Airworthiness directives › 2013-11-01
AD 2013-11-01 Airworthiness Directives; Iniziative Industriali Italiane S.p.A. Airplanes
Models named: Sky Arrow 650 TC, Sky Arrow 650 TCN, Sky Arrow 650TCS, Sky Arrow 650TCNS. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Iniziative Industriali Italiane S.p.A. Models Sky Arrow 650 TC, Sky Arrow 650 TCN, Sky Arrow 650TCS, and Sky Arrow 650TCNS airplanes, all serial numbers, certificated in any category.
Compliance
Unless already done, do the following actions. (1) Before further flight after June 19, 2013 (the effective date of this AD), and thereafter at intervals not to exceed 25 hours time-in-service (TIS), perform detailed visual inspections of the horizontal tail/elevator plane hinge assembly part number (P/N) R26208/00 following paragraph 4. INSTRUCTIONS of Magnaghi Aeronautica SpA Service Bulletin SB-C n. SB-005-2013-SKY ARROW, Issue 1, dated March 13, 2013. (2) If during any inspection required by paragraph (f)(1) of this AD, the spherical bearing is found partially or completely out of its seat and/or signs of cracks or corrosion of the hinges, hinge levers or hinge brackets are detected, before further flight send a detailed report to Magnaghi Aeronautica S.p.A. following paragraph 4. INSTRUCTIONS of Magnaghi Aeronautica SpA Service Bulletin SB-C n. SB-005-2013-SKY ARROW, Issue 1, dated March 13, 2013, to the address specified in paragraph (i)(3) of this AD, requesting an FAA-approved repair scheme and incorporating the repair. (3) As of June 19, 2013 (the effective date of this AD) do not install any spherical bearing P/N SKF GE-10 or horizontal tail/elevator plane hinge assembly P/N R26208/00 on any airplane, unless it has passed the inspection following paragraph 4. INSTRUCTIONS of Magnaghi Aeronautica SpA Service Bulletin SB-C n. SB-005-2013-SKY ARROW, Issue 1, dated March 13, 2013.
Required actions
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: Mike Kiesov, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4144; fax: (816) 329-4090; email: mike.kiesov@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.
Unsafe condition
This AD was prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as improper installation of the spherical bearing on the central hinge lever and a crack on the weld length of the horizontal tail/elevator plane hinge assembly. We are issuing this AD to correct this condition, which, if not corrected, could lead to the loss of the main elevator control and could result in loss of control.
Affected ADs
None.
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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