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2020-0228 : [Correction] Engine – Turbocharger Hose – Replacement

Number 2020-0228
Issued by Europe  Europe
Issue date 2020-12-03
Effective date 2020-10-27
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • CONTINENTAL AEROSPACE TECHNOLOGIES, GmbH
    • EASA STC 10014287
    • EASA STC 10014364
    • TAE125
      • TAE 125-02-114
      • TAE 125-02-99
  • PIPER AIRCRAFT INC.
    • PA-28 (Archer)
      • PA-28-180
      • PA-28-181 (Archer III)
    • PA-28 (Cadet)
      • PA-28-161
    • PA-28 (Cherokee)
      • PA-28-140 (Cruiser)
      • PA-28-150
      • PA-28-160
      • PA-28-180
    • PA-28 (Warrior)
      • PA-28-151 (Warrior)
      • PA-28-161 (Warrior II)
      • PA-28-161 (Warrior III)
  • TEXTRON AVIATION INC.
    • 172 (Skyhawk)
      • 172F
      • 172G
      • 172H
      • 172I
      • 172K
      • 172L
      • 172M
      • 172N
      • 172P
      • 172R
      • 172S
    • F172
      • F172F
      • F172G
      • F172H
      • F172K
      • F172L
      • F172M
      • F172N
      • F172P
Revision Not applicable
Correction This AD is republished to correct and clarify the list of aeroplane models which may have a TAE 125-02-99 or TAE 125-02-114 engine installed through EASA STC 10014287 or EASA STC 10014364, as applicable. This AD also adds SB CG 601-1014 P1 Revision 02 (correcting the "Type affected") to the reference publications.
Supersedure None
Publication(s) and related information Continental Aerospace Technologies SB CG 601-1014 P1 original issue dated 05 October 2020, or Revision 01 dated 15 October 2020, or Revision 02 dated 24 November 2020. Continental Aerospace Technologies SB CG 651-1009 P1 original issue dated 05 October 2020 or Revision 01 dated 15 October 2020. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness 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.