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PAD 24-138 : Flight Controls – Horizontal Tailplane Drive Lower Bearing – Modification

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Number 24-138
Issued by Europe  Europe
Issue date 2024-11-13
EASA approval number
Contributor EASA General Aviation Department
ATA Chapter 27
Approval Holder
/ Type Designation
  • SCHEMPP HIRTH FLUGZEUGBAU
    • Standard Cirrus
      • Standard Cirrus
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information SCHEMPP-HIRTH TN 278-25 revision 1 dated 09 July 2024. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
Remarks 1. This Proposed AD will be closed for consultation on 11 December 2024. 2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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.

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