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[Corrected]

---
identifier: "/us/fr/C1-2010-21870"
source: "fr"
legal_status: "authoritative_unofficial"
title: "[Corrected]"
title_number: 0
title_name: "Federal Register"
section_number: "C1-2010-21870"
section_name: "[Corrected]"
positive_law: false
currency: "2010-09-02"
last_updated: "2010-09-02"
format_version: "1.1.0"
generator: "[email protected]"
agency: "DEPARTMENT OF TRANSPORTATION"
document_number: "C1-2010-21870"
document_type: "rule"
publication_date: "2010-09-02"
agencies:
  - "DEPARTMENT OF TRANSPORTATION"
  - "Federal Aviation Administration"
cfr_references:
  - "14 CFR Part 39"
rin: "2120-AA64"
---

#  [Corrected]

**AGENCY:**

Federal Aviation Administration (FAA), DOT.

**ACTION:**

Final rule; correction.

**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:

§ 39.13

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.