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2024-0126 : Flight Controls – Automatic Elevator Connection – Inspection / Replacement

Number 2024-0126
Issued by Europe  Europe
Issue date 2024-07-02
Effective date 2024-07-16
EASA approval number
Contributor EASA General Aviation Department
ATA Chapter 27
Approval Holder
/ Type Designation
  • DG AVIATION GmbH
    • DG-100
      • DG-100 G
      • DG-100 G ELAN
    • DG-1000
      • DG-1000M
      • DG-1000S
      • DG-1000T
      • DG-1001E
    • DG-200
      • DG-200
      • DG-200/17
      • DG-200/17C
    • DG-300
      • DG-300
      • DG-300 CLUB ELAN
      • DG-300 CLUB ELAN ACRO
      • DG-300 ELAN
      • DG-300 ELAN ACRO
    • DG-400
      • DG-400
    • DG-500
      • DG-500 ELAN ORION
      • DG-500 ELAN TRAINER
      • DG-500 M
      • DG-500 MB
      • DG-500/20 ELAN
      • DG-500/22 ELAN
    • DG-600
      • DG-600
      • DG-600/18
      • DG-600/18M
      • DG-600/M
    • DG-800
      • DG-800 A
      • DG-800 B
      • DG-800 LA
      • DG-800 S
      • DG-808 C
      • DG-808 S
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information DG Aviation TN DG-SS-09, issue 01.f dated 05 March 2024. DG Aviation TN DG-500/17, issue 01.c dated 05 March 2024. DG Aviation TN 800/50, issue 01.c dated 05 March 2024. DG Aviation TN 1000/50, issue 01.c, dated 04 March 2024. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 24-044
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 15 April 2024 as PAD 24-044 for consultation until 13 May 2024. 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.