Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters, 35599-35601 [2021-14343]
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Federal Register / Vol. 86, No. 127 / Wednesday, July 7, 2021 / Rules and Regulations
consumer. Moreover, proper handling of
disputes not only ensures that
inaccuracies in the disputing
consumer’s report are resolved, it also
facilitates CRA and furnisher
identification of systemic problems
related to their consumer reporting and
furnishing practices.54
II. Compliance Guidance
As pandemic-related government
interventions aimed at protecting
renters begin to expire, the Bureau will
continue to look carefully at consumer
reporting agencies’ and furnishers’
compliance with their FCRA accuracy
obligations with respect to rental
information. CRAs and furnishers
should take immediate steps to ensure
they are fulfilling their obligations
under the law. If the Bureau determines
that a CRA or furnisher has engaged in
any acts or practices that violate the
FCRA, Regulation V, or other Federal
consumer financial laws, the Bureau
will take appropriate enforcement
action to address violations and seek all
appropriate corrective measures,
including remediation of harm to
consumers.
The Bureau plans to pay particular
attention to the areas outlined below.
khammond on DSKJM1Z7X2PROD with RULES
For CRAs Reporting Rental Information
1. Whether CRAs are reporting
accurate rental information.
2. Whether CRAs are using a
sufficient number of identifiers to match
consumer report information to the
consumer who is the subject of the
report, including whether CRAs are
using name-matching procedures or
limited identifiers likely to heighten the
risk of inaccurate matching.
3. Whether CRAs are reporting
eviction information that is inaccurate,
incomplete, or misleading (such as may
result from a failure to have reasonable
procedures to report information about
the disposition of an eviction filing, to
prevent the inclusion of multiple entries
for the same eviction action in the same
consumer report, or to prevent the
inclusion of eviction information that
has been sealed or expunged).
4. Whether CRAs are complying with
their obligations to investigate disputed
54 See, e.g., Fed. Trade Comm’n, 40 Years of
Experience with the Fair Credit Reporting Act: An
FTC Staff Report with Summary of Interpretations
67 (July 2011), https://www.ftc.gov/sites/default/
files/documents/reports/40-years-experience-faircredit-reporting-act-ftc-staff-report-summaryinterpretations/110720fcrareport.pdf (noting that
‘‘when a CRA learns or should reasonably be aware
of errors in its reports that may indicate systematic
problems (by virtue of information from consumers,
report users, from periodic review of its reporting
system, or otherwise), it must review its procedures
for assuring accuracy and take any necessary steps
to avoid future problems’’).
VerDate Sep<11>2014
15:58 Jul 06, 2021
Jkt 253001
information in a consumer report,
including whether they are conducting
timely and reasonable investigations.
For Furnishers Providing Rental
Information
1. Whether furnishers are providing
accurate rental information to CRAs.
2. Whether furnishers are providing
information about rental arrearages that
include amounts that were already paid
on behalf of a tenant through a
government grant or relief program,
such as the Emergency Rental
Assistance programs.
3. Whether furnishers are providing
information about rental arrearages that
include fees or penalties that CARES
Act section 4024(b) or other laws
prohibit charging.
4. Whether furnishers are complying
with their obligations to investigate
disputed information in a consumer
report, including whether they are
conducting timely and reasonable
investigations.
III. Conclusion
The Bureau issues this Bulletin to
highlight that the Bureau will hold
CRAs and furnishers accountable if they
do not comply with their accuracy and
dispute obligations under the FCRA and
Regulation V with respect to rental
information.
IV. Regulatory Requirements
This Bulletin constitutes a general
statement of policy exempt from the
notice and comment rulemaking
requirements of the Administrative
Procedure Act.55 It summarizes existing
legal requirements and articulates
considerations relevant to the Bureau’s
exercise of its enforcement discretion
for institutions under its jurisdiction. It
does not impose any legal requirements
on external parties, nor does it create or
confer any substantive rights on external
parties that could be enforceable in any
administrative or civil proceeding.
Because no notice of proposed
rulemaking is required in issuing this
Bulletin, the Regulatory Flexibility Act
also does not require an initial or final
regulatory flexibility analysis.56 The
Bureau has also determined that the
issuance of this Bulletin does not
impose any new or revise any existing
recordkeeping, reporting, or disclosure
requirements on covered entities or
members of the public that would be
collections of information requiring
approval by the Office of Management
PO 00000
55 5
56 5
U.S.C. 553(b).
U.S.C. 603(a), 604(a).
Frm 00005
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35599
and Budget under the Paperwork
Reduction Act of 1995.57
Dated: July 1, 2021.
David Uejio,
Acting Director, Bureau of Consumer
Financial Protection.
[FR Doc. 2021–14459 Filed 7–6–21; 8:45 am]
BILLING CODE 4810–AM–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2019–0293; Product
Identifier 2017–SW–052–AD; Amendment
39–21610; AD 2021–13–05]
RIN 2120–AA64
Airworthiness Directives; Airbus
Helicopters Deutschland GmbH
Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for Airbus
Helicopters Deutschland GmbH (Airbus
Helicopters) Model EC135P1, EC135P2,
EC135P2+, EC135P3, EC135T1,
EC135T2, EC135T2+, and EC135T3
helicopters. This AD requires modifying
the tail rotor (T/R) control installation,
a functional test, and corrective actions
as necessary. This AD was prompted by
cases of insufficient clearance between
a certain T/R control bearing connection
and the helicopter structure, which
were detected on the production line.
The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective August 11,
2021.
The Director of the Federal Register
approved the incorporation by reference
of a certain document listed in this AD
as of August 11, 2021.
ADDRESSES: For service information
identified in this final rule, contact
Airbus Helicopters, 2701 North Forum
Drive, Grand Prairie, TX 75052;
telephone 972–641–0000 or 800–232–
0323; fax 972–641–3775; or at https://
www.airbus.com/helicopters/services/
technical-support.html. You may view
the referenced service information at the
FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood
Pkwy., Room 6N–321, Fort Worth, TX
76177. Service information that is
incorporated by reference is also
available at https://www.regulations.gov
SUMMARY:
57 44
E:\FR\FM\07JYR1.SGM
U.S.C. 3501 et seq.
07JYR1
35600
Federal Register / Vol. 86, No. 127 / Wednesday, July 7, 2021 / Rules and Regulations
by searching for and locating Docket No.
FAA–2019–0293.
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2019–0293; 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
final rule, the European Aviation Safety
Agency (now European Union Aviation
Safety Agency) (EASA) AD, 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:
David Hatfield, Aviation Safety
Engineer, Aircraft Systems Section,
Technical Innovation Policy Branch,
FAA, 10101 Hillwood Pkwy., Fort
Worth, TX 76177; telephone 817–222–
5110; email david.hatfield@faa.gov.
SUPPLEMENTARY INFORMATION:
khammond on DSKJM1Z7X2PROD with RULES
Background
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to Airbus Helicopters Model
EC135P1, EC135P2, EC135P2+,
EC135P3, EC135T1, EC135T2,
EC135T2+, and EC135T3 helicopters
with serial number (S/N) up to and
including 1254 (except S/N 1235). The
NPRM published in the Federal
Register on April 16, 2021 (86 FR
20089). In the NPRM, the FAA proposed
to require modifying the T/R control
within 360 hours time-in-service (TIS)
by installing a Teflon washer and
performing a functional test in
accordance with specified portions of
Airbus Helicopters Alert Service
Bulletin ASB EC135–67A–031, Revision
0, dated March 30, 2017 (ASB EC135–
67A–031). Based on the results of the
functional test, the NPRM proposed to
require making repairs in accordance
with FAA-approved procedures. The
NPRM was prompted by EASA AD
2017–0147, dated August 10, 2017
(EASA AD 2017–0147), issued by
EASA, which is the Technical Agent for
the Member States of the European
Union, to correct an unsafe condition
for Airbus Helicopters Model EC135P1,
EC135P2, EC135P2+, EC135P3,
EC135T1, EC135T2, EC135T2+,
EC135T3, EC635P2+, EC635P3,
EC635T1, EC635T2+, and EC635T3
helicopters. EASA advises that several
cases of insufficient clearance between
VerDate Sep<11>2014
15:58 Jul 06, 2021
Jkt 253001
a certain T/R bearing connection and
the helicopter structure were detected
during inspections of helicopters on the
production line. EASA states that this
condition, if not corrected and in the
case of an unglued bearing, could lead
to blockage of the pedal controlling the
T/R thrust and loss of the T/R control.
EASA further advises that this could
result in a forced landing with damage
to the helicopter and injury to the
occupants.
Accordingly, EASA AD 2017–0147
requires modifying the T/R control
installation by adding a Teflon washer,
which reduces the degree of freedom in
case of a drifting bearing at the affected
connection. EASA AD 2017–0147 also
requires a functional test for clearance,
and depending on the results, either
accomplishing additional corrective
actions or contacting Airbus Helicopters
for instructions.
Comments
The FAA received no comments on
the NPRM or on the determination of
the costs.
Conclusion
These helicopters have been approved
by EASA and are approved for operation
in the United States. Pursuant to the
FAA’s bilateral agreement with the
European Union, EASA has notified the
FAA about the unsafe condition
described in its AD. The FAA reviewed
the relevant data and determined that
air safety requires adopting this AD as
proposed. Accordingly, the FAA is
issuing this AD to address the unsafe
condition on these helicopters.
Related Service Information Under 1
CFR Part 51
The FAA reviewed ASB EC135–67A–
031 for Airbus Helicopters Model
EC135P1, EC135P2, EC135P2+,
EC135P3, EC135T1, EC135T2,
EC135T2+, EC135T3, EC635P2+,
EC635P3, EC635T1, EC635T2+, and
EC635T3 helicopters. For S/Ns up to
1254 inclusive, except S/N 1235, this
service information specifies retrofitting
a Teflon washer on the T/R controls,
performing a functional test of the
modified T/R control installation to
inspect for clearance, and making any
necessary adjustments. This service
information advises that S/N 1255 and
up will have the Teflon washer installed
in production.
This service information is reasonably
available because the interested parties
have access to it through their normal
course of business or by the means
identified in the ADDRESSES section.
PO 00000
Frm 00006
Fmt 4700
Sfmt 4700
Differences Between This AD and the
EASA AD
The EASA AD sets compliance times
at 12 months, while this AD requires
compliance within 360 hours TIS. The
EASA AD applies to Airbus Helicopters
Model EC635T1, EC635T2+, EC635T3,
EC635P2+, and EC635P3 helicopters;
this AD does not because these models
do not have an FAA type certificate. The
EASA AD requires contacting Airbus
Helicopters for approved repair
procedures; this AD requires a repair
using FAA-approved procedures. The
EASA AD requires revising the ‘‘aircraft
maintenance program,’’ whereas this AD
does not because not all U.S. operators
are required to have a maintenance
program.
Costs of Compliance
The FAA estimates that this AD
affects 331 helicopters of U.S. registry.
Labor rates are estimated at $85 per
work-hour. Based on these numbers, the
FAA estimates the following costs to
comply with this AD.
Modifying the T/R control installation
and conducting a functional test takes
about 3 work-hours and parts cost about
$25 for an estimated cost of $280 per
helicopter and $92,680 for the U.S. fleet.
If required, adjusting the clearance
takes about 1 work-hour for an
estimated cost of $85 per helicopter.
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII:
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
The FAA is issuing this rulemaking
under the authority described in
Subtitle VII, Part A, Subpart III, Section
44701: General requirements. Under
that section, Congress charges the FAA
with promoting safe flight of civil
aircraft in air commerce by prescribing
regulations for practices, methods, and
procedures the Administrator finds
necessary for safety in air commerce.
This regulation is within the scope of
that authority because it addresses an
unsafe condition that is likely to exist or
develop on helicopters identified in this
rulemaking action.
Regulatory Findings
This AD will not have federalism
implications under Executive Order
13132. This AD will not have a
substantial direct effect on the States, on
the relationship between the national
government and the States, or on the
distribution of power and
E:\FR\FM\07JYR1.SGM
07JYR1
Federal Register / Vol. 86, No. 127 / Wednesday, July 7, 2021 / Rules and Regulations
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Will not affect intrastate aviation
in Alaska, and
(3) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
2021–13–05 Airbus Helicopters
Deutschland GmbH: Amendment 39–
21610; Docket No. FAA–2019–0293;
Product Identifier 2017–SW–052–AD.
(a) Effective Date
This airworthiness directive (AD) is
effective August 11, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Helicopters
Deutschland GmbH Model EC135P1,
EC135P2, EC135P2+, EC135P3, EC135T1,
EC135T2, EC135T2+, and EC135T3
helicopters with serial number (S/N) up to
and including 1254 (except S/N 1235),
certificated in any category.
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(d) Subject
Joint Aircraft Service Component (JASC)
Code: 6720, Tail Rotor Control System.
(e) Unsafe Condition
This AD defines the unsafe condition as
interference between the tail rotor (T/R)
control bearing connection close-tolerance
bolt and the helicopter structure, which
could lead to blockage of the pedal
controlling the T/R thrust. This condition
could result in loss of T/R control, prompting
a forced landing.
VerDate Sep<11>2014
15:58 Jul 06, 2021
Jkt 253001
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
Within 360 hours time-in-service, modify
the T/R control by installing a Teflon washer
and perform a functional test of the
modification in accordance with the
Accomplishment Instructions, paragraphs
3.B.2 through 3.B.4.2., of Airbus Helicopters
Alert Service Bulletin ASB EC135–67A–031,
Revision 0, dated March 30, 2017. If, during
the functional test, the clearance between the
end of the close-tolerance bolt, castellated
nut, and the lower stringer is less than 1.0
mm, repair in accordance with FAAapproved procedures.
(h) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, International Validation
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 International Validation
Branch, send it to the attention of the person
identified in paragraph (i)(1) of this AD.
Information may be emailed to: 9-AVS-AIR730-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.
(i) Related Information
(1) For more information about this AD,
contact David Hatfield, Aviation Safety
Engineer, Aircraft Systems Section,
Technical Innovation Policy Branch, FAA,
10101 Hillwood Pkwy., Fort Worth, TX
76177; telephone 817–222–5110; email
david.hatfield@faa.gov.
(2) The subject of this AD is addressed in
European Aviation Safety Agency (now
European Union Aviation Safety Agency)
(EASA) AD 2017–0147, dated August 10,
2017. You may view the EASA AD at https://
www.regulations.gov in Docket No. FAA–
2019–0293.
(j) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference of
the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless the AD specifies otherwise.
(i) Airbus Helicopters Alert Service
Bulletin ASB EC135–67A–031, Revision 0,
dated March 30, 2017.
(ii) [Reserved]
(3) For Airbus Helicopters service
information identified in this AD, contact
Airbus Helicopters, 2701 North Forum Drive,
Grand Prairie, TX 75052; telephone 972–641–
0000 or 800–232–0323; fax 972–641–3775; or
at https://www.airbus.com/helicopters/
services/technical-support.html.
PO 00000
Frm 00007
Fmt 4700
Sfmt 4700
35601
(4) You may view this service information
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.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
email: fedreg.legal@nara.gov, or go to:
https://www.archives.gov/federal-register/cfr/
ibr-locations.html.
Issued on June 10, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021–14343 Filed 7–6–21; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–0333; Project
Identifier MCAI–2020–00252–R; Amendment
39–21609; AD 2021–13–04]
RIN 2120–AA64
Airworthiness Directives; Airbus
Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
Airbus Helicopters Model AS332C,
AS332C1, AS332L, and AS332L1
helicopters. This AD was prompted by
a report of a yaw control failure that was
the result of the disconnection of the tail
rotor hub (TRH) pitch control rod from
the tail rotor servo-control, which
resulted from a seized TRH bearing. The
TRH bearing had grease dissolving after
contamination by leaked hydraulic fluid
from the tail rotor servo-control that
came through the TRH assembly boot.
This AD requires repetitive inspections
for hydraulic leaks, corrective actions if
necessary, and an optional modification
which constitutes terminating action, as
specified in a European Union Aviation
Safety Agency (EASA) AD, which is
incorporated by reference. The FAA is
issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective August 11,
2021.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of August 11, 2021.
ADDRESSES: For material incorporated
by reference (IBR) in this AD, contact
SUMMARY:
E:\FR\FM\07JYR1.SGM
07JYR1
Agencies
[Federal Register Volume 86, Number 127 (Wednesday, July 7, 2021)]
[Rules and Regulations]
[Pages 35599-35601]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-14343]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0293; Product Identifier 2017-SW-052-AD; Amendment
39-21610; AD 2021-13-05]
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters Deutschland GmbH
Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model EC135P1,
EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, and EC135T3
helicopters. This AD requires modifying the tail rotor (T/R) control
installation, a functional test, and corrective actions as necessary.
This AD was prompted by cases of insufficient clearance between a
certain T/R control bearing connection and the helicopter structure,
which were detected on the production line. The FAA is issuing this AD
to address the unsafe condition on these products.
DATES: This AD is effective August 11, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain document listed in this AD as of August 11,
2021.
ADDRESSES: For service information identified in this final rule,
contact Airbus Helicopters, 2701 North Forum Drive, Grand Prairie, TX
75052; telephone 972-641-0000 or 800-232-0323; fax 972-641-3775; or at
https://www.airbus.com/helicopters/services/technical-support.html. You
may view the referenced service information at the FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321,
Fort Worth, TX 76177. Service information that is incorporated by
reference is also available at https://www.regulations.gov
[[Page 35600]]
by searching for and locating Docket No. FAA-2019-0293.
Examining the AD Docket
You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2019-0293; 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 final rule, the
European Aviation Safety Agency (now European Union Aviation Safety
Agency) (EASA) AD, 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: David Hatfield, Aviation Safety
Engineer, Aircraft Systems Section, Technical Innovation Policy Branch,
FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-
5110; email [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to Airbus Helicopters
Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+,
and EC135T3 helicopters with serial number (S/N) up to and including
1254 (except S/N 1235). The NPRM published in the Federal Register on
April 16, 2021 (86 FR 20089). In the NPRM, the FAA proposed to require
modifying the T/R control within 360 hours time-in-service (TIS) by
installing a Teflon washer and performing a functional test in
accordance with specified portions of Airbus Helicopters Alert Service
Bulletin ASB EC135-67A-031, Revision 0, dated March 30, 2017 (ASB
EC135-67A-031). Based on the results of the functional test, the NPRM
proposed to require making repairs in accordance with FAA-approved
procedures. The NPRM was prompted by EASA AD 2017-0147, dated August
10, 2017 (EASA AD 2017-0147), issued by EASA, which is the Technical
Agent for the Member States of the European Union, to correct an unsafe
condition for Airbus Helicopters Model EC135P1, EC135P2, EC135P2+,
EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, EC635P2+, EC635P3,
EC635T1, EC635T2+, and EC635T3 helicopters. EASA advises that several
cases of insufficient clearance between a certain T/R bearing
connection and the helicopter structure were detected during
inspections of helicopters on the production line. EASA states that
this condition, if not corrected and in the case of an unglued bearing,
could lead to blockage of the pedal controlling the T/R thrust and loss
of the T/R control. EASA further advises that this could result in a
forced landing with damage to the helicopter and injury to the
occupants.
Accordingly, EASA AD 2017-0147 requires modifying the T/R control
installation by adding a Teflon washer, which reduces the degree of
freedom in case of a drifting bearing at the affected connection. EASA
AD 2017-0147 also requires a functional test for clearance, and
depending on the results, either accomplishing additional corrective
actions or contacting Airbus Helicopters for instructions.
Comments
The FAA received no comments on the NPRM or on the determination of
the costs.
Conclusion
These helicopters have been approved by EASA and are approved for
operation in the United States. Pursuant to the FAA's bilateral
agreement with the European Union, EASA has notified the FAA about the
unsafe condition described in its AD. The FAA reviewed the relevant
data and determined that air safety requires adopting this AD as
proposed. Accordingly, the FAA is issuing this AD to address the unsafe
condition on these helicopters.
Related Service Information Under 1 CFR Part 51
The FAA reviewed ASB EC135-67A-031 for Airbus Helicopters Model
EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+,
EC135T3, EC635P2+, EC635P3, EC635T1, EC635T2+, and EC635T3 helicopters.
For S/Ns up to 1254 inclusive, except S/N 1235, this service
information specifies retrofitting a Teflon washer on the T/R controls,
performing a functional test of the modified T/R control installation
to inspect for clearance, and making any necessary adjustments. This
service information advises that S/N 1255 and up will have the Teflon
washer installed in production.
This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.
Differences Between This AD and the EASA AD
The EASA AD sets compliance times at 12 months, while this AD
requires compliance within 360 hours TIS. The EASA AD applies to Airbus
Helicopters Model EC635T1, EC635T2+, EC635T3, EC635P2+, and EC635P3
helicopters; this AD does not because these models do not have an FAA
type certificate. The EASA AD requires contacting Airbus Helicopters
for approved repair procedures; this AD requires a repair using FAA-
approved procedures. The EASA AD requires revising the ``aircraft
maintenance program,'' whereas this AD does not because not all U.S.
operators are required to have a maintenance program.
Costs of Compliance
The FAA estimates that this AD affects 331 helicopters of U.S.
registry. Labor rates are estimated at $85 per work-hour. Based on
these numbers, the FAA estimates the following costs to comply with
this AD.
Modifying the T/R control installation and conducting a functional
test takes about 3 work-hours and parts cost about $25 for an estimated
cost of $280 per helicopter and $92,680 for the U.S. fleet.
If required, adjusting the clearance takes about 1 work-hour for an
estimated cost of $85 per helicopter.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on helicopters identified in this rulemaking action.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and
[[Page 35601]]
responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2021-13-05 Airbus Helicopters Deutschland GmbH: Amendment 39-21610;
Docket No. FAA-2019-0293; Product Identifier 2017-SW-052-AD.
(a) Effective Date
This airworthiness directive (AD) is effective August 11, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Helicopters Deutschland GmbH Model
EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, and
EC135T3 helicopters with serial number (S/N) up to and including
1254 (except S/N 1235), certificated in any category.
(d) Subject
Joint Aircraft Service Component (JASC) Code: 6720, Tail Rotor
Control System.
(e) Unsafe Condition
This AD defines the unsafe condition as interference between the
tail rotor (T/R) control bearing connection close-tolerance bolt and
the helicopter structure, which could lead to blockage of the pedal
controlling the T/R thrust. This condition could result in loss of
T/R control, prompting a forced landing.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Within 360 hours time-in-service, modify the T/R control by
installing a Teflon washer and perform a functional test of the
modification in accordance with the Accomplishment Instructions,
paragraphs 3.B.2 through 3.B.4.2., of Airbus Helicopters Alert
Service Bulletin ASB EC135-67A-031, Revision 0, dated March 30,
2017. If, during the functional test, the clearance between the end
of the close[hyphen]tolerance bolt, castellated nut, and the lower
stringer is less than 1.0 mm, repair in accordance with FAA-approved
procedures.
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, International Validation 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 International Validation Branch, send
it to the attention of the person identified in paragraph (i)(1) of
this AD. Information may be emailed to: [email protected].
(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.
(i) Related Information
(1) For more information about this AD, contact David Hatfield,
Aviation Safety Engineer, Aircraft Systems Section, Technical
Innovation Policy Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX
76177; telephone 817-222-5110; email [email protected].
(2) The subject of this AD is addressed in European Aviation
Safety Agency (now European Union Aviation Safety Agency) (EASA) AD
2017-0147, dated August 10, 2017. You may view the EASA AD at
https://www.regulations.gov in Docket No. FAA-2019-0293.
(j) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
(i) Airbus Helicopters Alert Service Bulletin ASB EC135-67A-031,
Revision 0, dated March 30, 2017.
(ii) [Reserved]
(3) For Airbus Helicopters service information identified in
this AD, contact Airbus Helicopters, 2701 North Forum Drive, Grand
Prairie, TX 75052; telephone 972-641-0000 or 800-232-0323; fax 972-
641-3775; or at https://www.airbus.com/helicopters/services/technical-support.html.
(4) You may view this service information 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.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, email: [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on June 10, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-14343 Filed 7-6-21; 8:45 am]
BILLING CODE 4910-13-P