Safety Publications Tool
leading to the decision not to take AD action similar to Federal Aviation Administration (FAA) AD 2019-24-01
2015-0139R1 : Flight Controls – Air Brake Bellcrank – Inspection / Replacement
EASA approval number
EASA General Aviation Section
/ Type Designation
SCHEMPP HIRTH FLUGZEUGBAU
Due Discus T
Duo Discus Sailplanes
Duo Discus C
Nimbus-4 Powered Sailplanes
This AD revises EASA AD 2015-0139 dated 10 July 2015.
Publication(s) and related information
Schempp-Hirth Flugzeugbau GmbH TN 380-2, 396-17, 868-22 and 890-14 Revision 1, dated 13 July 2015, and the related working instructions, dated 11 May 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
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.
EASA_AD_2015_0139_R1.pdf (220 kb)
EASA_AD_2015_0139.zip (705 kb)
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