Department of Transportation April 10, 2015 – Federal Register Recent Federal Regulation Documents

Retooling Recalls Workshop
Document Number: 2015-08257
Type: Notice
Date: 2015-04-10
Agency: National Highway Traffic Safety Administration, Department of Transportation
The National Highway Traffic Safety Administration (NHTSA) is announcing a workshop that will be held in Washington, DC on April 28, 2015 to discuss options to improve vehicle safety recall completion rates. The workshop will include brief NHTSA presentations outlining recent agency activities aimed at improving recall completion rates as well as recent examples of steps vehicle manufacturers have taken. Information on the date, time, location, and framework for this public event is included in this notice. Attendance requires prior registration; there will be no registration at the door. There are no fees to register or to attend this event.
Nittany and Bald Eagle Railroad Company-Trackage Rights Exemption-Norfolk Southern Railway Company
Document Number: 2015-08252
Type: Notice
Date: 2015-04-10
Agency: Surface Transportation Board, Department of Transportation
Research, Technical Assistance, and Training Programs: Application Instructions and Program Management Guidelines
Document Number: 2015-08246
Type: Notice
Date: 2015-04-10
Agency: Federal Transit Administration, Department of Transportation
The Federal Transit Administration (FTA) has placed in the docket and on its Web site, guidance in the form of an updated circular to assist applicants and recipients in implementing research, development, demonstration, and deployment projects, technical assistance projects, standards development projects, and human resources and training projects. The purpose of this circular is to provide FTA recipients updated instructions and guidance on application procedures and project management responsibilities. The revisions to FTA Circular 6100.1D are a result of changes made to FTA's Research, Development, Demonstration, and Deployment Program (Section 5312), its Technical Assistance and Standards Development Program (Section 5314), and its Human Resources and Training Program (Section 5322) as authorized or amended by the Moving Ahead for Progress in the 21st Century Act (MAP-21), Public Law 112-141.
Notice of Availability of a Record of Decision for the Trunk Highway 41 River Crossing Tier I Final Environmental Impact Statement
Document Number: 2015-08186
Type: Notice
Date: 2015-04-10
Agency: Federal Highway Administration, Department of Transportation
On March 16, 2015, the Minnesota Division of the FHWA signed the Record of Decision (ROD) for the Trunk Highway 41 River Crossing Tier I Final Environmental Impact Statement (FEIS). The ROD states the FHWA decision to declare the modified Alternative C-2 corridor as the selected alternative. The selected alternative involves the construction of a new east-west freeway connection between US 169 and US 212 within the modified Alternative C-2 corridor. The selected alternative is the environmentally-preferred alternative. The Tier I FEIS was made available to the public on December 12, 2014, through an NOA in the Federal Register (79 FR 73890) with a comment period that ended on January 12, 2015. See For Further Information Contact to request a copy of the ROD.
Illinois Central Railroad Company-Abandonment Exemption-in Champaign County, Ill
Document Number: 2015-08111
Type: Notice
Date: 2015-04-10
Agency: Surface Transportation Board, Department of Transportation
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2015-08072
Type: Proposed Rule
Date: 2015-04-10
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all The Boeing Company Model 767-200, -300, and -300F series airplanes. This proposed AD was prompted by a finding that certain barrel nuts installed at the vertical fin may be subject to stress corrosion and cracking. This proposed AD would require either repetitive inspections of vertical fin barrel nuts for corrosion or a magnetic check to identify certain barrel nuts, and corrective actions if necessary. We are proposing this AD to detect and correct corroded and loose barrel nuts that attach the vertical fin to body section 48, which could result in reduced structural integrity of the vertical fin attachment joint, loss of the vertical fin, and consequent loss of controllability of the airplane.
Interpretation of the Flight Time Limitations
Document Number: 2015-07991
Type: Proposed Rule
Date: 2015-04-10
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to interpret our regulations to not apply to flight segments that are flown by a flightcrew consisting of only two pilots and no other flight crewmembers.
Airworthiness Directives; GE Aviation Czech s.r.o. Turboprop Engines
Document Number: 2015-07865
Type: Proposed Rule
Date: 2015-04-10
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain serial number GE Aviation Czech s.r.o. M601E-11, M601E-11A, and M601F turboprop engines. This proposed AD was prompted by the determination that wear or cracking, and subsequent misalignment of the quill shaft of the engine and the power turbine (PT) shaft, may lead to rupture of the quill shaft, overspeed of the PT, and uncontained engine failure. This proposed AD would require inspection of the reduction gearbox and supporting cone. We are proposing this AD to prevent misalignment and rupture of the quill shaft, which could lead to overspeed of the PT, uncontained engine failure, and damage to the airplane.
Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
Document Number: 2015-07801
Type: Proposed Rule
Date: 2015-04-10
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all ATRGIE Avions de Transport R[eacute]gional Model ATR42 and ATR72 airplanes. This proposed AD was prompted by new occurrences of certain cracked main landing gear (MLG) rear hinge pins. This proposed AD would require identifying the serial number and part number of the MLG rear hinge pins, and replacement of pins or the MLG if necessary. We are proposing this AD to detect and correct cracked rear hinge pins, which could lead to MLG structural failure, possibly resulting in collapse of the MLG and consequent injury to the occupants of the airplane.
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