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

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 


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