Safety Publications Tool
2021-0098 : Flight Controls / Stabilizers – Aileron, Elevator and Rudder Hinge Bolt Installations – Inspection / Modification
EASA approval number
EASA General Aviation Department
/ Type Designation
PILATUS AIRCRAFT LTD
This AD supersedes EASA AD 2011-0230 dated 09 December 2011.
Publication(s) and related information
Pilatus Aircraft PC-6 SB 55-005 original issue dated 25 February 2021. The use of later approved revisions of the above-mentioned 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. This AD was posted on 18 March 2021 as PAD 21-044 for consultation until 01 April 2021. 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.
EASA_AD_2021_0098.pdf (203 kb)
EASA_PAD_21_044.zip (586 kb)
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