Airworthiness Directives; Eurocopter Deutschland GmbH Helicopters, 49115 [2013-19447]
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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
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DATES:
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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
]]>Agencies
[Federal Register Volume 78, Number 156 (Tuesday, August 13, 2013)]
[Rules and Regulations]
[Page 49115]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-19447]
-----------------------------------------------------------------------
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 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: 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
Sec. 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
