### 49115 Federal Register / Vol. 78, No. 156 / Tuesday, August 13, 2013 / Rules and Regulations

may review a copy of the service information at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137.

(2) The subject of this AD is addressed in Transport Canada Civil Aviation (TCCA) AD No. CF–2012–14R1, dated May 9, 2012. You may view a copy of the TCCA AD and a copy of STC No. SR01298NY in the AD Docket on the Internet at http:/www.regulations.gov

. (h) Subject

Joint Aircraft Service Component (JASC) Code: 3213: Main Landing Gear Strut/Axle/ Truck.

Issued in Fort Worth, Texas, on August 2, 2013. Lance T. Gant, Acting Directorate Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 2013–19434 Filed 8–12–13; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**
**[Docket No. FAA–2012–0566; Directorate Identifier 2011–SW–008–AD; Amendment**  **39–17065; AD 2012–11–02]**

**RIN 2120–AA64**
**Airworthiness Directives; Eurocopter Deutschland GmbH Helicopters** 

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final rule; correction.

**SUMMARY :**  The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. The AD applies to certain Eurocopter Deutschland GmbH (Eurocopter) Model EC135 helicopters. The reference to Title 14, Code of Federal Regulations (14 CFR) 91.173 in the Required Actions section is incorrect. This document corrects that error. In all other respects, the original document remains the

same.
**DATES :**  This final rule is effective August 13, 2013. The effective date for AD 2012–11–02 (77 FR 37790, June 25, 2012) remains July 10, 2012.

**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 :**  Sharon Miles, Aviation Safety Engineer, Rotorcraft Directorate, Regulations and Policy Group, FAA, 2601 Meacham Blvd., Fort Worth, TX 76137; phone: (817) 222–5110; fax: (817) 222–5110; email: sharon.y.miles@faa.gov

. **SUPPLEMENTARY INFORMATION :**  AD 2012– 11–02, Amendment 39–17065 (77 FR 37790, June 25, 2012), applies to certain Eurocopter Model EC135 helicopters. AD 2012–11–02 currently requires, in part, visually checking the ring frame which connects the tail rotor Fenestron housing to the tailboom for a crack before further flight and thereafter at each preflight check, and allows this check to be performed by a pilot if certain regulatory recordkeeping requirements are met. As such, AD 2012–11–02 currently includes the following as the last sentence under paragraph (f)(1): ‘‘The record must be maintained as required by 14 CFR 91.173, 121.380, or 134.439.’’

As published, the reference to 14 CFR 91.173 is incorrect. The correct reference is to 14 CFR 91.417.

No other part of the preamble or regulatory information has been changed; therefore, only the changed portion of the final rule is being published in the Federal Register

. Correction of Regulatory Text

**§ 39.13 [Corrected]**

In the Federal Register of June 25, 2012, on page 37792, in the third column, the last sentence of paragraph (f)(1) is corrected to read as follows:
* * * * *

The record must be maintained as required by 14 CFR 91.417, 121.380, or 135.439.
* * * * *

Issued in Fort Worth, Texas, on August 2,
2013. Lance T. Gant, Acting Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 2013–19447 Filed 8–12–13; 8:45 am]

**BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION** 

**Federal Aviation Administration**

**14 CFR Part 39**
**[Docket No. FAA–2012–1297; Directorate Identifier 2012–SW–100–AD; Amendment**  **39–17285; AD 2012–25–04]**

**RIN 2120–AA64**
**Airworthiness Directives; Eurocopter France Helicopters** 

**AGENCY :**  Federal Aviation Administration (FAA), DOT.
**ACTION :**  Final rule; correction.

**SUMMARY :**  The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register . The AD applies to certain Eurocopter France (Eurocopter) Model AS350B3 helicopters. The reference to Title 14, Code of Federal Regulations (14 CFR) 91.173 in the Required Actions section is incorrect. This document corrects that error. In all other respects, the original document remains the same.
**DATES :**  This final rule is effective August 13, 2013. The effective date for AD 2012–25–04 (78 FR 24041, April 24, 2013) remains May 9, 2013.
**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 :**  Robert Grant, Aviation Safety Engineer, Rotorcraft Directorate, Safety Management Group, FAA, 2601 Meacham Blvd., Fort Worth, TX 76137; phone: (817) 222–5110; fax: (817) 222– 5110; email: robert.grant@faa.gov.
**SUPPLEMENTARY INFORMATION :**  AD 2012– 25–04, Amendment 39–17285 (78 FR 24041, April 24, 2013), applies to certain Eurocopter Model AS350B3 helicopters. AD 2012–25–04 currently requires, in part, before further flight and thereafter after each flight without exceeding 3 hours time-in-service between two checks, visually checking each laminated half bearing for certain conditions, and allows this check to be performed by a pilot if certain regulatory recordkeeping requirements