Airworthiness Directives; CFE Company Turbofan Engines, 14646-14647 [2017-05242]
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14646
Federal Register / Vol. 82, No. 54 / Wednesday, March 22, 2017 / Proposed Rules
(l) Terminating Action Limitation
Accomplishment of corrective actions
required by paragraph (g) of this AD does not
constitute terminating action for the
repetitive inspections required by this AD.
jstallworth on DSK7TPTVN1PROD with PROPOSALS
(m) Terminating Action for Certain
Airplanes
(1) For airplanes with any MLG having P/
N 10–210 series: Modification of the bogie
beam of each MLG having P/N 10–210 series,
as specified in Airbus Service Bulletin A330–
32–3268, Revision 01, dated September 21,
2015; or Airbus Service Bulletin A340–32–
4300, dated April 20, 2015; or Revision 01,
dated September 21, 2015; as applicable; and
in accordance with the Accomplishment
Instructions of Messier-Bugatti-Dowty
Service Bulletin A33/34–32–305, including
Appendix A, dated April 13, 2015;
constitutes terminating action for the
repetitive inspection requirements of this AD
for that airplane, provided that, following inservice modification, the airplane remains in
post-service bulletin configuration.
(2) For airplanes with any MLG having P/
N 201252 series or P/N 201490 series:
Installation of both left-hand and right-hand
MLG having P/N 201252 series or P/N
201490 series that has an improved bogie
beam, as required by paragraph (k) of this
AD, constitutes terminating action for the
repetitive inspections requirements of this
AD for that airplane, provided that, following
in-service modification, the airplane remains
in post-service bulletin configuration.
(n) Parts Installation Prohibition
Do not install on any airplane a pre-Airbus
modification MLG having P/N 201252 series
or pre-Airbus modification MLG having P/N
201490 series, as specified in paragraph
(n)(1) or (n)(2) of this AD, as applicable; or
a pre-Airbus modification MLG having P/N
10–210 series, as specified in paragraph
(n)(3) or (n)(4) of this AD, as applicable.
(1) For any airplane that is in post-Airbus
Modification 205289 configuration, or on
which the modification required by
paragraph (k) of this AD has been done: From
the effective date of this AD.
(2) For any airplane that is in pre-Airbus
Modification 205289 configuration, or on
which the modification required by
paragraph (k) of this AD has not been done:
After modification of that airplane, as
required by paragraph (k) of this AD.
(3) For any airplane that is in post-Airbus
Modification 204421 configuration, or on
which the modification specified in
paragraph (m)(1) of this AD has been done:
From the effective date of this AD.
(4) For an airplane that is in pre-Airbus
Modification 204421, or on which the
modification required by paragraph (m)(1) of
this AD has not been done: After
modification of that airplane, as required by
paragraph (m)(1) of this AD.
(o) Credit for Previous Actions
(1) This paragraph provides credit for the
actions required by paragraph (g) of this AD,
if those actions were performed before the
effective date of this AD using the service
information identified in paragraphs (o)(1)(i)
through (o)(1)(vii) or (o)(2) of this AD, as
applicable.
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(i) Airbus Service Bulletin A330–32–3248,
dated October 5, 2011, which is not
incorporated by reference in this AD.
(ii) Airbus Service Bulletin A330–32–3248,
Revision 01, including Appendix 01, dated
December 13, 2012, which was incorporated
by reference in AD 2013–10–03, Amendment
39–17456 (78 FR 31386, May 24, 2013).
(iii) Airbus Service Bulletin A330–32–
3248, Revision 02, dated April 16, 2014,
which is not incorporated by reference in this
AD.
(iv) Airbus Service Bulletin A330–32–
3248, Revision 03, dated November 27, 2015,
which is not incorporated by reference in this
AD.
(v) Airbus Service Bulletin A330–32–3248,
Revision 04, dated January 5, 2016, which is
not incorporated by reference in this AD.
(vi) Airbus Service Bulletin A340–32–
4286, dated October 5, 2011, which was
incorporated by reference in AD 2013–10–03,
Amendment 39–17456 (78 FR 31386, May 24,
2013).
(vii) Airbus Service Bulletin A340–32–
4286, Revision 01, dated November 27, 2015,
which is not incorporated by reference in this
AD.
(2) This paragraph provides credit for the
actions required by paragraph (k) of this AD,
if those actions were performed before the
effective date of this AD using MessierBugatti-Dowty Service Bulletin A33/34–32–
306, dated December 21, 2015, which is not
incorporated by reference in this AD.
(p) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Branch, ANM–116, Transport Airplane
Directorate, FAA, has the authority to
approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19.
In accordance with 14 CFR 39.19, send your
request to your principal inspector or local
Flight Standards District Office, as
appropriate. If sending information directly
to the International Branch, send it to ATTN:
Vladimir Ulyanov, Aerospace Engineer,
International Branch, ANM–116, Transport
Airplane Directorate, FAA, 1601 Lind
Avenue SW., Renton, WA 98057–3356;
telephone: 425–227–1138; fax: 425–227–
1149. Information may be emailed to: 9ANM-116-AMOC-REQUESTS@faa.gov.
(i) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office. The AMOC
approval letter must specifically reference
this AD.
(ii) AMOCs approved previously for AD
2013–10–03 are not approved as AMOCs
with this AD.
(2) Contacting the Manufacturer: As of the
effective date of this AD, for any requirement
in this AD to obtain corrective actions from
a manufacturer, the action must be
accomplished using a method approved by
the Manager, International Branch, ANM–
116, Transport Airplane Directorate, FAA; or
EASA; or Airbus’s EASA DOA. If approved
by the DOA, the approval must include the
DOA-authorized signature.
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(3) Required for Compliance (RC): Except
as required by paragraph (j) of this AD: If any
service information contains procedures or
tests that are identified as RC, those
procedures and tests must be done to comply
with this AD; any procedures or tests that are
not identified as RC are recommended. Those
procedures and tests that are not identified
as RC may be deviated from using accepted
methods in accordance with the operator’s
maintenance or inspection program without
obtaining approval of an AMOC, provided
the procedures and tests identified as RC can
be done and the airplane can be put back in
an airworthy condition. Any substitutions or
changes to procedures or tests identified as
RC require approval of an AMOC.
(q) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA AD
2016–0108, dated June 8, 2016, for related
information. This MCAI may be found in the
AD docket on the Internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2016–3984.
(2) For Airbus service information
identified in this AD, contact Airbus SAS,
Airworthiness Office—EAL, 1 Rond Point
Maurice Bellonte, 31707 Blagnac Cedex,
France; telephone: +33 5 61 93 36 96; fax:
+33 5 61 93 45 80; email:
airworthiness.A330-A340@airbus.com;
Internet https://www.airbus.com. For MessierBugatti-Dowty service information identified
in this AD, contact Messier Services
Americas, Customer Support Center, 45360
Severn Way, Sterling, VA 20166–8910;
phone: 703–450–8233; fax: 703–404–1621;
Internet: https://techpubs.services/messierdowty.com. You may view this service
information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton,
WA. For information on the availability of
this material at the FAA, call 425–227–1221.
Issued in Renton, Washington, on March 9,
2017.
Michael Kaszycki,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2017–05251 Filed 3–21–17; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2016–9380; Directorate
Identifier 2016–NE–21–AD
RIN 2120–AA64
Airworthiness Directives; CFE
Company Turbofan Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Proposed rule; withdrawal.
AGENCY:
The FAA is withdrawing a
notice of proposed rulemaking (NPRM).
The NPRM proposed a new
SUMMARY:
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Federal Register / Vol. 82, No. 54 / Wednesday, March 22, 2017 / Proposed Rules
airworthiness directive (AD) for certain
CFE Company (CFE) turbofan engines
that published in the Federal Register
on January 5, 2017. The proposed action
that published in the Federal Register
on January 5, 2017 was a duplicate of
an NPRM, Directorate Identifier 2016–
NE–21–AD, that published in the
Federal Register on January 3, 2017.
Accordingly, we withdraw the proposed
rule that published in the Federal
Register on January 5, 2017.
As of March 22, 2017, the
proposed rule published January 5, 2017
(82 FR 52) is withdrawn.
DATES:
FOR FURTHER INFORMATION CONTACT:
Issued in Burlington, Massachusetts, on
March 8, 2017.
Carlos A. Pestana,
Acting Assistant Manager, Engine & Propeller
Directorate, Aircraft Certification Service.
[FR Doc. 2017–05242 Filed 3–21–17; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF HEALTH AND
HUMAN SERVICES
Food and Drug Administration
21 CFR Part 1132
[Docket No. FDA–2016–N–2527]
Tobacco Product Standard for NNitrosonornicotine Level in Finished
Smokeless Tobacco Products;
Extension of Comment Period
The FAA
proposed to amend 14 CFR part 39 with
a proposed AD (82 FR 1258, January 5,
2017). Since we published the NPRM,
Directorate Identifier 2016–NE–21–AD,
in the Federal Register on January 5,
2017 (82 FR 1258), we discovered that
it was a duplicate of an NPRM,
Directorate Identifier 2016–NE–21–AD,
that published in the Federal Register
on January 3, 2017 (82 FR 52). This
duplication created overlapping
comment periods with different
comment period closing dates, which is
confusing to commenters.
Withdrawal of the NPRM (82 FR 1258,
January 5, 2017) constitutes only such
action, and does not preclude the
agency from issuing another notice in
the future, nor does it commit the
agency to any course of action in the
future.
Since this action only withdraws a
notice of proposed rulemaking, it is
neither a proposed nor a final rule.
Therefore, Executive Order 12866, the
Regulatory Flexibility Act, or DOT
Regulatory Policies and Procedures (44
FR 11034, February 26, 1979) do not
cover this withdrawal.
HHS.
jstallworth on DSK7TPTVN1PROD with PROPOSALS
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Withdrawal
Accordingly, the notice of proposed
rulemaking, Docket No. FAA–2016–
9380; Directorate Identifier 2016–NE–
21–AD, published in the Federal
Register on January 5, 2017 (82 FR
1258), is withdrawn.
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mail/hand delivery/courier (for written/
paper submissions) will be considered
timely if they are postmarked or the
delivery service acceptance receipt is on
or before that date.
ADDRESSES: You may submit comments
as follows:
Electronic Submissions
Martin Adler, Aerospace Engineer,
Engine Certification Office, FAA, 1200
District Avenue, Burlington, MA 01803;
phone: 781–238–7157; fax: 781–238–
7199; email: martin.adler@faa.gov.
SUPPLEMENTARY INFORMATION:
14647
AGENCY:
Food and Drug Administration,
Proposed rule; extension of
comment period.
ACTION:
The Food and Drug
Administration (FDA or the Agency) is
extending the comment period for the
proposed rule that appeared in the
Federal Register of January 23, 2017. In
the proposed rule, FDA requested
comments on its proposal to establish a
limit of N-nitrosonornicotine (NNN) in
finished smokeless tobacco products.
The Agency is taking this action in
response to requests for an extension to
allow interested persons additional time
to submit comments. The Agency is also
providing notice of a typographical error
in a formula in the Laboratory
Information Bulletin (LIB) titled,
‘‘Determination of N-nitrosonornicotine
(NNN) in Smokeless Tobacco and
Tobacco Filler by HPLC–MS/MS’’ (LIB
No. 4620, January 2017). In accordance
with the memorandum of January 20,
2017, from the Assistant to the President
and Chief of Staff, entitled ‘‘Regulatory
Freeze Pending Review’’, the Agency is
also taking this opportunity to provide
notice that, as with all regulatory
actions subject to such memorandum,
this proposed rule is being reviewed
consistent with the memorandum.
DATES: FDA is extending the comment
period on the proposed rule published
January 23, 2017 (82 FR 8004). Submit
either electronic or written comments
by July 10, 2017[. Late, untimely filed
comments will not be considered.
Electronic comments must be submitted
on or before July 10, 2017. The https://
www.regulations.gov electronic filing
system will accept comments until
midnight Eastern Time at the end of
[July 10, 2017. Comments received by
SUMMARY:
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Submit electronic comments in the
following way:
• Federal eRulemaking Portal:
https://www.regulations.gov. Follow the
instructions for submitting comments.
Comments submitted electronically,
including attachments, to https://
www.regulations.gov will be posted to
the docket unchanged. Because your
comment will be made public, you are
solely responsible for ensuring that your
comment does not include any
confidential information that you or a
third party may not wish to be posted,
such as medical information, your or
anyone else’s Social Security number, or
confidential business information, such
as a manufacturing process. Please note
that if you include your name, contact
information, or other information that
identifies you in the body of your
comments, that information will be
posted on https://www.regulations.gov.
• If you want to submit a comment
with confidential information that you
do not wish to be made available to the
public, submit the comment as a
written/paper submission and in the
manner detailed (see ‘‘Written/Paper
Submissions’’ and ‘‘Instructions’’).
Written/Paper Submissions
Submit written/paper submissions as
follows:
• Mail/Hand delivery/Courier (for
written/paper submissions): Division of
Dockets Management (HFA–305), Food
and Drug Administration, 5630 Fishers
Lane, Rm. 1061, Rockville, MD 20852.
• For written/paper comments
submitted to the Division of Dockets
Management, FDA will post your
comment, as well as any attachments,
except for information submitted,
marked and identified, as confidential,
if submitted as detailed in
‘‘Instructions.’’
Instructions: All submissions received
must include the Docket No. FDA–
2016–N–2527 for ‘‘Tobacco Product
Standard for N-nitrosonornicotine Level
in Finished Smokeless Tobacco
Products.’’ Received comments, those
filed in a timely manner (see DATES),
will be placed in the docket and, except
for those submitted as ‘‘Confidential
Submissions,’’ publicly viewable at
https://www.regulations.gov or at the
Division of Dockets Management
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Agencies
[Federal Register Volume 82, Number 54 (Wednesday, March 22, 2017)]
[Proposed Rules]
[Pages 14646-14647]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-05242]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2016-9380; Directorate Identifier 2016-NE-21-AD
RIN 2120-AA64
Airworthiness Directives; CFE Company Turbofan Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Proposed rule; withdrawal.
-----------------------------------------------------------------------
SUMMARY: The FAA is withdrawing a notice of proposed rulemaking (NPRM).
The NPRM proposed a new
[[Page 14647]]
airworthiness directive (AD) for certain CFE Company (CFE) turbofan
engines that published in the Federal Register on January 5, 2017. The
proposed action that published in the Federal Register on January 5,
2017 was a duplicate of an NPRM, Directorate Identifier 2016-NE-21-AD,
that published in the Federal Register on January 3, 2017. Accordingly,
we withdraw the proposed rule that published in the Federal Register on
January 5, 2017.
DATES: As of March 22, 2017, the proposed rule published January 5,
2017 (82 FR 52) is withdrawn.
FOR FURTHER INFORMATION CONTACT: Martin Adler, Aerospace Engineer,
Engine Certification Office, FAA, 1200 District Avenue, Burlington, MA
01803; phone: 781-238-7157; fax: 781-238-7199; email:
martin.adler@faa.gov.
SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39
with a proposed AD (82 FR 1258, January 5, 2017). Since we published
the NPRM, Directorate Identifier 2016-NE-21-AD, in the Federal Register
on January 5, 2017 (82 FR 1258), we discovered that it was a duplicate
of an NPRM, Directorate Identifier 2016-NE-21-AD, that published in the
Federal Register on January 3, 2017 (82 FR 52). This duplication
created overlapping comment periods with different comment period
closing dates, which is confusing to commenters.
Withdrawal of the NPRM (82 FR 1258, January 5, 2017) constitutes
only such action, and does not preclude the agency from issuing another
notice in the future, nor does it commit the agency to any course of
action in the future.
Since this action only withdraws a notice of proposed rulemaking,
it is neither a proposed nor a final rule. Therefore, Executive Order
12866, the Regulatory Flexibility Act, or DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979) do not cover this
withdrawal.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Withdrawal
Accordingly, the notice of proposed rulemaking, Docket No. FAA-
2016-9380; Directorate Identifier 2016-NE-21-AD, published in the
Federal Register on January 5, 2017 (82 FR 1258), is withdrawn.
Issued in Burlington, Massachusetts, on March 8, 2017.
Carlos A. Pestana,
Acting Assistant Manager, Engine & Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 2017-05242 Filed 3-21-17; 8:45 am]
BILLING CODE 4910-13-P