[Federal Register Volume 87, Number 107 (Friday, June 3, 2022)]
[Notices]
[Page 33802]
[FR Doc No: 2022-11906]

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DEPARTMENT OF HOMELAND SECURITY

Federal Emergency Management Agency

[Internal Agency Docket No. FEMA-4496-DR; Docket ID FEMA-2022-0001]

Massachusetts; Amendment No. 8 to Notice of a Major Disaster
Declaration

AGENCY: Federal Emergency Management Agency, DHS.

ACTION: Notice.

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SUMMARY: This notice amends the notice of a major disaster declaration
for the Commonwealth of Massachusetts (FEMA-4496-DR), dated March 27,
2020, and related determinations.

DATES: This change occurred on May 17, 2022.

FOR FURTHER INFORMATION CONTACT: Dean Webster, Office of Response and
Recovery, Federal Emergency Management Agency, 500 C Street SW,
Washington, DC 20472,<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: The Federal Emergency Management Agency
(FEMA) hereby gives notice that pursuant to the authority vested in the
Administrator, under Executive Order 12148, as amended, Lori A.
Ehrlich, of FEMA is appointed to act as the Federal Coordinating
Officer for this disaster.
    This action terminates the appointment of Paul F. Ford as Federal
Coordinating Officer for this disaster.

    The following Catalog of Federal Domestic Assistance Numbers
(CFDA) are to be used for reporting and drawing funds: 97.030,
Community Disaster Loans; 97.031, Cora Brown Fund; 97.032, Crisis
Counseling; 97.033, Disaster Legal Services; 97.034, Disaster
Unemployment Assistance (DUA); 97.046, Fire Management Assistance
Grant; 97.048, Disaster Housing Assistance to Individuals and
Households In Presidentially Declared Disaster Areas; 97.049,
Presidentially Declared Disaster Assistance--Disaster Housing
Operations for Individuals and Households; 97.050, Presidentially
Declared Disaster Assistance to Individuals and Households--Other
Needs; 97.036, Disaster Grants--Public Assistance (Presidentially
Declared Disasters); 97.039, Hazard Mitigation Grant.

Deanne Criswell,
Administrator, Federal Emergency Management Agency.
[FR Doc. 2022-11906 Filed 6-2-22; 8:45 am]
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[Federal Register Volume 85, Number 32 (Tuesday, February 18, 2020)]
[Notices]
[Pages 8858-8859]
[FR Doc No: 2020-03155]

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ENVIRONMENTAL PROTECTION AGENCY

[FRL-10005-08-Region 8]

Public Water System Supervision Program Revision for the State of
South Dakota

AGENCY: Environmental Protection Agency (EPA).

ACTION: Notice.

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SUMMARY: Public notice is hereby given that the state of South Dakota
has revised its Public Water System Supervision (PWSS) Program by
adopting federal regulations for the Revised Total Coliform Rule (RTCR)
that correspond to the National Primary Drinking Water Regulations
(NPDWR). The EPA has reviewed South Dakota's regulations and determined
they are no less stringent than the federal regulations. The EPA is
proposing to approve South Dakota's primacy revision for the RTCR.
    This approval action does not extend to public water systems in
Indian country. Please see SUPPLEMENTARY INFORMATION, section B.

DATES: Any member of the public is invited to request a public hearing
on this determination by March 19, 2020. Please see SUPPLEMENTARY
INFORMATION, section C, for details. Should no timely and appropriate
request for a hearing be received, and the Regional Administrator (RA)
does not elect to hold a hearing on his/her own motion, this
determination shall become applicable March 19, 2020. If a public
hearing is requested and granted, then this determination shall not
become applicable until such time following the hearing as the RA
issues an order affirming or rescinding this action.

ADDRESSES: Requests for a public hearing should be addressed to: Robert
Clement, Drinking Water B Section, EPA Region 8, 1595 Wynkoop Street,
Denver, CO 80202-1129.
    All documents relating to this determination are available for
inspection at: EPA Region 8, Drinking Water Section (5th floor), 1595
Wynkoop Street, Denver, Colorado.

FOR FURTHER INFORMATION CONTACT: Robert Clement, Drinking Water B
Section, EPA Region 8, 1595 Wynkoop Street, Denver, CO 80202-1129,
phone<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: In accordance with the provisions of section
1413 of the Safe Drinking Water Act (SDWA), 42 U.S.C. 300g-2, and 40
CFR 142.13, public notice is hereby given that the state of South
Dakota has revised its PWSS program by adopting federal regulations for
the RTCR that correspond to the NPDWR in 40 CFR parts 141 and 142. The
EPA has reviewed South Dakota's regulations and determined they are no
less stringent than the federal regulations. The EPA is proposing to
approve South Dakota's primacy revision for the RTCR.
    This approval action does not extend to public water systems in
Indian country as defined in 18 U.S.C. 1151. Please see SUPPLEMENTARY
INFORMATION, section B.

A. Why are revisions to State programs necessary?

    States with primary PWSS enforcement authority must comply with the
requirements of 40 CFR part 142 to maintain primacy. They must adopt
regulations that are at least as stringent as the NPDWRs at 40 CFR
parts 141 and 142, as well as adopt all new and revised NPDWRs in order
to retain primacy (40 CFR 142.12(a)).

B. How does this action affect Indian country (18 U.S.C. 1151) in South
Dakota?

    The EPA's approval of South Dakota's revised PWSS program does not
extend to Indian country as defined in 18 U.S.C. 1151. Indian country
in South Dakota generally includes (1) lands within the exterior
boundaries of the following Indian reservations located within South
Dakota, in part or in full: The Cheyenne River Reservation, the Crow
Creek Reservation, the Flandreau Indian Reservation, the Lower Brule
Reservation, the Pine Ridge Reservation, the Rosebud Indian
Reservation, the Standing Rock Reservation, and the Yankton Reservation
(subject to federal court decisions removing lands from Indian country
status within the Yankton Reservation); (2) any land held in trust by
the United States for an Indian tribe; and (3) any other areas which
are ``Indian country'' within the meaning of 18 U.S.C. 1151. The EPA or
eligible Indian tribes, as appropriate, will retain PWSS program
responsibilities over public water systems in Indian country.

C. Requesting a Hearing

    Any member of the public may request a hearing on this
determination within thirty (30) days of this notice. All requests
shall include the following information: Name, address, and telephone
number of the individual, organization, or other entity requesting a
hearing; a brief statement of interest and information to be submitted
at the hearing; and a signature of the interested individual or
responsible official, if made on behalf of an organization or other
entity. Frivolous or insubstantial requests for a hearing may be denied
by the RA.
    Notice of any hearing shall be given not less than fifteen (15)
days prior to the time scheduled for the hearing and will be made by
the RA in the Federal Register and in a newspaper of general
circulation in the state. A notice will also be sent to both the
person(s) requesting the hearing and the state. The hearing notice will
include a statement of purpose of the hearing, information regarding
time and location for the hearing, and the address and telephone number
where interested persons may obtain further information. The RA will
issue an order affirming or rescinding the determination upon review of
the hearing record.
    Please bring this notice to the attention of any persons known by
you to have an interest in this determination.

    Dated: December 19, 2019.
Gregory E. Sopkin,
Regional Administrator, Region 8.
[FR Doc. 2020-03155 Filed 2-14-20; 8:45 am]
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[Federal Register Volume 77, Number 18 (Friday, January 27, 2012)]
[Rules and Regulations]
[Pages 4217-4219]
[FR Doc No: 2012-1607]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-0956; Directorate Identifier 2011-NE-23-AD;
Amendment 39-16928; AD 2012-02-05]
RIN 2120-AA64

Airworthiness Directives; Thielert Aircraft Engines GmbH
Reciprocating Engines

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for all
Thielert Aircraft Engines GmbH (TAE)

TAE 125-02-99 and TAE 125-02-114 reciprocating engines. This AD was
prompted by in-flight engine shutdown incidents reported on airplanes
equipped with TAE 125 engines. We are issuing this AD to prevent in-
flight engine shutdown, which could result in loss of control of the
airplane.

DATES: This AD is effective March 2, 2012.

ADDRESSES: For service information identified in this AD, contact
Thielert Aircraft Engines GmbH, Platanenstrasse 14 D-09350,
Lichtenstein, Germany, telephone: +49-37204-696-0; fax: +49-37204-696-
55; email<EMAIL_ADDRESS>You may review copies of the
referenced service information at the FAA, Engine & Propeller
Directorate, 12 New England Executive Park, Burlington, MA. For
information on the availability of this material at the FAA, call (781)
238-7125.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (phone:<PHONE_NUMBER>) is Document Management Facility,
U.S. Department of Transportation, Docket Operations, M-30, West
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE.,
Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Alan Strom, Aerospace Engineer, Engine
Certification Office, FAA, 12 New England Executive Park, Burlington,
MA; phone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, issued EASA AD
2011-0087-E, dated May 12, 2011 (referred to after this as ``the
MCAI''), to correct an unsafe condition for the specified products. The
MCAI states:

    In-flight engine shutdown incidents have been reported on
aeroplanes equipped with TAE 125 engines.
    Preliminary investigations showed that it was mainly the result
of the sensitivity of friction disk Part Number (P/N) 05-7211-
K010201 against possible misalignment of gearbox and core engine
during assembly.
    This condition, if not corrected, could result in further cases
of engine in-flight shutdown and consequent loss of control of the
aeroplane.
    To address this unsafe condition, Thielert Aircraft Engines GmbH
has developed a new friction disk.

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM published in the Federal Register on October 18, 2011 (76 FR
64289). That NPRM was proposed to require on all TAE 125-02-99 and TAE
125-02-114 reciprocating engines, replacing the friction disk, P/N 05-
7211-K010201.

Comments

    We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (76 FR 64289, October 18,
2011).

Conclusion

    We reviewed the relevant data and determined that air safety and
the public interest require adopting the AD as proposed.

Costs of Compliance

    Based on the service information, we estimate that this AD will
affect about 206 TAE 125-02-99 and TAE 125-02-114 reciprocating engines
installed on airplanes of U.S. registry. We also estimate that it will
take about 3 work-hours per engine to comply with this AD. The average
labor rate is $85 per work-hour. Required parts will cost about $1,500
per engine. Based on these figures, we estimate the cost of the AD on
U.S. operators to be $361,530. Our cost estimate is exclusive of
possible warranty coverage.

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.
    We are 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

    This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866,
    (2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness
directive (AD):

2012-02-05 Thielert Aircraft Engines GmbH: Amendment 39-16928;
Docket No. FAA-2011-0956; Directorate Identifier 2011-NE-23-AD.

(a) Effective Date

    This AD is effective March 2, 2012.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all Thielert Aircraft Engines GmbH TAE 125-
02-99 and TAE-125-02-114 reciprocating engines with friction disk,
part number (P/N) 05-7211-K010201, installed.

(d) Reason

    This AD was prompted by in-flight engine shutdown incidents
reported on airplanes equipped with TAE 125 engines. Preliminary
investigations showed that it was mainly the result of the
sensitivity of friction disk P/N

05-7211-K010201 against possible misalignment of gearbox and core
engine during assembly. We are issuing this AD to prevent in-flight
engine shutdown, which could result in loss of control of the
airplane.

(e) Actions and Compliance

    Unless already done, do the following actions.

(1) TAE 125-02-99 Engines, P/Ns 05-7200-K000201; 05-7200-K000701; 05-
7200-K000101; 05-7200-K000901; 05-7200-K001101; and 05-7200-K001301;
and TAE 125-02-114 Engines, P/Ns 05-7200-K000501; 05-7200-K000801; and
05-7200-K001401

    For TAE 125-02-99 engines, P/Ns 05-7200-K000201; 05-7200-
K000701; 05-7200-K000101; 05-7200-K000901; 05-7200-K001101; and 05-
7200-K001301; and TAE 125-02-114 engines, P/Ns 05-7200-K000501; 05-
7200-K000801; and 05-7200-K001401, remove friction disk, P/N 05-
7211-K010201, within 100 flight hours (FH) time-since-new (TSN) on
the clutch or within 10 FH time-in-service (TIS) after the effective
date of this AD, whichever is later.

(2) TAE 125-02-99 Engines, P/Ns 05-7200-K000301

    For TAE 125-02-99 engines, P/N 05-7200-K000301, installed on
multiengine aircraft, remove friction disk, P/N 05-7211-K010201, on
one engine within 100 FH TSN on the clutch or within 10 FH TIS after
the effective date of this AD, whichever is later. Remove friction
disk, P/N 05-7211-K010201, from the other engine within 300 FH TSN
on the clutch or within 10 FH TIS after the effective date of this
AD, whichever is later.

(f) Installation Prohibition

    After the effective date of this AD:
    (1) Do not install any friction disk, P/N 05-7211-K010201, into
any engine.
    (2) Do not install any TAE 125-02-99 engine, P/N 05-7200-
K000201, 05-7200-K000301, or 05-7200-K000701, or TAE 125-02-114
engine, P/N 05-7200-K00801 or 05-7200-K00501, that has a friction
disk, P/N 05-7211-K010201 installed, onto any airplane.

(g) Operating Prohibition

    Do not operate any multi-engine aircraft after 300 FH TSN on the
clutch or 10 FH TIS after the effective date of this AD, whichever
is later, which has installed a friction disk, P/N 05-7211-K010201.

(h) Alternative Methods of Compliance (AMOCs)

    The Manager, Engine Certification Office, may approve AMOCs for
this AD. Use the procedures found in 14 CFR 39.19 to make your
request.

(i) Related Information

    (1) For more information about this AD, contact Alan Strom,
Aerospace Engineer, Engine Certification Office, FAA, 12 New England
Executive Park, Burlington, MA; phone:<PHONE_NUMBER>; fax: (781)
238-7199; email<EMAIL_ADDRESS>    (2) Refer to EASA Airworthiness Directive 2011-0087-E, dated May
12, 2011, and Thielert Service Bulletin No. TM TAE 125-1013 P1, for
related information.
    (3) Contact Thielert Aircraft Engines GmbH, Platanenstrasse 14
D-09350, Lichtenstein, Germany, telephone: +49-37204-696-0; fax:
+49-37204-696-55; email<EMAIL_ADDRESS>for a copy of
this service information.
    (4) You may review copies of the service information at the FAA,
Engine & Propeller Directorate, 12 New England Executive Park,
Burlington, MA. For information on the availability of this material
at the FAA, call<PHONE_NUMBER>.

(j) Material Incorporated by Reference

    None.

    Issued in Burlington, Massachusetts, on January 19, 2012.
Peter A. White,
Manager, Engine & Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2012-1607 Filed 1-26-12; 8:45 am]
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