Rules and Regulations. Final rule; correction

412 words·~2 min read·/register/2006/04/21/06-3797

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BILLING CODE 4910-13-P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24364; Directorate Identifier 2004-NM-272-AD; Amendment 39-14534; AD 2006-07-07] RIN 2120-AA64 Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes) AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; correction. SUMMARY: The FAA is correcting a typographical error in an existing airworthiness directive

(AD)that was published in the **Federal Register** on March 31, 2006 (71 FR 16206). The error resulted in an incorrect Docket No. This AD applies to certain Airbus Model A300-600 series airplanes. This AD requires modifying nine bolt holes in the vertical flange to prevent cracking before the inspection threshold of AD 98-18-02. DATES: Effective April 17, 2006. ADDRESSES: The AD docket contains the proposed AD, comments, and any final disposition. You may examine the AD docket on the Internet at *http://dms.dot.gov,* or in person at the Docket Management Facility office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Management Facility office (telephone

(800)647-5227) is located on the plaza level of the Nassif Building at the U.S. Department of Transportation, 400 Seventh Street, SW., room PL-401, Washington, DC. This docket number is FAA-2006-24364; the directorate identifier for this docket is 2004-NM-272-AD. FOR FURTHER INFORMATION CONTACT: Tim Backman, Aerospace Engineer, ANM-116, International Branch, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone

(425)227-2797; fax

(425)227-1149. SUPPLEMENTARY INFORMATION: On March 15, 2006, the FAA issued AD 2006-07-07, amendment 39-14534 (71 FR 16206, March 31, 2006), for certain Airbus Model A300-600 series airplanes. The AD requires modifying nine bolt holes in the vertical flange to prevent cracking before the inspection threshold of AD 98-18-02. As published, the AD lists the Docket No. as FAA-2006-24124. The correct Docket No. is FAA-2006-24364. No other part of the regulatory information has been changed; therefore, the final rule is not republished in the **Federal Register** . The effective date of this AD remains April 17, 2006. In the **Federal Register** of March 31, 2006, on page 16206, in the first column; on page 16207, in the third column; and on page 16208 in the second column; the Docket No. of AD 2006-07-07 is corrected to read as follows: FAA-2006-24364. Issued in Renton, Washington, on April 13, 2006. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 06-3797 Filed 4-20-06; 8:45 am]

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Final rule; correction

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