Airworthiness directives › 2013-04-09
AD 2013-04-09 Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes
Makes named: tecnam. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Costruzioni Aeronautiche Tecnam srl P2006T airplanes, serial numbers 001/US through 9999/US, certificated in any category.
Compliance
Unless already done, do the following actions following the Inspection Instructions, paragraph 2, numbers 1 through 8, in Costruzioni Aeronautiche TECNAM Service Bulletin No. SB 102-CS-Rev2, dated July 3, 2012: (1) At the compliance times below, inspect all aileron hinge supports part numbers (P/N) 26-1-1082-1/3, P/N 26-1-1081-1/3, P/N 26-1-1081-2/4, and P/N 26-1-1082-2/4 for cracks: (i) For airplanes with 600 or more hours time-in-service (TIS) as of April 9, 2013 (the effective date of this AD): Within 30 days after April 9, 2013 (the effective date of this AD) or within the next 25 hours TIS after April 9, 2013 (the effective date of this AD), whichever occurs first, and repetitively thereafter at intervals not to exceed 100 hours TIS or 12 months, whichever occurs first, (ii) For airplanes with less than 600 hours TIS as of April 9, 2013 (the effective date of this AD): Within 30 days after accumulating 600 hours TIS or within 25 hours TIS after accumulating 600 hours TIS, whichever occurs first, and thereafter at intervals not to exceed 100 hours TIS or 12 months, whichever occurs first. (2) If a crack is found during any inspection required by paragraph (f)(1) of this AD, before further flight, contact: Costruzioni Aeronautiche TECNAM at Costruzioni Aeronautiche TECNAM Airworthiness Office, Via Maiorise—81043 Capua (CE) Italy; telephone: +39 0823 620134; fax: +39 0823 622899; email: m.oliva@tecnam.com or g.paduano@tecnam.com; Internet: www.tecnam.com/it-IT/documenti/service-bulletins.aspx; for replacement instructions and accomplish them accordingly.
Required actions
This AD provides credit for the actions required in this AD if already done before April 9, 2013 (the effective date of this AD) following Costruzioni Aeronautiche TECNAM Service Bulletin No. SB 102-CS-Rev1, dated June 29, 2012.
Unsafe condition
This AD was prompted by multiple cracks found on the outboard aileron hinge support of a P2006T airplane during an inspection. We are issuing this AD to require actions to address the unsafe condition on these products.
Affected ADs
None.
Read the original on the Federal Register →
You just looked this one up by hand
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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