[Federal Register: March 3, 2008 (Volume 73, Number 42)]
[Proposed Rules]
[Page 11363-11364]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr03mr08-15]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-0177; Directorate Identifier 2007-CE-093-AD]
RIN 2120-AA64
Airworthiness Directives; Taylorcraft Models A, B, and F Series
Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking; correction.
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SUMMARY: This document makes a correction to a current notice of
proposed rulemaking (NPRM), which was published in the Federal Register
on February 20, 2008 (73 FR 9239), and applies to certain Taylorcraft
Models A, B, and F series airplanes. The NPRM proposed to require
inspection of the wing strut attach fittings for corrosion or cracks
and would require repair or replacement if corrosion or cracks are
found. The docket number was incorrectly referenced at ``FAA-2007-
0177'' instead of ``FAA-2008-0177.'' The NPRM is posted in the FAA-
2008-0177 docket section of the Federal Docket Management System
(FDMS). This document corrects the docket number and should further
reduce the confusion associated with the inadvertent error.
DATES: We must receive comments on this proposed AD by March 21, 2008.
ADDRESSES: Use one of the following addresses to comment on this
proposed AD:
Federal eRulemaking Portal: Go to http://
www.regulations.gov. Follow the instructions for submitting comments.
Fax: (202) 493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
FOR FURTHER INFORMATION CONTACT: Andy McAnaul, Aerospace Engineer,
10100 Reunion Place, San Antonio, Texas 78216; telephone: (210) 308-
3365; fax: (210) 308-3370.
SUPPLEMENTARY INFORMATION:
Discussion
On February 12, 2008, the FAA issued an NPRM (73 FR 9239; February
20,
[[Page 11364]]
2008), which applies to certain Taylorcraft Models A, B, and F series
airplanes. This proposed AD would require inspection of the wing strut
attach fittings for corrosion or cracks and would require repair or
replacement if corrosion or cracks are found.
The docket number was incorrectly referenced as ``FAA-2007-0177''
instead of ``FAA-2008-0177.'' The NPRM is posted in the FAA-2008-0177
docket section of the FDMS.
Need for the Correction
This correction is needed to identify the docket number and should
further reduce the confusion associated with the inadvertent error.
Correction of Publication
Accordingly, the publication of February 20, 2008 (73 FR 9239),
which was the subject of FR Doc. E8-2995, is corrected as follows:
On page 9239, in the second column, in the first line under 14 CFR
Part 39, replace ``[Docket No. FAA-2007-0177;'' with ``[Docket No. FAA-
2008-0177;''
On page 9240, in the first column, in the second line from the top
of the page, replace ``FAA-2007-0177;'' with ``FAA-2008-0177''.
On page 9241, in the first column, in the third line under Sec.
39.13 [Amended], replace ``FAA-2007-0177;'' with ``FAA-2008-0177''.
Action is taken herein to correct this reference in the NPRM.
Issued in Kansas City, Missouri, on February 25, 2008.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 08-892 Filed 2-29-08; 8:45 am]
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