Airworthiness Directives; Turbomeca Turboshaft Engines, 1009 [2012-79]
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1009
Rules and Regulations
Federal Register
Vol. 77, No. 5
Monday, January 9, 2012
This section of the FEDERAL REGISTER
contains regulatory documents having general
applicability and legal effect, most of which
are keyed to and codified in the Code of
Federal Regulations, which is published under
50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by
the Superintendent of Documents. Prices of
new books are listed in the first FEDERAL
REGISTER issue of each week.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2010–0710; Directorate
Identifier 2010–NE–26–AD; Amendment 39–
16892; AD 2010–19–06R1]
RIN 2120–AA64
Airworthiness Directives; Turbomeca
Turboshaft Engines
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. That
AD applies to Turbomeca Arriel 1 series
turboshaft engines. The AD number is
incorrect in the preamble and in the
Regulatory text. This document corrects
those errors. In all other respects, the
original document remains the same.
DATES: This final rule revision is
effective January 17, 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:
Frederick Zink, Aerospace Engineer,
Engine Certification Office, FAA, 12
New England Executive Park,
Burlington, MA; phone: (781) 238–7779;
tkelley on DSK3SPTVN1PROD with RULES
SUMMARY:
VerDate Mar<15>2010
16:19 Jan 06, 2012
Jkt 226001
fax: (781) 238–7199; email:
frederick.zink@faa.gov.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
SUPPLEMENTARY INFORMATION:
Airworthiness Directive 2011–26–02,
Amendment 39–16892 (76 FR 77378,
December 13, 2011), currently requires
removing from service certain gas
generator second stage turbine discs,
part number (P/N) 0 292 25 040 0, that
are not marked with ‘‘CFR’’ before the
discs exceed 4,000 cycles-in-service
(CIS) since new. That AD also requires
removing from service certain gas
generator second stage turbine discs,
P/N 0 292 25 040 0, that are marked
with ‘‘CFR’’ before the discs exceed
6,500 CIS since new.
As published, the AD number 2011–
26–02 in the preamble of the AD and
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 revision
remains January 17, 2012.
Correction of Non-Regulatory Text
In the Federal Register of December
13, 2011, AD 2011–26–02; Amendment
39–16892 is corrected as follows:
On page 77378, in the second column,
on line 3 under 14 CFR Part 39, change
AD 2011–26–02 to AD 2010–19–06R1.
Correction of Regulatory Text
§ 39.13
[Corrected]
In the Federal Register of December
13, 2011, on page 77379, in the second
column, lines 6 and 7 under § 39.13
[Amended] of AD 2011–26–02, are
corrected to read as follows:
*
*
*
*
*
■
AD 2010–19–06R1 Turbomeca:
Amendment 39–16892; Docket No.
FAA–2010–0710;
*
*
*
*
*
Issued in Burlington, Massachusetts, on
December 29, 2011.
Peter A. White,
Manager, Engine & Propeller Directorate,
Aircraft Certification Service.
[FR Doc. 2012–79 Filed 1–6–12; 8:45 am]
BILLING CODE 4910–13–P
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Frm 00001
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14 CFR Part 39
[Docket No. FAA–2009–0162; Directorate
Identifier 2004–NE–19–AD; Amendment 39–
16803; AD 2011–18–21]
RIN 2120–AA64
Airworthiness Directives; Rolls-Royce
plc (RR) RB211–524 Series Turbofan
Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
We are superseding an
existing airworthiness directive (AD) for
the products listed above. That AD
currently requires initial and repetitive
borescope inspections of the head
section and meterpanel assembly of the
combustion liner, and replacement if
necessary. This new AD requires those
same inspections, and replacement.
This AD also expands the applicability
to include part numbers (P/N) of
additional combustion liners. This AD
was prompted by an inquiry submitted
by an operator, which resulted in RR
performing a complete review of the
affected front combustion liner part
numbers. We are issuing this AD to
prevent deterioration of the engine
combustion liner, which can result in
combustion liner breakup, case burnthrough, engine fire, and damage to the
airplane.
DATES: This AD is effective February 13,
2012.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of February 9, 2005 (70 FR 680,
January 5, 2005).
ADDRESSES: For service information
identified in this AD, contact RollsRoyce plc, P.O. Box 31, Derby, DE24
8BJ, United Kingdom; phone: 011–44–
1332–242424; fax: 011–44–1332–
249936, for the service information
identified in this proposed AD. You
may review copies of the referenced
service information at the FAA, Engine
& Propeller Directorate, 12 New England
Executive Park, Burlington, MA. For
information on the availability of this
material at the FAA, call (781) 238–
7125.
SUMMARY:
E:\FR\FM\09JAR1.SGM
09JAR1
]]>Agencies
[Federal Register Volume 77, Number 5 (Monday, January 9, 2012)]
[Rules and Regulations]
[Page 1009]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2012-79]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
Prices of new books are listed in the first FEDERAL REGISTER issue of each
week.
========================================================================
Federal Register / Vol. 77, No. 5 / Monday, January 9, 2012 / Rules
and Regulations
[[Page 1009]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-0710; Directorate Identifier 2010-NE-26-AD;
Amendment 39-16892; AD 2010-19-06R1]
RIN 2120-AA64
Airworthiness Directives; Turbomeca Turboshaft Engines
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. That AD applies to Turbomeca Arriel
1 series turboshaft engines. The AD number is incorrect in the preamble
and in the Regulatory text. This document corrects those errors. In all
other respects, the original document remains the same.
DATES: This final rule revision is effective January 17, 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: Frederick Zink, Aerospace Engineer,
Engine Certification Office, FAA, 12 New England Executive Park,
Burlington, MA; phone: (781) 238-7779; fax: (781) 238-7199; email:
frederick.zink@faa.gov.
SUPPLEMENTARY INFORMATION: Airworthiness Directive 2011-26-02,
Amendment 39-16892 (76 FR 77378, December 13, 2011), currently requires
removing from service certain gas generator second stage turbine discs,
part number (P/N) 0 292 25 040 0, that are not marked with ``CFR''
before the discs exceed 4,000 cycles-in-service (CIS) since new. That
AD also requires removing from service certain gas generator second
stage turbine discs, P/N 0 292 25 040 0, that are marked with ``CFR''
before the discs exceed 6,500 CIS since new.
As published, the AD number 2011-26-02 in the preamble of the AD
and 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 revision remains January 17, 2012.
Correction of Non-Regulatory Text
In the Federal Register of December 13, 2011, AD 2011-26-02;
Amendment 39-16892 is corrected as follows:
On page 77378, in the second column, on line 3 under 14 CFR Part
39, change AD 2011-26-02 to AD 2010-19-06R1.
Correction of Regulatory Text
Sec. 39.13 [Corrected]
0
In the Federal Register of December 13, 2011, on page 77379, in the
second column, lines 6 and 7 under Sec. 39.13 [Amended] of AD 2011-26-
02, are corrected to read as follows:
* * * * *
AD 2010-19-06R1 Turbomeca: Amendment 39-16892; Docket No. FAA-2010-
0710;
* * * * *
Issued in Burlington, Massachusetts, on December 29, 2011.
Peter A. White,
Manager, Engine & Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2012-79 Filed 1-6-12; 8:45 am]
BILLING CODE 4910-13-P
