[Federal Register Volume 75, Number 245 (Wednesday, December 22, 2010)]
[Rules and Regulations]
[Pages 80293-80294]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-31964]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-0611; Directorate Identifier 2009-SW-18-AD;
Amendment 39-16487; AD 2010-22-08]
RIN 2120-AA64
Airworthiness Directives; Eurocopter France Model AS 350 B, BA,
B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
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SUMMARY: The FAA is correcting an airworthiness directive (AD) that was
published in the Federal Register. That AD applies to the specified
model helicopters. Table 1 of the AD has two part numbers that do not
contain the ``SC'' prefix. This document adds the prefix and corrects
that error. In all other respects, the original document remains the
same.
DATES: This final rule is effective December 22, 2010. The effective
date for AD 2010-22-08 remains November 26, 2010.
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (phone: 800-647-5527) is Document Management Facility,
U.S. Department of Transportation, Docket Operations, M-30, West
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: DOT/FAA Southwest Region, Matt
Wilbanks, ASW-111, Aviation Safety Engineer, Rotorcraft Directorate,
Regulations and Policy Group, 2601 Meacham Blvd., Fort Worth, Texas
76137, telephone (817) 222-5051, fax (817) 222-5961.
SUPPLEMENTARY INFORMATION: This AD, Amendment 39-16487 (75 FR 65222,
October 22, 2010), requires replacing all servo-controls that are
identified in the Applicability section, Table 1, of the AD.
As published, two part numbers shown in Table 1 on Federal Register
page 65224, under item 2. of PART 39--AIRWORTHINESS DIRECTIVES section,
are incorrect. The first incorrect part number (P/N) is ``5084;'' the
correct P/N is ``SC5084.'' The second incorrect P/N is ``5084-1;'' the
correct P/N is ``SC5084-1.'' The other P/Ns shown in Table 1 remain
unchanged.
No other part of the preamble or regulatory information has been
changed; therefore, only Table 1 of the final rule is being published
in the Federal Register.
The effective date of this AD is November 26, 2010.
Correction of Regulatory Text
Sec. 39.13 [Corrected]
0
In the Federal Register document 2010-26565, filed October 21, 2010 and
published on October 22, 2010 (75 FR 65222), on pages 65223 and 65224,
Table 1 containing the part numbers 5084 and 5084-1 without the correct
prefix ``SC'' is corrected to read as follows:
Table 1
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Component Part No. (P/N) Serial No. (S/N)
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Main rotor servo-control...... P/N SC5083....... S/N 270M, 272M, 409M,
423M, 452M, or 1573.
P/N SC5083-1..... S/N 2902 through
2921, inclusive.
P/N SC5084....... S/N 30, 84, 104, 186,
438, 575, or 695.
P/N SC5084-1..... S/N 1462 through
1481, inclusive.
Tail rotor servo-control...... P/N SC5072....... S/N 222M, 306M, or
309.
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[[Page 80294]]
Issued in Fort Worth, Texas, on December 10, 2010.
Lance T. Gant,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2010-31964 Filed 12-21-10; 8:45 am]
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