May 16, 2013 – Federal Register Recent Federal Regulation Documents

Results 151 - 161 of 161
William D. Ford Federal Direct Loan Program
Document Number: 2013-11515
Type: Rule
Date: 2013-05-16
Agency: Department of Education
The Secretary amends the William D. Ford Federal Direct Loan Program (Direct Loan Program) regulations to reflect changes made to the program by the Moving Ahead for Progress in the 21st Century Act (MAP-21), Public Law 112-141. Specifically, these interim final regulations reflect the provisions in MAP-21 that amended the Higher Education Act of 1965, as amended (HEA) to extend the 3.4 percent interest rate on Direct Subsidized Loans from July 1, 2012, to July 1, 2013, and to ensure that a borrower may not receive Direct Subsidized Loans for more than 150 percent of the published length of the educational program in which the borrower is enrolled. Under the changes made by MAP-21, if the borrower exceeds this Direct Subsidized Loan limit, the borrower also becomes responsible for the accruing interest on the Direct Subsidized Loans.
Defense Federal Acquisition Regulation Supplement; Forward Pricing Rate Proposal Adequacy Checklist (DFARS Case 2012-D035)
Document Number: 2013-11402
Type: Proposed Rule
Date: 2013-05-16
Agency: Defense Acquisition Regulations System, Department of Defense
DoD is proposing to amend the Defense Federal Acquisition Regulation Supplement (DFARS) to provide guidance to contractors for the submittal of forward pricing rate proposals to ensure the adequacy of forward pricing rate proposals submitted to the Government.
Defense Federal Acquisition Regulation Supplement: Preparation of Letter of Offer and Acceptance (DFARS Case 2012-D048)
Document Number: 2013-11401
Type: Proposed Rule
Date: 2013-05-16
Agency: Defense Acquisition Regulations System, Department of Defense
DoD is proposing to amend the Defense Federal Acquisition Regulation Supplement (DFARS) to address the contracting officer role in assisting the DoD implementing agency in preparation of the letter of offer and acceptance for a foreign military sales program that will require an acquisition.
Defense Federal Acquisition Regulation Supplement: Detection and Avoidance of Counterfeit Electronic Parts (DFARS Case 2012-D055)
Document Number: 2013-11400
Type: Proposed Rule
Date: 2013-05-16
Agency: Defense Acquisition Regulations System, Department of Defense
DoD is proposing to amend the Defense Federal Acquisition Regulation Supplement (DFARS) in partial implementation of a section of the National Defense Authorization Act for Fiscal Year 2012, and a section of the National Defense Authorization Act for Fiscal Year 2013, relating to the detection and avoidance of counterfeit electronic parts.
Defense Federal Acquisition Regulation Supplement: Only One Offer-Further Implementation (DFARS Case 2013-D001)
Document Number: 2013-11399
Type: Proposed Rule
Date: 2013-05-16
Agency: Defense Acquisition Regulations System, Department of Defense
DoD is proposing to amend the Defense Federal Acquisition Regulation Supplement (DFARS) to further implement DoD policy relating to competitive acquisitions in which only one offer is received, providing additional exceptions, and further addressing requests for data other than certified cost or pricing data from the Canadian Commercial Corporation.
Defense Federal Acquisition Regulation Supplement: System for Award Management Name Changes, Phase 1 Implementation (DFARS Case 2012-D053)
Document Number: 2013-11398
Type: Rule
Date: 2013-05-16
Agency: Defense Acquisition Regulations System, Department of Defense
DoD is issuing a final rule amending the Defense Federal Acquisition Regulation Supplement (DFARS) to reflect the joining of the Central Contractor Registration (CCR), Online Representations and Certification Application (ORCA), and Excluded Parties Listing System (EPLS) databases into the System for Award Management (SAM) database.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2013-11387
Type: Rule
Date: 2013-05-16
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for certain The Boeing Company Model 757-200 and -200PF series airplanes. That AD currently requires modifying the nacelle strut and wing structure, and repairing any damage found during the modification. This new AD specifies a maximum compliance time limit that overrides the optional threshold formula results. This AD was prompted by reports indicating that the actual operational loads applied to the nacelle are higher than the analytical loads that were used during the initial design. Subsequent analysis and service history, which includes numerous reports of fatigue cracking on certain strut and wing structure, indicated that fatigue cracking can occur on the primary strut structure before an airplane reaches its design service objective. We are issuing this AD to prevent fatigue cracking in primary strut structure and consequent reduced structural integrity of the strut.
Airworthiness Directives; Spectrolab Nightsun XP Searchlight
Document Number: 2013-11383
Type: Rule
Date: 2013-05-16
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for a certain Spectrolab Nightsun XP Searchlight Assembly (searchlight) installed on, but not limited to Agusta S.p.A. (Agusta) Model AB139 and Model AW139 helicopters, Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters, and Eurocopter Deutschland GmbH (Eurocopter) Model EC135 and Model MBB-BK 117 C-2 helicopters. This AD requires, before further flight, inserting information into the Normal Procedures section of the Rotorcraft Flight Manual (RFM), a daily check of the searchlight, and at a specified time interval or if certain conditions are found, modifying any affected searchlight gimbal assembly. This AD was prompted by a report of a searchlight vibrating and an investigation that revealed that the gimbal azimuth top nut was loose. A loose nut, if not detected and corrected, could result in a gap between the rubber edging of the top shroud and the gimbal frame, leading to degradation of pointing accuracy and stability performance of the searchlight and excessive vibration. If the nut were to entirely disengage, the searchlight could disconnect partially or totally from the helicopter, resulting in damage to the helicopter and injury to persons on the ground. The actions of this AD are intended to ensure that the searchlight remains firmly attached to the helicopter.
Information Collection Activities; Proposed Collection; Comment Request
Document Number: 2013-11340
Type: Notice
Date: 2013-05-16
Agency: Department of Health and Human Services, Agency for Healthcare Research and Quality Agency Information Collection Activities
This notice announces the intention of the Agency for Healthcare Research and Quality (AHRQ) to request that the Office of Management and Budget (OMB) approve the proposed information collection project: ``Collection of Information for Agency for Healthcare Research and Quality's (AHRQ) Hospital Survey on Patient Safety Culture Comparative Database.'' In accordance with the Paperwork Reduction Act, 44 U.S.C. 3501-3521, AHRQ invites the public to comment on this proposed information collection.
Airworthiness Directives; Agusta S.p.A. Helicopters
Document Number: 2013-10903
Type: Rule
Date: 2013-05-16
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model A119 and AW119 MKII helicopters. The existing AD currently requires inspecting the pilot and copilot engine rotary variable differential transformer (RVDT) control box assemblies to determine if the control gear locking pin is in its proper position. Since we issued that AD, Agusta has developed a terminating action for this inspection. This AD requires the same actions as the existing AD as well as modifying the RVDT control box assemblies. The actions of this AD are intended to prevent failure of an RVDT control box assembly, loss of manual control of the engine throttle, and subsequent loss of control of the helicopter.
Airworthiness Directives; Slingsby Sailplanes Ltd. Sailplanes
Document Number: 2013-10794
Type: Rule
Date: 2013-05-16
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for all Slingsby Sailplanes Ltd. Models Dart T.51, Dart T.51/17, and Dart T.51/17R sailplanes equipped with aluminum alloy spar booms. 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 an incident of glue joint failure on a starboard wing caused by water entering the area of the airbrake box that resulted in delamination and corrosion in the area of the aluminum alloy spar booms and the wing attach fittings. We are issuing this AD to require actions to address the unsafe condition on these products.