This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510. The Code of Federal Regulations is sold by the Superintendent of Documents. Prices of new books are listed in the first FEDERAL REGISTER issue of each week. 

# Rules and Regulations Federal Register 

### 24063

Vol. 69, No. 85 Monday, May 3, 2004

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39 [Docket No. 2003–NM–47–AD; Amendment 39–13566; AD 2004–07–22] RIN 2120–AA64 Airworthiness Directives; Boeing Model 747 Series Airplanes
AGENCY : Federal Aviation Administration, DOT. ACTION : Final rule; correction.

SUMMARY : This document corrects a typographical error that appeared in airworthiness directive (AD) 2004–07– 22 that was published in the Federal Register on April 7, 2004 (69 FR 18250). The typographical error resulted in reference to an incorrect paragraph number. This AD is applicable to all Boeing Model 747 series airplanes. This AD requires that the FAA-approved maintenance inspection program be revised to include inspections that will give no less than the required damage tolerance rating for each structural significant item, and repair of cracked structure. DATES : Effective May 12, 2004. FOR FURTHER INFORMATION CONTACT : Tamara L. Anderson, Aerospace Engineer, Airframe Branch, ANM–120S, FAA, Transport Airplane Directorate, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055–4056; telephone (425) 917–6421; fax (425) 917–6590. SUPPLEMENTARY INFORMATION : Airworthiness Directive (AD) 2004–07– 22, amendment 39–13566, applicable to all Boeing Model 747 series airplanes, was published in the Federal Register on April 7, 2004 (69 FR 18250). That AD requires that the FAA-approved maintenance inspection program be revised to include inspections that will give no less than the required damage tolerance rating for each structural significant item, and repair of cracked structure.

As published, Note 1 of the AD has a typographical error in the paragraph reference of the sentence ‘‘requesting approval for an alternative method of compliance per paragraph (h)(1) of this AD.’’ The correct reference is paragraph (g)(1) of this AD.

Since no other part of the regulatory information has been changed, the final rule is not being republished in the Federal Register

.

The effective date of this AD remains May 12, 2004. § 39.13 [Corrected]
■ On page 18254, in the first column, Note 1 of AD 2004–07–22 is corrected to read as follows: * * * * *

Note 1: * * * For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance per paragraph (g)(1) of this AD.

*** * * * * *

Issued in Renton, Washington, on April 21, 2004. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04–9899 Filed 4–30–04; 8:45 am]
BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71 [Docket No. FAA–2004–17148; Airspace Docket No. 04–ACE–14] Modification of Class E Airspace; Festus, MO
AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Direct final rule; confirmation of effective date.

SUMMARY : This document confirms the effective date of the direct final rule which revises Class E airspace at Festus, MO. DATES : Effective Date: 0901 UTC, June 10, 2004. FOR FURTHER INFORMATION CONTACT : Brenda Mumper, Air Traffic Division, Airspace Branch, ACE–520A, DOT Regional Headquarters Building, Federal Aviation Administration, 901 Locust, Kansas City, MO 64106; telephone: (816) 329–2524. SUPPLEMENTARY INFORMATION : The FAA published this direct final rule with a request for comments in the Federal Register on March 8, 2004 (69 FR 10606). The FAA uses the direct finalrulemaking procedure for a noncontroversial rule where the FAA believes that there will be no adverse public comment. This direct final rule advised the public that no adverse comments were anticipated, and that unless a written adverse comment, or a written notice of intent to submit such an adverse comment, were received within the comment period, the regulation would become effective on June 10, 2004. No adverse comments were received, and thus this notice confirms that this direct final rule will become effective on that date.

Issued in Kansas City, MO, on April 19, 2004. Elizabeth S. Wallis, Acting Manager, Air Traffic Division, Central Region. [FR Doc. 04–9920 Filed 4–30–04; 8:45 am]
BILLING CODE 4910–13–M

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71 [Docket No. FAA–2004–17149; Airspace Docket No. 04–ACE–15] Modification of Class E Airspace; Fulton, MO
AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Direct final rule; confirmation of effective date.

SUMMARY : This document confirms the effective date of the direct final rule which revises Class E airspace at Fulton, MO. EFFECTIVE DATE : 0901 UTC, June 10, 2004. FOR FURTHER INFORMATION CONTACT : Brenda Mumper, Air Traffic Division, Airspace Branch, ACE–520A, DOT Regional Headquarters Building, Federal