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2021-0230 : Stabilizers – Elevators – Inspection

Number 2021-0230
Issued by Europe  Europe
Issue date 2021-10-14
Effective date 2021-10-28
EASA approval number
Contributor EASA General Aviation Department
ATA Chapter 55
Approval Holder
/ Type Designation
  • SCHLEICHER, ALEXANDER
    • AS-K 13
      • AS-K 13
    • ASK 16
      • ASK 16
      • ASK 16 B
    • 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 LBA AD (Lufttuechtigkeitsanweisung) 72-7/3 dated 13 December 1989.
Publication(s) and related information Schleicher ASK 18 TN No. 10 original issue dated 26 May 2021. Schleicher ASK 16 No. 17 original issue dated 26 May 2021. Schleicher AS-K 13 No. 20 original issue dated 26 May 2021. Schleicher K 8 TN No. 31 original issue dated 26 May 20211 Schleicher K 7 TN No. 25 original issue dated 26 May 2021. Schleicher Ka 6 TN No. 27 original issue dated 26 May 2021. Schleicher ASK 18 TN No. 6, AS-K 13 TN No. 12, K 8 TN 23, K 7 TN No. 18 and Ka 6 TN No. 21, issued as a single document, original issue dated 04 October 1989. Appendix 01-2021 to Schleicher ASK 18 AFM dated 01 March 2021. Appendix 01-2021 to Schleicher ASK 16 AFM dated 01 March 2021. Appendix 01-2021 to Schleicher AS-K 13 AFM dated 01 March 2021. Appendix 01-2021 to Schleicher K 8 AFM dated 01 March 2021. Appendix 01-2021 to Schleicher K 7 AFM dated 01 March 2021. Appendix 01-2021 to Schleicher Ka 6 AFM dated 01 March 2021. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 21-100
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 13 July 2021 as PAD 21-100 for consultation until 10 August 2021. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.