Proceedings To Determine Removability of Aliens in the United States, 65485 [2018-27859]
Download as PDF
<![CDATA[
65485
Rules and Regulations
Federal Register
Vol. 83, No. 245
Friday, December 21, 2018
This section of the FEDERAL REGISTER
contains regulatory documents having general
applicability and legal effect, most of which
are keyed to and codified in the Code of
Federal Regulations, which is published under
50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by
the Superintendent of Documents.
Background
DEPARTMENT of JUSTICE
Executive Office for Immigration
Review
8 CFR Part 1240
Proceedings To Determine
Removability of Aliens in the United
States
CFR Correction
In Title 8 of the Code of Federal
Regulations, revised as of January 1,
2018, on pages 1017–1018, in § 1240.26,
paragraphs (b)(1)(iii) and (iv) are
redesignated as paragraphs (b)(3)(iii)
and (iv).
■
[FR Doc. 2018–27859 Filed 12–20–18; 8:45 am]
BILLING CODE 1301–00–D
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
The primary category for aircraft was
created specifically for the simple, low
performance personal aircraft. Section
21.17(f) provides a means for applicants
to propose airworthiness standards for
their particular primary category
aircraft. The FAA procedure
establishing appropriate airworthiness
standards includes reviewing and
possibly revising the applicants’
proposal, publication of the submittal in
the Federal Register for public review
and comment, and addressing the
comments. After all necessary revisions,
the standards are published as approved
FAA airworthiness standards.
Comments
Proposed Primary Category
Airworthiness Design Standards;
Vertical Aviation Technologies (VAT)
Model S–52L rotorcraft was published
in the Federal Register on September
26, 2018 (83 FR 48574). No comments
were received, and the airworthiness
design standards are adopted as
proposed.
14 CFR Part 21
Applicability
Docket No. FAA–2018–0860]
These airworthiness design standards
under the primary category rule are
applicable to the VAT Model S–52L
rotorcraft. Should VAT wish to apply
these airworthiness design standards to
other rotorcraft models, VAT must
submit a new airworthiness design
standard application under the primary
rule category.
Primary Category Airworthiness
Design Standards; Vertical Aviation
Technologies (VAT) Model S–52L
Rotorcraft
Federal Aviation
Administration, DOT.
ACTION: Issuance of final airworthiness
design standards.
AGENCY:
These airworthiness design
standards are issued to Vertical Aviation
Technologies (VAT) for certification of
the Model S–52L rotorcraft under the
regulations for primary category aircraft.
DATES: These airworthiness design
standards are effective January 22, 2019.
FOR FURTHER INFORMATION CONTACT:
Michael Hughlett, Aviation Safety
Engineer, Rotorcraft Standards Branch,
Policy and Innovation Division, FAA,
10101 Hillwood Pkwy., Fort Worth,
SUMMARY:
amozie on DSK3GDR082PROD with RULES
Texas 76177; telephone (817) 222–5110;
email Michael.Hughlett@faa.gov.
SUPPLEMENTARY INFORMATION: Any
person may obtain a copy of this
information by contacting the person
named above under FOR FURTHER
INFORMATION CONTACT.
VerDate Sep<11>2014
16:23 Dec 20, 2018
Jkt 247001
Conclusion
This action affects only certain
airworthiness design standards on the
VAT Model S–52L rotorcraft. It is not a
standard of general applicability and it
affects only the applicant who applied
to the FAA for approval of these features
on the rotorcraft.
Citation
The authority citation for these
airworthiness standards is as follows:
Authority: 49 U.S.C. 106(g), 40113 and
44701.
PO 00000
Frm 00001
Fmt 4700
Sfmt 4700
Final Airworthiness Standards for
Acceptance Under the Primary
Category
CAR 13 effective 03/5/1952 as follows:
13.0, 13.10, 13.11, 13.12, 13.13, 13.14,
13.16(a), 13.16(b), 13.16(d), 13.17, 13.18,
13.19, 13.20, 13.21, 13.100, 13.101,
13.102, 13.103, 13.104, 13.110, 13.111,
13.112, 13.113, 13.114, 13.115, 13.150,
13.151, 13.153, 13.155, 13.156, 13.157.
CAR 13 effective 05/16/1953 as
follows:
13.1, 13.15, 13.152, 13.154.
14 CFR 33 through amendment 33–9
as follows:
33.4, Appendix A33.
14 CFR 33 through amendment 33–30
as follows:
33.7(b).
14 CFR 27 through amendment 27–0,
except as noted below:
• 27.853 at amendment 27–37,
• 27.1351 at amendment 27–13,
• 27.1357 at amendment 27–13,
• 27.1529 at amendment 27–18,
• 27.561 is replaced with VAT.561,
• 27.785 is replaced with VAT.785.
14 CFR 27 through amendment 27–30
as follows:
27.952(a), 27.952(c), 27.952(f),
27.952(g).
14 CFR 27 through amendment 27–35
as follows:
27.975(b).
VAT.561 General:
(a) The rotorcraft, although it may be
damaged in emergency landing
conditions on land or water, must be
designed as prescribed in this section to
protect the occupants under those
conditions.
(b) The structure must be designed to
give each occupant every reasonable
chance of escaping serious injury in a
minor crash landing when—
(1) Proper use is made of seats, belts,
and other safety design provisions;
(2) The wheels are retracted (where
applicable); and
(3) The occupant experiences the
following ultimate inertia forces relative
to the surrounding structure:
(i) Upward—4.0g.
(ii) Forward—8.0g.
(iii) Sideward—8.0g.
(iv) Downward—12.0g.
(v) Rearward—4.0g.
(c) The supporting structure must be
designed to restrain, under any ultimate
inertial load up to those specified in this
paragraph, any item of mass above and/
or behind the crew and passenger
E:\FR\FM\21DER1.SGM
21DER1
]]>Agencies
[Federal Register Volume 83, Number 245 (Friday, December 21, 2018)]
[Rules and Regulations]
[Page 65485]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-27859]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
========================================================================
Federal Register / Vol. 83, No. 245 / Friday, December 21, 2018 /
Rules and Regulations
[[Page 65485]]
DEPARTMENT of JUSTICE
Executive Office for Immigration Review
8 CFR Part 1240
Proceedings To Determine Removability of Aliens in the United
States
CFR Correction
0
In Title 8 of the Code of Federal Regulations, revised as of January
1, 2018, on pages 1017-1018, in Sec. 1240.26, paragraphs (b)(1)(iii)
and (iv) are redesignated as paragraphs (b)(3)(iii) and (iv).
[FR Doc. 2018-27859 Filed 12-20-18; 8:45 am]
BILLING CODE 1301-00-D
