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EASA SIB 2017-21

Lennuamet · 15. märts 2018
Viit
3.4-4/18/1323-1
Registreeritud
15. märts 2018
Dokumendi liik
Kiri sissetulev
Adressaat
EASA
Saabumis/saatmisviis
e-post
Funktsioon
3.4 Euroopa lennuohutusametiga (EASA) koostöö korraldamine
Sari
3.4-4 Kirjavahetus lennundusküsimustes
Toimik
3.4-4/2018
Vastutaja
Kalle Allikson (Juhtkond, Lennundustehnika osakond)

Failid

  • 📎E-kiri.pdf203 KB
  • 📎EASA_SIB_2017_21_Withdrawn.pdf1189 KB
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Sisu (failidest)

Dear Madam/Sir, Please find attached hereto a withdrawn EASA Safety Information Bulletin (SIB) which has already been posted on our web site and can be viewed at https://ad.easa.europa.eu/ad/2017-21 . EASA ADs and other Safety Publications are available online at http://ad.easa.europa.eu Safety Information Section Email: [email protected] EASA Website (Attachment is in Acrobat PDF format) Postal: : Postfach 10 12 53, 50452 Cologne, Germany An agency of the European Union This message is intended for the use of the addressee only and may contain information that is privileged and confidential. If you are not the intended recipient, you are notified that any dissemination of this communication is strictly prohibited. If you have received this communication in error, please notify us immediately by returning this e-mail. Sender accepts no liability for damage of any kind resulting from the risks inherent in the electronic transmission of messages. This communication does not constitute any formal commitment on behalf of the European Aviation Safety Agency. EASA SIB No.: 2017-21 Safety Information Bulletin Airworthiness SIB No.: 2017-21 Issued: 15 December 2017 Subject: Check of the Engine and Propeller Control System Ref. Publications: Aircraft Industries a.s. (AI) Service Bulletin (SB) L410UVP-E/492b Revision 1 dated 04 December 2017. Applicability: n L 410UVP-E20 aeroplanes, manufacturer serial numbers from 2904 and up, if equipped with GE Aviation H80-200 engine and Avia Propeller AV-725 propeller. Description: aw Preliminary investigation of an accident on 15 November 2017 with an L 410 aeroplane near Khabarovsk, Russia, identified an un-commanded activation of the beta mode signalization of a propeller during the final approach. For the time being, as a preliminary preventive measure, AI issued Revision 1 of SB L410UVP-E/492b, providing instructions to check the components of dr engine and propeller control system, including the beta switch. At this time, the safety concern described in this SIB is not considered to be an unsafe condition that would warrant Airworthiness Directive (AD) action under Regulation (EU) 748/2012, ith Part 21.A.3B. As soon as the investigation identifies the root cause and/or contributing factors of the accident, EASA may take further action. Recommendation(s): W EASA recommends owners and operators to accomplish the actions as specified in Revision 1 of AI SB L410UVP-E/492b. Contact(s): For further information contact the EASA Safety Information Section, Certification Directorate. E-mail: [email protected]. For a copy of the referenced SB, or further information regarding the technical content of this SIB, please contact Aircraft Industries a.s. via e-mail: [email protected]. This is information only. Recommendations are not mandatory. TE.CAP.00117-006 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 1 of 1 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union
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