April 5, 2012 – Federal Register Recent Federal Regulation Documents

Results 101 - 113 of 113
Plant Variety Protection Board; Open Meeting
Document Number: 2012-8126
Type: Notice
Date: 2012-04-05
Agency: Department of Agriculture
This notice is intended to notify the public of their opportunity to attend an open meeting of the Plant Variety Protection Board.
Revision of Cotton Classification Procedures for Determining Cotton Leaf Grade
Document Number: 2012-8125
Type: Rule
Date: 2012-04-05
Agency: Agricultural Marketing Service, Department of Agriculture
The Agricultural Marketing Service (AMS) is amending the procedures for determining the official leaf grade for Upland and Pima cotton. The leaf grade is a part of the official classification which denotes cotton fiber quality used in cotton marketing and manufacturing of cotton products. Previously, the leaf grade was determined by visual examination and comparison to the Universal Cotton Standards for Leaf Grade that serves as the official cotton standards by qualified cotton classers. Amended procedures replace the classer's leaf determination with the instrument leaf measurement made by the High Volume Instrument (HVI) system, which has been used in official cotton classification for Upland Cotton since 1991.
Change in Bank Control Notices; Acquisitions of Shares of a Bank or Bank Holding Company
Document Number: 2012-8118
Type: Notice
Date: 2012-04-05
Agency: Federal Reserve System, Agencies and Commissions
Airworthiness Directives; Agusta S.p.A. Helicopters
Document Number: 2012-8058
Type: Rule
Date: 2012-04-05
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model AB412 helicopters with certain tail rotor blades (blades) installed. This AD requires, before further flight, removing and replacing each affected blade with an airworthy blade. This AD is prompted by incidents where a blade tip weight separated from a blade in flight on other model helicopters with common part-numbered blades. It has been determined that this unsafe condition may also exist on the specified Agusta model helicopters. The actions specified in this AD are intended to prevent loss of the blade tip weight, loss of a blade, and subsequent loss of control of the helicopter.
Defense Federal Acquisition Regulation Supplement: Solicitation Provisions and Contract Clauses for Acquisitions of Commercial Items
Document Number: 2012-8053
Type: Proposed Rule
Date: 2012-04-05
Agency: Defense Acquisition Regulations System, Department of Defense
DoD is proposing to amend the Defense Federal Acquisition Regulation Supplement (DFARS) to simplify prescriptions for provisions and clauses that are applicable to the acquisition of commercial items and to specify flowdown of clauses to commercial subcontracts.
Airworthiness Directives; Bombardier, Inc. Model BD-100-1A10 (Challenger 300) Airplanes
Document Number: 2012-8041
Type: Rule
Date: 2012-04-05
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Bombardier, Inc. Model BD-100-1A10 (Challenger 300) airplanes. This AD was prompted by reports that the horizontal stabilizer trim actuator (HSTA) no-back and the number 1 motor brake assembly (MBA) can both fail dormant. This AD requires revising the airplane maintenance schedule to include new functional tests of the HSTA no-back and HSTA brake system. We are issuing this AD to prevent dormant failure of the HSTA no-back and the number 1 MBA, which along with additional component failure could result in an uncontrollable horizontal stabilizer surface runaway without the ability to retrim, and consequent loss of the airplane.
Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes
Document Number: 2012-8040
Type: Rule
Date: 2012-04-05
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for all Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model L-1011-385-1, L-1011-385-1-14, and L-1011-385-1-15 airplanes. That AD currently requires implementation of a Supplemental Inspection Document (SID) program of structural inspections to detect fatigue cracking, and repair if necessary, to ensure continued airworthiness of these airplanes as they approach the manufacturer's original fatigue design life goal. This new AD adds Model L-1011-385-3 airplanes to the applicability, changes certain inspection thresholds, adds three new structurally significant details (SSDs), and removes an SSD that has been addressed by a different AD. This AD was prompted by an evaluation by the manufacturer of usage and flight data that provided additional information about certain SSDs where fatigue damage is likely to occur. We are issuing this AD to prevent fatigue cracking that could compromise the structural integrity of these airplanes.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2012-8038
Type: Rule
Date: 2012-04-05
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-600, -700, -700C, -800, and -900 series airplanes. This AD was prompted by reports of heat damage to the inner wall of the thrust reversers, which could result in separation of adjacent components and consequent structural damage to the airplane, damage to other airplanes, and injury to people on the ground. This AD requires modifying the thrust reverser inner walls, inspecting for damage of the upper and lower inner wall insulation blankets, measuring the electrical conductivity on the aluminum upper compression pads 2 and 3 as applicable, inspecting for discrepancies of the inner wall of the thrust reverser, and corrective actions if necessary. This AD also requires, for certain airplanes, doing various concurrent actions (including replacing the inner wall blanket insulation, installing updated full-authority digital electronic control software, and modifying the thrust reverser inner wall and insulation blankets). We are issuing this AD to correct the unsafe condition on these products.
Airworthiness Directives; 328 Support Services GmbH Airplanes
Document Number: 2012-7850
Type: Rule
Date: 2012-04-05
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for all 328 Support Services GmbH (Type Certificate previously held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt GmbH) Model 328-100 and -300 airplanes. That AD currently requires performing a detailed visual inspection of the cockpit door locking device and the surrounding area for proper installation, and corrective action if necessary. This new AD requires removing or replacing the locking device of the cockpit door; performing operational tests, and repair if necessary; and, for certain airplanes, installing gap filler parts. This AD was prompted by a report that a right-hand power lever jammed in flight-idle position during the landing roll-out, and the airplane was stopped by excessive braking. We are issuing this AD to detect and correct interference with the engine and flight control cables, which could result in reduced controllability of the airplane.
Airworthiness Directives; Airbus Airplanes
Document Number: 2012-7848
Type: Rule
Date: 2012-04-05
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Airbus Model A340-500 and -600 series airplanes. This AD requires repetitive inspections of the forward and aft attachment fittings and of the swan neck for cracks, and replacing the attachment fittings and the swan neck with serviceable ones if necessary. This AD was prompted by reports of cracks on the forward attachment fittings of the left and right sides of the forward hinge of the nose landing gear (NLG) aft door. We are issuing this AD to detect and correct cracks of the forward attachment fittings and the swan neck, which could lead to the in-flight detachment of the NLG aft door and result in injury to persons on the ground or damage to the airplane.
Notice of Procedures for Submitting Clarifying Questions Concerning the Flight, Duty, and Rest Requirements of Part 117
Document Number: 2012-7739
Type: Rule
Date: 2012-04-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA published a final rule on January 4, 2012 that amends the existing flight, duty and rest regulations applicable to certificate holders and their flightcrew members. Since then, the FAA has received questions from stakeholders concerning the provisions of the final rule. In response to these questions, the FAA is issuing this document, which announces the procedures for submitting clarifying questions to the final rule.
Connect America Fund; A National Broadband Plan for Our Future; Establishing Just and Reasonable Rates for Local Exchange Carriers; High-Cost Universal Service Support
Document Number: 2012-7057
Type: Rule
Date: 2012-04-05
Agency: Federal Communications Commission, Agencies and Commissions
In this document, the Federal Communications Commission clarifies certain rules. The order clarifies, but does not otherwise modify, the USF/ICC Transformation Order. The petition for Clarification or, in the Alternative, for Reconsideration of Verizon is granted in part and dismissed in part, and the Petition for Reconsideration of United States Telecom Association is dismissed in part.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2012-6642
Type: Rule
Date: 2012-04-05
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 757 airplanes. This AD requires replacing the power control relays for the fuel boost pumps and override pumps with new relays having a ground fault interrupter (GFI) feature. This AD also requires an electrical bonding resistance measurement for certain GFI relays to verify that certain bonding requirements are met. This AD also requires, for certain airplanes, an inspection to ensure that certain screws are properly installed, and installing longer screws if necessary. This AD was prompted by fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent damage to the fuel pumps caused by electrical arcing that could introduce an ignition source in the fuel tank, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
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