Safety Publications Tool

US-2013-20-18 : Main Rotor Yoke - Life Limit / Reidentification

Number US-2013-20-18
Issued by United States of America  United States of America
Issue date 2013-11-19
Effective date 2013-11-29
EASA approval number
ATA Chapter 62
Approval Holder
/ Type Designation
  • BELL TEXTRON INC. (BTI)
    • 412
      • 412
      • 412CF
      • 412EP
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2009-05-09, dated 16 March 2009.
Publication(s) and related information Bell Helicopter Textron, Inc. ASB No. 412-08-128, Revision A, dated April 14, 2009. For a copy of this service information, 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/files/.
Remarks At the time of adoption of this AD, the model 412CF has not been validated in Europe. 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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