DG Flugzeugbau GmbH Technical note No. 800/42, dated May 29, 2013. (ii) DG Flugzeugbau GmbH Technical note No. 500/06, dated May 29, 2013. Note 1 to paragraph (i)(2): DG Flugzeugbau GmbH Technical note No. 800/42, dated May 29, 2013, and DG Flugzeugbau GmbH Technical note No. 500/06, dated May 29, 2013, are co-published as one document. (3) For DG-Flugzeugbau GmbH service information identified in this AD, contact DG-Flugzeugbau GmbH, 76646 Bruchsal, Germany; telephone: +49 7251 3020 140; fax: +49 7251 3020 269; Internet: http://www.dg-flugzeugbau.de/index.php?id=1329; email: [email protected]. (4) You mayview this service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. (5) You may view this service information that is incorporated by reference 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/cfr/ibr-locations.html.