Airworthiness directives › 2008-04-17
AD 2008-04-17 Airworthiness Directives; Bombardier Model DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315 Airplanes, and Model DHC-8-400 Series Airplanes
Models named: DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, DHC-8-315, DHC-8-400 series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Bombardier Model DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315 airplanes, serial numbers 003 through 639; and Model DHC-8-400 series airplanes, serial numbers 4003, 4004, 4006, and 4008 through 4149; certificated in any category.
Compliance
Within 18 months after the effective date of this AD, unless already done, do the following actions. (1) For Model DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315 airplanes: Install Bombardier Modsum 8Q101603 to replace the affected carbon molded resistive element potentiometers with wire-wound type potentiometers for both the pilot and co-pilot utility lights, in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 8-33-53, Revision A, dated March 14, 2007. (2) For Model DHC-8-400 series airplanes: Install Bombardier Modsum 4-126381 to replace the affected carbon molded resistive element potentiometers with wire-wound type potentiometers for the pilot, co-pilot, and observer utility lights, in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 84-33-10, Revision A, dated March 14, 2007. (3) Actions done before the effective date of this AD in accordance with Bombardier Service Bulletin 8-33-53 or 84-33-10, both dated December 1, 2006, as applicable, are considered acceptable for compliance with the corresponding actions specified in this AD. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No difference. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, New York Aircraft Certification Office (ACO), 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: Wing Chan, Aerospace Engineer, Systems and Flight Test Branch, ANE-172, FAA, New York Aircraft Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New York 11590; telephone (516) 228-7311; fax (516) 794-5531. Before using any approved AMOC on any airplane 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. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI Canadian Airworthiness Directive CF-2007-11, dated August 9, 2007; Bombardier Service Bulletin 8-33-53, Revision A, dated March 14, 2007; and Bombardier Service Bulletin 84-33-10, Revision A, dated March 14, 2007; for related information. Material Incorporated by Reference (i) You must use Bombardier Service Bulletin 8-33-53, Revision A, dated March 14, 2007; or Bombardier Service Bulletin 84-33-10, Revision A, dated March 14, 2007; 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., Bombardier Regional Aircraft Division, 123 Garratt Boulevard, Downsview, Ontario M3K 1Y5, Canada. (3) You may review copies 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/cfr/ibr-locations.html . Issued in Renton, Washington, on February 13, 2008. Stephen P. Boyd, Assistant Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-3397 Filed 2-27-08; 8:45 am] BILLING CODE 4910-13-P
Required actions
Within 18 months after the effective date of this AD, unless already done, do the following actions. (1) For Model DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315 airplanes: Install Bombardier Modsum 8Q101603 to replace the affected carbon molded resistive element potentiometers with wire-wound type potentiometers for both the pilot and co-pilot utility lights, in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 8-33-53, Revision A, dated March 14, 2007. (2) For Model DHC-8-400 series airplanes: Install Bombardier Modsum 4-126381 to replace the affected carbon molded resistive element potentiometers with wire-wound type potentiometers for the pilot, co-pilot, and observer utility lights, in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 84-33-10, Revision A, dated March 14, 2007. (3) Actions done before the effective date of this AD in accordance with Bombardier Service Bulletin 8-33-53 or 84-33-10, both dated December 1, 2006, as applicable, are considered acceptable for compliance with the corresponding actions specified in this AD. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No difference. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, New York Aircraft Certification Office (ACO), 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: Wing Chan, Aerospace Engineer, Systems and Flight Test Branch, ANE-172, FAA, New York Aircraft Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New York 11590; telephone (516) 228-7311; fax (516) 794-5531. Before using any approved AMOC on any airplane 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. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI Canadian Airworthiness Directive CF-2007-11, dated August 9, 2007; Bombardier Service Bulletin 8-33-53, Revision A, dated March 14, 2007; and Bombardier Service Bulletin 84-33-10, Revision A, dated March 14, 2007; for related information. Material Incorporated by Reference (i) You must use Bombardier Service Bulletin 8-33-53, Revision A, dated March 14, 2007; or Bombardier Service Bulletin 84-33-10, Revision A, dated March 14, 2007; 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., Bombardier Regional Aircraft Division, 123 Garratt Boulevard, Downsview, Ontario M3K 1Y5, Canada. (3) You may review copies 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/cfr/ibr-locations.html . Issued in Renton, Washington, on February 13, 2008. Stephen P. Boyd, Assistant Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-3397 Filed 2-27-08; 8:45 am] BILLING CODE 4910-13-P
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