2018-15-07: Flight Controls

Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2018-15-07 Costruzioni Aeronautiche Tecnam srl: Amendment 39-19339; Docket No. FAA-2018-0204; Product Identifier 2018-CE-003-AD. (a) Effective Date This AD becomes effective September 4, 2018. (b) Affected ADs None. (c) Applicability This AD applies to Costruzioni Aeronautiche Tecnam srl Model P2006T airplanes, all serial numbers that do not incorporate design change TECNAM modification (Mod) 2006/322 at production, certificated in any category. (d) Subject Air Transport Association of America (ATA) Code 27: Flight Controls. (e) Reason This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and address an unsafe condition on an aviation product. The MCAI describes the unsafe condition as an incorrect part number for the rudder trim actuator is referenced in the Airworthiness Limitations section of the FAA-approved maintenance program (e.g., maintenance manual), and the life limit for that part may not be properly applied in service. We are issuing this AD to prevent failure of the rudder trim actuator, which could cause the rudder control system to fail. This failure could result in reduced control of the airplane. (f) Actions and Compliance Unless already done, do the following actions in paragraphs (f)(1) through (3) of this AD. The hours time-in-service (TIS) specified in paragraph (f)(1) of this AD are those accumulated on the rudder trim actuator, part number (P/N) B6-7T, since first installed on an airplane. If the total hours TIS are unknown, the hours TIS on the airplane must be used. (1) Initially replace the rudder trim actuator, P/N B6-7T, at the compliance time in paragraph (f)(1)(i) or (ii) of this AD that occurs later: (i) Before accumulating 1,000 hours TIS; or (ii) Within the next 25 hours TIS after September 4, 2018 (the effective date of this AD) or within the next 30 days after September 4, 2018 (the effective date of this AD), whichever occurs first. (2) After the initial replacement required in paragraph (f)(1) of this AD, repetitively thereafter replace the rudder trim actuator, P/N B6-7T, at intervals not to exceed 1,000 hours TIS. (3) Within the next 12 months after September 4, 2018 (the effective date of this AD), revise the Airworthiness Limitations section of the FAA-approved maintenance program (e.g., maintenance manual) by establishing a 1,000-hour life limit for the rudder trim actuator P/N B6-7T. You may refer to Costruzioni Aeronautiche Tecnam srl (TECNAM) Service Bulletin No. SB 285-CS-Ed 1, Revision 1 (dated November 7, 2017) or Revision 2 (dated February 2, 2018) for more information. (g) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Small Airplane Standards Branch, 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: Jim Rutherford, Aerospace Engineer, FAA, Small Airplane Standards Branch, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4165; fax: (816) 329- 4090; email: jim.rutherford@faa.gov. 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) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, Small Airplane Standards Branch, FAA; or the European Aviation Safety Agency (EASA). (h) Related Information Refer to MCAI European Aviation Safety Agency (EASA) AD No. 2018-0029, dated January 31, 2018, and Costruzioni Aeronautiche Tecnam srl Service Bulletin No. SB 285-CS-Ed 1, Revision 1, dated November 7, 2017, and Revision 2, dated February 2, 2018, for related information. You may examine the MCAI on the internet https://www.regulations.gov/document?D=FAA-2018-0204-0002. [[Page 36401]]