AD 2006-10-21

[Federal Register Volume 71, Number 116 (Friday, June 16, 2006)]
[Rules and Regulations]
[Page 34811]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 06-5427]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-21331; Directorate Identifier 2005-NE-07-AD; 
Amendment 39-14604; AD 2006-10-21]
RIN 2120-AA64


Airworthiness Directives; Engine Components Incorporated (ECi) 
Reciprocating Engine Connecting Rods; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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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 Sec.  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:


Sec.  39.13  [Corrected]

0
On page 28771, in the third column, under Sec.  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.
[FR Doc. 06-5427 Filed 6-15-06; 8:45 am]
BILLING CODE 4910-13-P