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2015-02-09: Engine Exhaust

FAA order 2015-02-09 is an airworthiness directive in force since March 5, 2015. The FAA's subject line: Engine Exhaust. It names Costruzioni Aeronautiche Tecna P2006: about 104 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Costruzioni Aeronautiche Tecnam srl
Models
P2006T
On this site
Costruzioni Aeronautiche Tecna P2006 104 registered

Dates and paperwork

In force since
March 5, 2015
Published
January 29, 2015 (signed January 14, 2015)
Docket
FAA-2014-0876
Status
Current
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 Costruzioni Aeronautiche Tecnam srl Model P2006T airplanes. 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 cracking found in the engine exhaust pipe. We are issuing this AD to require actions to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (6,575 characters)
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 AD: 2015-02-09 Costruzioni Aeronautiche Tecnam srl: Amendment 39-18076; Docket No. FAA-2014-0876; Directorate Identifier 2014-CE-032-AD. (a) Effective Date This airworthiness directive (AD) becomes effective March 5, 2015. (b) Affected ADs None. (c) Applicability This AD applies to Costruzioni Aeronautiche Tecnam srl P2006T airplanes, all serial numbers, certificated in any category. (d) Subject Air Transport Association of America (ATA) Code 78: Engine Exhaust. (e) Reason This AD was prompted by mandatory continuing airworthinessinformation (MCAI) originated 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 cracking found in the engine exhaust pipe. We are issuing this AD to detect and correct cracked engine exhaust pipes, which could lead to engine damage, possibly resulting in damage to the airplane and injury to the occupants. (f) Actions and Compliance Unless already done, do the following actions as specified in paragraphs (f)(1) through (f)(3) of this AD: (1) Within 25 hours time-in-service (TIS) after March 5, 2015 (the effective date of this AD) or within the next 30 days after March 5, 2015 (the effective date of this AD), whichever occurs first, do a detailed inspection of all engine exhaust pipes following the inspection instructions in Costruzioni Aeronautiche TECNAM Service Bulletin No. SB 170-CS-Ed 1, Rev 1, dated September 25, 2014. (2) If any deformation, cracks, or any other defects are detected during the inspection as required by paragraph (f)(1) of this AD, before further flight, replace the affected pipe with an airworthy part or contact Costruzioni Aeronautiche TECNAM for FAA- approved repair instructions approved specifically for compliance with this AD and incorporate those instructions. Use the information in paragraph (i)(3) of this AD to contact Costruzioni Aeronautiche TECNAM. (3) Within 30 days after the inspection required by paragraph (f)(1) of this AD or within 30 days after March 5, 2015 (the effective date of this AD), whichever occurs later, report the results (including no findings) by using the occurrence report in Costruzioni Aeronautiche TECNAM Service Bulletin No. SB 170-CS-Ed 1, Rev 1, dated September 25, 2014. (g) Other FAA AD Provisions 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; email: albert.mercado@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) 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, a federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to be approximately 5 minutes per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance Officer, AES-200. (h) Related Information Refer to European Aviation Safety Agency (EASA) AD No.: 2014- 0220, dated September 30, 2014, for related information. The MCAI can be found in the AD docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2014-0876-0002. (i) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this [[Page 4769]] paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Costruzioni Aeronautiche TECNAM Service Bulletin No. SB 170- CS-Ed 1, Rev 1, dated September 25, 2014. (ii) Reserved. (3) For Costruzioni Aeronautiche TECNAM service information identified in this AD, contact Costruzioni Aeronautiche Tecnam Airworthiness Office, Via Maiorise-81043 Capua (CE) Italy; telephone: +39 0823 997538; fax: +39 0823 622899; email: technical.support@tecnam.com; Internet: http://www.tecnam.com/Customer-Care/Service-Bulletins.aspx. (4) You may review this referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. In addition, you can access this service information on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014-0876. (5) You may view this service information that is incorporated by reference 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

2017-11-15CE-18-03 · TIME LIMITS/MAINTENANCE CHECKS - Costruzioni Aeronautiche Tecnam P2006T Wrong Rudder Trim Actuator Part Number

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 5, 2026. Connections as data: /graph/directive/2015-02-09.json · aircraft systems.