Airworthiness Directives; Leonardo S.p.a. Helicopters, 54124-54126 [2021-21102]
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54124
Proposed Rules
Federal Register
Vol. 86, No. 187
Thursday, September 30, 2021
This section of the FEDERAL REGISTER
contains notices to the public of the proposed
issuance of rules and regulations. The
purpose of these notices is to give interested
persons an opportunity to participate in the
rule making prior to the adoption of the final
rules.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–0834; Project
Identifier MCAI–2021–00298–R]
RIN 2120–AA64
Airworthiness Directives; Leonardo
S.p.a. Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for
certain Leonardo S.p.a. Model A109S
and AW109SP helicopters. This
proposed AD was prompted by the
discovery that rubber protection of
certain electrical wiring had not been
installed in the baggage avionics bay
during production. This proposed AD
would require installing protective
rubber borders on the edge of the
baggage avionics bay frames, 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 November 15,
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–
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
LOTTER on DSK11XQN23PROD with PROPOSALS1
DATES:
VerDate Sep<11>2014
17:59 Sep 29, 2021
Jkt 253001
p.m., Monday through Friday, except
Federal holidays.
For EASA material that is proposed
for IBR in this AD, contact EASA,
Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221
8999 000; email ADs@easa.europa.eu;
internet www.easa.europa.eu. You may
find the EASA material on the EASA
website at https://ad.easa.europa.eu.
For Leonardo Helicopters service
information identified in this NPRM,
contact Leonardo S.p.A. Helicopters,
Emanuele Bufano, Head of
Airworthiness, Viale G.Agusta 520,
21017 C.Costa di Samarate (Va) Italy;
telephone +39–0331–225074; fax +39–
0331–229046; or at https://
customerportal.leonardocompany.com/
en-US/. 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. The EASA material
is also available at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2021–
0834.
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2021–0834; 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, the EASA AD, any comments
received, and other information. The
street address for Docket Operations is
listed above.
FOR FURTHER INFORMATION CONTACT: Hal
Jensen, Aerospace Engineer, Operational
Safety Branch, Compliance &
Airworthiness Division, FAA, 950
L’Enfant Plaza N SW, Washington, DC
20024; telephone (202) 267–9167; email
hal.jensen@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–2021–0834; Project Identifier
MCAI–2021–00298–R’’ at the beginning
of your comments. The most helpful
comments reference a specific portion of
PO 00000
Frm 00001
Fmt 4702
Sfmt 4702
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
information as described in 14 CFR
11.35, the FAA will post all comments
received, without change, to https://
www.regulations.gov, including any
personal information you provide. The
agency will also post a report
summarizing each substantive verbal
contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
(FOIA) (5 U.S.C. 552), CBI is exempt
from public disclosure. If your
comments responsive to this NPRM
contain commercial or financial
information that is customarily treated
as private, that you actually treat as
private, and that is relevant or
responsive to this NPRM, it is important
that you clearly designate the submitted
comments as CBI. Please mark each
page of your submission containing CBI
as ‘‘PROPIN.’’ The FAA will treat such
marked submissions as confidential
under the FOIA, and they will not be
placed in the public docket of this
NPRM. Submissions containing CBI
should be sent to Hal Jensen, Aerospace
Engineer, Operational Safety Branch,
Compliance & Airworthiness Division,
FAA, 950 L’Enfant Plaza N SW,
Washington, DC 20024; telephone (202)
267–9167; email hal.jensen@faa.gov.
Any commentary that the FAA receives
that is not specifically designated as CBI
will be placed in the public docket for
this rulemaking.
Background
EASA, which is the Technical Agent
for the Member States of the European
Union, has issued EASA AD 2021–0065,
dated March 8, 2021 (EASA AD 2021–
0065), to correct an unsafe condition for
certain serial-numbered Leonardo S.p.A.
Helicopters, formerly Finmeccanica
S.p.A., AgustaWestland S.p.A., Agusta
S.p.A., Model A109S and AW109SP
helicopters.
This proposed AD was prompted by
the discovery that rubber protection of
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Federal Register / Vol. 86, No. 187 / Thursday, September 30, 2021 / Proposed Rules
certain electrical wiring had not been
installed in the baggage avionics bay
during production. The FAA is
proposing this AD to prevent chafing of
electrical wiring, which could result in
fire ignition and smoke in the baggage
compartment and subsequent loss of
control of the helicopter. See EASA AD
2021–0065 for additional background
information.
Related Service Information Under 1
CFR Part 51
EASA AD 2021–0065 requires
installing rubber protections on the
electrical wiring in the baggage/avionics
compartment.
This material 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.
Other Related Service Information
The FAA reviewed Leonardo
Helicopters Alert Service Bulletin (ASB)
No. 109S–100, dated February 2, 2021,
for Model A109S helicopters, and
Leonardo Helicopters ASB No. 109SP–
142, also dated February 2, 2021, for
Model AW109SP helicopters. This
service information specifies procedures
for installing protective rubber borders
on the edge of the baggage avionics bay
frames.
FAA’s Determination
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 is
proposing this AD after evaluating all
known relevant information and
determining that the unsafe condition
described previously is likely to exist or
develop on other helicopters of these
same type designs.
LOTTER on DSK11XQN23PROD with PROPOSALS1
Proposed AD Requirements in This
NPRM
This proposed AD would require
accomplishing the actions specified in
EASA AD 2021–0065, described
previously, as incorporated by
reference, except for any differences
identified as exceptions in the
regulatory text of this proposed AD.
Explanation of Required Compliance
Information
In the FAA’s ongoing efforts to
improve the efficiency of the AD
process, the FAA developed a process to
use some civil aviation authority (CAA)
ADs as the primary source of
information for compliance with
VerDate Sep<11>2014
17:59 Sep 29, 2021
Jkt 253001
54125
requirements for corresponding FAA
ADs. The FAA has been coordinating
this process with manufacturers and
CAAs. As a result, the FAA proposes to
incorporate EASA AD 2021–0065 by
reference in the FAA final rule. This
proposed AD would, therefore, require
compliance with EASA AD 2021–0065
in its entirety through that
incorporation, except for any differences
identified as exceptions in the
regulatory text of this proposed AD.
Using common terms that are the same
as the heading of a particular section in
EASA AD 2021–0065 does not mean
that operators need comply only with
that section. For example, where the AD
requirement refers to ‘‘all required
actions and compliance times,’’
compliance with this AD requirement is
not limited to the section titled
‘‘Required Action(s) and Compliance
Time(s)’’ in EASA AD 2021–0065.
Service information referenced in EASA
AD 2021–0065 for compliance will be
available at https://www.regulations.gov
by searching for and locating Docket No.
FAA–2021–0834 after the FAA final
rule is published.
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 products identified in this
rulemaking action.
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 3
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 proposed AD.
Installing protective rubber borders on
the edge of the baggage avionics bay
frames would take about 2 work-hours
and parts would cost about $24 for an
estimated cost of $194 per helicopter
and $582 for the U.S. fleet.
The FAA has included all known
costs in its cost estimate. According to
the manufacturer, however, some of the
costs of this proposed AD may be
covered under warranty, thereby
reducing the cost impact on affected
operators.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
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
PO 00000
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Fmt 4702
Sfmt 4702
Regulatory Findings
The FAA determined that this
proposed AD would not have federalism
implications under Executive Order
13132. This proposed AD would 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
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify this proposed regulation:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Would not affect intrastate
aviation in Alaska, and
(3) Would not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 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:
■
Leonardo S.p.a.: Docket No. FAA–2021–
0834; Project Identifier MCAI–2021–
00298–R.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by November
15, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Leonardo S.p.a. Model
A109S and AW109SP helicopters,
certificated in any category, as identified in
European Union Aviation Safety Agency
(EASA) AD 2021–0065, dated March 8, 2021
(EASA AD 2021–0065).
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Federal Register / Vol. 86, No. 187 / Thursday, September 30, 2021 / Proposed Rules
(d) Subject
Joint Aircraft Service Component (JASC)
Code: 2497, Electrical Power System Wiring.
(e) Unsafe Condition
This AD was prompted by the discovery
that rubber protection of certain electrical
wiring had not been installed in the baggage
avionics bay during production. The FAA is
issuing this AD to prevent chafing of
electrical wiring. The unsafe condition, if not
addressed, could result in fire ignition and
smoke in the baggage compartment and
subsequent loss of control of the helicopter.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
BILLING CODE 4910–13–P
(h) Exceptions to EASA AD 2021–0065
(1) Where EASA AD 2021–0065 requires
compliance in terms of flight hours, this AD
requires using hours time-in-service.
(2) Where EASA AD 2021–0065 refers to its
effective date, this AD requires using the
effective date of this AD.
(3) This AD does not mandate compliance
with the ‘‘Remarks’’ section of EASA AD
2021–0065.
(i) No Reporting Requirement
Although the service information
referenced in EASA AD 2021–0065 specifies
to submit certain information to the
manufacturer, this AD does not include that
requirement.
(j) Special Flight Permit
Special flight permits are prohibited.
LOTTER on DSK11XQN23PROD with PROPOSALS1
(k) 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 (l)(2) 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.
(l) Related Information
(1) For EASA AD 2021–0065, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; internet
www.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.
17:59 Sep 29, 2021
Jkt 253001
Issued on September 23, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021–21102 Filed 9–29–21; 8:45 am]
(g) Requirements
Except as specified in paragraph (h) of this
AD: Comply with all required actions and
compliance times specified in, and in
accordance with, EASA AD 2021–0065.
VerDate Sep<11>2014
For information on the availability of this
material at the FAA, call (817) 222–5110.
This material may be found in the AD docket
at https://www.regulations.gov by searching
for and locating Docket No. FAA–2021–0834.
(2) For more information about this AD,
contact Hal Jensen, Aerospace Engineer,
Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 950 L’Enfant
Plaza N SW, Washington, DC 20024;
telephone (202) 267–9167; email hal.jensen@
faa.gov.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–0838; Project
Identifier AD–2020–01590–A]
RIN 2120–AA64
Airworthiness Directives; Honda
Aircraft Company, LLC Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for
certain Honda Aircraft Company, LLC
(Honda) Model HA–420 airplanes. This
proposed AD was prompted by a report
of in-flight smoke and fire that initiated
from the windshield heat power wire
braid. This proposed AD would require
incorporating temporary revisions into
the airplane flight manual (AFM) and
the quick reference handbook (QRH)
that modify procedures for windshield
heat operation until the affected
windshield assemblies are replaced. The
FAA proposes this AD to address the
unsafe condition on these products.
DATES: The FAA must receive comments
on this proposed AD by November 15,
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–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
SUMMARY:
PO 00000
Frm 00003
Fmt 4702
Sfmt 4702
• Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
For service information identified in
this proposed rule, contact Honda
Aircraft Company, LLC, 6430 Ballinger
Road, Greensboro, NC 27410; phone:
(336) 662–0246; website: https://
www.hondajet.com. You may view this
service information at the FAA,
Airworthiness Products Section,
Operational Safety Branch, 901 Locust,
Kansas City, MO 64106. For information
on the availability of this material at the
FAA, call (816) 329–4148.
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2021–0838; 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.
FOR FURTHER INFORMATION CONTACT:
Bryan Long, Aviation Safety Engineer,
Atlanta ACO Branch, FAA, 1701
Columbia Avenue, College Park, GA
30337; phone: (404) 474–5578; fax: (404)
474–5606; email: bryan.long@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–2021–0838; Project Identifier AD–
2020–01590–A’’ 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
information as described in 14 CFR
11.35, the FAA will post all comments
received, without change, to https://
www.regulations.gov, including any
personal information you provide. The
agency will also post a report
summarizing each substantive verbal
contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
E:\FR\FM\30SEP1.SGM
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Agencies
[Federal Register Volume 86, Number 187 (Thursday, September 30, 2021)]
[Proposed Rules]
[Pages 54124-54126]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-21102]
========================================================================
Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
========================================================================
Federal Register / Vol. 86, No. 187 / Thursday, September 30, 2021 /
Proposed Rules
[[Page 54124]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-0834; Project Identifier MCAI-2021-00298-R]
RIN 2120-AA64
Airworthiness Directives; Leonardo S.p.a. Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Leonardo S.p.a. Model A109S and AW109SP helicopters. This
proposed AD was prompted by the discovery that rubber protection of
certain electrical wiring had not been installed in the baggage
avionics bay during production. This proposed AD would require
installing protective rubber borders on the edge of the baggage
avionics bay frames, 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.
DATES: The FAA must receive comments on this proposed AD by November
15, 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-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 EASA material that is proposed for IBR in this AD, contact
EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221
8999 000; email [email protected]; internet www.easa.europa.eu. You
may find the EASA material on the EASA website at https://ad.easa.europa.eu. For Leonardo Helicopters service information
identified in this NPRM, contact Leonardo S.p.A. Helicopters, Emanuele
Bufano, Head of Airworthiness, Viale G.Agusta 520, 21017 C.Costa di
Samarate (Va) Italy; telephone +39-0331-225074; fax +39-0331-229046; or
at https://customerportal.leonardocompany.com/en-US/. 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. The EASA material is also available at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-
0834.
Examining the AD Docket
You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0834; 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, the EASA AD,
any comments received, and other information. The street address for
Docket Operations is listed above.
FOR FURTHER INFORMATION CONTACT: Hal Jensen, Aerospace Engineer,
Operational Safety Branch, Compliance & Airworthiness Division, FAA,
950 L'Enfant Plaza N SW, Washington, DC 20024; telephone (202) 267-
9167; email [email protected].
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-2021-0834; Project Identifier
MCAI-2021-00298-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 information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
https://www.regulations.gov, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to Hal
Jensen, Aerospace Engineer, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 950 L'Enfant Plaza N SW, Washington, DC
20024; telephone (202) 267-9167; email [email protected]. Any
commentary that the FAA receives that is not specifically designated as
CBI will be placed in the public docket for this rulemaking.
Background
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2021-0065, dated March 8, 2021 (EASA
AD 2021-0065), to correct an unsafe condition for certain serial-
numbered Leonardo S.p.A. Helicopters, formerly Finmeccanica S.p.A.,
AgustaWestland S.p.A., Agusta S.p.A., Model A109S and AW109SP
helicopters.
This proposed AD was prompted by the discovery that rubber
protection of
[[Page 54125]]
certain electrical wiring had not been installed in the baggage
avionics bay during production. The FAA is proposing this AD to prevent
chafing of electrical wiring, which could result in fire ignition and
smoke in the baggage compartment and subsequent loss of control of the
helicopter. See EASA AD 2021-0065 for additional background
information.
Related Service Information Under 1 CFR Part 51
EASA AD 2021-0065 requires installing rubber protections on the
electrical wiring in the baggage/avionics compartment.
This material 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.
Other Related Service Information
The FAA reviewed Leonardo Helicopters Alert Service Bulletin (ASB)
No. 109S-100, dated February 2, 2021, for Model A109S helicopters, and
Leonardo Helicopters ASB No. 109SP-142, also dated February 2, 2021,
for Model AW109SP helicopters. This service information specifies
procedures for installing protective rubber borders on the edge of the
baggage avionics bay frames.
FAA's Determination
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 is proposing this AD
after evaluating all known relevant information and determining that
the unsafe condition described previously is likely to exist or develop
on other helicopters of these same type designs.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in EASA AD 2021-0065, described previously, as incorporated by
reference, except for any differences identified as exceptions in the
regulatory text of this proposed AD.
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some civil aviation
authority (CAA) ADs as the primary source of information for compliance
with requirements for corresponding FAA ADs. The FAA has been
coordinating this process with manufacturers and CAAs. As a result, the
FAA proposes to incorporate EASA AD 2021-0065 by reference in the FAA
final rule. This proposed AD would, therefore, require compliance with
EASA AD 2021-0065 in its entirety through that incorporation, except
for any differences identified as exceptions in the regulatory text of
this proposed AD. Using common terms that are the same as the heading
of a particular section in EASA AD 2021-0065 does not mean that
operators need comply only with that section. For example, where the AD
requirement refers to ``all required actions and compliance times,''
compliance with this AD requirement is not limited to the section
titled ``Required Action(s) and Compliance Time(s)'' in EASA AD 2021-
0065. Service information referenced in EASA AD 2021-0065 for
compliance will be available at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0834 after the FAA final
rule is published.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 3 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 proposed AD.
Installing protective rubber borders on the edge of the baggage
avionics bay frames would take about 2 work-hours and parts would cost
about $24 for an estimated cost of $194 per helicopter and $582 for the
U.S. fleet.
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some of the costs of this
proposed AD may be covered under warranty, thereby reducing the cost
impact on affected operators.
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 products identified in this rulemaking action.
Regulatory Findings
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 responsibilities among the various levels of government.
For the reasons discussed above, I certify this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would 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 Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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:
Leonardo S.p.a.: Docket No. FAA-2021-0834; Project Identifier MCAI-
2021-00298-R.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by November 15, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Leonardo S.p.a. Model A109S and AW109SP
helicopters, certificated in any category, as identified in European
Union Aviation Safety Agency (EASA) AD 2021-0065, dated March 8,
2021 (EASA AD 2021-0065).
[[Page 54126]]
(d) Subject
Joint Aircraft Service Component (JASC) Code: 2497, Electrical
Power System Wiring.
(e) Unsafe Condition
This AD was prompted by the discovery that rubber protection of
certain electrical wiring had not been installed in the baggage
avionics bay during production. The FAA is issuing this AD to
prevent chafing of electrical wiring. The unsafe condition, if not
addressed, could result in fire ignition and smoke in the baggage
compartment and subsequent loss of control of the helicopter.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, EASA AD 2021-0065.
(h) Exceptions to EASA AD 2021-0065
(1) Where EASA AD 2021-0065 requires compliance in terms of
flight hours, this AD requires using hours time-in-service.
(2) Where EASA AD 2021-0065 refers to its effective date, this
AD requires using the effective date of this AD.
(3) This AD does not mandate compliance with the ``Remarks''
section of EASA AD 2021-0065.
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2021-0065
specifies to submit certain information to the manufacturer, this AD
does not include that requirement.
(j) Special Flight Permit
Special flight permits are prohibited.
(k) 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 (l)(2) 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.
(l) Related Information
(1) For EASA AD 2021-0065, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
[email protected]; internet www.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. This material may be found in the AD docket at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2021-0834.
(2) For more information about this AD, contact Hal Jensen,
Aerospace Engineer, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 950 L'Enfant Plaza N SW, Washington, DC
20024; telephone (202) 267-9167; email [email protected].
Issued on September 23, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-21102 Filed 9-29-21; 8:45 am]
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