Safety Publications Tool

US-2020-19-08 : Main Rotor - Main Rotor Hub Tension-torsion Strap Assembly - Life Limit / Removal

Number US-2020-19-08
Issued by United States of America  United States of America
Issue date 2020-10-14
Effective date 2020-10-21
EASA approval number
ATA Chapter 62
Approval Holder
/ Type Designation
  • BELL TEXTRON INC. (BTI)
    • 204B
    • 205
      • 205A-1
    • 212
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Bell Helicopter Textron ASB No. 204-78-3 for Model 204B helicopters, ASB No. 205-78-2 for Model 205A-1 helicopters, and ASB No. 212-78-4 for Model 212 helicopters, all dated April 19, 1978. For a copy of this service information, contact Bell Textron Inc., P.O. Box 482, Fort Worth, TX 76101; telephone 817-280-3391; fax 817-280-6466; or at https://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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