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Airworthiness directives › 2008-03-15

AD 2008-03-15 Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

2008-03-11
2008-02-05
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Airframe
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Makes named: socata. Models named: TBM 700. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Model TBM 700 airplanes, serial numbers 126 through 322, that are: (1) Equipped with a pilot door; and (2) Certificated in any category.

Compliance

Do the following actions, unless already done: (1) Any incorrect length pilot door locking stop-fittings replaced following the inspection required in paragraph (f) of this AD in accordance with AD 2007-04-08, using the original issue of EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, dated July 2005, must be replaced again within the next 12 months after March 11, 2008 (the effective date of this AD). Do the replacement using EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, Amendment 1, dated June 2007. (2) Any incorrect length pilot door locking stop-fittings found during the inspection required in paragraph (f) of this AD and not previously replaced in accordance with AD 2007-04-08, must be replaced before further flight after March 11, 2008 (the effective date this AD). Do the replacement using EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, Amendment 1, dated June 2007. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (h) 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: Albert Mercado, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090. 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. Special Flight Permit (i) If you have ordered parts and they are not available, then you may fly unpressurized until parts become available or for a period not to exceed 90 days after the inspection required in paragraph (f) of this AD, whichever occurs first. You must also fabricate and install a placard as described below. Completing the action of paragraph (g)(2) of this AD terminates the placard requirement. (1) Fabricate (using letters at least 1/8 inch in height) a warning placard that states “This airplane is prohibited from pressurized flight.” (2) Install the placard in full view of the pilot. The owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7) may install the placard as required in paragraph (h) of this AD. Related Information (j) Refer to MCAI Direction générale de l'aviation civile (DGAC) AD No. F-2007-016, October 10, 2007; and EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, Amendment 1, dated June 2007, for related information. Material Incorporated by Reference (k) You must use EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, dated July 2005, or EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, Amendment 1, dated June 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 EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, Amendment 1, dated June 2007, under 5 U.S.C. 552(a) and 1 CFR part 51. (2) On March 23, 2007 (72 FR 7559, February 16, 2007), the Director of the Federal Register previously approved the incorporation by reference of EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, dated July 2005. (3) For service information identified in this AD, contact EADS SOCATA, Direction des Services, 65921 Tarbes Cedex 9, France; telephone: 33 (0)5 62 41 73 00; fax: 33 (0)5 62 41 76 54; or SOCATA Aircraft, Inc., North Perry Airport, 7501 South Airport Rd., Pembroke Pines, FL 33023; telephone: (954) 893-1400; fax: (954) 964-4141. (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 January 29, 2008. John Colomy, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-2026 Filed 2-4-08; 8:45 am] BILLING CODE 4910-13-P

Required actions

Do the following actions, unless already done: (1) Any incorrect length pilot door locking stop-fittings replaced following the inspection required in paragraph (f) of this AD in accordance with AD 2007-04-08, using the original issue of EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, dated July 2005, must be replaced again within the next 12 months after March 11, 2008 (the effective date of this AD). Do the replacement using EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, Amendment 1, dated June 2007. (2) Any incorrect length pilot door locking stop-fittings found during the inspection required in paragraph (f) of this AD and not previously replaced in accordance with AD 2007-04-08, must be replaced before further flight after March 11, 2008 (the effective date this AD). Do the replacement using EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, Amendment 1, dated June 2007. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (h) 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: Albert Mercado, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090. 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. Special Flight Permit (i) If you have ordered parts and they are not available, then you may fly unpressurized until parts become available or for a period not to exceed 90 days after the inspection required in paragraph (f) of this AD, whichever occurs first. You must also fabricate and install a placard as described below. Completing the action of paragraph (g)(2) of this AD terminates the placard requirement. (1) Fabricate (using letters at least 1/8 inch in height) a warning placard that states “This airplane is prohibited from pressurized flight.” (2) Install the placard in full view of the pilot. The owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7) may install the placard as required in paragraph (h) of this AD. Related Information (j) Refer to MCAI Direction générale de l'aviation civile (DGAC) AD No. F-2007-016, October 10, 2007; and EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, Amendment 1, dated June 2007, for related information. Material Incorporated by Reference (k) You must use EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, dated July 2005, or EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, Amendment 1, dated June 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 EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, Amendment 1, dated June 2007, under 5 U.S.C. 552(a) and 1 CFR part 51. (2) On March 23, 2007 (72 FR 7559, February 16, 2007), the Director of the Federal Register previously approved the incorporation by reference of EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-131, dated July 2005. (3) For service information identified in this AD, contact EADS SOCATA, Direction des Services, 65921 Tarbes Cedex 9, France; telephone: 33 (0)5 62 41 73 00; fax: 33 (0)5 62 41 76 54; or SOCATA Aircraft, Inc., North Perry Airport, 7501 South Airport Rd., Pembroke Pines, FL 33023; telephone: (954) 893-1400; fax: (954) 964-4141. (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 January 29, 2008. John Colomy, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-2026 Filed 2-4-08; 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