Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes, 2295-2298 [2023-00263]
Download as PDF
Federal Register / Vol. 88, No. 9 / Friday, January 13, 2023 / Proposed Rules
Comply with this AD within the
compliance times specified, unless already
done.
(4) The provisions specified in paragraphs
(4) and (5) of EASA AD 2022–0166 do not
apply to this AD.
(5) The ‘‘Remarks’’ section of EASA AD
2022–0166 does not apply to this AD.
(g) Retained Revision of the Existing
Maintenance or Inspection Program, With
No Changes
(k) New Provisions for Alternative Actions
and Intervals
(f) Compliance
This paragraph restates the requirements of
paragraph (g) of AD 2018–20–07, with no
changes. Within 90 days after November 7,
2018 (the effective date of AD 2018–20–07),
revise the maintenance or inspection
program, as applicable, to incorporate the
information specified in Chapter 5–40,
Airworthiness Limitations, DGT 113872,
Revision 24, dated July 2017, of the Dassault
Falcon 50/50EX Maintenance Manual. The
initial compliance times for doing the tasks
are at the time specified in Chapter 5–40,
Airworthiness Limitations, DGT 113872,
Revision 24, dated July 2017, of the Dassault
Falcon 50/50EX Maintenance Manual, or
within 90 days after November 7, 2018,
whichever occurs later. Accomplishing the
revision of the existing maintenance or
inspection program required by paragraph (i)
of this AD terminates the requirements of this
paragraph.
(h) Retained Restrictions on Alternative
Actions and Intervals With No Changes
This paragraph restates the requirements of
paragraph (h) of AD 2018–20–07, with no
changes. After the maintenance or inspection
program has been revised as required by
paragraph (g) of this AD, no alternative
actions (e.g., inspections) or intervals may be
used unless the actions or intervals are
approved as an alternative method of
compliance (AMOC) in accordance with the
procedures specified in paragraph (m)(1) of
this AD.
(i) New Revision of the Existing Maintenance
or Inspection Program
Except as specified in paragraph (j) of this
AD: Comply with all required actions and
compliance times specified in, and in
accordance with, EASA AD 2022–0166,
dated August 11, 2022 (EASA AD 2022–
0166). Accomplishing the maintenance or
inspection program revision required by this
paragraph terminates the requirements of
paragraph (g) of this AD.
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(j) Exceptions to EASA AD 2022–0166
(1) The requirements specified in
paragraphs (1) and (2) of EASA AD 2022–
0166 do not apply to this AD.
(2) Paragraph (3) of EASA AD 2022–0166
specifies revising ‘‘the approved AMP’’
within 12 months after its effective date, but
this AD requires revising the existing
maintenance or inspection program, as
applicable within 90 days after the effective
date of this AD.
(3) The initial compliance time for doing
the tasks specified in paragraph (3) of EASA
AD 2022–0166 is at the applicable
‘‘limitations’’ and ‘‘associated thresholds’’ as
incorporated by the requirements of
paragraph (3) of EASA AD 2022–0166, or
within 90 days after the effective date of this
AD, whichever occurs later.
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After the maintenance or inspection
program has been revised as required by
paragraph (g) of this AD, no alternative
actions (e.g., inspections) or intervals are
allowed unless they are approved as
specified in the provisions of the ‘‘Ref.
Publications’’ section of EASA AD 2022–
0166.
(l) Terminating Actions for AD 2010–26–05
Accomplishing the actions required by
paragraph (g) or (i) of this AD terminates the
requirements of AD 2010–26–05 for Dassault
Aviation Model MYSTERE-FALCON 50
airplanes only.
(m) Additional AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): 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
responsible Flight Standards Office, as
appropriate. If sending information directly
to the International Validation Branch, send
it to the attention of the person identified in
paragraph (n) of this AD. Information may be
emailed to: 9-AVS-AIR-730-AMOC@faa.gov.
Before using any approved AMOC, notify
your appropriate principal inspector, or
lacking a principal inspector, the manager of
the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, International Validation
Branch, FAA; or EASA; or Dassault
Aviation’s EASA Design Organization
Approval (DOA). If approved by the DOA,
the approval must include the DOAauthorized signature.
(n) Additional Information
(o) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) 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 this AD specifies otherwise.
(3) The following service information was
approved for IBR on [DATE 35 DAYS AFTER
PUBLICATION OF THE FINAL RULE].
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Fmt 4702
Sfmt 4702
(i) European Union Aviation Safety Agency
(EASA) AD 2022–0166, dated August 11,
2022.
(ii) [Reserved]
(4) The following service information was
approved for IBR on November 7, 2018 (83
FR 49789, October 3, 2018).
(i) Chapter 5–40, Airworthiness
Limitations, DGT 113872, Revision 24, dated
July 2017, of the Dassault Falcon 50/50EX
Maintenance Manual.
(ii) [Reserved]
(5) For EASA AD 2022–0166, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; website
easa.europa.eu. You may find this EASA AD
on the EASA website at ad.easa.europa.eu.
(6) For service information identified in
this AD, contact Dassault Falcon Jet
Corporation, Teterboro Airport, P.O. Box
2000, South Hackensack, NJ 07606;
telephone 201–440–6700; website
dassaultfalcon.com.
(7) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th
St., Des Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195.
(8) 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 fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on January 6, 2023.
Gaetano A. Sciortino,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–00372 Filed 1–12–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2023–0012; Project
Identifier MCAI–2022–01317–T]
RIN 2120–AA64
For more information about this AD,
contact Tom Rodriguez, Aerospace Engineer,
Large Aircraft Section, International
Validation Branch, FAA, 2200 South 216th
St., Des Moines, WA 98198; telephone 206–
231–231–3226; email tom.rodriguez@faa.gov.
PO 00000
2295
Airworthiness Directives; ATR—GIE
Avions de Transport Re´gional
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 ATR—GIE Avions de Transport
Re´gional Model ATR42–500 and 72–
212A airplanes. This proposed AD was
prompted by in-service experience that
has shown that the lateral flight
guidance of the flight director/auto pilot
SUMMARY:
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Federal Register / Vol. 88, No. 9 / Friday, January 13, 2023 / Proposed Rules
may not limit HI BANK turns in severe
icing conditions. This proposed AD
would require the replacement of the
affected new avionics suite (NAS), as
specified in a European Union Aviation
Safety Agency (EASA) AD, which is
proposed for incorporation by reference
(IBR). This proposed AD would also
prohibit the installation of the affected
NAS on any airplane. 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 February 27,
2023.
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
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.
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2023–0012; 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 mandatory
continuing airworthiness information
(MCAI), any comments received, and
other information. The street address for
Docket Operations is listed above.
Material Incorporated by Reference:
• For EASA material that is proposed
for IBR in this NPRM, contact EASA,
Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221
8999 000; email ADs@easa.europa.eu;
website easa.europa.eu. You may find
this material on the EASA website at
ad.easa.europa.eu. It is also available at
regulations.gov under Docket No. FAA–
2023–0012.
FOR FURTHER INFORMATION CONTACT:
Shahram Daneshmandi, Aerospace
Engineer, Large Aircraft Section, FAA,
International Validation Branch, 2200
South 216th St., Des Moines, WA 98198;
telephone 206–231–3220; email
Shahram.Daneshmandi@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
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18:06 Jan 12, 2023
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under ADDRESSES. Include ‘‘Docket No.
FAA–2023–0012; Project Identifier
MCAI–2022–01317–T’’ 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
regulations.gov, including any personal
information you provide. The agency
will also post a report summarizing each
substantive verbal contact received
about this NPRM.
limit HI BANK turns in severe icing
conditions. The airplane is only
protected during LO BANK turns. This
condition, if not addressed, could result
in loss of control of the airplane.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2023–0012.
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 Shahram
Daneshmandi, Aerospace Engineer,
Large Aircraft Section, FAA,
International Validation Branch, 2200
South 216th St., Des Moines, WA 98198;
telephone 206–231–3220; email
Shahram.Daneshmandi@faa.gov. Any
commentary that the FAA receives
which is not specifically designated as
CBI will be placed in the public docket
for this rulemaking.
FAA’s Determination
This product has been approved by
the aviation authority of another
country and is approved for operation in
the United States. Pursuant to the FAA’s
bilateral agreement with the State of
Design Authority, it has notified the
FAA of the unsafe condition described
in the MCAI described above. The FAA
is issuing this NPRM after determining
that the unsafe condition described
previously is likely to exist or develop
in other products of the same type
design.
Background
EASA, which is the Technical Agent
for the Member States of the European
Union, has issued EASA AD 2022–0206,
dated October 7, 2022 (EASA AD 2022–
0206) (also referred to as the MCAI), to
correct an unsafe condition for certain
ATR—GIE Avions de Transport
Re´gional Model ATR42–500 and
ATR72–212A airplanes. The MCAI
states that in-service experience has
shown that the lateral flight guidance of
the flight director/auto pilot may not
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Fmt 4702
Sfmt 4702
Related Service Information Under 1
CFR Part 51
EASA AD 2022–0206 specifies
procedures for replacement of the
affected NAS with NAS standard 2.2 or
3.1, or later approved NAS standard.
EASA AD 2022–0206 also prohibits the
installation of the affected NAS on any
airplane. 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 ADDRESSES.
Proposed AD Requirements in This
NPRM
This proposed AD would require
accomplishing the actions specified in
EASA AD 2022–0206 described
previously, 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 2022–0206 by
reference in the FAA final rule. This
proposed AD would, therefore, require
compliance with EASA AD 2022–0206
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
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Federal Register / Vol. 88, No. 9 / Friday, January 13, 2023 / Proposed Rules
EASA AD 2022–0206 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 2022–0206.
Service information required by EASA
AD 2022–0206 for compliance will be
available at regulations.gov under
Docket No. FAA–2023–0012 after the
FAA final rule is published.
2297
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 20
airplanes of U.S. registry. The FAA
estimates the following costs to comply
with this proposed AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
1 work-hour × $85 per hour = $85 ..............................................................................................
* $0
$85
$1,700
* The FAA has received no definitive data on which to base the cost estimates for the parts specified in this proposed AD.
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.
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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,
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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:
■
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:
■
ATR—GIE Avions de Transport Re´gional:
Docket No. FAA–2023–0012; Project
Identifier MCAI–2022–01317–T.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by February 27,
2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to ATR—GIE Avions de
Transport Re´gional Model ATR42–500 and
ATR72–212A airplanes, certificated in any
category, as identified in European Union
Aviation Safety Agency (EASA) AD 2022–
0206, dated October 7, 2022 (EASA AD
2022–0206).
(d) Subject
Air Transport Association (ATA) of
America Code 31, Instruments.
(e) Unsafe Condition
This AD was prompted by in-service
experience that has shown that the lateral
flight guidance of the flight director/auto
pilot may not limit HI BANK turns in severe
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Fmt 4702
Sfmt 4702
icing conditions. The FAA is issuing this AD
to address the lateral flight guidance not
limiting HI BANK turns in severe icing
conditions. The unsafe condition, if not
addressed, could result in loss of control of
the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Requirements
Except as specified in paragraph (h) and (i)
of this AD: Comply with all required actions
and compliance times specified in, and in
accordance with, EASA AD 2022–0206.
(h) Exceptions to EASA AD 2022–0206
(1) Where EASA AD 2022–0206 refers to its
effective date, this AD requires using the
effective date of this AD.
(2) This AD does not adopt the ‘‘Remarks’’
section of EASA AD 2022–0206.
(i) No Reporting Requirement
Although the service information
referenced in EASA AD 2022–0206 specifies
to submit certain information to the
manufacturer, this AD does not include that
requirement.
(j) Additional AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): 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
responsible Flight Standards Office, as
appropriate. If sending information directly
to the International Validation Branch, send
it to the attention of the person identified in
paragraph (k) of this AD. Information may be
emailed to: 9-AVS-AIR-730-AMOC@faa.gov.
Before using any approved AMOC, notify
your appropriate principal inspector, or
lacking a principal inspector, the manager of
the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, International Validation
Branch, FAA; or EASA; or ATR—GIE Avions
de Transport Re´gional’s EASA Design
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13JAP1
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Federal Register / Vol. 88, No. 9 / Friday, January 13, 2023 / Proposed Rules
Organization Approval (DOA). If approved by
the DOA, the approval must include the
DOA-authorized signature.
(k) Additional Information
For more information about this AD,
contact Shahram Daneshmandi, Aerospace
Engineer, Large Aircraft Section, FAA,
International Validation Branch, 2200 South
216th St., Des Moines, WA 98198; telephone
206–231–3220; email
Shahram.Daneshmandi@faa.gov.
(l) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) 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 this AD specifies otherwise.
(i) European Union Aviation Safety Agency
(EASA) AD 2022–0206, dated October 7,
2022.
(ii) [Reserved]
(3) For EASA AD 2022–0206, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; website
easa.europa.eu. You may find this EASA AD
on the EASA website at ad.easa.europa.eu.
(4) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th
St., Des Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195.
(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 fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on January 5, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–00263 Filed 1–12–23; 8:45 am]
BILLING CODE 4910–13–P
ENVIRONMENTAL PROTECTION
AGENCY
40 CFR Part 49
[EPA–R01–OAR–2022–0961, FRL–10562–
01–R1]
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Approval and Promulgation of Air
Quality Implementation Plan; Mohegan
Tribe of Indians of Connecticut
Environmental Protection
Agency (EPA).
ACTION: Proposed rule.
AGENCY:
The Environmental Protection
Agency (EPA) is proposing to approve
amendments to the Mohegan Tribe of
Indians of Connecticut (the Mohegan
SUMMARY:
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18:06 Jan 12, 2023
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Tribe, Mohegans, or the Tribe) Tribal
Implementation Plan (TIP) under the
Clean Air Act (CAA) to regulate air
pollution within the exterior boundaries
of the Tribe’s reservation. EPA approved
the Tribe for treatment in the same
manner as a State (Treatment as State or
TAS) for purposes of administering New
Source Review (NSR) under the CAA on
December 26, 2006. The proposed TIP
includes permitting requirements for
minor sources of air pollution not
covered by the Tribe’s existing federally
approved TIP. The purpose of the
proposed TIP is to enable the Tribe to
attain and maintain the National
Ambient Air Quality Standards
(NAAQS) within the exterior boundaries
of its reservation by establishing new
elements to its federally enforceable
preconstruction air permitting program.
DATES: Written comments must be
received on or before February 13, 2023.
ADDRESSES: Submit your comments,
identified by Docket ID No. EPA–R01–
OAR–2022–0961 at https://
www.regulations.gov, or via email to
Isenberg.Madeline@epa.gov. For
comments submitted at Regulations.gov,
follow the online instructions for
submitting comments. Once submitted,
comments cannot be edited or removed
from Regulations.gov. For either manner
of submission, the EPA may publish any
comment received to its public docket.
Do not submit electronically any
information you consider to be
Confidential Business Information (CBI)
or other information whose disclosure is
restricted by statute. Multimedia
submissions (audio, video, etc.) must be
accompanied by a written comment.
The written comment is considered the
official comment and should include
discussion of all points you wish to
make. The EPA will generally not
consider comments or comment
contents located outside of the primary
submission (i.e. on the web, cloud, or
other file sharing system). For
additional submission methods, please
contact the person identified in the FOR
FURTHER INFORMATION CONTACT section.
For the full EPA public comment policy,
information about CBI or multimedia
submissions, and general guidance on
making effective comments, please visit
https://www.epa.gov/dockets/
commenting-epa-dockets. Publicly
available docket materials are available
at https://www.regulations.gov or at the
U.S. Environmental Protection Agency,
EPA Region 1 Regional Office, Air and
Radiation Division, 5 Post Office
Square—Suite 100, Boston, MA. EPA
requests that, if at all possible, you
contact the contact listed in the FOR
FURTHER INFORMATION CONTACT section to
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Fmt 4702
Sfmt 4702
schedule your inspection. The Regional
Office’s official hours of business are
Monday through Friday, 8:30 a.m. to
4:30 p.m., excluding legal holidays and
facility closures due to COVID–19.
FOR FURTHER INFORMATION CONTACT:
Madeline Isenberg, Air Permits, Toxics
and Indoor Programs Branch, EPA
Region 1, 5 Post Office Square (Mail
Code: 05–2), Boston, MA, 02109–3912,
telephone number (617) 918–1271,
email: Isenberg.Madeline@epa.gov
SUPPLEMENTARY INFORMATION:
Throughout this document whenever
‘‘we,’’ ‘‘us,’’ or ‘‘our’’ is used, we mean
EPA.
Table of Contents
I. CAA Requirements and the Role of Indian
Tribes
II. Background on the Mohegan Tribe and
CAA Requirements
III. Background on Mohegan Tribe’s TIP
IV. Overview of the Mohegan Tribe’s July
2022 TIP Revision
V. EPA’s Evaluation of the Mohegan Tribe’s
July 2022 TIP Revision
VI. Proposed Action
VII. Incorporation by Reference
VIII. Statutory and Executive Order Reviews
I. CAA Requirements and the Role of
Indian Tribes
A. How did the 1990 CAA amendments
include Indian Tribes?
Under the 1990 amendments to the
CAA, the EPA may approve eligible
Tribes to administer certain provisions
of the CAA. Pursuant to section
301(d)(2) of the CAA, EPA promulgated
the Tribal Authority Rule (TAR) on
February 12, 1998 (63 FR 7254). The
TAR specifies the CAA provisions for
which it is appropriate to treat Tribes in
the same manner as states, the eligibility
criteria the Tribes must meet if they
choose to seek such treatment, and the
procedure by which EPA reviews a
Tribe’s request for an eligibility
determination.
As a general matter, EPA determined
in the TAR that it is not appropriate to
treat Tribes in the same manner as states
for purposes of specific plan submittal
and implementation deadlines for
NAAQS-related requirements. See 40
CFR 49.4. Thus, Tribes are generally not
subject to CAA provisions which
specify a deadline by which something
must be accomplished. For example,
provisions mandating the submission of
state implementation plans do not apply
to the Tribes. Furthermore, under the
TAR at 40 CFR 49.7(c), a Tribe may
choose to implement reasonably
severable portions of the various CAA
programs, as long as it can demonstrate
that its proposed air program is not
integrally related to program elements
E:\FR\FM\13JAP1.SGM
13JAP1
Agencies
[Federal Register Volume 88, Number 9 (Friday, January 13, 2023)]
[Proposed Rules]
[Pages 2295-2298]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-00263]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-0012; Project Identifier MCAI-2022-01317-T]
RIN 2120-AA64
Airworthiness Directives; ATR--GIE Avions de Transport
R[eacute]gional Airplanes
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 ATR--GIE Avions de Transport R[eacute]gional Model ATR42-
500 and 72-212A airplanes. This proposed AD was prompted by in-service
experience that has shown that the lateral flight guidance of the
flight director/auto pilot
[[Page 2296]]
may not limit HI BANK turns in severe icing conditions. This proposed
AD would require the replacement of the affected new avionics suite
(NAS), as specified in a European Union Aviation Safety Agency (EASA)
AD, which is proposed for incorporation by reference (IBR). This
proposed AD would also prohibit the installation of the affected NAS on
any airplane. 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 February
27, 2023.
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 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.
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-0012; 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 mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
street address for Docket Operations is listed above.
Material Incorporated by Reference:
For EASA material that is proposed for IBR in this NPRM,
contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone
+49 221 8999 000; email [email protected]; website easa.europa.eu. You
may find this material on the EASA website at ad.easa.europa.eu. It is
also available at regulations.gov under Docket No. FAA-2023-0012.
FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace
Engineer, Large Aircraft Section, FAA, International Validation Branch,
2200 South 216th St., Des Moines, WA 98198; telephone 206-231-3220;
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-2023-0012; Project Identifier
MCAI-2022-01317-T'' 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
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
Shahram Daneshmandi, Aerospace Engineer, Large Aircraft Section, FAA,
International Validation Branch, 2200 South 216th St., Des Moines, WA
98198; telephone 206-231-3220; email [email protected]. Any
commentary that the FAA receives which 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 2022-0206, dated October 7, 2022
(EASA AD 2022-0206) (also referred to as the MCAI), to correct an
unsafe condition for certain ATR--GIE Avions de Transport
R[eacute]gional Model ATR42-500 and ATR72-212A airplanes. The MCAI
states that in-service experience has shown that the lateral flight
guidance of the flight director/auto pilot may not limit HI BANK turns
in severe icing conditions. The airplane is only protected during LO
BANK turns. This condition, if not addressed, could result in loss of
control of the airplane.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2023-0012.
Related Service Information Under 1 CFR Part 51
EASA AD 2022-0206 specifies procedures for replacement of the
affected NAS with NAS standard 2.2 or 3.1, or later approved NAS
standard. EASA AD 2022-0206 also prohibits the installation of the
affected NAS on any airplane. 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 ADDRESSES.
FAA's Determination
This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with the State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI
described above. The FAA is issuing this NPRM after determining that
the unsafe condition described previously is likely to exist or develop
in other products of the same type design.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in EASA AD 2022-0206 described previously, 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 2022-0206 by reference in the FAA
final rule. This proposed AD would, therefore, require compliance with
EASA AD 2022-0206 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
[[Page 2297]]
EASA AD 2022-0206 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 2022-0206. Service information
required by EASA AD 2022-0206 for compliance will be available at
regulations.gov under Docket No. FAA-2023-0012 after the FAA final rule
is published.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 20 airplanes 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.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
1 work-hour x $85 per hour = $85............................. * $0 $85 $1,700
----------------------------------------------------------------------------------------------------------------
* The FAA has received no definitive data on which to base the cost estimates for the parts specified in this
proposed AD.
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:
ATR--GIE Avions de Transport R[eacute]gional: Docket No. FAA-2023-
0012; Project Identifier MCAI-2022-01317-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by February 27, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to ATR--GIE Avions de Transport R[eacute]gional
Model ATR42-500 and ATR72-212A airplanes, certificated in any
category, as identified in European Union Aviation Safety Agency
(EASA) AD 2022-0206, dated October 7, 2022 (EASA AD 2022-0206).
(d) Subject
Air Transport Association (ATA) of America Code 31, Instruments.
(e) Unsafe Condition
This AD was prompted by in-service experience that has shown
that the lateral flight guidance of the flight director/auto pilot
may not limit HI BANK turns in severe icing conditions. The FAA is
issuing this AD to address the lateral flight guidance not limiting
HI BANK turns in severe icing conditions. The unsafe condition, if
not addressed, could result in loss of control of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) and (i) of this AD: Comply
with all required actions and compliance times specified in, and in
accordance with, EASA AD 2022-0206.
(h) Exceptions to EASA AD 2022-0206
(1) Where EASA AD 2022-0206 refers to its effective date, this
AD requires using the effective date of this AD.
(2) This AD does not adopt the ``Remarks'' section of EASA AD
2022-0206.
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2022-0206
specifies to submit certain information to the manufacturer, this AD
does not include that requirement.
(j) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): 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 responsible Flight Standards Office, as
appropriate. If sending information directly to the International
Validation Branch, send it to the attention of the person identified
in paragraph (k) of this AD. Information may be emailed to: [email protected]. Before using any approved AMOC, notify your
appropriate principal inspector, or lacking a principal inspector,
the manager of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
Validation Branch, FAA; or EASA; or ATR--GIE Avions de Transport
R[eacute]gional's EASA Design
[[Page 2298]]
Organization Approval (DOA). If approved by the DOA, the approval
must include the DOA-authorized signature.
(k) Additional Information
For more information about this AD, contact Shahram Daneshmandi,
Aerospace Engineer, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone 206-231-3220; email [email protected].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) 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 this AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2022-0206,
dated October 7, 2022.
(ii) [Reserved]
(3) For EASA AD 2022-0206, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
[email protected]; website easa.europa.eu. You may find this EASA
AD on the EASA website at ad.easa.europa.eu.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability
of this material at the FAA, call 206-231-3195.
(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: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on January 5, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-00263 Filed 1-12-23; 8:45 am]
BILLING CODE 4910-13-P