Department of Transportation 2006 – Federal Register Recent Federal Regulation Documents

Results 101 - 150 of 3,043
Noise Exposure Map Notice: Receipt of Noise Compatibility Program and Request for Review
Document Number: 06-9752
Type: Notice
Date: 2006-12-18
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces its determination that the noise exposure maps submitted by Saint Louis County for Spirit of St. Louis Airport under the provisions of 49 U.S.C. 47501 et. seq (Aviation Safety and Noise Abatement Act) and 14 CFR Part 150 are in compliance with applicable requirements. The FAA also announces that it is reviewing a proposed noise compatibility program that was submitted for Spirit of St. Louis Airport under Part 150 in conjunction with the noise exposure map, and that this program will be approved or disapproved on or before June 10, 2007
Approval of Noise Compatibility Program for McClellan Palomar Airport, Carlsbad, CA
Document Number: 06-9740
Type: Notice
Date: 2006-12-18
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces its findings on the noise compatibility program submitted by San Diego County, California under the provisions of Title I of the Aviation Safety and Noise Abatement Act, as amended, (Public Law96-193) (hereinafter referred to as ``the Act'') and 14 CFR Part 150. These findings are made in recognition of the description of Federal and nonfederal responsibilities in Senate Report No. 96-52 (1980). On April 26, 2005, the FAA determined that the noise exposure maps submitted by San Diego County under Part 150 were in compliance with applicable requirements.
Forum on Human Factors Research Necessary To Support Advanced Vehicle Safety Technologies; Correction
Document Number: 06-9735
Type: Notice
Date: 2006-12-18
Agency: National Highway Traffic Safety Administration, Department of Transportation
NHTSA published a document in the Federal Register of November 20, 2006, concerning a meeting notice for a forum on Human Factors Research Necessary to Support Advanced Vehicle Safety Technologies. The document did not contain the Docket Number.
Shippers-General Requirements for Shipments and Packagings
Document Number: 06-55531
Type: Rule
Date: 2006-12-18
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
Airworthiness Directives; Airbus Model A320 Series Airplanes
Document Number: E6-21354
Type: Proposed Rule
Date: 2006-12-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A320 series airplanes. This proposed AD would require replacing the carbon fiber reinforced plastic (CFRP) actuator fittings of the rudder with aluminum actuator fittings and doing related investigative and corrective actions. This proposed AD results from rupture of a CFRP actuator fitting during maintenance. We are proposing this AD to prevent rupture of a rudder actuator fitting, which could result in reduced controllability of the airplane.
Britax Child Safety, Inc., Receipt of Petition for Decision of Inconsequential Noncompliance
Document Number: E6-21329
Type: Notice
Date: 2006-12-15
Agency: National Highway Traffic Safety Administration, Department of Transportation
Hankook Tire Company, Ltd., Receipt of Petition for Decision of Inconsequential Noncompliance
Document Number: E6-21328
Type: Notice
Date: 2006-12-15
Agency: National Highway Traffic Safety Administration, Department of Transportation
Minimum Levels of Financial Responsibility for Motor Carriers; Petitions for Rulemaking
Document Number: E6-21314
Type: Proposed Rule
Date: 2006-12-15
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
The Federal Motor Carrier Safety Administration (FMCSA) announces it is considering whether to amend its financial responsibility requirements for motor carriers in response to two petitions for rulemaking. The Government of Canada (Canada) petitioned FMCSA to amend these requirements to permit, as acceptable evidence of financial responsibility, a policy of insurance issued by a Canadian insurance company legally authorized to issue such policies in the Province or Territory of Canada where the motor carrier has its principal place of business. Canada believes the FMCSA's current regulations place Canada-domiciled motor carriers operating in the United States at a competitive disadvantage with U.S.-domiciled carriers. The Property Casualty Insurers Association of America (PCI) petitioned FMCSA to make revisions to the MCS-90 and MCS-90B endorsements to clarify that language in the endorsements imposing liability for negligence occurring ``on any route or in any territory authorized to be served by the insured or elsewhere'' does not include liability connected with transportation within Mexico. FMCSA seeks input from the public in the form of data or other information in response to several questions posed in the ANPRM to assist the Agency in evaluating these proposals.
Fortress Investment Group LLC, et al.-Control Exemption-RailAmerica, Inc., et al.
Document Number: E6-21302
Type: Notice
Date: 2006-12-15
Agency: Surface Transportation Board, Department of Transportation
Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A and CL-601-3R) Airplanes
Document Number: E6-21268
Type: Rule
Date: 2006-12-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL- 600-2B16 (CL-601-3A and CL-601-3R) airplanes. This AD requires implementing a corrosion prevention and control program (CPCP) either by accomplishing specific tasks or by revising the maintenance inspection program to include a CPCP. This AD results from the determination that, as airplanes age, they are more likely to exhibit indications of corrosion. We are issuing this AD to prevent structural failure of the airplane due to corrosion.
Airworthiness Directives; Bombardier Model DHC-8-400 Series Airplanes
Document Number: E6-21267
Type: Rule
Date: 2006-12-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-400 series airplanes. This AD requires repetitive cleaning/inspecting of the drain hole of each pitot static probe and repetitive cleaning of the pitot lines in the pitot static system. This AD results from reports of incidents of airspeed mismatch between the pilot, co-pilot, and standby airspeed indications caused by contamination in the pitot static system. We are issuing this AD to prevent erroneous/misleading altitude and airspeed information from a contaminated pitot static system to the flightcrew, which could reduce the ability of the flightcrew to maintain the safe flight and landing of the airplane.
Human Space Flight Requirements for Crew and Space Flight Participants
Document Number: E6-21193
Type: Rule
Date: 2006-12-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA is establishing requirements for human space flight as required by the Commercial Space Launch Amendments Act of 2004, including rules on crew qualifications and training, and informed consent for crew and space flight participants. The requirements should provide an acceptable level of safety to the general public and ensure individuals on board are aware of the risks associated with a launch or reentry. The rule also applies existing financial responsibility and waiver of liability requirements to human space flight and experimental permits. Experimental permits are the subject of a separate rulemaking.
Airworthiness Directives; Sicma Aero Seat; Third Occupant Seat Assemblies, 133 Series
Document Number: E6-21186
Type: Rule
Date: 2006-12-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Sicma Aero Seat third occupant seat assemblies, 133 series. This AD requires visually inspecting the installation of the two headrest bushings and installing Mecanindus pins to secure the bushings. This AD results from Sicma's determination that missing or incorrectly secured bushings could loosen and cause disengagement of the headrest from the seat during a high-energy stop of the airplane, possibly injuring the seat occupant. We are issuing this AD to prevent disengagement of the headrest from the seat during a high-energy stop of the airplane that could injure the seat occupant.
Office of Hazardous Materials Safety; Notice of Application for Special Permits
Document Number: 06-9725
Type: Notice
Date: 2006-12-15
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
In accordance with the procedures governing the application for, and the processing of, special permits from the Department of Transportation's Hazardous Material Regulations (49 CFR Part 107, Subpart B), notice is hereby given that the Office of Hazardous Materials Safety has received the application described herein. Each mode of transportation for which a particular special permit is requested is indicated by a number in the ``Nature of Application'' portion of the table below as follows: 1Motor vehicle, 2Rail Freight, 3Cargo Vessel, 4Cargo aircraft only, 5Passenger-carrying aircraft.
Office of Hazardous Materials Safety; Notice of Applications for Modification of Special Permit
Document Number: 06-9724
Type: Notice
Date: 2006-12-15
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
In accordance with the procedures governing the application for, and the processing of, special permits from the Department of Transportation's Hazardous Material Regulations (49 CFR Part 107, Subpart B), notice is hereby given that the Office of Hazardous Materials Safety has received the application described herein. This notice is abbreviated to expedite docketing and public notice. Because the sections affected, modes of transportation, and the anture of application have been shown in earlier Federal Register publications, they are not repeated here. Request of modifications of special permits (e.g. to provide for additional hazardous materials, packaging design changes, additional mode of transportation, etc.) are described in footnotes to the application number. Application numbers with the suffix ``M'' denote a modification request. These applications have been separated from the new applications for special permits to facilitate processing.
Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)
Document Number: E6-21262
Type: Proposed Rule
Date: 2006-12-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Model A300-600 series airplanes. This proposed AD would require revising the Airworthiness Limitations Section of the Instructions for Continued Airworthiness to incorporate new limitations for fuel tank systems. This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors caused by latent failures, alterations, repairs, or maintenance actions, could result in fuel tank explosions and consequent loss of the airplane.
Traffic Control Devices on Federal-Aid and Other Streets and Highways; Standards
Document Number: E6-21228
Type: Rule
Date: 2006-12-14
Agency: Federal Highway Administration, Department of Transportation
The FHWA is revising its regulation that prescribes procedures for obtaining basic uniformity of traffic control devices on Federal- aid and other streets and highways. This final rule makes some nomenclature changes, removes outdated references, and provides clarification on the meaning of roads ``open to public travel'' and ``substantial conformance.''
National Safe Routes to School Task Force to the Secretary of Transportation
Document Number: E6-21226
Type: Notice
Date: 2006-12-14
Agency: Federal Highway Administration, Department of Transportation
This document announces the first meeting of the National Safe Routes to School Task Force to the Secretary of Transportation. This is the first meeting of the task force. The purpose of the Task Force is to advise the Secretary of Transportation, through the Federal Highway Administration (FHWA) Office of Safety, on strategies to advance Safe Routes to School (SRTS) Programs nationwide and to encourage children, including those with disabilities, to walk and bicycle to school pursuant to Section 1404(h) of the Safe, Accountable, Flexible, Efficient Transportation Equity Act: A Legacy for Users (SAFETEA-LU) (Pub. L. 109-59). This meeting is open to the public and will have time allocated for public testimony. The public is welcome to present written or oral comments to the Task Force.
Airworthiness Directives; Schempp-Hirth Flugzeugbau GmbH Model Duo Discus T Gliders
Document Number: E6-21212
Type: Rule
Date: 2006-12-14
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as the possible failure of the attachment of the propeller blades. This AD requires actions that are intended to address the unsafe condition described in the MCAI.
Establishment of Alaskan High Altitude Reporting Points; AK
Document Number: E6-21190
Type: Rule
Date: 2006-12-14
Agency: Federal Aviation Administration, Department of Transportation
This action establishes four high altitude reporting points AYZOL, BORAN, EMSOW, and TIBOY in Alaska. The designation of these high altitude reporting points is needed to facilitate the separation of air traffic in Alaska.
Airworthiness Directives; Rolls-Royce Corporation AE 2100D3 Turboprop Engines
Document Number: E6-21185
Type: Rule
Date: 2006-12-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce Corporation (RRC) AE 2100D3 turboprop engines. This AD requires removing certain part number (P/N) compressor cone shaft assemblies at a new reduced cyclic life limit of 5,000 engine cycles. This AD results from low-cycle-fatigue testing and analysis of certain P/N compressor cone shaft assemblies, by RRC. We are issuing this AD to prevent uncontained failure of the compressor cone shaft assembly, leading to engine shutdown and damage to the airplane.
Nevada Pacific Railroad Corporation-Lease and Operation Exemption-Rail Lines of Pan Western Corporation
Document Number: E6-21174
Type: Notice
Date: 2006-12-14
Agency: Surface Transportation Board, Department of Transportation
Establishment of Class D Airspace; Castle Airport, Atwater, CA
Document Number: 06-9694
Type: Rule
Date: 2006-12-14
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class D airspace at Castle Airport, Atwater, CA. A contract Airport Traffic Control Tower (ATCT) is being established at Castle Airport, Atwater, CA, which will meet criteria for Class D airspace. Class D airspace is required when the ATCT is open, and to contain and protect Standard Instrument Approach Procedures (SIAPs) and other Instrument Flight Rules (IFR) operations at the airport. This action would establish Class D airspace extending upward from the surface to 2,500 feet Mean Sea Level (MSL) within a 4.5 nautical mile radius of the airport.
Anthropomorphic Test Devices; SID-IIs Side Impact Crash Test Dummy 5th Percentile Adult Female
Document Number: 06-9555
Type: Rule
Date: 2006-12-14
Agency: National Highway Traffic Safety Administration, Department of Transportation
This final rule amends the agency's regulation on anthropomorphic test devices to add specifications and qualification requirements for the 5th percentile adult female crash test dummy, called the SID-IIs Build Level D (``SID-IIs'') test dummy. The SID-IIs dummy is instrumented in the head, thorax, abdomen and pelvis, which enables it to assess in a comprehensive manner the performance of vehicles in protecting small-stature occupants in side impacts. NHTSA plans to use the SID-IIs dummy in an upgraded Federal motor vehicle safety standard on side impact protection.
Anthropomorphic Test Devices; ES-2re Side Impact Crash Test Dummy 50th Percentile Adult Male
Document Number: 06-9554
Type: Rule
Date: 2006-12-14
Agency: National Highway Traffic Safety Administration, Department of Transportation, Docket No. Nhtsa-2004-25441
This final rule amends the agency's regulation on anthropomorphic test devices to add specifications and qualification requirements for a new mid-size adult male crash test dummy, called the ``ES-2re'' test dummy. The ES-2re dummy has enhanced injury assessment capabilities compared to devices existing today, which allows for a fuller assessment of the types and magnitudes of the injuries occurring in side impacts and of the efficacy of countermeasures in improving occupant protection. The agency plans to use the ES-2re dummy in an upgraded Federal Motor Vehicle Safety Standard on side impact protection.
U.S. Bus Corporation, Receipt of Petition for Decision of Inconsequential Noncompliance
Document Number: E6-21224
Type: Notice
Date: 2006-12-13
Agency: National Highway Traffic Safety Administration, Department of Transportation
Hankook Tire Company, Ltd., Receipt of Petition for Decision of Inconsequential Noncompliance
Document Number: E6-21223
Type: Notice
Date: 2006-12-13
Agency: National Highway Traffic Safety Administration, Department of Transportation
Hankook Tire Company, Ltd., Receipt of Petition for Decision of Inconsequential Noncompliance
Document Number: E6-21220
Type: Notice
Date: 2006-12-13
Agency: National Highway Traffic Safety Administration, Department of Transportation
Maxon Industry Inc. DBA Maxonlift Corp., Receipt of Petition for Decision of Inconsequential Noncompliance
Document Number: E6-21210
Type: Notice
Date: 2006-12-13
Agency: National Highway Traffic Safety Administration, Department of Transportation
The Braun Corporation, Receipt of Petition for Decision of Inconsequential Noncompliance
Document Number: E6-21208
Type: Notice
Date: 2006-12-13
Agency: National Highway Traffic Safety Administration, Department of Transportation
Federal Motor Vehicle Safety Standards; Brake Hoses
Document Number: E6-21207
Type: Rule
Date: 2006-12-13
Agency: National Highway Traffic Safety Administration, Department of Transportation
NHTSA published a final rule in December 2004 that amended the Federal motor vehicle safety standard on brake hoses, and announced an effective date of December 20, 2006. The agency has received several petitions for reconsideration of the rule and a petition to delay the effective date of the final rule. To allow for more time to respond to petitions for reconsideration, and to give industry more time to meet new requirements, this document delays the effective date of the final rule for one year, to December 20, 2007. This decision was made after NHTSA published a notice of proposed rulemaking on November 15, 2006, soliciting public comment on whether the effective date should be extended. All commenters wrote in support of extending the effective date.
The Braun Corporation, Receipt of Petition for Decision of Inconsequential Noncompliance
Document Number: E6-21206
Type: Notice
Date: 2006-12-13
Agency: National Highway Traffic Safety Administration, Department of Transportation
Special Conditions: Airbus Model A380-800 Airplane; Fire Protection
Document Number: E6-21191
Type: Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Airbus A380-800 airplane, which has novel and unusual design features, such as a full- length, double deck passenger cabin and electrical equipment bays distributed throughout the airplane. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding fire protection. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. Additional special conditions will be issued for other novel or unusual design features of the Airbus Model A380-800 airplane.
Special Conditions: Airbus Model A380-800 Airplane, Lithium Ion Battery Installation
Document Number: E6-21188
Type: Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Airbus A380-800 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The Airbus A380-800 will incorporate the use of high capacity lithium ion battery technology in on-board systems. For this design feature, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding lithium ion batteries. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Airworthiness Directives; MT-Propeller Entwicklung GmbH Propellers
Document Number: E6-21184
Type: Proposed Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) for certain MT-Propeller Entwicklung GmbH variable pitch and fixed pitch propellers manufactured before 1995 which had not been overhauled since April 1994. That AD currently requires overhauling the propeller blades and performing initial and repetitive visual inspections of affected propeller blades. That AD also requires removing all propeller blades from service with damaged erosion sheath bonding or loose erosion sheaths and installing any missing or damaged polyurethane protective strips. This proposed AD would require the same actions. This proposed AD results from the need to clarify the population of affected propellers previously listed in AD 2006-05-05. We are proposing this AD to prevent erosion sheath separation leading to damage of the airplane.
Aviation Proceedings, Agreements Filed the Week Ending December 1, 2006
Document Number: E6-21182
Type: Notice
Date: 2006-12-13
Agency: Office of the Secretary, Department of Transportation
Aviation Proceedings, Agreements Filed the Week Ending November 24, 2006
Document Number: E6-21180
Type: Notice
Date: 2006-12-13
Agency: Office of the Secretary, Department of Transportation
BNSF Railway Company-Trackage Rights Exemption-Stillwater Central Railroad
Document Number: E6-21175
Type: Notice
Date: 2006-12-13
Agency: Surface Transportation Board, Department of Transportation
Qualification of Drivers; Exemption Applications; Diabetes
Document Number: E6-21136
Type: Notice
Date: 2006-12-13
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces receipt of applications from 66 individuals for exemptions from the prohibition against persons with insulin- treated diabetes mellitus (ITDM) operating commercial motor vehicles (CMVs) in interstate commerce. If granted, the exemptions would enable these individuals with ITDM to operate commercial motor vehicles in interstate commerce.
BNSF Railway Company-Trackage Rights Exemption-Stillwater Central Railroad
Document Number: E6-21043
Type: Notice
Date: 2006-12-13
Agency: Surface Transportation Board, Department of Transportation
Standard Instrument Approach Procedures; Miscellaneous Amendments
Document Number: E6-20941
Type: Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
This amendment amends Standard Instrument Approach Procedures (SIAPs) for operations at certain airports. These regulatory actions are needed because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, addition of new obstacles, or changes in air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Standard Instrument Approach Procedures, Weather Takeoff Minimums; Miscellaneous Amendments
Document Number: E6-20919
Type: Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
This amendment establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and/or Weather Takeoff Minimums for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, addition of new obstacles, or changes in air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines
Document Number: 06-9674
Type: Proposed Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for GE CF6-80C2 series turbofan engines. This proposed AD would require replacing certain installed part number (P/N) and serial number (SN) cast titanium weld-repaired forward engine mount platforms and cast titanium forward mount yokes, with a forged titanium or a non-welded cast titanium part. This proposed AD results from the discovery of cracks, in a weld-repaired area on a forward engine mount platform and a forward engine mount yoke, found during a fluorescent penetrant inspection (FPI). These parts were weld-repaired during manufacture. We are proposing this AD to prevent cracks in the forward engine mount platform and forward engine mount yoke that could result in possible separation of the engine from the airplane.
Establishment of Class D Airspace; Eastman, GA; Correction
Document Number: 06-9662
Type: Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
This document contains a correction to the final rule (FAA- 2006-25270; 06-ASO-9), which was published in the Federal Register on November 30, 2006 (71 FR 69191), establishing Class D airspace at Eastman, GA. This action corrects the effective date of the Class D airspace.
Office of Hazardous Materials Safety; Notice of Delays in Processing of Special Permit Applications
Document Number: 06-9659
Type: Notice
Date: 2006-12-13
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
In accordance with the requirements of 49 U.S.C. 5117(c), PHMSA is publishing the following list of special permit applications that have been in process for 180 days or more. The reason(s) for delay and the expected completion date for action on each application is provided in association with each identified application.
Notice of Final Federal Agency Actions on State Highway 130 in Texas
Document Number: 06-9654
Type: Notice
Date: 2006-12-13
Agency: Federal Highway Administration, Department of Transportation
This notice announces actions taken by the FHWA and other Federal agencies that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to a proposed highway project, State Highway 130 (SH 130), north of Georgetown at I-35, south to IH 10 East of Seguin in Williamson, Travis, Caldwell, and Guadalupe Counties in the State of Texas. The Federal actions, taken as a result of an environmental review process conducted in accordance with the National Environmental Policy Act, 42 U.S.C. 4321-4351 (NEPA), determined certain issues relating to the proposed project. Those actions grant licenses, permits, and approvals for the project.
Airworthiness Directives; Rolls-Royce plc RB211-524 Series Turbofan Engines; Correction
Document Number: E6-21122
Type: Rule
Date: 2006-12-12
Agency: Federal Aviation Administration, Department of Transportation
This document makes a correction to airworthiness directive (AD) 2004-26-05 applicable to certain Rolls-Royce plc (RR) RB211-524 series turbofan engines that was published in the Federal Register on January 5, 2005. The part number UL29916 in the Applicability section is incorrect. This document corrects that part number. In all other respects, the original document remains the same.
Union Pacific Railroad Company-Temporary Trackage Rights Exemption-BNSF Railway Company
Document Number: E6-21046
Type: Notice
Date: 2006-12-12
Agency: Surface Transportation Board, Department of Transportation
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