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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

CFR Citation: 14 CFR Part 39

Docket ID: [Docket No. 2003-NM-47-AD; Amendment 39-13566; AD 2004-07-22]

RIN ID: RIN 2120-AA64

NOTICE: RULES

ACTION: Airworthiness directives:

DOCUMENT ACTION: Final rule; correction.

SUBJECT CATEGORY: Airworthiness Directives; Boeing Model 747 Series Airplanes

DATES: Effective May 12, 2004.

DOCUMENT SUMMARY: This document corrects a typographical error that appeared in airworthiness directive (AD) 20040722 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 FAAapproved 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.

SUMMARY: Boeing; correction,

SUPPLEMENTAL INFORMATION

Airworthiness Directive (AD) 2004-07-22, amendment 3913566, 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 FAAapproved 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. Sec. 39.13 [Corrected]
On page 18254, in the first column, Note 1 of AD 20040722 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. 049899 Filed 43004; 8:45 am]
BILLING CODE 491013P

FOR FURTHER INFORMATION CONTACT Tamara L. Anderson, Aerospace Engineer, Airframe Branch, ANM120S, FAA, Transport Airplane Directorate, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 980554056; telephone (425) 9176421; fax (425) 9176590.