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FAA orders · airworthiness directive · historical

2007-06-11: Vertical stabilizer attachment fitting

FAA order 2007-06-11 is an airworthiness directive in force since April 20, 2007. The FAA's subject line: Vertical stabilizer attachment fitting. It names Daher (Socata) TBM-700 TBM 700 through TBM 960: about 1,006 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: airframe structure.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
SOCATA
Models
TBM 700
On this site
Daher (Socata) TBM-700 TBM 700 through TBM 960 1,006 registered

Dates and paperwork

In force since
April 20, 2007
Published
March 16, 2007 (signed March 7, 2007)
Docket
FAA-2006-26166
Replaced by
2025-26-02
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: Cracks on a vertical stabilizer attachment fitting due to corrosion, have been found on an aircraft in service. We are issuing this AD to require actions to correct the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (4,416 characters)
2007-06-11 EADS SOCATA Model TBM 700 Airplanes: Amendment 39-14992; Docket No. FAA-2006-26166; Directorate Identifier 2006-CE-58-AD. Effective Date (a) This airworthiness directive (AD) becomes effective April 20, 2007. Affected ADs (b) None. Applicability (c) 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. Actions and Compliance (e) 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 generale 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 .

Related safety bulletins advice on the same designs, not orders

2016-01-25CE-16-12 · AUTO FLIGHT - Autopilot
2006-10-27CE-07-07 · Anchor Nuts
2006-08-11CE-06-60 ·
2006-08-11CE-06-61 ·
2005-06-27CE-05-62 ·

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 7, 2026. Connections as data: /graph/directive/2007-06-11.json · aircraft systems.