[Federal Register: May 25, 2005 (Volume 70, Number 100)]
[Rules and Regulations]
[Page 29940-29941]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr25my05-8]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-21027; Directorate Identifier 2005-NM-048-AD;
Amendment 39-14070; AD 2005-09-02]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 747 Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
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SUMMARY: The FAA is correcting a typographical error in an existing
airworthiness directive (AD) that was published in the Federal Register
on April 25, 2005 (70 FR 21141). The error resulted in omission of a
reference to an inspection area. This AD applies to all Boeing Model
747 series airplanes. This AD requires repetitive inspections for
cracking of the top and side panel webs and panel stiffeners of the
nose wheel well (NWW), and corrective actions if necessary.
DATES: Effective May 10, 2005.
ADDRESSES: The AD docket contains the proposed AD, comments, and any
final disposition. You can 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-2005-21027; the directorate
identifier for this docket is 2005-NM-048-AD.
FOR FURTHER INFORMATION CONTACT: Nick Kusz, Airframe Branch, ANM-120S,
FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW.,
Renton, Washington 98055-4056; telephone (425) 917-6432; fax (425) 917-
6590.
SUPPLEMENTARY INFORMATION: On April 13, 2005, the FAA issued AD 2005-
09-02, amendment 39-14070 (70 FR 21141, April 25, 2005), for all Boeing
Model 747 series airplanes. This AD requires repetitive inspections for
cracking of the top and side panel webs and panel stiffeners of the
nose wheel well (NWW), and corrective actions if necessary.
As published, we inadvertently did not specify a certain area for a
required
[[Page 29941]]
inspection. Where paragraph (i) of the AD specifies ``Do a UT
inspection of the sidewall panel web for cracks, * * *,'' the correct
areas to inspect are the top and sidewall panel web. References to the
inspection areas are all identified correctly in all other parts of the
AD.
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 May 10, 2005.
PART 39--[AMENDED]
Sec. 39.13 [Corrected]
0
In the Federal Register of April 25, 2005, on page 21144, in the second
column, paragraph (i) of AD 2005-09-02 is corrected to read as follows:
* * * * *
(i) Do a UT inspection of the top and sidewall panel webs for
cracks, in accordance with Boeing ASB 747-53A2465, Revision 4, dated
February 24, 2005, at the later of the times specified in paragraphs
(i)(l) and (i)(2) of this AD. Repeat the inspections thereafter at
intervals not to exceed 500 flight cycles.
* * * * *
Issued in Renton, Washington, on May 16, 2005.
Michael J. Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-10424 Filed 5-24-05; 8:45 am]
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