Airworthiness Directives; Airbus Helicopters Deutschland GmbH, 17329-17330 [2021-06768]
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Federal Register / Vol. 86, No. 62 / Friday, April 2, 2021 / Proposed Rules
the effective date of this AD using RRD Alert
NMSB SB–BR700–72–A900584, Revision 1,
dated October 5, 2017, or original issue,
dated January 31, 2017.
For the purpose of this AD, an affected LLP
is: an LPC disk, LPC fan blade, fan shaft, lowpressure turbine (LPT) stage 1 disk, LPT stage
2 disk, LPT rotor shaft and annulus filler,
high-pressure compressor (HPC) stage 1–6
rotor disk, HPC stage 7–10 rotor disk, curvic
ring, high pressure turbine (HPT) stage 1
disk, and an HPT stage 2 disk.
(j) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, ECO Branch, 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 manager of the certification office,
send it to the attention of the person
identified in Related Information. You may
email your request to: ANE-AD-AMOC@
faa.gov.
(2) 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.
(k) Related Information
(1) For more information about this AD,
contact Wego Wang, Aviation Safety
Engineer, ECO Branch, FAA, 1200 District
Avenue, Burlington, MA 01803; phone: (781)
238–7134; fax: (781) 238–7199; email:
Wego.Wang@faa.gov.
(2) Refer to European Union Aviation
Safety Agency (EASA) AD 2018–0268, dated
December 11, 2018, for more information.
You may examine the EASA AD in the AD
docket at https://www.regulations.gov by
searching for and locating it in Docket No.
FAA–2021–0257.
(3) For service information identified in
this AD, contact Rolls-Royce Deutschland Ltd
& Co KG, Eschenweg 11, Dahlewitz, 15827
Blankenfelde-Mahlow, Germany; phone: +49
(0) 33 7086–4040; website: https://www.rollsroyce.com/contact-us.aspx. You may view
this referenced service information at the
FAA, Airworthiness Products Section,
Operational Safety Branch, 1200 District
Avenue, Burlington, MA 01803. For
information on the availability of this
material at the FAA, call (781) 238–7759.
jbell on DSKJLSW7X2PROD with PROPOSALS
Federal Aviation Administration
14 CFR Part 39
(i) Definition
Issued on March 29, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021–06800 Filed 4–1–21; 8:45 am]
BILLING CODE 4910–13–P
VerDate Sep<11>2014
DEPARTMENT OF TRANSPORTATION
16:28 Apr 01, 2021
Jkt 253001
[Docket No. FAA–2020–0985; Project
Identifier 2018–SW–064–AD]
RIN 2120–AA64
Airworthiness Directives; Airbus
Helicopters Deutschland GmbH
Federal Aviation
Administration (FAA), DOT.
ACTION: Proposed rule; withdrawal.
AGENCY:
The FAA is withdrawing a
notice of proposed rulemaking (NPRM)
that proposed to adopt a new
airworthiness directive (AD) that would
have applied to certain Airbus
Helicopters Deutschland GmbH Model
EC135P1, EC135T1, EC135P2, EC135T2,
EC135P2+, EC135T2+, EC135P3, and
EC135T3 helicopters. The NPRM was
prompted by a deviation from a new
manufacturing process and a
determination that the deviation
resulted in a reduced life limit (service
life limit) for certain tail rotor (TR)
blades. The NPRM would have required
a reduced life limit for those TR blades
and require a new life limit for certain
other TR blades. Since issuance of the
NPRM, the FAA has determined that the
deviation from the new manufacturing
process does not reduce the life limit of
certain TR blades and that a new life
limit is not needed for certain other
blades. Accordingly, the NPRM is
withdrawn.
DATES: As of April 2, 2021, the proposed
rule, which was published in the
Federal Register on November 9, 2020
(85 FR 71286), is withdrawn.
ADDRESSES:
SUMMARY:
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2020–
0985; or in person at Docket Operations
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this AD action,
any comments received, and other
information. The street address for
Docket Operations is 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:
Kristin Bradley, Aerospace Engineer,
General Aviation & Rotorcraft Section,
International Validation Branch,
Compliance & Airworthiness Division,
PO 00000
Frm 00008
Fmt 4702
Sfmt 4702
17329
FAA, 10101 Hillwood Pkwy., Fort
Worth, TX 76177; telephone 817–222–
5110; email Kristin.Bradley@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
The FAA has issued an NPRM that
proposed to amend 14 CFR part 39 by
adding an AD that would apply to the
specified products. The NPRM was
published in the Federal Register on
November 9, 2020 (85 FR 71286). The
NPRM was prompted by a deviation
from a new manufacturing process and
a determination that the deviation
resulted in a reduced life limit (service
life limit) for certain TR blades.
The NPRM proposed to require a
reduced life limit for those TR blades
and require a new life limit for certain
other TR blades.
Actions Since the NPRM was Issued
Since issuance of the NPRM, the FAA
determined that the deviation from the
new manufacturing process does not
reduce the life limit of certain TR blades
and that a new life limit is not needed
for certain other blades. Affected parts
can continue operation until the normal
life limit with no compensation factor
applied to reduce the life of the part.
Therefore, the FAA has determined that
AD action is not appropriate.
Withdrawal of the NPRM constitutes
only such action and does not preclude
the FAA from further rulemaking on
this issue, nor does it commit the FAA
to any course of action in the future.
Comments
The FAA gave the public the
opportunity to comment on the NPRM.
The following presents the comments
received on the NPRM and the FAA’s
response to each comment.
Request To Withdraw NPRM
Airbus Helicopters requested that the
NPRM be withdrawn. The commenter
stated that EASA would be cancelling
EASA AD 2018–0168, dated July 27,
2018, which prompted this NPRM. The
commenter also noted that Airbus
Helicopters service information was
revised to remove the reduced life limit
for the TR blades.
The FAA agrees with the commenter’s
request. Since publication of the NPRM,
EASA has issued EASA AD 2018–
0168R1, dated December 18, 2020
(EASA AD 2018–0168R1). EASA has
determined, and the FAA concurs, that
the deviation in the new manufacturing
process does not affect the life limit of
the TR blades. Airbus Helicopters has
revised the corresponding service
information accordingly. The revised
EASA AD allows continued operation of
E:\FR\FM\02APP1.SGM
02APP1
17330
Federal Register / Vol. 86, No. 62 / Friday, April 2, 2021 / Proposed Rules
the affected parts until the normal life
limit. The FAA has determined that this
NPRM is unnecessary and will
withdraw this NPRM.
List of Subjects in 14 CFR Part 39
Request To Delay Issuance of the AD
The Withdrawal
One commenter requested that the
FAA delay issuance of the final rule
because Airbus Helicopters had revised
its service information to restore the
original life limits of the TR blades, and
based on the revised service information
it would appear that EASA will issue a
revised AD to revise the life limits
accordingly. The commenter asked that
the revised EASA AD be taken into
account in the final rule.
The FAA acknowledges the
commenter’s request. As previously
stated, the FAA has determined that this
NPRM is unnecessary and will
withdraw this NPRM.
■
Request To Include Link To Document
Referenced in the NPRM
One commenter requested that the
FAA provide a link in the NPRM to the
EASA AD that is referred to in the
NPRM. The commenter stated that if it
is the FAA’s new policy to refer to
another Civil Aviation Authority’s AD it
would be more convenient for operators
to have a link instead of having to
search another website.
The FAA acknowledges the
commenter’s request. If the FAA would
have issued a final rule, the EASA AD
would have been incorporated by
reference. The material that is
incorporated by reference in an FAA AD
is available in the AD docket on the
internet at https://www.regulations.gov
by searching for and locating the
applicable AD docket. The AD docket
contains the NPRM, any comments
received, material that is incorporated
by reference, and other information. As
previously stated, the FAA has
determined that this NPRM is
unnecessary and will withdraw this
NPRM.
FAA’s Conclusions
Upon further consideration, the FAA
has determined that the NPRM is
unnecessary. Accordingly, the NPRM is
withdrawn.
jbell on DSKJLSW7X2PROD with PROPOSALS
Regulatory Findings
Since this action only withdraws an
NPRM, it is neither a proposed nor a
final rule. This action therefore is not
covered under Executive Order 12866,
the Regulatory Flexibility Act, or DOT
Regulatory Policies and Procedures (44
FR 11034, February 26, 1979).
VerDate Sep<11>2014
16:28 Apr 01, 2021
Jkt 253001
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Accordingly, the notice of proposed
rulemaking, Docket No. FAA–2020–
0985, which was published in the
Federal Register on November 9, 2020
(85 FR 71286), is withdrawn.
Issued on March 25, 2021.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives,
Compliance & Airworthiness Division,
Aircraft Certification Service.
[FR Doc. 2021–06768 Filed 4–1–21; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–0254; Project
Identifier MCAI–2020–00481–R]
RIN 2120–AA64
Airworthiness Directives; Airbus
Helicopters Deutschland GmbH
Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for all
Airbus Helicopters Deutschland GmbH
Model MBB–BK 117 D–2 helicopters.
This proposed AD was prompted by
reports of chafing marks on the wiring
harness behind the middle side panels
in the area of the front passenger (PAX)
panels. This proposed AD would
require inspecting, modifying, and
rerouting the wiring harness, as
specified in a European Union Aviation
Safety Agency (EASA) AD, which is
proposed for incorporation by reference
(IBR). The FAA is proposing this AD to
address the unsafe condition on these
products.
SUMMARY:
The FAA must receive comments
on this proposed AD by May 17, 2021.
ADDRESSES: You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
DATES:
PO 00000
Frm 00009
Fmt 4702
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30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
• Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
For material that is proposed for IBR
in this AD, contact the EASA, KonradAdenauer-Ufer 3, 50668 Cologne,
Germany; telephone +49 221 8999 000;
email ADs@easa.europa.eu; internet
www.easa.europa.eu. You may find this
material on the EASA website at https://
ad.easa.europa.eu. You may view this
material at the FAA, Office of the
Regional Counsel, Southwest Region,
10101 Hillwood Pkwy., Room 6N–321,
Fort Worth, TX 76177. For information
on the availability of this material at the
FAA, call 817–222–5110. It is also
available in the AD docket on the
internet at https://www.regulations.gov
by searching for and locating Docket No.
FAA–2021–0254.
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2021–
0254; or in person at Docket Operations
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this NPRM, any
comments received, and other
information. The street address for
Docket Operations is listed above.
Comments will be available in the AD
docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT:
Blaine Williams, Aerospace Engineer,
Los Angeles ACO Branch, Compliance &
Airworthiness Division, 3960
Paramount Blvd., Lakewood, California
90712; telephone 562–627–5371; email
blaine.williams@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any
written relevant data, views, or
arguments about this proposal. Send
your comments to an address listed
under ADDRESSES. Include ‘‘Docket No.
FAA–2021–0254; Project Identifier
MCAI–2020–00481–R’’ at the beginning
of your comments. The most helpful
comments reference a specific portion of
the proposal, explain the reason for any
recommended change, and include
supporting data. The FAA will consider
all comments received by the closing
date and may amend this proposal
because of those comments.
Except for Confidential Business
Information (CBI) as described in the
following paragraph, and other
E:\FR\FM\02APP1.SGM
02APP1
Agencies
[Federal Register Volume 86, Number 62 (Friday, April 2, 2021)]
[Proposed Rules]
[Pages 17329-17330]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-06768]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0985; Project Identifier 2018-SW-064-AD]
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters Deutschland GmbH
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Proposed rule; withdrawal.
-----------------------------------------------------------------------
SUMMARY: The FAA is withdrawing a notice of proposed rulemaking (NPRM)
that proposed to adopt a new airworthiness directive (AD) that would
have applied to certain Airbus Helicopters Deutschland GmbH Model
EC135P1, EC135T1, EC135P2, EC135T2, EC135P2+, EC135T2+, EC135P3, and
EC135T3 helicopters. The NPRM was prompted by a deviation from a new
manufacturing process and a determination that the deviation resulted
in a reduced life limit (service life limit) for certain tail rotor
(TR) blades. The NPRM would have required a reduced life limit for
those TR blades and require a new life limit for certain other TR
blades. Since issuance of the NPRM, the FAA has determined that the
deviation from the new manufacturing process does not reduce the life
limit of certain TR blades and that a new life limit is not needed for
certain other blades. Accordingly, the NPRM is withdrawn.
DATES: As of April 2, 2021, the proposed rule, which was published in
the Federal Register on November 9, 2020 (85 FR 71286), is withdrawn.
ADDRESSES:
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-
0985; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this AD action, any comments received, and other information. The
street address for Docket Operations is 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: Kristin Bradley, Aerospace Engineer,
General Aviation & Rotorcraft Section, International Validation Branch,
Compliance & Airworthiness Division, FAA, 10101 Hillwood Pkwy., Fort
Worth, TX 76177; telephone 817-222-5110; email [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
The FAA has issued an NPRM that proposed to amend 14 CFR part 39 by
adding an AD that would apply to the specified products. The NPRM was
published in the Federal Register on November 9, 2020 (85 FR 71286).
The NPRM was prompted by a deviation from a new manufacturing process
and a determination that the deviation resulted in a reduced life limit
(service life limit) for certain TR blades.
The NPRM proposed to require a reduced life limit for those TR
blades and require a new life limit for certain other TR blades.
Actions Since the NPRM was Issued
Since issuance of the NPRM, the FAA determined that the deviation
from the new manufacturing process does not reduce the life limit of
certain TR blades and that a new life limit is not needed for certain
other blades. Affected parts can continue operation until the normal
life limit with no compensation factor applied to reduce the life of
the part. Therefore, the FAA has determined that AD action is not
appropriate.
Withdrawal of the NPRM constitutes only such action and does not
preclude the FAA from further rulemaking on this issue, nor does it
commit the FAA to any course of action in the future.
Comments
The FAA gave the public the opportunity to comment on the NPRM. The
following presents the comments received on the NPRM and the FAA's
response to each comment.
Request To Withdraw NPRM
Airbus Helicopters requested that the NPRM be withdrawn. The
commenter stated that EASA would be cancelling EASA AD 2018-0168, dated
July 27, 2018, which prompted this NPRM. The commenter also noted that
Airbus Helicopters service information was revised to remove the
reduced life limit for the TR blades.
The FAA agrees with the commenter's request. Since publication of
the NPRM, EASA has issued EASA AD 2018-0168R1, dated December 18, 2020
(EASA AD 2018-0168R1). EASA has determined, and the FAA concurs, that
the deviation in the new manufacturing process does not affect the life
limit of the TR blades. Airbus Helicopters has revised the
corresponding service information accordingly. The revised EASA AD
allows continued operation of
[[Page 17330]]
the affected parts until the normal life limit. The FAA has determined
that this NPRM is unnecessary and will withdraw this NPRM.
Request To Delay Issuance of the AD
One commenter requested that the FAA delay issuance of the final
rule because Airbus Helicopters had revised its service information to
restore the original life limits of the TR blades, and based on the
revised service information it would appear that EASA will issue a
revised AD to revise the life limits accordingly. The commenter asked
that the revised EASA AD be taken into account in the final rule.
The FAA acknowledges the commenter's request. As previously stated,
the FAA has determined that this NPRM is unnecessary and will withdraw
this NPRM.
Request To Include Link To Document Referenced in the NPRM
One commenter requested that the FAA provide a link in the NPRM to
the EASA AD that is referred to in the NPRM. The commenter stated that
if it is the FAA's new policy to refer to another Civil Aviation
Authority's AD it would be more convenient for operators to have a link
instead of having to search another website.
The FAA acknowledges the commenter's request. If the FAA would have
issued a final rule, the EASA AD would have been incorporated by
reference. The material that is incorporated by reference in an FAA AD
is available in the AD docket on the internet at https://www.regulations.gov by searching for and locating the applicable AD
docket. The AD docket contains the NPRM, any comments received,
material that is incorporated by reference, and other information. As
previously stated, the FAA has determined that this NPRM is unnecessary
and will withdraw this NPRM.
FAA's Conclusions
Upon further consideration, the FAA has determined that the NPRM is
unnecessary. Accordingly, the NPRM is withdrawn.
Regulatory Findings
Since this action only withdraws an NPRM, it is neither a proposed
nor a final rule. This action therefore is not covered under Executive
Order 12866, the Regulatory Flexibility Act, or DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979).
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Withdrawal
0
Accordingly, the notice of proposed rulemaking, Docket No. FAA-2020-
0985, which was published in the Federal Register on November 9, 2020
(85 FR 71286), is withdrawn.
Issued on March 25, 2021.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021-06768 Filed 4-1-21; 8:45 am]
BILLING CODE 4910-13-P