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’’). 


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