## 68360 Federal Register / Vol. 78, No. 220 / Thursday, November 14, 2013 / Rules and Regulations

(h) Other FAA AD Provisions

The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Mike Kiesov, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329–4144; fax: (816) 329– 4090; email: mike.kiesov@faa.gov. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO.

(2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (i) Special Flight Permit

Special flight permits are permitted with the following limitation: Aerobatic maneuvers are prohibited until the actions of the AD are complied with. (j) Related Information

Refer to MCAI European Aviation Safety Agency (EASA) AD No.: 2012–0228R1, dated November 13, 2012, for related information. You may examine the MCAI on the Internet
at http://www.regulations.gov by searching for and locating it in Docket No. FAA–2013–
0939. (k) Material Incorporated by Reference

(1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.

(i) Alenia Aermacchi Una Societa Finmeccanica Mandatory Bollettino Tecnico (English Translation: Technical Bulletin) No. 205B65, Revision 1, dated November 12,
2012.

(ii) Alenia Aermacchi Una Societa Finmeccanica Mandatory Bollettino Tecnico (English Translation: Technical Bulletin) No. 260SB–136, Revision 1, dated November 12,
2012.

(3) For service information identified in this AD, contact Alenia Aermacchi S.p.A, Via Paola Foresio, 1, 21040 Venegono Superiore (Varese)—Italy; telephone: 0331–813111; fax: 0331–827595; Internet: http:// www.aleniaaermacchi.it/en-US/Pages/ custsupp.aspx.

(4) You may view this referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329–4148.

(5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: http://www.archives.gov/federal-register/cfr/ibrlocations.html.

Issued in Kansas City, Missouri, on October 31, 2013. Earl Lawrence, Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2013–26681 Filed 11–13–13; 8:45 am]

**BILLING CODE 4910–13–P**



### DEPARTMENT OF TRANSPORTATION

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2013–0029; Directorate Identifier 2013–NE–01–AD; Amendment 39–**  **17599; AD 2013–19–17]**

**RIN 2120–AA64**



### Airworthiness Directives; Rolls-Royce **plc Turbofan Engines**

**AGENCY** 

### : Federal Aviation Administration (FAA), DOT.

**ACTION** 

### : Final rule; correction.

**SUMMARY** 

### : The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to all Rolls-Royce plc (RR) RB211–535E4–B–37 series turbofan engines. The AD number is incorrect in the Regulatory text. This document corrects that error. In all other respects, the original document remains the

same.

**DATES** 

### : This final rule is effective November 7, 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 Green, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; phone: 781–238–7754; fax: 781–238– 7199; email: robert.green@faa.gov. **SUPPLEMENTARY INFORMATION** 

### : Airworthiness Directive 2013–19–17, Amendment 39–17599 (78 FR 61171, October 3, 2013), currently requires removal of affected parts using a drawdown plan for all RR RB211– 535E4–B–37 series turbofan engines.

As published, the AD number 2013– 19–17 under § 39.13 [Amended], is incorrect.

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

.

The effective date of this AD remains November 7, 2013. Correction of Regulatory Text

**§ 39.13 [Corrected]**



### In the Federal Register of October 3, 2013, on page 61173, in the first column, lines 4 and 5, under § 39.13 [Amended] of AD 2013–19–17, are corrected to read as follows:
* * * * * 2013–19–17 Rolls-Royce plc: Amendment 39–17599; Docket No. FAA–2013–0029;


### * * * * *

Issued in Burlington, Massachusetts, on October 25, 2013. Colleen M. D’Alessandro, Assistant Directorate Manager, Engine & Propeller Directorate, Aircraft Certification Service.
[FR Doc. 2013–27190 Filed 11–13–13; 8:45 am]

**BILLING CODE 4910–13–P**



### DEPARTMENT OF TRANSPORTATION

**Federal Aviation Administration**

**14 CFR Part 91**

**[Docket No. FAA–2013–0061]**


### Unmanned Aircraft System Test Site **Program**

**AGENCY** 

### : Federal Aviation Administration (FAA), DOT.

**ACTION** 

### : Notice of availability of final privacy requirements for the unmanned aircraft system (‘‘UAS’’) test site program; response to comments.

**SUMMARY** 

### : On February 22, 2013 the FAA published and requested public comment on the proposed privacy requirements (the ‘‘Draft Privacy Requirements’’) for UAS test sites (the ‘‘Test Sites’’) that the FAA will establish pursuant to the FAA Modernization and Reform Act of 2012 (‘‘FMRA’’). This document responds to the public comments received and publishes the FAA’s final privacy requirements for the Test Sites (the ‘‘Final Privacy Requirements’’).