Airworthiness directives › 2007-02-12
AD 2007-02-12 Airworthiness Directives; Reims Aviation S.A. F406 Airplanes
Applicability*9
This AD applies to the following model and serial number airplanes, certificated in any category. Model Serial Nos. F406 0002, 0003, 0004, 0006, 0008, 0009, 0010, 0012, 0013, 0017, 0024, 0025, 0039, 0042, 0044, 0045, 0066, 0070, 0073, 0074, 0075, 0077, 0080 through 0090, and 0092. Reason (d) The mandatory continuing airworthiness information (MCAI) states: * * * several reports regarding discovery of cracks about the rudder pulley bracket part number 6015511-1. This pulley bracket is installed with the “Camera Hole” option. This condition, if left uncorrected, could result in the loss of rudder control on the airplane.
Compliance
Unless already done, do the following actions. (1) Within the next 10 hours time-in-service (TIS) after February 13, 2007. (the effective of this AD), perform the initial inspection as specified in REIMS AVIATION INDUSTRIES Service Bulletin No. F406-58, Rev. 1, dated October 27, 2006. (2) If no cracking is found following the initial inspection required in paragraph (e)(1) of this AD, repeat the inspection every 50 flight hours or 1 month, whichever occurs first, until the conditions specified in paragraph (e)(3) of this AD are met. (3) Within the next 100 hours TIS or 2 months after February 13, 2007. (the effective of this AD), whichever occurs first, install the modified pulley bracket as specified in REIMS AVIATION INDUSTRIES Service Bulletin No F406-58, Rev. 1, dated October 27, 2006. (4) If any cracking is found during the inspection required in paragraph (e)(1) of this AD, prior to next flight, install the modified pulley bracket as specified in REIMS AVIATION INDUSTRIES Service Bulletin No F406-58, Rev. 1, dated October 27, 2006. (5) The modified pulley bracket specified in REIMS AVIATION INDUSTRIES Service Bulletin No F406-58, Rev. 1, dated October 27, 2006, may be installed at any time after the inspection required in paragraph (e)(1) of this AD, but must be installed prior to further flight if cracking is found. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (f) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Staff, FAA, Small Airplane Directorate, ATTN: Mike Kiesov, Aerospace Engineer, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4144; fax: (816) 329-4090, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. (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 (g) Refer to Direction Ge ne rale de L'Aviation Civile AD No. F-2005-080, Issue date: May 25, 2005, and REIMS AVIATION INDUSTRIES Service Bulletin No. F406-58, Rev. 1, dated October 27, 2006, for related information. Material Incorporated by Reference (h) You must use REIMS AVIATION INDUSTRIES Service Bulletin No. F406-58, Rev. 1, dated October 27, 2006, 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 REIMS AVIATION INDUSTRIES, Ae rodrome de Reims Prunay, 51360 Prunay, France, A l'attention du Support Client; telephone 03.26.48.46.53; fax: 03.26.49.18.57. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; 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/code_of_federal_regulations/ibr_locations.html. Issued in Kansas City, Missouri on January 12, 2007. Kim Smith, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-774 Filed 1-23-07; 8:45 am] BILLING CODE 4910-13-P
Required actions
Unless already done, do the following actions. (1) Within the next 10 hours time-in-service (TIS) after February 13, 2007. (the effective of this AD), perform the initial inspection as specified in REIMS AVIATION INDUSTRIES Service Bulletin No. F406-58, Rev. 1, dated October 27, 2006. (2) If no cracking is found following the initial inspection required in paragraph (e)(1) of this AD, repeat the inspection every 50 flight hours or 1 month, whichever occurs first, until the conditions specified in paragraph (e)(3) of this AD are met. (3) Within the next 100 hours TIS or 2 months after February 13, 2007. (the effective of this AD), whichever occurs first, install the modified pulley bracket as specified in REIMS AVIATION INDUSTRIES Service Bulletin No F406-58, Rev. 1, dated October 27, 2006. (4) If any cracking is found during the inspection required in paragraph (e)(1) of this AD, prior to next flight, install the modified pulley bracket as specified in REIMS AVIATION INDUSTRIES Service Bulletin No F406-58, Rev. 1, dated October 27, 2006. (5) The modified pulley bracket specified in REIMS AVIATION INDUSTRIES Service Bulletin No F406-58, Rev. 1, dated October 27, 2006, may be installed at any time after the inspection required in paragraph (e)(1) of this AD, but must be installed prior to further flight if cracking is found. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (f) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Staff, FAA, Small Airplane Directorate, ATTN: Mike Kiesov, Aerospace Engineer, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4144; fax: (816) 329-4090, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. (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 (g) Refer to Direction Ge ne rale de L'Aviation Civile AD No. F-2005-080, Issue date: May 25, 2005, and REIMS AVIATION INDUSTRIES Service Bulletin No. F406-58, Rev. 1, dated October 27, 2006, for related information. Material Incorporated by Reference (h) You must use REIMS AVIATION INDUSTRIES Service Bulletin No. F406-58, Rev. 1, dated October 27, 2006, 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 REIMS AVIATION INDUSTRIES, Ae rodrome de Reims Prunay, 51360 Prunay, France, A l'attention du Support Client; telephone 03.26.48.46.53; fax: 03.26.49.18.57. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; 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/code_of_federal_regulations/ibr_locations.html. Issued in Kansas City, Missouri on January 12, 2007. Kim Smith, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-774 Filed 1-23-07; 8:45 am] BILLING CODE 4910-13-P
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