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  Safety Publications Tool

2024-0221 : Exhaust – Engine / Turbocharger Exhaust System / Components – Inspection

Number 2024-0221
Issued by Europe  Europe
Issue date 2024-11-22
Effective date 2024-12-06
EASA approval number
Contributor EASA Environment & Propulsion Systems Department
ATA Chapter 78
Approval Holder
/ Type Designation
  • APPLIANCES
    • ATA 72 RECIPROCATING ENGINE
      • Turbochargers
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.
PAD number 23-096
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 17 August 2023 as PAD 23-096 for consultation until 14 September 2023. 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.