Airworthiness Directives; Rolls-Royce plc Turbofan Engines, 68360 [2013-27190]
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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.
TKELleY on DSK3SPTVN1PROD with RULES
(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 https://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: https://
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
VerDate Mar<15>2010
15:50 Nov 13, 2013
Jkt 232001
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
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
RIN 2120–AA64
Airworthiness Directives; Rolls-Royce
plc Turbofan Engines
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.
SUMMARY:
This final rule is effective
November 7, 2013.
ADDRESSES: You may examine the AD
docket on the Internet at https://
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.
DATES:
Fmt 4700
Sfmt 4700
[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;
*
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
Frm 00034
Correction of Regulatory Text
§ 39.13
[Docket No. FAA–2013–0029; Directorate
Identifier 2013–NE–01–AD; Amendment 39–
17599; AD 2013–19–17]
PO 00000
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.
*
*
*
*
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
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.
AGENCY:
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’’).
SUMMARY:
E:\FR\FM\14NOR1.SGM
14NOR1
]]>Agencies
[Federal Register Volume 78, Number 220 (Thursday, November 14, 2013)]
[Rules and Regulations]
[Page 68360]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-27190]
-----------------------------------------------------------------------
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 https://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 Sec. 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
Sec. 39.13 [Corrected]
In the Federal Register of October 3, 2013, on page 61173, in the
first column, lines 4 and 5, under Sec. 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
