[Corrected]

---
identifier: "/us/fr/06-5427"
source: "fr"
legal_status: "authoritative_unofficial"
title: "[Corrected]"
title_number: 0
title_name: "Federal Register"
section_number: "06-5427"
section_name: "[Corrected]"
positive_law: false
currency: "2006-06-16"
last_updated: "2006-06-16"
format_version: "1.1.0"
generator: "[email protected]"
agency: "DEPARTMENT OF TRANSPORTATION"
document_number: "06-5427"
document_type: "rule"
publication_date: "2006-06-16"
agencies:
  - "DEPARTMENT OF TRANSPORTATION"
  - "Federal Aviation Administration"
cfr_references:
  - "14 CFR Part 39"
rin: "2120-AA64"
---


#  [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.