Department of Transportation November 15, 2012 – Federal Register Recent Federal Regulation Documents

2017 and Later Model Year Light-Duty Vehicle Greenhouse Gas Emissions and Corporate Average Fuel Economy Standards
Document Number: C1-2012-21972
Type: Rule
Date: 2012-11-15
Agency: Environmental Protection Agency, National Highway Traffic Safety Administration, Department of Transportation
Orders Limiting Operations at John F. Kennedy International Airport, LaGuardia Airport, and Newark Liberty International Airport; High Density Rule at Reagan Washington National Airport
Document Number: 2012-27844
Type: Notice
Date: 2012-11-15
Agency: Federal Aviation Administration, Department of Transportation
This action announces a limited waiver of the requirement to use Operating Authorizations (slots) at John F. Kennedy International Airport (JFK), LaGuardia Airport (LGA), and Newark Liberty International Airport (EWR). This action also declines to grant a waiver of the requirement to use slots at Reagan Washington National Airport. This waiver is effective from October 28, 2012 through November 2, 2012.
Proposed Agency Information Collection Activities; Comment Request
Document Number: 2012-27790
Type: Notice
Date: 2012-11-15
Agency: Federal Railroad Administration, Department of Transportation
In accordance with the Paperwork Reduction Act of 1995 and its implementing regulations, the Federal Railroad Administration (FRA) hereby announces that it is seeking renewal of the following currently approved information collection activities. Before submitting these information collection requirements for clearance by the Office of Management and Budget (OMB), FRA is soliciting public comment on specific aspects of the activities identified below.
Qualification of Drivers; Exemption Applications; Vision
Document Number: 2012-27697
Type: Notice
Date: 2012-11-15
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces its decision to renew the exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations for 12 individuals. FMCSA has statutory authority to exempt individuals from the vision requirement if the exemptions granted will not compromise safety. The Agency has concluded that granting these exemption renewals will provide a level of safety that is equivalent to or greater than the level of safety maintained without the exemptions for these commercial motor vehicle (CMV) drivers.
Qualification of Drivers; Exemption Applications; Vision
Document Number: 2012-27695
Type: Notice
Date: 2012-11-15
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces its decision to renew the exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations for 11 individuals. FMCSA has statutory authority to exempt individuals from the vision requirement if the exemptions granted will not compromise safety. The Agency has concluded that granting these exemption renewals will provide a level of safety that is equivalent to or greater than the level of safety maintained without the exemptions for these commercial motor vehicle (CMV) drivers.
Qualification of Drivers; Exemption Applications; Vision
Document Number: 2012-27693
Type: Notice
Date: 2012-11-15
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces its decision to renew the exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations for 32 individuals. FMCSA has statutory authority to exempt individuals from the vision requirement if the exemptions granted will not compromise safety. The Agency has concluded that granting these exemption renewals will provide a level of safety that is equivalent to or greater than the level of safety maintained without the exemptions for these commercial motor vehicle (CMV) drivers.
Modification of Class E Airspace; Pullman, WA
Document Number: 2012-27668
Type: Rule
Date: 2012-11-15
Agency: Federal Aviation Administration, Department of Transportation
This action modifies Class E airspace at Pullman/Moscow Regional Airport, Pullman, WA. Controlled airspace is necessary to accommodate aircraft using Area Navigation (RNAV) Global Positioning System (GPS) standard instrument approach procedures at Pullman/Moscow Regional Airport. This action also makes a minor change to the legal description in reference to Class E airspace extending upward from 700 feet above the surface. This improves the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Establishment of Class E Airspace; Coaldale, NV
Document Number: 2012-27666
Type: Rule
Date: 2012-11-15
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Coaldale VHF Omni- Directional Radio Range Tactical Air Navigational Aid (VORTAC), Coaldale, NV to facilitate vectoring of Instrument Flight Rules (IFR) aircraft under control of Oakland Air Route Traffic Control Center (ARTCC). This action enhances the safety and management of IFR operations within the National Airspace System.
Amendment of Class D and Class E Airspace; Lewiston, ID
Document Number: 2012-27659
Type: Rule
Date: 2012-11-15
Agency: Federal Aviation Administration, Department of Transportation
This action modifies the Class D and Class E airspace areas at Lewiston, ID, to accommodate aircraft using Area Navigation (RNAV) (GPS) standard instrument approach procedures at Lewiston-Nez Perce County Airport. Also, the geographic coordinates are updated for the airport and navigational aids. This improves the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Notice of Final Federal Agency Actions on Proposed Highway in Indiana
Document Number: 2012-27617
Type: Notice
Date: 2012-11-15
Agency: Federal Highway Administration, Department of Transportation
This notice announces actions taken by the FHWA and the USACE that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to proposed highway projects for a 26.7 mile segment of I-69 in the Counties of Greene and Monroe, State of Indiana, and grant licenses, permits, and approvals for the project.
Airworthiness Directives; Bell Helicopter Textron Helicopters
Document Number: 2012-27059
Type: Rule
Date: 2012-11-15
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Bell Helicopter Textron (BHT) Model 412, 412EP, and 412CF helicopters. This AD requires a repetitive inspection of the collective lever for a crack, and if there is a crack, before further flight, replacing the collective lever with an airworthy collective lever. This AD was prompted by a reported failure of a collective lever. The actions are intended to detect a crack in the collective lever, which could lead to failure of the collective lever and subsequent loss of control of the helicopter.
Airworthiness Directives; Fokker Services B.V. Airplanes
Document Number: 2012-27057
Type: Rule
Date: 2012-11-15
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for all Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. That AD currently requires revising the airworthiness limitations section (ALS) of the instructions for continued airworthiness for certain airplanes, and the FAA-approved maintenance program for certain other airplanes, to incorporate new limitations. This new AD requires revising the maintenance program to incorporate the limitations, tasks, thresholds, and intervals specified in certain revised Fokker maintenance review board (MRB) documents. This AD was prompted by a revised Fokker 70/100 MRB document with revised limitations, tasks, thresholds, and intervals. We are issuing this AD to reduce the potential of structural failures or 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.
Airworthiness Directives; Airbus Airplanes
Document Number: 2012-27055
Type: Rule
Date: 2012-11-15
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Airbus Model A300 B4-600 and A300 B4-600R, Model A300, and Model A310 series airplanes. This AD was prompted by reports of fatigue cracking in the crossbeams at the junction of the actuator beam of the lower deck cargo door. This AD requires repetitive inspections of the crossbeams of certain fuselage frames, and repair if necessary. We are issuing this AD to detect and correct cracking of the crossbeams at the junction of the actuator beam of the lower deck cargo door, which could result in failure to withstand ultimate load conditions, and consequent reduced structural integrity of the airplane.
Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters
Document Number: 2012-27050
Type: Rule
Date: 2012-11-15
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing Emergency airworthiness directive (AD) for Sikorsky Aircraft Corporation (Sikorsky) Model S-70, S-70A, S-70C, S-70C(M), and S-70C(M1) helicopters with a certain part- numbered intermediate gearbox (IGB). The existing Emergency AD requires a one-time inspection of the internal oil passages of the IGB for an obstruction. That Emergency AD was prompted by an accident that resulted from blockage of oil in the IGB by a plug that was inadvertently left in the IGB during the coating of the IGB housing. We are issuing this supersedure to that Emergency AD to include two additional part numbers of affected IGBs and identify a specific date since new or overhaul of the affected IGBs. The actions specified by this AD are intended to detect a plug in the IGB and prevent overheating and seizing of the IGB, failure of the tail rotor drive output shaft, loss of tail rotor drive, and subsequent loss of control of the helicopter.
Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters
Document Number: 2012-27049
Type: Rule
Date: 2012-11-15
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Sikorsky Aircraft Corporation (Sikorsky) Model S-76C helicopters. This AD requires installing an improved throttle stop and a wider trigger on the engine control levers (ECL). This AD was prompted by a bird-strike to the windshield that resulted in unintended movement of the engine control levers from the forward position and towards the flight-idle position, which reduced power on both engines. These actions are intended to prevent unintended movement of the ECLs, resulting in main rotor speed decay and subsequent loss of control of the aircraft.
Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters
Document Number: 2012-26907
Type: Rule
Date: 2012-11-15
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This AD requires inspecting the tail rotor (T/R) pylon for a loose or missing fastener, a crack, damage, or corrosion and adding an internal doubler to the aft shear deck tunnel assembly. This AD was prompted by the discovery of cracks in T/R pylons. The actions are intended to detect a loose or missing fastener, a crack, damage, or corrosion on the T/R pylon and, if present, to repair the T/R pylon and install a doubler on the aft shear deck tunnel assembly or to replace the T/R pylon and install a doubler on the aft shear deck tunnel assembly. The actions are intended to prevent failure of the T/R pylon or other T/R components, which could lead to the loss of control of the helicopter.
Airworthiness Directives; Fokker Services B.V. Airplanes
Document Number: 2012-26781
Type: Rule
Date: 2012-11-15
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for certain Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. That AD currently requires performing a detailed visual inspection for cracks of the pistons on the main landing gear (MLG), and replacing the affected pistons if necessary. This new AD also requires modifying the MLG by installing a piston containing a certain part number, and revising the airplane maintenance program. This AD was prompted by a new modification developed to safeguard the integrity of the MLG assembly and improve surface protection of the affected area of the MLG piston. We are issuing this AD to prevent MLG failure, possibly resulting in loss of control of the airplane during the landing roll- out.
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