Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters, 7368-7369 [2022-02131]
Download as PDF
<![CDATA[
7368
Federal Register / Vol. 87, No. 27 / Wednesday, February 9, 2022 / Rules and Regulations
4. Amend § 5001.204 by revising
paragraph (b) to read as follows:
§ 5001.204 Personal, partnership, and
corporate guarantees.
*
*
*
*
*
(b) When warranted by an Agency
assessment of potential financial risk,
the Agency may require the following:
(1) Guarantees to be secured;
(2) Guarantees from any person or
entity owning less than a 20-percent
Interest or membership in the borrower;
and
(3) Guarantees from persons whose
ownership Interest in the borrower is
held indirectly through intermediate or
affiliated entities.
*
*
*
*
*
§ 5001.451
[Amended]
5. Amend § 5001.451 by redesignating
the second paragraph (b)(3)(xiii) and
paragraph (b)(3)(xiv) as paragraphs
(b)(3)(xiv) and (xv), respectively.
■
Justin Maxson,
Deputy Under Secretary, Rural Development.
[FR Doc. 2022–02710 Filed 2–8–22; 8:45 am]
BILLING CODE 3410–15–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–1003; Project
Identifier AD–2021–01141–R; Amendment
39–21899; AD 2022–02–02]
RIN 2120–AA64
Airworthiness Directives; Bell Textron
Inc. (Type Certificate Previously Held
by Bell Helicopter Textron Inc.)
Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
The FAA is correcting an
airworthiness directive (AD) that
published in the Federal Register. That
AD applies to Bell Textron Inc. (type
certificate previously held by Bell
Helicopter Textron Inc.) Model 204B,
205A, 205A–1, 205B, 210, and 212
helicopters with a certain outboard
main rotor hub strap pin (pin) installed.
As published, the AD number specified
in the regulatory text is incorrect. This
document corrects that error. In all other
respects, the original document remains
the same.
DATES: This correction is effective
February 16, 2022. The effective date of
AD 2022–02–02 remains February 16,
2022.
lotter on DSK11XQN23PROD with RULES1
SUMMARY:
VerDate Sep<11>2014
16:18 Feb 08, 2022
Jkt 256001
You may examine the AD
docket at https://www.regulations.gov
by searching for and locating Docket No.
FAA–2021–1003, or in person at Docket
Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal
holidays. The AD docket contains this
final rule, any comments received, and
other information. The address for
Docket Operations is U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
ADDRESSES:
■
FOR FURTHER INFORMATION CONTACT:
David Wilson, Aerospace Engineer,
DSCO Branch, Compliance &
Airworthiness Division, FAA, 10101
Hillwood Pkwy., Fort Worth, TX 76177;
telephone (817) 222–5786; email
david.wilson@faa.gov.
AD 2022–
02–02, Amendment 39–21899 (87 FR
1668, January 12, 2022) (AD 2022–02–
02), requires removing any pin part
number 204–012–104–005 with a serial
number prefix ‘‘FNFS’’ from service and
prohibits installing the affected pin on
any helicopter.
SUPPLEMENTARY INFORMATION:
Need for the Correction
As published, the AD number
specified in the regulatory text is
incorrect. The incorrectly specified AD
number was FAA–2021–1003; the
correct AD number is 2022–02–02.
Correction of Publication
This document corrects an error and
correctly adds the AD as an amendment
to 14 CFR 39.13. Although no other part
of the preamble or regulatory
information has been corrected, the
FAA is publishing the entire rule in the
Federal Register.
The effective date of this AD remains
February 16, 2022.
Since this action only corrects the AD
number, it has no adverse economic
impact and imposes no additional
burden on any person. Therefore, the
FAA has determined that notice and
public comment procedures are
unnecessary.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Correction
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
PO 00000
Frm 00002
Fmt 4700
Sfmt 4700
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
[Corrected]
2. The FAA amends § 39.13 by:
a. Removing Airworthiness Directive
2021–15–51, Amendment 39–21678 (86
FR 43406, August 9, 2021); and
■ b. Adding the following new
airworthiness directive:
■
■
2022–02–02 Bell Textron Inc. (Type
Certificate Previously Held by Bell
Helicopter Textron Inc.): Amendment
39–21899; Docket No. FAA–2021–1003;
Project Identifier AD–2021–01141–R.
(a) Effective Date
This airworthiness directive (AD) is
effective February 16, 2022.
(b) Affected ADs
This AD replaces AD 2021–15–51,
Amendment 39–21678 (86 FR 43406, August
9, 2021) (AD 2021–15–51).
(c) Applicability
This AD applies to Bell Textron Inc. (type
certificate previously held by Bell Helicopter
Textron Inc.) Model 204B, 205A, 205A–1,
205B, 210, and 212 helicopters, certificated
in any category, with an outboard main rotor
hub strap pin (pin) part number 204–012–
104–005 with a serial number prefix ‘‘FNFS’’
installed.
(d) Subject
Joint Aircraft System Component (JASC)
Code: 6200, Main Rotor System.
(e) Unsafe Condition
This AD was prompted by a fatal accident
in which a pin sheared off during flight,
which resulted in the main rotor blade and
the main rotor head detaching from the
helicopter. The FAA is issuing this AD to
address this unsafe condition and prevent
loss of control of the helicopter.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
(1) For Model 204B, 205A, 205A–1, 205B,
and 212 helicopters:
(i) Before further flight from August 24,
2021 (the effective date of AD 2021–15–51),
remove from service any pin that is identified
in paragraph (c) of this AD.
(ii) After August 24, 2021 (the effective
date of AD 2021–15–51), do not install any
pin that is identified in paragraph (c) of this
AD on any helicopter.
(2) For Model 210 helicopters:
(i) Before further flight after the effective
date of this AD, remove from service any pin
that is identified in paragraph (c) of this AD.
(ii) As of the effective date of this AD, do
not install any pin that is identified in
paragraph (c) of this AD on any helicopter.
E:\FR\FM\09FER1.SGM
09FER1
Federal Register / Vol. 87, No. 27 / Wednesday, February 9, 2022 / Rules and Regulations
(h) Special Flight Permits
Special flight permits are prohibited.
(i) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, DSCO Branch,
Compliance & Airworthiness Division, 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 DSCO Branch,
send it to the attention of the person
identified in paragraph (j) of this AD.
Information may be emailed to: 9-ASW-190COS@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.
(j) Related Information
For more information about this AD,
contact David Wilson, Aerospace Engineer,
DSCO Branch, Compliance & Airworthiness
Division, FAA, 10101 Hillwood Pkwy., Fort
Worth, TX 76177; telephone (817) 222–5786;
email david.wilson@faa.gov.
(k) Material Incorporated by Reference
None.
Issued on January 27, 2022.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives,
Compliance & Airworthiness Division,
Aircraft Certification Service.
[FR Doc. 2022–02131 Filed 2–8–22; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF THE TREASURY
Office of Foreign Assets Control
31 CFR Parts 501, 510, 535, 536, 539,
541, 542, 544, 546, 547, 548, 549, 551,
552, 560, 561, 566, 576, 583, 584, 588,
590, 592, 594, 597, and 598
Inflation Adjustment of Civil Monetary
Penalties
Office of Foreign Assets
Control, Treasury.
ACTION: Final rule.
AGENCY:
The Department of the
Treasury’s Office of Foreign Assets
Control (OFAC) is issuing this final rule
to adjust certain civil monetary
penalties for inflation pursuant to the
Federal Civil Penalties Inflation
Adjustment Act of 1990, as amended by
the Federal Civil Penalties Inflation
Adjustment Act Improvements Act of
2015.
DATES: This rule is effective February 9,
2022.
FOR FURTHER INFORMATION CONTACT:
OFAC: Assistant Director for Licensing,
202–622–2480; Assistant Director for
Regulatory Affairs, 202–622–4855;
Assistant Director for Sanctions
Compliance & Evaluation, 202–622–
2490.
SUPPLEMENTARY INFORMATION:
SUMMARY:
Electronic Availability
This document and additional
information concerning OFAC are
available from OFAC’s website:
www.treasury.gov/ofac.
Background
Section 4 of the Federal Civil
Penalties Inflation Adjustment Act
(1990 Pub. L. 101–410, 104 Stat. 890; 28
U.S.C. 2461 note), as amended by the
Federal Civil Penalties Inflation
Adjustment Act Improvements Act of
2015 (Pub. L. 114–74, 129 Stat. 599, 28
U.S.C. 2461 note) (the FCPIA Act),
requires each federal agency with
statutory authority to assess civil
monetary penalties (CMPs) to adjust
CMPs annually for inflation according
to a formula described in section 5 of
the FCPIA Act. One purpose of the
FCPIA Act is to ensure that CMPs
continue to maintain their deterrent
effect through periodic cost-of-living
based adjustments.
OFAC has adjusted its CMPs seven
times since the Federal Civil Penalties
Inflation Adjustment Act Improvements
Act went into effect on November 2,
2015: An initial catch-up adjustment on
August 1, 2016 (81 FR 43070, July 1,
2016); an additional initial catch-up
adjustment related to CMPs for failure to
comply with a requirement to furnish
information, the late filing of a required
7369
report, and failure to maintain records
(‘‘recordkeeping CMPs’’) that were
inadvertently omitted from the August
1, 2016 initial catch-up adjustment on
October 5, 2020 (85 FR 54911,
September 3, 2020); and annual
adjustments on February 10, 2017 (82
FR 10434, February 10, 2017); March 19,
2018 (83 FR 11876, March 19, 2018);
June 14, 2019 (84 FR 27714, June 14,
2019); April 9, 2020 (85 FR 19884, April
9, 2020); and March 17, 2021 (86 FR
14534, March 17, 2021).
Method of Calculation
The method of calculating CMP
adjustments applied in this final rule is
required by the FCPIA Act. Under the
FCPIA Act and the Office of
Management and Budget guidance
required by the FCPIA Act, annual
inflation adjustments subsequent to the
initial catch-up adjustment are to be
based on the percent change between
the Consumer Price Index for all Urban
Consumers (‘‘CPI–U’’) for the October
preceding the date of the adjustment
and the prior year’s October CPI–U. As
set forth in Office of Management and
Budget Memorandum M–22–07 of
December 15, 2021, the adjustment
multiplier for 2022 is 1.06222. In order
to complete the 2022 annual
adjustment, each current CMP is
multiplied by the 2022 adjustment
multiplier. Under the FCPIA Act, any
increase in CMP must be rounded to the
nearest multiple of $1.
New Penalty Amounts
OFAC imposes CMPs pursuant to the
penalty authority in five statutes: The
Trading With the Enemy Act (50 U.S.C.
4301–4341, at 4315) (TWEA); the
International Emergency Economic
Powers Act (50 U.S.C. 1701–1706, at
1705) (IEEPA); the Antiterrorism and
Effective Death Penalty Act of 1996 (18
U.S.C. 2339B) (AEDPA); the Foreign
Narcotics Kingpin Designation Act (21
U.S.C. 1901–1908, at 1906) (FNKDA);
and the Clean Diamond Trade Act (19
U.S.C. 3901–3913, at 3907) (CDTA).
The table below summarizes the
existing and new maximum CMP
amounts for each statute.
TABLE 1—MAXIMUM CMP AMOUNTS FOR RELEVANT STATUTES
Existing maximum
CMP amount
lotter on DSK11XQN23PROD with RULES1
Statute
TWEA ...........................................................................................................................................................
IEEPA ..........................................................................................................................................................
AEDPA .........................................................................................................................................................
FNKDA .........................................................................................................................................................
CDTA ...........................................................................................................................................................
VerDate Sep<11>2014
16:18 Feb 08, 2022
Jkt 256001
PO 00000
Frm 00003
Fmt 4700
Sfmt 4700
E:\FR\FM\09FER1.SGM
$91,816
311,562
82,244
1,548,075
14,074
09FER1
Maximum CMP
amount effective
February 9, 2022
$97,529
330,947
87,361
1,644,396
14,950
]]>Agencies
[Federal Register Volume 87, Number 27 (Wednesday, February 9, 2022)]
[Rules and Regulations]
[Pages 7368-7369]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-02131]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-1003; Project Identifier AD-2021-01141-R;
Amendment 39-21899; AD 2022-02-02]
RIN 2120-AA64
Airworthiness Directives; Bell Textron Inc. (Type Certificate
Previously Held by Bell Helicopter Textron Inc.) Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting an airworthiness directive (AD) that
published in the Federal Register. That AD applies to Bell Textron Inc.
(type certificate previously held by Bell Helicopter Textron Inc.)
Model 204B, 205A, 205A-1, 205B, 210, and 212 helicopters with a certain
outboard main rotor hub strap pin (pin) installed. As published, the AD
number specified in the regulatory text is incorrect. This document
corrects that error. In all other respects, the original document
remains the same.
DATES: This correction is effective February 16, 2022. The effective
date of AD 2022-02-02 remains February 16, 2022.
ADDRESSES: You may examine the AD docket at https://www.regulations.gov
by searching for and locating Docket No. FAA-2021-1003, or in person at
Docket Operations between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket contains this final rule, any
comments received, and other information. The address for Docket
Operations is U.S. Department of Transportation, Docket Operations, M-
30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue
SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: David Wilson, Aerospace Engineer, DSCO
Branch, Compliance & Airworthiness Division, FAA, 10101 Hillwood Pkwy.,
Fort Worth, TX 76177; telephone (817) 222-5786; email
[email protected].
SUPPLEMENTARY INFORMATION: AD 2022-02-02, Amendment 39-21899 (87 FR
1668, January 12, 2022) (AD 2022-02-02), requires removing any pin part
number 204-012-104-005 with a serial number prefix ``FNFS'' from
service and prohibits installing the affected pin on any helicopter.
Need for the Correction
As published, the AD number specified in the regulatory text is
incorrect. The incorrectly specified AD number was FAA-2021-1003; the
correct AD number is 2022-02-02.
Correction of Publication
This document corrects an error and correctly adds the AD as an
amendment to 14 CFR 39.13. Although no other part of the preamble or
regulatory information has been corrected, the FAA is publishing the
entire rule in the Federal Register.
The effective date of this AD remains February 16, 2022.
Since this action only corrects the AD number, it has no adverse
economic impact and imposes no additional burden on any person.
Therefore, the FAA has determined that notice and public comment
procedures are unnecessary.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Correction
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 [Corrected]
0
2. The FAA amends Sec. 39.13 by:
0
a. Removing Airworthiness Directive 2021-15-51, Amendment 39-21678 (86
FR 43406, August 9, 2021); and
0
b. Adding the following new airworthiness directive:
2022-02-02 Bell Textron Inc. (Type Certificate Previously Held by
Bell Helicopter Textron Inc.): Amendment 39-21899; Docket No. FAA-
2021-1003; Project Identifier AD-2021-01141-R.
(a) Effective Date
This airworthiness directive (AD) is effective February 16,
2022.
(b) Affected ADs
This AD replaces AD 2021-15-51, Amendment 39-21678 (86 FR 43406,
August 9, 2021) (AD 2021-15-51).
(c) Applicability
This AD applies to Bell Textron Inc. (type certificate
previously held by Bell Helicopter Textron Inc.) Model 204B, 205A,
205A-1, 205B, 210, and 212 helicopters, certificated in any
category, with an outboard main rotor hub strap pin (pin) part
number 204-012-104-005 with a serial number prefix ``FNFS''
installed.
(d) Subject
Joint Aircraft System Component (JASC) Code: 6200, Main Rotor
System.
(e) Unsafe Condition
This AD was prompted by a fatal accident in which a pin sheared
off during flight, which resulted in the main rotor blade and the
main rotor head detaching from the helicopter. The FAA is issuing
this AD to address this unsafe condition and prevent loss of control
of the helicopter.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
(1) For Model 204B, 205A, 205A-1, 205B, and 212 helicopters:
(i) Before further flight from August 24, 2021 (the effective
date of AD 2021-15-51), remove from service any pin that is
identified in paragraph (c) of this AD.
(ii) After August 24, 2021 (the effective date of AD 2021-15-
51), do not install any pin that is identified in paragraph (c) of
this AD on any helicopter.
(2) For Model 210 helicopters:
(i) Before further flight after the effective date of this AD,
remove from service any pin that is identified in paragraph (c) of
this AD.
(ii) As of the effective date of this AD, do not install any pin
that is identified in paragraph (c) of this AD on any helicopter.
[[Page 7369]]
(h) Special Flight Permits
Special flight permits are prohibited.
(i) Alternative Methods of Compliance (AMOCs)
(1) The Manager, DSCO Branch, Compliance & Airworthiness
Division, 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 DSCO Branch, send it to
the attention of the person identified in paragraph (j) 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.
(j) Related Information
For more information about this AD, contact David Wilson,
Aerospace Engineer, DSCO Branch, Compliance & Airworthiness
Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone
(817) 222-5786; email [email protected].
(k) Material Incorporated by Reference
None.
Issued on January 27, 2022.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022-02131 Filed 2-8-22; 8:45 am]
BILLING CODE 4910-13-P
