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Hoist – Inspection of the Cable Retention Setscrews

Lennuamet · 24. mai 2017
Viit
3-1/17/2478-1
Registreeritud
24. mai 2017
Dokumendi liik
Bulletin
Funktsioon
3 Rahvusvahelise koostöö korraldamine
Sari
3-1 Kirjavahetus lennundusküsimustes
Toimik
3-1/2017
Vastutaja
Karl Rattassep

Failid

  • 📎E-kiri.pdf204 KB
  • 📎EASA_SIB_2017_07.pdf328 KB

Sisu (failidest)

Dear Madam/Sir, Please find attached hereto an 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/2017-07 . 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.: 2017-07 Safety Information Bulletin Airworthiness SIB No.: 2017-07 Issued: 23 May 2017 Subject: Hoist – Inspection of the Cable Retention Setscrews Ref. Publications: Airbus Helicopters Safety Information Notice N° 3102-S-25 dated 21 December 2016. Leonardo Helicopters Information Letter AW139-17-086 dated 10 May 2017. Applicability: All helicopters equipped with Goodrich / UTAS hoist Part Number 42315, 42325, 44301, 44311, 44312, 44314, 44316 or 44318 (any suffix). These hoists are known to be installed on, but not limited to, Airbus Helicopters AS 365 N3, EC175 B, EC 225 LP, AS 332 L2; Airbus Helicopters Deutschland MBB-BK 117 C-2 and D-2, EC135 (all models and variants); and Leonardo S.p.A. AB139 and AW139 helicopters. Description: During a maintenance action in service, a Goodrich / UTAS hoist was found with the hoist cable improperly attached to the storage drum. Last recorded intervention in this area of the hoist was performed by the manufacturer. This condition could result, under certain conditions, in the cable peeling out completely and subsequent loss of the load. 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, Part 21.A.3B. Recommendation(s): EASA recommends operators of affected helicopters to accomplish the inspection in accordance with the instructions of the relevant approval holder as listed in Ref. Publications. Contact(s): For further information contact the EASA Safety Information Section, Certification Directorate. E-mail: [email protected]. For any question concerning the technical content of this SIB, please contact: For Airbus Helicopters and Airbus Helicopters Deutschland: Web portal: https://keycopter.airbushelicopters.com > Technical Requests Management This is information only. Recommendations are not mandatory. TE.CAP.00117-006 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 1 of 2 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union EASA SIB No.: 2017-07 E-mail: [email protected] For Leonardo S.p.A. Helicopters: http://www.leonardocompany.com/customer-support/elicotteri-helicopter/support/directory This is information only. Recommendations are not mandatory. TE.CAP.00117-006 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 2 of 2 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union
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