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Preliminary EASA SIB

Lennuamet · 9. oktoober 2017
Viit
3.4-4/17/5199-1
Registreeritud
9. oktoober 2017
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
3.4-4/2017
Vastutaja
Kaupo Toodu (Juhtkond, Lennutegevuse osakond)

Failid

  • 📎E-kiri.pdf211 KB
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  • 📎Slow Rotation on Take-off.pdf359 KB

Sisu (failidest)

EASA SIB No.: 2017-XX Safety Information Bulletin Operations SIB No.: 2017-XX Issued: dd Month 2017 Subject: Slow Rotation on Take-off Ref. Publications: None. Applicability: Operators of 4-engine wide-body aeroplanes, air training organisations (ATOs) providing relevant flight training, and their competent authorities. Description: The intent of this SIB is to raise awareness about a safety issue identified during an on-going investigation of a serious incident involving a 4-engine wide-body aeroplane. In this event, the aeroplane took-off from a high altitude and limitative runway, near its maximum performance weight. The aeroplane needed a very long take-off run and, when passing the opposite runway threshold, was still below the minimum required height. The analysis of preliminary information gathered by the investigating authority, in cooperation with the affected operator and manufacturer, showed that slow aeroplane rotation was a main contributing factor to the event. The preliminary findings of the investigation also highlighted that similar events had occurred at the same airport, involving another 4-engine wide-body aeroplane operator, and that slow rotation rates were applied in a significant number of take-offs. Furthermore, the Agency identified one more event that occurred at another high altitude airport, affecting a different type 4-engine wide-body aeroplane. As a consequence, pending the outcome of the full investigation, the Agency deems it appropriate to promptly address the issue of slow rotation on take-off in the abovementioned operational context. Certification Aspects: Take-off performance for large transport aeroplanes is certified against CS-25 standards, which include various requirements regarding the parameters affecting take-off. During certification, take-off distances are established carrying out the manufacturer’s recommended take-off procedure, which is described in the operational documentation. The application of the manufacturer take-off technique is fundamental to ensure that the required take-off performance is achieved (e.g. a take-off path with adequate clearance from obstacles), in particular in case of one-engine-inoperative take-off. Recommendation(s): The Agency recommends operators of 4-engine wide-body aeroplanes, and ATOs providing relevant flight training, to assess whether their operating procedures may be affected by the identified safety issue. If so, they should apply their hazard identification and risk management processes, as follows: 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-XX  identify whether slow rotation on take-off is a hazard in their operation (e.g. through the analysis of FDM, occurrence reports, training & checking activities);  if a hazard is identified, assess the associated risks; and  if these risks are assessed as not acceptable, establish controls to mitigate the risks to an acceptable level. These controls may include the provision of ad-hoc training on rotation techniques. The unintended introduction of additional risks (e.g. tail strikes) should also be considered when analysing possible mitigating measures. The Agency also recommends the relevant competent authorities to consider this SIB as part of the continuing oversight of applicable operators and ATOs. The Agency will consider the need for additional actions that may be triggered from any further lesson learnt in the course of the investigation or the thorough analysis of the safety issue. At this time, the safety concern described in this SIB does not warrant the issuance of an operational directive under Regulation (EU) 965/2012, Annex II, ARO.GEN.135(c). Contact(s): For further information contact the EASA Safety Information Section, Certification Directorate. 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 2 of 2 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union Dear Madam/Sir, Please find attached hereto a preliminary draft for an EASA Safety Information Bulletin (SIB) [task 2017.168] regarding Slow Rotation on Take-off for consultation until 20 October 2017. We would be grateful to you if you could send any comment(s) to [email protected] by making reference to [task 2017.168], no later than the above-mentioned deadline. 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.
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