80 FR 23443 - Temporary Employment of Foreign Workers in the United States; CFR Correction
DEPARTMENT OF LABOR
Employment and Training Administration Federal Register Volume 80, Issue 81 (April 28, 2015)
Employment and Training Administration
Federal Register Volume 80, Issue 81 (April 28, 2015)
| Page Range | 23443-23443 | |
| FR Document | 2015-09948 |
[Federal Register Volume 80, Number 81 (Tuesday, April 28, 2015)] [Rules and Regulations] [Page 23443] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-09948] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF LABOR Employment and Training Administration 20 CFR Part 655 Temporary Employment of Foreign Workers in the United States; CFR Correction In Title 20 of the Code of Federal Regulations, Parts 500 to 656, revised as of April 1, 2014, on page 314, in Sec. 655.10, the second paragraph (h) and the second paragraph (i) are removed. [FR Doc. 2015-09948 Filed 4-27-15; 8:45 am] BILLING CODE 1505-01-P
![Federal Register / Vol. 80, No. 81 / Tuesday, April 28, 2015 / Rules and Regulations 23443
well. The angle of installation and performance, then additional analysis or ‘‘Guidance for Demonstrating
detailed design features will determine separate test(s) may be necessary to Compliance with Seat Dynamic Testing
the nature of the occupant response. evaluate performance. for Plinths and Pallets,’’ is acceptable to
The FAA will amend these special 3. Neck Injury Criteria: The seating the FAA.
conditions or issue new special system must protect the occupant from
experiencing serious neck injury. The Inflatable Lapbelt Conditions
conditions, should unusual occupant
response in the required dynamic tests, assessment of neck injury must be If inflatable lapbelts are installed on
or additional research into occupant- conducted with the inflatable restraint single-place side-facing seats, the
injury mechanisms, indicate these activated unless there is reason to also inflatable lapbelt(s) must meet Special
special conditions are inadequate. Any consider that the neck-injury potential Conditions 25–431–SC.
future special conditions would include would be higher below the inflatable- Issued in Renton, Washington, on April 14,
due public notice. restraint threshold. 2015.
a. The Nij must be below 1.0, where Michael Kaszycki,
Conclusion
Nij = Fz/Fzc + My/Myc, and Nij intercepts Acting Manager, Transport Airplane
This action affects only certain novel limited to: Directorate, Aircraft Certification Service.
or unusual design features on one model i. Fzc = 1530 lb for tension.
[FR Doc. 2015–09784 Filed 4–27–15; 8:45 am]
of airplane. It is not a rule of general ii. Fzc = 1385 lb for compression.
applicability. iii. Myc = 229 lb-ft in flexion. BILLING CODE 4910–13–P
Under standard practice, the effective iv. Myc = 100 lb-ft in extension.
date of final special conditions would b. In addition, peak Fz must be below
be 30 days after the date of publication 937 lb in tension and 899 lb in DEPARTMENT OF LABOR
in the Federal Register; however, as the compression.
certification date for the Boeing Model c. Rotation of the head about its Employment and Training
787–9 airplane is imminent, the FAA vertical axis relative to the torso is Administration
finds that good cause exists to make limited to 105 degrees in either
these special conditions effective upon direction from forward-facing. 20 CFR Part 655
publication in the Federal Register. d. The neck must not impact any
surface. Temporary Employment of Foreign
List of Subjects in 14 CFR Part 25 4. Spine and Torso Injury Criteria: Workers in the United States; CFR
Aircraft, Aviation safety, Reporting a. The shoulders must remain aligned Correction
and recordkeeping requirements. with the hips throughout the impact
sequence, or support for the upper torso In Title 20 of the Code of Federal
The authority citation for these Regulations, Parts 500 to 656, revised as
special conditions is as follows: must be provided to prevent forward or
lateral flailing beyond 45 degrees from of April 1, 2014, on page 314, in
Authority: 49 U.S.C. 106(g), 40113, 44701, § 655.10, the second paragraph (h) and
44702, 44704. the vertical during significant spinal
loading. the second paragraph (i) are removed.
The Special Conditions b. Significant concentrated loading on [FR Doc. 2015–09948 Filed 4–27–15; 8:45 am]
Accordingly, pursuant to the the occupant’s spine, in the area BILLING CODE 1505–01–P
authority delegated to me by the between the pelvis and shoulders
Administrator, the following special during impact, including rebound, is
conditions are issued as part of the type- not acceptable. During this type of DEPARTMENT OF THE TREASURY
certification basis for Boeing Model contact, the interval for any rearward (X
787–9 airplanes modified by Boeing. direction) acceleration exceeding 20g Internal Revenue Service
must be less than 3 milliseconds as
Side-Facing Seats Conditions measured by the thoracic 26 CFR Part 301
In addition to the requirements of instrumentation specified in 49 CFR
§ 25.562: part 572, subpart E, filtered in [TD 9718]
1. Existing Criteria: Compliance with accordance with SAE International
RIN 1545–BH37
§ 25.562(c)(5) is required, except that, if (SAE) J211–1.
the anthropomorphic test device (ATD) c. Occupant must not interact with Period of Limitations on Assessment
has no apparent contact with the seat/ the armrest or other seat components in for Listed Transactions Not Disclosed
structure but has contact with an any manner significantly different than Under Section 6011; Correction
inflatable restraint, a head-injury would be expected for a forward-facing
criterion (HIC) unlimited score in excess seat installation. AGENCY: Internal Revenue Service (IRS),
of 1000 is acceptable, provided the 5. Longitudinal test(s), as necessary, Treasury.
HIC15 score for that contact is less than must be performed with the FAA ACTION: Correcting amendments.
700. Hybrid III ATD, undeformed floor, most-
2. Body-to-Wall/Furnishing Contact: If critical yaw case(s) for injury, and with SUMMARY: This document contains
a seat is installed aft of structure (e.g., all lateral structural supports (armrests/ corrections to final regulations (TD
an interior wall or furnishing) that does walls) installed. For the pass/fail injury 9718) that were published in the
not provide a homogenous contact assessments, see the criteria listed in Federal Register on Tuesday, March 31,
surface for the expected range of special conditions 1 through 4, above. 2015 (80 FR 16973). The final
mstockstill on DSK4VPTVN1PROD with RULES
occupants and yaw angles, then Note: Boeing must demonstrate that regulations relating to the exception to
additional analysis and/or test(s) may be the installation of seats via plinths or the general three-year period of
required to demonstrate that the injury pallets meets all applicable limitations on assessment under section
criteria are met for the area which an requirements. Compliance with the 6501(c)(10) of the Internal Revenue
occupant could contact. For example, if guidance contained in FAA Policy Code (Code) for listed transactions that
different yaw angles could result in Memorandum PS–ANM–100–2000– taxpayer failed to disclosed as required
different inflatable-restraint 00123, dated February 2, 2000, titled under section 6011.
VerDate Sep<11>2014 16:35 Apr 27, 2015 Jkt 235001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\28APR1.SGM 28APR1](https://thefederalregister.org/doc/80_FR_23524/page/1.svg)
Document Created: 2015-12-16 08:35:42
Document Modified: 2015-12-16 08:35:42
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| FR Citation | 80 FR 23443 |
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