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CF-2016-17R2 : Wings - Life Limit Introduction for Side Brace Fitting Shaft Installed on Main Landing Gear (MLG)

Number CF-2016-17R2
Issued by Canada  Canada
Issue date 2016-07-04
Effective date 2016-07-05
EASA approval number
ATA Chapter 57, 40
Approval Holder
/ Type Designation
  • BOMBARDIER
    • CL-600 (Challenger)
      • CL-600-1A11
      • CL-600-2A12 (601 Variant)
      • CL-600-2B16 (601-3A Variant)
      • CL-600-2B16 (601-3R Variant)
      • CL-600-2B16 (604 Variant)
Revision The revision 2 of this AD is issued to correct/update the TLMC data in Table A of the Corrective Actions section.
Correction Not applicable
Supersedure None
Publication(s) and related information Bombardier Service Bulletins (SB) listed below, or later revision approved by the Chief, Continuing Airworthiness, Transport Canada: For CL-600-1A11 aeroplanes (serial numbers 1004 through 1085), SB 600-0768, Basic Issue, dated 9 September 2014. For CL-600-2A12 (serial numbers 3001 through 3066) and CL-600-2B16 aeroplanes (serial numbers 5001 through 5194), SB 601-0636, Revision 01, dated 10 May 2016. For CL-600-2B16 aeroplanes (serial numbers 5301 through 5665), SB 604-57-005, Basic Issue, dated 9 September 2014. For CL-600-2B16 aeroplanes (serial numbers 5701 through 5851), SB 605-57-003, Basic Issue, dated 9 September 2014.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu