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US-2024-16-01 : Fuselage - Tail Boom Attachment Cap Angle - Inspection

Number US-2024-16-01
Issued by United States of America  United States of America
Issue date 2024-08-22
Effective date 2024-09-04
EASA approval number
Contributor Federal Aviation Administration (FAA)
ATA Chapter 53
Approval Holder
/ Type Designation
  • BELL TEXTRON INC. (BTI)
    • 205
      • 205A
      • 205A-1
      • 205B
    • 212
    • 412
      • 412
      • 412CF
      • 412EP
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2000-18-09 dated 13 September 2000.
Publication(s) and related information Bell Alert Service Bulletin (ASB) 205-24-122, dated April 22, 2024. Bell ASB 205B-24-77, dated April 22, 2024. Bell ASB 212-24-169, dated April 22, 2024. Bell ASB 412-24-197, dated April 22, 2024. Bell ASB 412CF-24-77, dated April 22, 2024. For Bell material identified in this AD, contact Bell Textron, Inc., P.O. Box 482, Fort Worth, TX76101; phone: (450) 437-2862 or (800) 363-8023; fax: (450) 433-0272; email: productsupport[at]bellflight[dot]com; website: bellflight[dot]com/support/contact-support.
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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