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US-2014-12-04 : Main Rotor Drive - Main Rotor Grip - Inspection / Replacement

Number US-2014-12-04
Issued by United States of America  United States of America
Issue date 2014-06-23
Effective date 2014-07-24
EASA approval number
ATA Chapter 62
Approval Holder
/ Type Designation
  • BELL TEXTRON INC. (BTI)
    • 204B
    • 205
      • 205A
      • 205A-1
      • 205B
    • 210
    • 212
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2003-01-04, dated January 15, 2003.
Publication(s) and related information Bell Helicopter Textron Inc. (BHTI) Non-destructive Inspection Procedure, Log No. 00-340, Revision E, dated April 9, 2002. ASB No. 212-94-92, Revision A, dated March 13, 1995; BHTI ASB No. 212-02-116, Revision A, dated October 30, 2002; BHTI 205B-02-39, Revision B, dated November 22, 2002; BHTI ASB No. 204-02-58 and ASB No. 205-02-88, both dated November 26, 2002; BHTI ASB No. 210-08-02, dated September 10, 2008; BHTI Operations Safety Notice 204-85-6, 205-85-9, and 212-85-13, all dated November 14, 1985; and BHTI Information Letter, 204-08-23, 205-08-38, 205B-08-21, and 212-08-62, Revision A, dated July 23, 2008. For service information identified in this AD, contact BHTI, 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 models 205A, 205B and 210 are not validated in Europe. Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu

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