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Airworthiness directives › 2010-21-02

AD 2010-21-02 Airworthiness Directives; Bombardier, Inc. Model DHC-8 Airplanes

2010-11-12
2010-10-07
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Airframe
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Models named: DHC-8-101, -102, -103, -106, -201, -202, -301, -311, -315, DHC-8-400. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Bombardier, Inc. Model DHC-8-101, -102, -103, -106, -201, -202, -301, -311, and -315 airplanes, serial numbers 003 through 658 inclusive. (2) Bombardier, Inc. Model DHC-8-400, -401, -402 airplanes, serial numbers 4001, 4003, 4004, 4006, and 4008 through 4187 inclusive.

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. Actions (g) Within 6,000 flight hours or 36 months after the effective date of this AD, whichever comes first: Replace the latch assembly of the access panel for the alternate extension system for the landing gear with a modified latch assembly, in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 8-32-166, Revision B, dated March 2, 2010 (for Model DHC-8-100, DHC-8-200, and DHC-8-300 series airplanes); or Bombardier Service Bulletin 84-32-57, Revision A, dated June 15, 2009 (for Model DHC-8-400 series airplanes). Credit for Actions Accomplished in Accordance With Previous Service Information (h) Actions accomplished before the effective date of this AD in accordance with the service information identified in Table 1 of this AD are considered acceptable for compliance with the corresponding actions specified in this AD. Table 1—Previous Service Information Bombardier Service Bulletin— Revision— Dated— 8-32-166 Original April 14, 2008. 8-32-166 A January 29, 2009. 84-32-57 Original April 30, 2008. FAA AD Differences Note 1: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (i) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, New York Aircraft Certification Office, ANE-170, 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: Program Manager, Continuing Operational Safety, FAA, New York ACO, 1600 Stewart Avenue, Suite 410, Westbury, New York, 11590; telephone 516-228-7300; fax 516-794-5531. Before using any approved AMOC on any airplane to which the AMOC applies, notify your principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office. The AMOC approval letter must specifically reference this AD. (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. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et seq. ), the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (j) Refer to MCAI Canadian Airworthiness Directive CF-2009-46, dated December 14, 2009; Bombardier Service Bulletin 8-32-166, Revision B, dated March 2, 2010; and Bombardier Service Bulletin 84-32-57, Revision A, dated June 15, 2009; for related information. Material Incorporated by Reference (k) You must use Bombardier Service Bulletin 84-32-57, Revision A, dated June 15, 2009; or Bombardier Service Bulletin 8-32-166, Revision B, dated March 2, 2010; as applicable; to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Bombardier, Inc., 400 Côte-Vertu Road West, Dorval, Québec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-7401; e-mail thd.qseries@aero.bombardier.com; Internet http://www.bombardier.com. (3) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221. (4) You may also review copies of the 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/code_of_federal_regulations/ibr_locations.html. Issued in Renton, Washington, on September 23, 2010. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2010-25016 Filed 10-6-10; 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