Show the full text (3,735 characters)
2006-22-11 EADS SOCATA: Amendment 39-14808; Docket No. FAA-2006- 25332; Directorate Identifier 2006-CE-40-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective December 1, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to the following Model TBM 700 airplanes that are certificated in any U.S. category: Serial numbers 1 through 32, 34, 36 through 69, 71 through 76, 79, 81 through 92, 96 through 98, 101, 102, 107 through 109, 112 through 114, 116, 118 through 124, 126 through 130, 132 through 135, 137, 138, 140 through 145, 148 through 155, 157, 158, 161 through 268, and 270 through 304.
Reason
(d) The mandatory continuing airworthiness information (MCAI) states that the aircraft manufacturer has determined that unsatisfactory initial elevator trim actuator greasing may lead to the icing of the elevator trim and generate an untrimmed nose-up attitude after an autopilot disconnection. If not corrected, this conditioncould result in pitch-up, out-of-trim condition when the autopilot is disconnected.
Actions and Compliance
(e) Unless already done, do the following except as stated in paragraph (f) below.
(1) Within the next 25 hours time-in-service after December 1, 2006 (the effective date of this AD), lubricate the elevator trim tab actuator rods without removal.
(2) Do the action required in paragraph (e)(1) of the AD in accordance with EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB70-124, Amendment 1, ATA No. 27, dated January 2005.
FAA AD Differences
(f) None.
Other FAA AD Provisions
(g) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Staff, FAA, Small Airplane Directorate, ATTN: Gunnar Berg, Aerospace Engineer, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4141; 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) Return to Airworthiness: When complying with this AD, perform FAA-approved corrective actions before returning the product to an airworthy condition.
(3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120- 0056.
Related Information
(h) This AD is related to French AD No. F-2005-034, Issue date: February 16, 2005, which references EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB70-124, Amendment 1, ATA No. 27, dated January 2005.
Material Incorporated by Reference
(i) You must use EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB70-124, Amendment 1, ATA No. 27, dated January 2005, 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 62.41.76.54; or SOCATA Aircraft, INC., North Perry Airport, 7501 Airport Road, Pembroke Pines, Florida 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 .
