AD 2007-06-11 Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Makes named: socata. Read the applicability below — it usually turns on serial or part numbers too.

This AD applies to SOCATA TBM 700 airplanes, serial numbers 1 through 308, plus the serial number 310, certificated in any category. Note 1: This AD does not apply to airplanes in which both modifications No. MOD70-127-55 and MOD70-129-53 have been factory installed. Reason (d) The mandatory continuing airworthiness information (MCAI) states that: Cracks on a vertical stabilizer attachment fitting due to corrosion have been found on an aircraft in service.

Unless already done, do the following actions. (1) Within the next 600 hours time-in-service (TIS) or the next 12 months, whichever occurs first, after the effective date of this AD, inspect the vertical stabilizer attachment fittings and bolts for cracks or corrosion, and, if necessary, repair or replace the damaged part and then apply a corrosion protection reinforcement, following EADS SOCATA Service Bulletin SB 70-104, Amendment 1, dated August 2004 or EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-104, Amendment 2, dated January 2007. (2) Repeat the actions of paragraph (e)(1) every 1,200 hours TIS or every 24 months, whichever occurs first, following EADS SOCATA Service Bulletin SB 70-104, Amendment 1, dated August 2004 or EADS SOCATA Service Bulletin SB 70-104, Amendment 2, dated January 2007. FAA AD Differences Note 2: This AD differs from the MCAI and/or service information as follows: This AD permits Amendment 2 of the SB to be used. Other FAA AD Provisions (f) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Staff, FAA, ATTN: Albert J. Mercado, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. 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 (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 (DGAC) AD No F-2003-366 R1, dated November 24, 2004; EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-104, Amendment 1, dated August 2004; and EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-104, Amendment 2, dated January 2007 for related information. Material Incorporated by Reference (h) You must use EADS SOCATA TBM Aircraft Mandatory Service Bulletin No. SB 70-104, Amendment 1, dated August 2004, or EADS SOCATA TBM Aircraft Mandatory Service Bulletin No. SB 70-104, Amendment 2, dated January 2007 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. (3) For service information identified in this AD, contact EADS SOCATA, Direction des Services, 65921 Tarbes Cedex 9, France. (4) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, 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/cfr/ibr-locations.html . Issued in Kansas City, Missouri, on March 7, 2007. David R. Showers, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-4724 Filed 3-15-07; 8:45 am] BILLING CODE 4910-13-P

Unless already done, do the following actions. (1) Within the next 600 hours time-in-service (TIS) or the next 12 months, whichever occurs first, after the effective date of this AD, inspect the vertical stabilizer attachment fittings and bolts for cracks or corrosion, and, if necessary, repair or replace the damaged part and then apply a corrosion protection reinforcement, following EADS SOCATA Service Bulletin SB 70-104, Amendment 1, dated August 2004 or EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-104, Amendment 2, dated January 2007. (2) Repeat the actions of paragraph (e)(1) every 1,200 hours TIS or every 24 months, whichever occurs first, following EADS SOCATA Service Bulletin SB 70-104, Amendment 1, dated August 2004 or EADS SOCATA Service Bulletin SB 70-104, Amendment 2, dated January 2007. FAA AD Differences Note 2: This AD differs from the MCAI and/or service information as follows: This AD permits Amendment 2 of the SB to be used. Other FAA AD Provisions (f) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Staff, FAA, ATTN: Albert J. Mercado, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. 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 (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 (DGAC) AD No F-2003-366 R1, dated November 24, 2004; EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-104, Amendment 1, dated August 2004; and EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-104, Amendment 2, dated January 2007 for related information. Material Incorporated by Reference (h) You must use EADS SOCATA TBM Aircraft Mandatory Service Bulletin No. SB 70-104, Amendment 1, dated August 2004, or EADS SOCATA TBM Aircraft Mandatory Service Bulletin No. SB 70-104, Amendment 2, dated January 2007 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. (3) For service information identified in this AD, contact EADS SOCATA, Direction des Services, 65921 Tarbes Cedex 9, France. (4) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, 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/cfr/ibr-locations.html . Issued in Kansas City, Missouri, on March 7, 2007. David R. Showers, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-4724 Filed 3-15-07; 8:45 am] BILLING CODE 4910-13-P