Safety Publications Tool
22-154R1 : Navigation – Weather Radar System Redundant Wiring – Modification
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EASA approval number
EASA General Aviation Department
/ Type Designation
PILATUS AIRCRAFT LTD
This PAD is revised to include additional modification instructions according to Pilatus PC-24 Service Bulletin (SB) 34-010 Revision 1.
Publication(s) and related information
Pilatus PC-24 SB 34-010 original issue dated 22 September 2022, or Revision 1 dated 29 November 2022. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
1. This Proposed AD will be closed for consultation on 13 December 2022. 2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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_PAD_22_154_R1.pdf (194 kb)
EASA_PAD_22_154.zip (364 kb)
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