# [Corrected]
**AGENCY:**
Federal Aviation Administration, DOT.
**ACTION:**
Final rule; correction.
**SUMMARY:**
This document makes a correction to Airworthiness Directive (AD) 2006-10-21. That AD applies to Engine Components Incorporated (ECi) reciprocating engine connecting rods. We published AD 2006-10-21 in the *Federal Register* on May 18, 2006, (71 FR 28769). An incorrect amendment number exists under the § 39.13 amended heading. This document corrects the amendment number. In all other respects, the original document remains the same.
**DATES:**
*Effective Date:* Effective June 16, 2006.
**FOR FURTHER INFORMATION CONTACT:**
Peter Hakala, Aerospace Engineer, Special Certification Office, FAA, Rotorcraft Directorate, 2601 Meacham Blvd., Fort Worth, TX 76193; telephone (817) 222-5145; fax (817) 222-5785.
**SUPPLEMENTARY INFORMATION:**
A final rule AD, FR Doc. 06-4046, that applies to Engine Components Incorporated (ECi) reciprocating engine connecting rods was published in the *Federal Register* on May 18, 2006, (71 FR 28769). The following correction is needed:
§ 39.13
On page 28771, in the third column, under § 39.13 [Amended], in the fifth and sixth lines, “Amendment 39-14605” is corrected to read “Amendment 39-14604”.
Issued in Burlington, MA, on June 9, 2006.
Thomas A. Boudreau,
Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service.