2013 – Federal Register Recent Federal Regulation Documents

EPA is proposing to partially approve and partially disapprove State Implementation Plan (SIP) revisions submitted by the State of Utah on September 20, 1999. The September 20, 1999 submittal revised the numbering and format of the Utah Administrative Code (UAC) rules within Utah's SIP. In this action, EPA is acting on those rules from the September 20, 1999 submittal that still require EPA action. Specifically, EPA is proposing to approve R307-110-16, ``Section IX, Control Measures for Area and Point Sources, Part G, Fluoride,'' and to disapprove R307-110-29, ``Section XXI, Diesel Inspection and Maintenance Program.'' In conjunction with our proposed disapproval of R307-110-29, we are also proposing to disapprove the Utah Diesel Inspection and Maintenance Program, which Utah submitted as a revision to the SIP on February 6, 1996, and which was incorporated by reference in R307-110-29 as part of the September 20, 1999 submittal. This action is being taken under section 110 of the CAA.

On January 2, 2013, the U.S. Department of Energy (DOE) issued a notice of proposed rulemaking (NOPR) to amend the test procedures for residential clothes dryers. DOE also published a supplemental NOPR (SNOPR) on February 7, 2013, to propose additional amendments to the clothes dryer test procedure. Those proposed rulemakings serve as the basis for today's action. This final rule updates the reference to the latest edition of the International Electrotechnical Commission (IEC) Standard 62301, ``Household electrical appliancesMeasurement of standby power,'' Edition 2.0 2011-01. For the test procedures at both appendix D and appendix D1 to the same subpart, DOE is adopting amendments to clarify the cycle settings used for the test cycle, the requirements for the gas supply for gas clothes dryers, the installation conditions for console lights, the method for measuring the drum capacity, the maximum allowable weighing scale range, and the allowable use of a relative humidity meter. This final rule also amends the DOE clothes dryer test procedure to create a new appendix D2 that includes the amendments discussed above and testing methods for more accurately measuring the effects of automatic cycle termination.

We propose to revise airworthiness directive (AD) 98-15-18 that applies to certain Maule Aerospace Technology, Inc. M-4, M-5, M-6, M-7, MT-7, MX-7, MXT-7, and M-8 airplanes that are equipped with rear wing lift struts, part number (P/N) 2079E, and/or front wing lift struts, P/N 2080E. AD 98-15-18 currently requires repetitively inspecting certain wing lift struts for internal corrosion and replacing of any wing lift strut where corrosion is found. Since we issued AD 98-15-18, we have been informed by the manufacturer that Model MXT-7-420 airplanes are no longer in existence, are no longer type certificated, and should be removed from the Applicability section. We have also been informed that paragraph (b) in AD 98-15-18 is being misinterpreted and is causing confusion. This proposed AD would remove Model MXT-7-420 airplanes from the Applicability section and clarify the intent of the language currently in paragraph (b) of AD 98-15-18. This proposed AD would retain all other requirements of the existing AD. We are proposing this AD to correct the unsafe condition on these products.

NMFS implements management measures described in a regulatory amendment (Regulatory Amendment 15) to the Fishery Management Plan for the Snapper-Grouper Fishery of the South Atlantic Region (FMP), as prepared by the South Atlantic Fishery Management Council (Council). This final rule increases the commercial and recreational ACLs for yellowtail snapper, decreases the commercial ACL for gag, and revises the accountability measure (AM) for gag by removing the requirement that all other South Atlantic shallow-water grouper (SASWG) are prohibited from harvest when the gag commercial ACL is met or projected to be met. In addition, Regulatory Amendment 15 revises the optimum yield (OY) for yellowtail snapper and increases the recreational annual catch target (ACT) for yellowtail snapper harvested in or from the South Atlantic exclusive economic zone (EEZ). This final rule also includes several administrative changes to regulatory text, which are unrelated to the measures contained in Regulatory Amendment 15. The purpose of Regulatory Amendment 15 and this final rule is to provide socio-economic benefits to snapper-grouper fishermen and communities that utilize the snapper-grouper resource, while maintaining fishing mortality at sustainable levels according to the best scientific information available.

The Bureau of Indian Affairs (BIA) is confirming the interim final rule published and effective on March 3, 2013, addressing the addition of two Indian tribes to the list of tribes with Courts of Indian Offenses (also known as CFR Courts), and deletion of five tribes from those under the jurisdiction of CFR Courts. The March 3, 2013, publication stated that the BIA would review comments on the interim final rule and either confirm the rule or initiate a proposed rulemaking. BIA did not receive any comments, and therefore confirms the rule without change.

Modified Base (1% annual-chance) Flood Elevations (BFEs) are finalized for the communities listed below. These modified BFEs will be used to calculate flood insurance premium rates for new buildings and their contents.

The U.S. Department of Energy (DOE) proposes to determine that natural draft commercial packaged boilers meet the criteria for covered equipment under Part A-1 of Title III of the Energy Policy and Conservation Act (EPCA), as amended. DOE proposes that classifying equipment of such type as covered equipment is necessary to carry out the purpose of Part A-1 of EPCA, which is to improve the efficiency of certain industrial equipment to conserve the energy resources of the Nation.

We propose to adopt a new airworthiness directive (AD) for certain EADS CASA (Type Certificate Previously Held by Construcciones Aeron[aacute]uticas, S.A.) Model C-212-CB, C-212-CC, C-212-CD, C-212- CE, and C-212-DF airplanes. This proposed AD was prompted by a report of the propeller pitch control (PPC) lever becoming disconnected from the engine due to a missing bolt. This proposed AD would require modifying the PPC lever attachment system. We are proposing this AD to prevent PPC shaft disconnection, which could lead to a loss of propeller pitch control, possibly resulting in uncommanded change to the engine power settings and consequent reduced controllability of the airplane.

We propose to supersede airworthiness directive (AD) 2009-24- 07, which applies to certain The Boeing Company Model 737-600, -700, - 700C, and -800 series airplanes. AD 2009-24-07 currently requires repetitive lubrications of the right and left main landing gear (MLG) forward trunnion pins. AD 2009-24-07 also requires an inspection for discrepancies of the transition radius of the MLG forward trunnion pins, and corrective actions if necessary. For certain airplanes, AD 2009-24-07 requires repetitive detailed inspections for discrepancies (including finish damage, corrosion, pitting, and base metal scratches) of the transition radius of the left and right MLG trunnion pins, and corrective action if necessary. Replacing or overhauling the trunnion pins would terminate the actions required by AD 2009-24-07. This proposed AD would add airplanes to the applicability of AD 2009-24-07. We are proposing this AD to prevent stress corrosion cracking of the forward trunnion pins, which could result in fracture of the pins and consequent collapse of the MLG.

We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This proposed AD was prompted by a report that a batch of main landing gear (MLG) door actuators with a certain part number having certain serial numbers could be assembled with the scraper installed backward. This proposed AD would require repetitive functional checks of the MLG alternate extension system (AES) and eventual replacement of certain MLG door actuators with actuators that have either been reworked or do not have certain serial numbers. We are proposing this AD to prevent incorrectly installed scrapers, which could hinder the operation of the MLG AES, and result in failure of the MLG AES on one side, and consequent unsafe asymmetrical landing configuration.

We are revising an earlier proposed airworthiness directive (AD), for all The Boeing Company Model 727 airplanes, which proposed to supersede an existing AD. That NPRM proposed to retain repetitive inspections of the in-tank fuel boost pump wiring, installation of sleeving over the in-tank fuel boost pump wires, repetitive inspections of a certain electrical wire, sleeve, and conduit, and applicable investigative and corrective actions; and repetitive engine fuel suction feed operational tests. That NPRM proposed to also require replacement of the wire bundles for the wing and center fuel boost pumps, installation of convoluted liners, and related investigative and corrective actions if necessary. That NPRM also proposed to require replacement of the fuel quantity indicating system (FQIS) wires; a low- frequency eddy current inspection for cracking; and repair if necessary. That NPRM also proposed to require revising the maintenance program to incorporate changes to the airworthiness limitations section. That NPRM was prompted by a report of damage found to the sleeve, jacket, and insulation on an electrical wire during a repetitive inspection. This action revises that NPRM by revising certain compliance times, specifying a terminating action, and adding a proposed requirement to incorporate another change to the airworthiness limitations section. We are proposing this supplemental NPRM to prevent chafing of the fuel boost pump electrical wiring and leakage of fuel into the conduit, and to prevent electrical arcing between the wiring and the surrounding conduit, which could result in arc-through of the conduit, and consequent fire or explosion of the fuel tank. Since these actions impose an additional burden over that proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.

We propose to supersede an existing airworthiness directive (AD) that applies to certain Learjet Inc. Model 60 airplanes. The existing AD currently requires determining if a certain fuel crossflow tube is installed; and follow-on/corrective actions, as applicable. Since we issued that AD, we have received a report that airplanes produced since 2003 might also be subject to the unsafe condition; and that the minimum allowable clearance is not established in the airplane maintenance information, and therefore, must be addressed by this proposed AD. This proposed AD would retain all actions in the previous AD, and would require determining if a certain fuel crossflow tube is installed, performing repetitive measurements of the fuel crossflow tube and surrounding valves and cables, and doing corrective actions if applicable. In addition, this proposed AD expands the applicability of the existing AD. We are proposing this AD to prevent chafing and consequent failure of the fuel crossflow tube due to inadequate clearance between the tube and the flight control cables, which could result in loss of fuel from one fuel tank during normal operating conditions or loss of fuel from both main fuel tanks during fuel cross- feeding operations.

This document contains proposed regulations relating to relief from joint and several tax liability under section 6015 of the Internal Revenue Code (Code) and relief from the Federal income tax liability resulting from the operation of state community property laws under section 66. The proposed regulations provide guidance to taxpayers on when and how to request relief under sections 66 and 6015. This document also invites comments from the public regarding these proposed regulations.

This action modifies Class E airspace at Brigham City Airport, Brigham City, UT. Decommissioning of the Brigham City Nondirectional Radio Beacon (NDB) has made this action necessary for the safety and management of Instrument Flight Rules (IFR) operations at the airport. This action also makes an adjustment to the geographic coordinates of the airport.

The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. The AD applies to certain Eurocopter Deutschland GmbH (Eurocopter) Model EC135 helicopters. The reference to Title 14, Code of Federal Regulations (14 CFR) 91.173 in the Required Actions section is incorrect. This document corrects that error. In all other respects, the original document remains the same.

We are adopting a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model AB412 and AB412 EP, and Bell Helicopter Textron (Bell) Model 412, 412CF, and 412EP helicopters with certain DART Aerospace Ltd. (Dart) high gear aft crosstubes (crosstube) installed. This AD requires adding a life limit of 10,000 landings to the crosstube and removing from service any crosstubes with more than 10,000 accumulated landings. This AD is prompted by five separate reports of crosstube failures. The actions in this AD are intended to prevent failure of the crosstube and subsequent collapse of the landing gear.

We are adopting a new airworthiness directive (AD) for certain Pratt & Whitney Canada Corp. (P&WC) PW118A, PW118B, PW119B, PW119C, PW123, PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B, PW125B, PW126A, PW127, PW127E, PW127F, PW127G, and PW127M turboprop engines. This AD was prompted by reports of fractures of the first-stage power turbine (PT) blade. This AD requires inspection of the first-stage PT blades and the removal from service of those blades that fail the inspection or their replacement with blades eligible for installation. We are issuing this AD to prevent fracture of the first-stage PT blade, possible engine fire, and damage to the airplane.

We, the U.S. Fish and Wildlife Service, determine that Sphaeralcea gierischii (Gierisch mallow) meets the definition of an endangered species under the Endangered Species Act of 1973, as amended (Act). Gierisch mallow is a plant species found in Mohave County, Arizona, and Washington County, Utah. This final rule implements the Federal protections provided by the Act for this species. The effect of this regulation is to add this species to the List of Endangered and Threatened Plants.

NMFS announces that the Mid-Atlantic Fishery Management Council (Council) has submitted Amendment 14 to the Atlantic Mackerel, Squid, and Butterfish Fishery Management Plan (Amendment 14), incorporating the Final Environmental Impact Statement (FEIS) and the Initial Regulatory Flexibility Analysis (IRFA), for review by the Secretary of Commerce, and is requesting comments from the public.

The Environmental Protection Agency (EPA) Region 6 is issuing a Notice of Intent to Delete the Mosley Road Sanitary Landfill (MRSL) Superfund Site (Site) located in Oklahoma City, Oklahoma County, Oklahoma, from the National Priorities List (NPL) and requests public comments on this proposed action. The NPL, promulgated pursuant to section 105 of the Comprehensive Environmental Response, Compensation, and Liability Act (CERCLA) of 1980, as amended, is an appendix of the National Oil and Hazardous Substances Pollution Contingency Plan (NCP). The EPA and the State of Oklahoma, through the Oklahoma Department of Environmental Quality (ODEQ), have determined that all appropriate response actions under CERCLA have been completed. However, this deletion does not preclude future actions under Superfund.

This document announces an extension of the time period for submitting comments on the proposed determination that computer servers (servers) qualify as a covered product.

We propose to supersede airworthiness directive (AD) 2007-16- 19, which applies to certain The Boeing Company Model 747-200B, 747- 300, and 747-400 series airplanes. AD 2007-16-19 requires repetitive detailed inspections for cracking of the aft tension tie channels from body station (BS) 1120 to BS 1220 and from BS 880 to BS 1100, and corrective actions if necessary, and optional terminating action. Since we issued that AD, analysis has indicated the need to mandate the previously optional modification. This proposed AD would retain the existing requirements, limit the area of the detailed inspection, add repetitive surface high-frequency eddy current inspections, and mandate the previously optional terminating action. We are proposing this AD to prevent fatigue cracking of the tension ties, which could result in reduced structural integrity of the airplane and rapid depressurization of the airplane.

We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 767-200, -300, -300F, and -400ER airplanes. This proposed AD was prompted by reports indicating that a standard access door was located where an impact-resistant access door was required, and stencils were missing from some impact-resistant access doors. This proposed AD would require an inspection of the left- and right-hand wing fuel tank access doors to determine that impact- resistant access doors are installed in the correct locations, and to replace any door with an impact-resistant access door if necessary. This proposed AD also would require an inspection for stencils and index markers on impact-resistant access doors, and application of new stencils or index markers if necessary. This proposed AD would also require revising the maintenance program to incorporate changes to the airworthiness limitations section. We are proposing this AD to prevent foreign object penetration of the fuel tank, which could cause a fuel leak near an ignition source (e.g., hot brakes or engine exhaust nozzle), consequently leading to a fuel-fed fire.

This action proposes to amend Class E airspace at Kankakee, IL. Additional controlled airspace is necessary to accommodate amended Standard Instrument Approach Procedures (SIAP) at Greater Kankakee Airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR) operations for SIAPs at the airport. Geographic coordinates would also be updated.

This action proposes to establish Class D airspace at Mesquite, TX. Establishment of an air traffic control tower at Mesquite Metro Airport has made this action necessary for the safety and management of Instrument Flight Rules (IFR) operations at Mesquite Metro Airport.