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Published 2010-12-22 · Federal Register document 2010-31964

Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters

Publication 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.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:33.146842+00:00. The title, summary and date are source facts.

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federal_register_ad_metadata_2010-a7267cd3a71dbd26
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results[409]
Raw source SHA-256
a7267cd3a71dbd2645583c8a673df65e4a7fa9360a96e3be0de5b81f9d68c9a0

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2010-22-08
Effective date printed in this edition
Unknown

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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: f03e00b3f3011cb897a13677cf0f9a8aa8b4a68558662041c89cf9b85655f9ec. Source manifest: b07f00fded853c98f7d57595287fd2d9f641f58648228e6829d2e58996bb02d6.

Official source · 2010-12-22

Publication text

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Read the complete official publication text
[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]


=======================================================================
-----------------------------------------------------------------------

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]
BILLING CODE 4910-13-P


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