Safety Publications Tool

CF-2009-11R3 : Failure of the Main Landing Gear Stabilizer Braces

Number CF-2009-11R3
Issued by Canada  Canada
Issue date 2019-02-01
Effective date 2019-02-13
EASA approval number
ATA Chapter 32
Approval Holder
/ Type Designation
  • DE HAVILLAND AIRCRAFT OF CANADA LTD.
    • DHC-8
      • DHC-8-400
      • DHC-8-401
      • DHC-8-402
Revision This AD revises AD CF-2009-11R2, issued 31 May 2018.
Correction Not applicable
Supersedure None
Publication(s) and related information Bombardier Repair Drawing (RD) 8/4-32-099, Issue 1, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada. Bombardier All Operators Message (AOM) No. 338. Bombardier Service Bulletin (SB) 84-32-69, Revision C, dated 20 January 2011, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada. Bombardier SB 84-32-76, Initial Issue, dated 20 May 2010, or later revisions approved by the Chief, Continuing Airworthiness.
Remarks At the moment of adoption of this AD, the model 400 has not been validated in Europe. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu.