[Federal Register Volume 75, Number 170 (Thursday, September 2, 2010)]
[Rules and Regulations]
[Page 53846]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C1-2010-21870]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-0201; Directorate Identifier 2008-NE-47-AD;
Amendment 39-16314; AD 2010-11-09]
RIN 2120-AA64
Airworthiness Directives; Thielert Aircraft Engines GmbH (TAE)
Models TAE 125-01 and TAE 125-02-99 Reciprocating Engines Installed In,
But Not Limited To, Diamond Aircraft Industries Model DA 42 Airplanes;
Correction
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
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SUMMARY: The FAA is correcting airworthiness directive (AD) 2010-11-09,
which published in the Federal Register. That AD applies to TAE models
TAE 125-01 and TAE 125-02-99 reciprocating engines, installed in, but
not limited to, Diamond Aircraft Industries model DA 42 airplanes. The
part number for engine model TAE 125-01 is missing a digit in paragraph
(c) and in paragraph (e)(3). This document corrects those part numbers.
In all other respects, the original document remains the same.
DATES: This correction is effective September 2, 2010. The compliance
times of AD 2010-11-09 remain unchanged.
FOR FURTHER INFORMATION CONTACT: Tara Chaidez, Aerospace Engineer,
Engine Certification Office, FAA, Engine and Propeller Directorate, 12
New England Executive Park, Burlington, MA 01803; e-mail:
[email protected]; telephone (781) 238-7773; fax (781) 238-7199.
SUPPLEMENTARY INFORMATION: On June 8, 2010 (75 FR 32253), we published
a final rule AD, FR Doc. 2010-12540, in the Federal Register. That AD
applies to TAE models TAE 125-01 and TAE 125-02-99 reciprocating
engines, installed in, but not limited to, Diamond Aircraft Industries
model DA 42 airplanes. We need to make the following corrections:
Sec. 39.13 [Corrected]
On page 32254, in the second column, in paragraph (c), in the fifth
line, ``or 02-7200-1401R1'' is corrected to read ``or 02-7200-
14017R1''.
On page 32254, in the second column, in paragraph (e)(3), in the
second line, ``engine P/N 02-7200-1401R1'' is corrected to read
``engine P/N 02-7200-14017R1''
Issued in Burlington, Massachusetts, on August 26, 2010.
Thomas A. Boudreau,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. C1-2010-21870 Filed 9-1-10; 8:45 am]
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