Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 19 July 2021 as PAD 21-102 for consultation until 16 August 2021. No
comments were received during the consultation period.
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.
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