AD 2010-22-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus Helicopters | AS355E | Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters |
| aircraft | Airbus Helicopters | AS355F | Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters |
| aircraft | Airbus Helicopters | AS355F1 | Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters |
| aircraft | Airbus Helicopters | AS355F2 | Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters |
| aircraft | Airbus Helicopters | AS355N | Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters |
| aircraft | Airbus Helicopters | AS350B | Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters |
| aircraft | Airbus Helicopters | AS350B1 | Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters |
| aircraft | Airbus Helicopters | AS350B2 | Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters |
| aircraft | Airbus Helicopters | AS350B3 | Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters |
| aircraft | Airbus Helicopters | AS350BA | Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters |
| aircraft | Airbus Helicopters | AS350D | Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters |
Unsafe Condition
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.
Required Actions
Replace all servo-controls identified in Table 1 of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N helicopters, as specified in Table 1 of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
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.
Document Text
Show stored source text (verify against official source)
[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 [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[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 <a href="http://www.regulations.gov">http://www.regulations.gov</a>; 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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Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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