Airworthiness Directives; Leonardo S.p.a. Helicopters, 35690-35692 [2021-14401]
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35690
Federal Register / Vol. 86, No. 127 / Wednesday, July 7, 2021 / Proposed Rules
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–0505; Project
Identifier 2018–SW–004–AD]
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 AB139
and AW139 helicopters. This proposed
AD was prompted by reports of spurious
in-flight disconnections of the automatic
flight control system (AFCS). This
proposed AD would require updating
certain ‘‘Primus Epic’’ system software,
as specified in a European Aviation
Safety Agency (now 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 August 23,
2021.
SUMMARY:
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 ADs@easa.europa.eu;
internet www.easa.europa.eu. You may
find this IBR material on the EASA
website at https://ad.easa.europa.eu.
You may view EASA 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 EASA material at the
FAA, call (817) 222–5110. The EASA
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ADDRESSES:
VerDate Sep<11>2014
16:33 Jul 06, 2021
Jkt 253001
material is also available at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2021–
0505.
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2021–0505; 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–2021–0505; Project Identifier
2018–SW–004–AD’’ 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
PO 00000
Frm 00031
Fmt 4702
Sfmt 4702
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 2018–0002,
dated January 4, 2018 (EASA AD 2018–
0002), to correct an unsafe condition for
certain Leonardo S.p.a. Model AB139
and AW139 helicopters.
This proposed AD was prompted by
reports of spurious in-flight
disconnections of the AFCS. The
investigation revealed that these AFCS
disconnect events relate to uncommanded single channel autopilot
disengagement for most of the cases,
and to some instances of untimely dual
channel autopilot disengagement. The
disconnections occurred in random
flight conditions and appeared to be
temporary disruptions of the AFCS’ full
availability because all functionalities
could be restored by re-engaging the
complete system through the AFCS
control panel. The FAA is proposing
this AD to address spurious degradation
or unavailability of the full availability
of the AFCS. The unsafe condition, if
not addressed, could result in temporary
impairment of the automated flight aid
for control of the helicopter and
increase the flightcrew’s workload. See
EASA AD 2018–0002 for additional
background information.
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.
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Federal Register / Vol. 86, No. 127 / Wednesday, July 7, 2021 / Proposed Rules
Related Service Information Under 1
CFR Part 51
identified as exceptions in the
regulatory text of this proposed AD.
EASA AD 2018–0002 requires
installation of certain ‘‘Primus Epic’’
system software, depending on the
helicopter configuration. EASA AD
2018–0002 allows installation of
‘‘Primus Epic’’ system software on a
helicopter after that helicopter has had
the software upgrade installed.
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.
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 certain 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, EASA AD 2018–0002
will be incorporated by reference in the
FAA final rule. This proposed AD
would, therefore, require compliance
with EASA AD 2018–0002 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
Proposed AD Requirements in This
NPRM
This proposed AD would require
accomplishing the actions specified in
EASA AD 2018–0002, described
previously, as incorporated by
reference, except for any differences
35691
particular section in EASA AD 2018–
0002 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
2018–0002. Service information
specified in EASA AD 2018–0002 that is
required for compliance with it will be
available at https://www.regulations.gov
by searching for and locating Docket No.
FAA–2021–0505 after the FAA final
rule is published.
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 128
helicopters of U.S. registry. The FAA
estimates the following costs to comply
with this proposed AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Action
Labor cost
Software upgrade ............................................
24 work-hours × $85 per hour = $2,040 ........
The FAA has included all known
costs in its cost estimate. According to
the manufacturer, however, some or all
of the costs of this proposed AD may be
covered under warranty, thereby
reducing the cost impact on affected
operators.
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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
VerDate Sep<11>2014
16:33 Jul 06, 2021
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
1. The authority citation for part 39
continues to read as follows:
■
The FAA determined that this
proposed AD would not have federalism
Jkt 253001
PO 00000
Authority: 49 U.S.C. 106(g), 40113, 44701.
Frm 00032
Fmt 4702
Sfmt 4702
Cost per
product
Parts cost
$0
§ 39.13
$2,040
Cost on U.S.
operators
$261,120
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
Leonardo S.p.a.: Docket No. FAA–2021–
0505; Project Identifier 2018–SW–004–
AD.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by August 23,
2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Leonardo S.p.a. Model
AB139 and AW139 helicopters, certificated
in any category, identified in paragraphs
(c)(1) and (2) of this AD, equipped with
‘‘Primus Epic’’ system software release 7.4
(Phase 7 V1), 7.7 (Phase 7 V3) or 7.10 (Phase
7 V4).
(1) Model AB139 and AW19 helicopters
having serial number (S/N) 31005, 31006,
and S/Ns 31008 through 31157 inclusive; and
S/Ns 41001 through 41023 inclusive.
(2) Model AW139 helicopters having S/N
31201 and subsequent, and S/N 41201 and
subsequent.
(d) Subject
Joint Aircraft Service Component (JASC)
Code: 2200, Auto Flight System.
(e) Unsafe Condition
This AD was prompted by reports of
spurious in-flight disconnections of the
automatic flight control system (AFCS). The
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07JYP1
35692
Federal Register / Vol. 86, No. 127 / Wednesday, July 7, 2021 / Proposed Rules
FAA is issuing this AD to address spurious
degradation or unavailability of the full
AFCS. The unsafe condition, if not
addressed, could result in temporary
impairment of the automated flight aid for
control of the helicopter and increase the
flightcrew’s workload.
(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, European Aviation Safety
Agency (now European Union Aviation
Safety Agency) (EASA) AD 2018–0002, dated
January 4, 2018 (EASA AD 2018–0002).
(h) Exceptions to EASA AD 2018–0002
(1) Where EASA AD 2018–0002 refers to
flight hours (FH), this AD requires using
hours time-in-service.
(2) Where EASA AD 2018–0002 refers to its
effective date, this AD requires using the
effective date of this AD.
(3) The ‘‘Remarks’’ section of EASA AD
2018–0002 does not apply to this AD.
(4) Where the service information
referenced in EASA AD 2018–0002 specifies
to download an option file from a certain
website, that method of installation is not
required by this AD.
(i) No Reporting Requirement
Although the service information
referenced in EASA AD 2018–0002 specifies
to submit certain information to the
manufacturer, this AD does not include that
requirement.
khammond on DSKJM1Z7X2PROD with PROPOSALS
(j) 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 (k)(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.
(k) Related Information
(1) For EASA AD 2018–0002, 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.
For information on the availability of this
material at the FAA, call (817) 222–5110.
This material may be found in the AD docket
VerDate Sep<11>2014
16:33 Jul 06, 2021
Jkt 253001
at https://www.regulations.gov by searching
for and locating Docket No. FAA–2021–0505.
(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.
Issued on June 15, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021–14401 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–2021–0497; Project
Identifier 2019–SW–043–AD]
RIN 2120–AA64
Airworthiness Directives; Bell Textron
Canada Limited 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 Bell Textron Canada Limited
Model 429 helicopters. This proposed
AD was prompted by three reports of
unexpected forces or uncommanded
inputs to the directional (yaw) control
system. This proposed AD would
require revising the existing Rotorcraft
Flight Manual (RFM) for your
helicopter. 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 August 23,
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 between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal
holidays.
For service information identified in
this NPRM, contact Bell Textron Canada
SUMMARY:
PO 00000
Frm 00033
Fmt 4702
Sfmt 4702
Limited, 12,800 Rue de l’Avenir,
Mirabel, Quebec J7J1R4, Canada;
telephone (450) 437–2862 or (800) 363–
8023; fax (450) 433–0272; or at https://
www.bellcustomer.com. 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.
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2021–0497; 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 Transport Canada AD, any
comments received, and other
information. The street address for
Docket Operations is listed above.
FOR FURTHER INFORMATION CONTACT:
Mitch Soth, Flight Test Engineer,
Southwest Section, Flight Test Branch,
Compliance & Airworthiness Division,
FAA, 10101 Hillwood Pkwy., Fort
Worth, TX 76177; telephone (817) 222–
5110; email mitch.soth@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–2021–0497; Project Identifier
2019–SW–043–AD’’ 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
E:\FR\FM\07JYP1.SGM
07JYP1
Agencies
[Federal Register Volume 86, Number 127 (Wednesday, July 7, 2021)]
[Proposed Rules]
[Pages 35690-35692]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-14401]
[[Page 35690]]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-0505; Project Identifier 2018-SW-004-AD]
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 AB139 and AW139 helicopters. This
proposed AD was prompted by reports of spurious in-flight
disconnections of the automatic flight control system (AFCS). This
proposed AD would require updating certain ``Primus Epic'' system
software, as specified in a European Aviation Safety Agency (now
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 August 23,
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 this IBR material on the EASA website at https://ad.easa.europa.eu. You may view EASA 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 EASA
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-2021-0505.
Examining the AD Docket
You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0505; 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-2021-0505; Project Identifier
2018-SW-004-AD'' 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 2018-0002, dated January 4, 2018
(EASA AD 2018-0002), to correct an unsafe condition for certain
Leonardo S.p.a. Model AB139 and AW139 helicopters.
This proposed AD was prompted by reports of spurious in-flight
disconnections of the AFCS. The investigation revealed that these AFCS
disconnect events relate to un-commanded single channel autopilot
disengagement for most of the cases, and to some instances of untimely
dual channel autopilot disengagement. The disconnections occurred in
random flight conditions and appeared to be temporary disruptions of
the AFCS' full availability because all functionalities could be
restored by re-engaging the complete system through the AFCS control
panel. The FAA is proposing this AD to address spurious degradation or
unavailability of the full availability of the AFCS. The unsafe
condition, if not addressed, could result in temporary impairment of
the automated flight aid for control of the helicopter and increase the
flightcrew's workload. See EASA AD 2018-0002 for additional background
information.
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.
[[Page 35691]]
Related Service Information Under 1 CFR Part 51
EASA AD 2018-0002 requires installation of certain ``Primus Epic''
system software, depending on the helicopter configuration. EASA AD
2018-0002 allows installation of ``Primus Epic'' system software on a
helicopter after that helicopter has had the software upgrade
installed.
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.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in EASA AD 2018-0002, 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 certain 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,
EASA AD 2018-0002 will be incorporated by reference in the FAA final
rule. This proposed AD would, therefore, require compliance with EASA
AD 2018-0002 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 2018-0002 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 2018-
0002. Service information specified in EASA AD 2018-0002 that is
required for compliance with it will be available at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-
0505 after the FAA final rule is published.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 128 helicopters of U.S. registry. The FAA estimates the
following costs to comply with this proposed AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Software upgrade...................... 24 work-hours x $85 per $0 $2,040 $261,120
hour = $2,040.
----------------------------------------------------------------------------------------------------------------
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all 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-2021-0505; Project Identifier 2018-
SW-004-AD.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by August 23, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Leonardo S.p.a. Model AB139 and AW139
helicopters, certificated in any category, identified in paragraphs
(c)(1) and (2) of this AD, equipped with ``Primus Epic'' system
software release 7.4 (Phase 7 V1), 7.7 (Phase 7 V3) or 7.10 (Phase 7
V4).
(1) Model AB139 and AW19 helicopters having serial number (S/N)
31005, 31006, and S/Ns 31008 through 31157 inclusive; and S/Ns 41001
through 41023 inclusive.
(2) Model AW139 helicopters having S/N 31201 and subsequent, and
S/N 41201 and subsequent.
(d) Subject
Joint Aircraft Service Component (JASC) Code: 2200, Auto Flight
System.
(e) Unsafe Condition
This AD was prompted by reports of spurious in-flight
disconnections of the automatic flight control system (AFCS). The
[[Page 35692]]
FAA is issuing this AD to address spurious degradation or
unavailability of the full AFCS. The unsafe condition, if not
addressed, could result in temporary impairment of the automated
flight aid for control of the helicopter and increase the
flightcrew's workload.
(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, European Aviation Safety Agency (now European Union
Aviation Safety Agency) (EASA) AD 2018-0002, dated January 4, 2018
(EASA AD 2018-0002).
(h) Exceptions to EASA AD 2018-0002
(1) Where EASA AD 2018-0002 refers to flight hours (FH), this AD
requires using hours time-in-service.
(2) Where EASA AD 2018-0002 refers to its effective date, this
AD requires using the effective date of this AD.
(3) The ``Remarks'' section of EASA AD 2018-0002 does not apply
to this AD.
(4) Where the service information referenced in EASA AD 2018-
0002 specifies to download an option file from a certain website,
that method of installation is not required by this AD.
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2018-0002
specifies to submit certain information to the manufacturer, this AD
does not include that requirement.
(j) 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 (k)(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.
(k) Related Information
(1) For EASA AD 2018-0002, 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-2021-0505.
(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 June 15, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-14401 Filed 7-6-21; 8:45 am]
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