March 28, 2014 – Federal Register Recent Federal Regulation Documents

Results 151 - 158 of 158
Comment Requested To Refresh the Record in EB Docket No. 04-296, on Petition Filed By the Minority Media and Telecommunications Council Proposing Changes to Emergency Alert System Rules To Support Multilingual Alerting and Emergency Information
Document Number: 2014-06444
Type: Proposed Rule
Date: 2014-03-28
Agency: Federal Communications Commission, Agencies and Commissions
In this document the Federal Communication Commission's (Commission) Public Safety and Homeland Security Bureau (PSHSB), under authority delegated by the Commission, seeks to refresh the record in EB Docket No. 04-296 on issues raised in a Petition for Immediate Interim Relief (Petition) filed by the Independent Spanish Broadcasters Association, the Office of Communications of the United Church of Christ, Inc., and the Minority Media and Telecommunications Council (hereinafter collectively or individually referred to as ``MMTC''), regarding the ability of non-English speakers to access emergency information and similar multilingual issues. The Commission initially sought comment on the petition in the Commission's First EAS Report and Order and Further Notice of Proposed Rulemaking (First R&O and FNPRM in EB Docket 04-296, and subsequently sought comment on the petition in the Commission's Second EAS Report and Order and Further Notice of Proposed Rulemaking (Second R&O and FNPRM), in that docket. MMTC also has expanded upon the petition in subsequent ex parte filings before the Commission.
Airworthiness Directives; British Aerospace Regional Aircraft Airplanes
Document Number: 2014-06245
Type: Rule
Date: 2014-03-28
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for British Aerospace Regional Aircraft Jetstream Series 3101 and Jetstream Model 3201 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as stress corrosion cracking of the main landing gear yoke pintle housing on a Jetstream series 3100 airplane. We are issuing this AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; Bombardier Inc., Airplanes
Document Number: 2014-05939
Type: Rule
Date: 2014-03-28
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This AD was prompted by results from fuel system reviews conducted by the manufacturer. This AD requires accomplishing modifications to the fuel system. We are issuing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
Electronic Logging Devices and Hours of Service Supporting Documents
Document Number: 2014-05827
Type: Proposed Rule
Date: 2014-03-28
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
The Federal Motor Carrier Safety Administration (FMCSA) proposes amendments to the Federal Motor Carrier Safety Regulations (FMCSRs) to establish: Minimum performance and design standards for hours-of-service (HOS) electronic logging devices (ELDs); requirements for the mandatory use of these devices by drivers currently required to prepare HOS records of duty status (RODS); requirements concerning HOS supporting documents; and measures to address concerns about harassment resulting from the mandatory use of ELDs. This rulemaking supplements the Agency's February 1, 2011, Notice of Proposed Rulemaking (NPRM) and addresses issues raised by the U.S. Court of Appeals for the Seventh Circuit in its 2011 decision vacating the Agency's April 5, 2010, final rule concerning ELDs as well as subsequent statutory developments. The proposed requirements for ELDs would improve compliance with the HOS rules.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2014-05558
Type: Rule
Date: 2014-03-28
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2008-08-25 that applied to certain The Boeing Company Model 747-400 and 747-400F series airplanes. AD 2008-08-25 required installing drains and drain tubes to eliminate water accumulation in the drip shield above the M826 cardfile in the main equipment center. This new AD requires installing modified drain tubes, relocating wire bundle routing, installing a new drip shield and drip shield deflectors, and replacing insulation blankets. For certain airplanes, this new AD also concurrently requires sealing the drain slot, installing spuds, and installing drain tubes. This AD was prompted by reports of continued water damage to diode fire card 285U0072-1 in the M826 automatic fire overheat logic test system cardfile following a false FWD CARGO FIRE message, with no change in frequency, which resulted in an air turn back. We are issuing this AD to prevent water from exiting over the edge of the existing drip shield and contaminating electrical components in the M826 cardfile, which could result in an electrical short and potential loss of several functions essential for safe flight.
Airworthiness Directives; Rockwell Collins, Inc. Transponders
Document Number: 2014-05202
Type: Rule
Date: 2014-03-28
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Rockwell Collins TPR-720 and TPR-900 Mode select (S) transponders that are installed on airplanes. This AD was prompted by the identification that the TPR-720 and TPR-900 Mode S transponders respond intermittently to Mode S interrogations from both ground-based and traffic collision avoidance system (TCAS-) equipped airplanes. This AD requires testing and calibration of the alignment of the transponders. We are issuing this AD to correct the unsafe condition on these products.
Energy Conservation Program: Energy Conservation Standards for Commercial Refrigeration Equipment
Document Number: 2014-05082
Type: Rule
Date: 2014-03-28
Agency: Department of Energy
The Energy Policy and Conservation Act of 1975 (EPCA), as amended, prescribes energy conservation standards for various consumer products and certain commercial and industrial equipment, including commercial refrigeration equipment (CRE). EPCA also requires the U.S. Department of Energy (DOE) to determine whether more-stringent standards would be technologically feasible and economically justified, and would save a significant amount of energy. In this final rule, DOE is adopting more-stringent energy conservation standards for some classes of commercial refrigeration equipment. It has determined that the amended energy conservation standards for these products would result in significant conservation of energy, and are technologically feasible and economically justified.
Airworthiness Directives; Airbus Airplanes
Document Number: 2014-04954
Type: Rule
Date: 2014-03-28
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2008-08-04 for certain Airbus Model A318, A319, A320, and A321 series airplanes. AD 2008-08-04 required repetitive inspections for cracking in the forward lug of the support rib 5 fitting of the left and right main landing gear (MLG), and repair or replacement of any cracked MLG fitting if necessary. AD 2008-08-04 also required modification of the rib bushings of the left and right MLG, which ended the repetitive inspections. This new AD requires, for airplanes on which certain modifications or repairs have been done, repetitive inspections for cracks of the forward lug of each left-hand and right-hand MLG support rib 5 fitting, and repair if necessary; and adds Model A318 series airplanes to the applicability. Replacement of an MLG support rib 5 fitting terminates the repetitive inspection requirements for the MLG support rib 5 fitting at that position. This AD was prompted by reports of cracks found in the forward lug of the MLG support rib 5 fitting. We are issuing this AD to prevent cracking in the forward lug of the MLG, which could result in failure of the lug and consequent collapse of the MLG during takeoff or landing.
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