You are not logged in
  Safety Publications Tool

CF-2024-47 : Fuselage, Stabilizers, Wings - Lower Wing Plank at the Rear Spar WS 59 to WS 65 Web and/or Flange / VSTAB Front Spar to Frame Attachment Fittings Lower Legs FS 755.00 / Pressure Bulkhead Web between LBL 9 and RBL 9 at FS 409 - Inspections

Number CF-2024-47
Issued by Canada  Canada
Issue date 2025-01-06
Effective date 2025-01-06
EASA approval number
ATA Chapter 53, 55, 57
Approval Holder
/ Type Designation
  • BOMBARDIER
    • CL-600 (Challenger)
      • CL-600-2B16 (601-3A Variant)
      • CL-600-2B16 (601-3R Variant)
      • CL-600-2B16 (604 Variant)
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Ultrasound Inspection (UT) 57-20-001 procedure dated 25 March 2019, published in Part 04 of publication number CH 604 Non-Destructive Testing Manual (NDTM) Procedures. Eddy Current Inspection (ET) 57-20-020 procedure dated 02 June 2021, published in Part 06 of publication number CH 604 NDTM. UT 55-30-002 procedure dated 01 March 2018, published in Part 04 of publication number CH 604 NDTM. ET 55-30-003 procedure dated 01 March 2018, 2018, published in Part 06 of publication number CH 604 NDTM. UT 53-20-001 procedure dated 19 November 2018, published in Part 04 of publication number CH 604 NDTM. ET 53-20-011 procedure dated 19 November 2018, published in Part 06 of publication number CH 604 NDTM.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu