Airworthiness Directives; Eurocopter France Helicopters, 49115-49116 [2013-19444]
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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
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
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.
SUMMARY:
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 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
ehiers on DSK2VPTVN1PROD with RULES
DATES:
VerDate Mar<15>2010
15:29 Aug 12, 2013
Jkt 229001
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.
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.
SUPPLEMENTARY INFORMATION:
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
PO 00000
Frm 00007
Fmt 4700
Sfmt 4700
49115
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
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
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 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 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
SUMMARY:
E:\FR\FM\13AUR1.SGM
13AUR1
49116
Federal Register / Vol. 78, No. 156 / Tuesday, August 13, 2013 / Rules and Regulations
are met. As such, AD 2012–25–04
currently includes the following as the
last sentence under paragraph (f)(4):
‘‘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 April 24,
2013, on page 24046, in the second
column, the last sentence of paragraph
(f)(4) 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. 2013–19444 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–2011–1158; Directorate
Identifier 2010–SW–018–AD; Amendment
39–16847; AD 2011–22–05]
RIN 2120–AA64
Airworthiness Directives; Eurocopter
France Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
The FAA is correcting an
airworthiness directive (AD) that was
published in the Federal Register. The
AD applies to certain Eurocopter France
(Eurocopter) Model AS350B, B1, B2, B3,
BA, C, D, and D1 helicopters; and Model
AS355E, F, F1, F2, N, and NP
helicopters. The reference to Title 14,
Code of Federal Regulations (14 CFR)
91.173 in the Compliance 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
ehiers on DSK2VPTVN1PROD with RULES
SUMMARY:
VerDate Mar<15>2010
15:29 Aug 12, 2013
Jkt 229001
2011–22–05 (76 FR 70046, November
10, 2011) remains November 25, 2011.
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.
ADDRESSES:
Jim
Grigg, Rotorcraft Directorate, Safety
Management Group Manager, FAA,
2601 Meacham Blvd., Fort Worth, TX
76137; phone: (817) 222–5110; fax: (817)
222–5110; email: jim.grigg@faa.gov.
FOR FURTHER INFORMATION CONTACT:
AD 2011–
22–05, Amendment 39–16847 (76 FR
70046, November 10, 2011), applies to
certain Eurocopter Model AS350B, B1,
B2, B3, BA, C, D, and D1 and Model
AS355E, F, F1, F2, N, and NP
helicopters. AD 2011–22–05 currently
requires, in part, a daily check of the tail
rotor pitch control rod (control rod)
outboard spherical bearing (bearing) for
play, and allows this check to be
performed by a pilot if certain
regulatory recordkeeping requirements
are met. As such, AD 2011–22–05
currently includes the following as the
last sentence under paragraph (a): ‘‘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.
SUPPLEMENTARY INFORMATION:
Correction of Regulatory Text
§ 39.13
[Corrected]
In the Federal Register of November
10, 2011, on page 70048, in the third
column, the last sentence of paragraph
(a) is corrected to read as follows:
*
*
*
*
*
The record must be maintained as
required by 14 CFR 91.417, 121.380, or
135.439.
*
*
*
*
*
PO 00000
Frm 00008
Fmt 4700
Sfmt 4700
Issued in Fort Worth, Texas, on August 2,
2013.
Lance T. Gant,
Acting Manager, Rotorcraft Directorate,
Aircraft Certification Service.
[FR Doc. 2013–19457 Filed 8–12–13; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2013–0414; Airspace
Docket No. 13–ANM–14]
Modification of Class E Airspace;
Brigham City, UT
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
This action modifies Class E
airspace at Brigham City Airport,
Brigham City, UT. Decommissioning of
the Brigham City Nondirectional Radio
Beacon (NDB) has made this action
necessary for the safety and
management of Instrument Flight Rules
(IFR) operations at the airport. This
action also makes an adjustment to the
geographic coordinates of the airport.
DATES: Effective date, 0901 UTC,
October 17, 2013. The Director of the
Federal Register approves this
incorporation by reference action under
1 CFR Part 51, subject to the annual
revision of FAA Order 7400.9 and
publication of conforming amendments.
FOR FURTHER INFORMATION CONTACT:
Eldon Taylor, Federal Aviation
Administration, Operations Support
Group, Western Service Center, 1601
Lind Avenue SW., Renton, WA, 98057;
telephone (425) 203–4537.
SUPPLEMENTARY INFORMATION:
SUMMARY:
History
On June 5, 2013, the FAA published
in the Federal Register a notice of
proposed rulemaking (NPRM) to modify
controlled airspace at Brigham City, UT
(78 FR 33772). Interested parties were
invited to participate in this rulemaking
effort by submitting written comments
on the proposal to the FAA. No
comments were received.
Class E airspace designations are
published in paragraph 6005, of FAA
Order 7400.9W dated August 8, 2012,
and effective September 15, 2012, which
is incorporated by reference in 14 CFR
71.1. The Class E airspace designations
listed in this document will be
published subsequently in that Order.
E:\FR\FM\13AUR1.SGM
13AUR1
]]>Agencies
[Federal Register Volume 78, Number 156 (Tuesday, August 13, 2013)]
[Rules and Regulations]
[Pages 49115-49116]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-19444]
-----------------------------------------------------------------------
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 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 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
[[Page 49116]]
are met. As such, AD 2012-25-04 currently includes the following as the
last sentence under paragraph (f)(4): ``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
Sec. 39.13 [Corrected]
In the Federal Register of April 24, 2013, on page 24046, in the
second column, the last sentence of paragraph (f)(4) 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. 2013-19444 Filed 8-12-13; 8:45 am]
BILLING CODE 4910-13-P
