
[Federal Register: September 2, 2010 (Volume 75, Number 170)]
[Rules and Regulations]               
[Page 53846]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr02se10-3]                         

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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: 
tara.chaidez@faa.gov; 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]
BILLING CODE 4910-13-P

