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2013-0091 : Flight Controls – Automatic Elevator Control Connection in the Fuselage – Inspection / Replacement / Revision

Number 2013-0091
Issued by Europe  Europe
Issue date 2013-04-12
Effective date 2013-04-26
EASA approval number
Contributor EASA General Aviation Section
ATA Chapter 27
Approval Holder
/ Type Designation
  • SCHLEICHER, ALEXANDER
    • AS-K 13
      • AS-K 13
    • ASK 18
      • ASK 18
      • ASK 18 B
    • K 7
      • K 7
    • K 8
      • K 8
      • K 8 B
      • K 8 C
    • Ka 6
      • K 6
      • Ka 6 B
      • Ka 6 BR
      • Ka 6 C
      • Ka 6 CR
      • Ka 6/0
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2012-0246 dated 16 November 2012.
Publication(s) and related information Alexander Schleicher GmbH & Co. Technical Note (Ka 6 TN-Nr. 26; K 7 TN-Nr. 24, K 8 TN-Nr. 30, ASK 13 TN-Nr. 19; ASK 18 TN-Nr. 9), dated 08 January 2013, Alexander Schleicher GmbH & Co TN-Nr. 7 for K 7 sailplanes, dated 23 November 1961, Alexander Schleicher GmbH & Co TN-Nr. 8 for K 7 sailplanes, dated 23 November 1961, Alexander Schleicher GmbH & Co TN-Nr. 6 for K 8 sailplanes, dated 24 November 1961, Alexander Schleicher GmbH & Co TN-Nr. 7 for K 8 sailplanes, dated 24 November 1961. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.

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