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Airworthiness directives › 2007-21-10

AD 2007-21-10 Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

2007-11-21
2007-10-17
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Airframe
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Makes named: socata. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to TBM 700 airplanes, serial numbers 1 through 9, 11 through 17, 19 through 22, 25 through 27, 29 through 31, 33 and 34, 38, 46, and 49, that are: (1) certificated in any category; (2) not equipped with modification No. MOD70-019-25; and (3) equipped with an interior handle unlocking device through push-button.

Compliance

Unless already done, do the following actions: (1) Before each flight after November 21, 2007 (the effective date of this AD) until the actions of paragraph (f)(2) of this AD have been done, check the handle locking using paragraph A of the accomplishment instructions in EADS SOCATA Mandatory TBM Aircraft Service Bulletin SB 70-150, dated May 2007. If any discrepancy is found, do the following before further flight until the modification in paragraph (f)(2) of this AD is done: (i) Fabricate a placard using letters at least 1/8 inches in height with the words “FLIGHT ALLOWED WITH ONLY THE FLIGHT DECK SEATS OCCUPIED.” (ii) Install this placard on the instrument panel within clear view of the pilot. (iii) 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 do both the pre-flight checks and the placard requirements of this AD. Make an entry in the aircraft records showing compliance with this portion of the AD following section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (2) Within the next 12 months after November 21, 2007 (the effective date of this AD) modify the window trim panel using paragraph B of the accomplishment instructions in EADS SOCATA Mandatory TBM Aircraft Service Bulletin SB 70-150, dated May 2007. This modification terminates the requirements of paragraph (f)(1) of this AD. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Staff, 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. Related Information (h) Refer to MCAI European Aviation Safety Agency (EASA) Emergency AD No: 2007-0172-E, dated June 15, 2007; and EADS SOCATA Mandatory TBM Aircraft Service Bulletin SB 70-150, dated May 2007, for related information. Material Incorporated by Reference (i) You must use EADS SOCATA Mandatory TBM Aircraft Service Bulletin SB 70-150, dated May 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. (2) 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 7-54; or in the United States contact SOCATA AIRCRAFT, INC., North Perry Airport, 7501 South Airport Rd., Pembroke Pines, FL 33023; telephone: (954) 893-1400; fax: (954) 964-4141. (3) 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 October 4, 2007. David R. Showers, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-20140 Filed 10-16-07; 8:45 am] BILLING CODE 4910-13-P

Required actions

Unless already done, do the following actions: (1) Before each flight after November 21, 2007 (the effective date of this AD) until the actions of paragraph (f)(2) of this AD have been done, check the handle locking using paragraph A of the accomplishment instructions in EADS SOCATA Mandatory TBM Aircraft Service Bulletin SB 70-150, dated May 2007. If any discrepancy is found, do the following before further flight until the modification in paragraph (f)(2) of this AD is done: (i) Fabricate a placard using letters at least 1/8 inches in height with the words “FLIGHT ALLOWED WITH ONLY THE FLIGHT DECK SEATS OCCUPIED.” (ii) Install this placard on the instrument panel within clear view of the pilot. (iii) 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 do both the pre-flight checks and the placard requirements of this AD. Make an entry in the aircraft records showing compliance with this portion of the AD following section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (2) Within the next 12 months after November 21, 2007 (the effective date of this AD) modify the window trim panel using paragraph B of the accomplishment instructions in EADS SOCATA Mandatory TBM Aircraft Service Bulletin SB 70-150, dated May 2007. This modification terminates the requirements of paragraph (f)(1) of this AD. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Staff, 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. Related Information (h) Refer to MCAI European Aviation Safety Agency (EASA) Emergency AD No: 2007-0172-E, dated June 15, 2007; and EADS SOCATA Mandatory TBM Aircraft Service Bulletin SB 70-150, dated May 2007, for related information. Material Incorporated by Reference (i) You must use EADS SOCATA Mandatory TBM Aircraft Service Bulletin SB 70-150, dated May 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. (2) 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 7-54; or in the United States contact SOCATA AIRCRAFT, INC., North Perry Airport, 7501 South Airport Rd., Pembroke Pines, FL 33023; telephone: (954) 893-1400; fax: (954) 964-4141. (3) 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 October 4, 2007. David R. Showers, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-20140 Filed 10-16-07; 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