Number |
2020-0260 |
Issued by |
Europe |
Issue date |
2020-11-26 |
Effective date |
2020-12-10 |
EASA approval number |
|
ATA Chapter |
27 |
Approval Holder / Type Designation |
-
SCHEMPP HIRTH FLUGZEUGBAU
-
Janus Sailplanes
-
Mini Nimbus
-
Nimbus-2/-3 Sailplanes
-
Nimbus-2M Powered Sailplanes
-
Standard Cirrus
-
Standard Cirrus
-
Standard Cirrus B
-
Standard Cirrus CS 11-75 L
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Schempp-Hirth TN 278-40, 286-36, 295-33, 328-14, 798-4 (single document) dated 07 August 2020.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
PAD number |
20-176 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 06 November 2020 as PAD 20-176 for consultation until 20 November 2020. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness 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.
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