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CF-2019-30R1 : Compressor Turbine Blade Fracture due to Non-conforming CT Vane Installation

Number CF-2019-30R1
Issued by Canada  Canada
Issue date 2019-12-18
Effective date 2019-12-31
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • PRATT & WHITNEY CANADA
    • PT6A-100
      • PT6A-114
      • PT6A-114A
    • PT6A-30
      • PT6A-34
      • PT6A-34AG
      • PT6A-34B
Revision This AD revises AD CF-2019-30, issued 19 August 2019.
Correction Not applicable
Supersedure None
Publication(s) and related information Southwest Turbine Inc. (STI) repair specification number STI 72-50-254.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu