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  Safety Publications Tool

US-2005-11-04 : AFM Change - Control Column Microphone Jack Assembly Inspection / Modification

Number US-2005-11-04
Issued by United States of America  United States of America
Issue date 2005-05-27
Effective date 2005-05-27
EASA approval number
ATA Chapter 23
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)
  • RAYTHEON AIRCRAFT SERVICES, INC.
    • EASA STC 10015522
    • STC EASA.IM.A.S.01400
    • STC SA4900SW
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Raytheon SB 23-3727, dated May 2005. Bombardier Advisory Wire AW600-00-2247, Revision 2, dated March 24, 2005. For copies of the service information, contact Raytheon Aircraft Company, P.O. Box 3356, Little Rock, Arkansas 72203; or Bombardier, Inc., Canadair, Aerospace Group, P.O. Box 6087, Station Centre-ville, Montreal, Quebec H3C 3G9, Canada.
Remarks Raytheon STC SA4900SW was validated in Europe for installation on Model CL-600-2B16 aeroplanes under STC EASA.IM.A.S.01400, currently EASA STC Nr.10015522. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu.