Airworthiness Directives:

Federal Register: December 22, 2010 (Volume 75, Number 245)

Rules and Regulations

Page 80293-80294

From the Federal Register Online via GPO Access [wais.access.gpo.gov]

DOCID:fr22de10-4

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.

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

Component

Part No. (P/N)

Serial No. (S/N)

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.

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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