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US-2002-23-11 : Flight Controls - Elevator Balance Weight Attachment Screws - Inspection

Number US-2002-23-11
Issued by United States of America  United States of America
Issue date 2002-11-20
Effective date 2003-01-10
EASA approval number
ATA Chapter 27
Approval Holder
/ Type Designation
  • TEXTRON AVIATION INC.
    • 100 (King Air)
      • A100-1
    • 1900 (Airliner)
      • 1900
      • 1900C
      • 1900D
    • 200 (Super King Air)
      • 200
      • 200C
      • 200CT
      • 200T
      • A200
      • A200C
      • A200CT
      • B200
      • B200C
      • B200CT
      • B200T
    • 300 (Super King Air)
      • 300
      • 300LW
      • B300
      • B300C
    • 90 (King Air)
      • F90
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information (h) Are any service bulletins incorporated into this AD by reference? Actions required by this AD must be done in accordance with Raytheon Mandatory SB 27-3187, Revision 1, dated September 2001. You may get copies from Raytheon Aircraft Company, P.O. Box 85, Wichita, Kansas 67201-0085; telephone: (800) 429-5372 or (316) 676-3140.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu

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