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US-2002-22-14 : Main Rotor - Tension-Torsion Straps - Retirement (Life) Limit

Number US-2002-22-14
Issued by United States of America  United States of America
Issue date 2002-11-08
Effective date 2002-12-13
EASA approval number
ATA Chapter 62
Approval Holder
/ Type Designation
  • BELL TEXTRON INC. (BTI)
    • 204B
    • 205
      • 205A
      • 205A-1
      • 205B
    • 212
  • McDermott 214 Holdings, LLC
    • 214
      • 214B
      • 214B-1
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 80-17-09, dated August 14, 1980.
Publication(s) and related information For a copy of service information related to this AD, if any, contact Bell Helicopter Textron, Inc., P.O. Box 482, Fort Worth, TX 76101; telephone (817) 280-3391; fax (817) 280-6466; or at http://www.bellcustomer.com/
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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