Please feel free to send us your comments by email at
ADs [at] easa.europa [dot] eu
|
Number |
23-096 |
Issued by |
Europe |
Issue date |
2023-08-17 |
EASA approval number |
|
Contributor |
EASA Environment & Propulsion Systems Department |
ATA Chapter |
78 |
Approval Holder / Type Designation |
-
APPLIANCES
-
ATA 72 RECIPROCATING ENGINE
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
FAA Best Practice Guide for Maintaining Exhaust System Turbocharger to Tailpipe Affected parts/Clamps.
FAA SAIB CE-03-46 dated 21 July 2003.
FAA SAIB CE-04-22 dated 17 December 2003.
FAA SAIB CE-05-13 dated 09 November 2004.
FAA SAIB CE-09-11 dated 09 February 2009.
FAA SAIB CE-10-33R1 dated 16 August 2010.
FAA SAIB CE-13-07R1 dated 01 May 2013.
FAA SAIB CE-13-45 dated 05 September 2013.
FAA SAIB CE-18-07 dated 14 December 2017.
FAA SAIB CE-18-21 dated 13 July 2018.
FAA SAIB CE-18-22 dated 13 July 2018. |
Remarks |
1. This Proposed AD will be closed for consultation on 14 September 2023.
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.
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