AD 2004-07-22

[Federal Register Volume 69, Number 85 (Monday, May 3, 2004)]
[Rules and Regulations]
[Page 24063]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 04-9899]



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Federal Register / Vol. 69, No. 85 / Monday, May 3, 2004 / Rules and 
Regulations

[[Page 24063]]



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.


Sec.  39.13  [Corrected]

0
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]
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