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PROPOSED AD AIRBUS HELICOPTERS DEUTSCHLAND GMBH: [Docket No. FAA-2020-0985; Project Identifier 2018-SW-064-AD] RIN 2120-AA64
THE WITHDRAWAL

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71286), is withdrawn.

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Federal Register on November 9, 2020 (85 FR 71286), is withdrawn.
PREAMBLE 

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.

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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 Accordingly, the NPRM is withdrawn.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the Federal Register on November 9, 2020 (85 FR 71286), is withdrawn.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 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
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


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.