Department of Transportation February 11, 2005 – Federal Register Recent Federal Regulation Documents

Compass Port LLC Liquefied Natural Gas Deepwater Port License Application; Draft Environmental Impact Statement
Document Number: 05-2804
Type: Notice
Date: 2005-02-11
Agency: Coast Guard, Department of Homeland Security, Maritime Administration, Department of Transportation
The U.S. Coast Guard and the Maritime Administration announce the availability of the draft environmental impact statement for this license application. The application describes a project that would be located in the Outer Continental Shelf and Mississippi Sound areas of the Gulf of Mexico, approximately 11 miles south of Dauphin Island, AL, in lease block Mobile 910. The draft environmental impact statement is a Coast Guard document with several agencies, including the U.S. Army Corps of Engineers and the Federal Energy Regulatory Commission acting as cooperating agencies in the National Environmental Policy Act of 1969 process, as described by 40 CFR 1501.6. The Coast Guard is the lead federal agency in the preparation of the draft environmental impact statement for the liquefied natural gas terminal, construction of the gravity-based structures, and the associated offshore and onshore pipelines. The joint document will satisfy the requirements of the Deepwater Port Act. The U.S. Army Corps of Engineers will assist in the preparation of the draft environmental impact statements for permits pursuant to section 10 of the Rivers and Harbors Act of 1899 (33 U.S.C. 403) and section 404 of the Clean Water Act (33 U.S.C. 1344). The Federal Energy Regulatory Commission will assist in the preparation of the draft environmental impact statement for the onshore pipeline. Even though an affiliate of Compass Port LLC must separately apply for and receive an authorization for the onshore pipeline, and from the Army Corps of Engineers for the appropriate section 10 and 404 permits, this draft environmental impact statement will assess the environmental impacts of both the onshore and offshore portions of the project. The lead agencies (Coast Guard and Maritime Administration), as well as the cooperating agencies (Federal Energy Regulatory Commission and U.S. Army Corps of Engineers), request public comments on the draft environmental impact statement.
Airworthiness Directives; Pilatus Aircraft Limited Models B4- PC11, B4-PC11A, and B4-PC11AF Sailplanes
Document Number: 05-2696
Type: Proposed Rule
Date: 2005-02-11
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all Pilatus Aircraft Limited (Pilatus) Models B4-PC11, B4-PC11A, and B4-PC11AF sailplanes. This proposed AD would require you to repetitively inspect the control-column support for cracks and, if any cracks are found, replace the control-column support with a new support. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. We are issuing this proposed AD to detect and correct cracks in the control-column support, which could result in failure of the support. This failure could lead to loss of the primary flight control system.
BNSF Railway CompanyTrackage Rights ExemptionUnion Pacific Railroad Company
Document Number: 05-2682
Type: Notice
Date: 2005-02-11
Agency: Surface Transportation Board, Department of Transportation
Airworthiness Directives; Bell Helicopter Textron, A Division of Textron Canada Model 222, 222B, 222U and 230 Helicopters
Document Number: 05-2609
Type: Rule
Date: 2005-02-11
Agency: Federal Aviation Administration, Department of Transportation
This amendment supersedes an existing airworthiness directive (AD) for Bell Helicopter Textron, A Division of Textron Canada (BHTC) Model 222, 222B, 222U, and 230 helicopters, that currently requires a visual check of each main rotor grip (grip) and pitch horn assembly without disassembling the main rotor hub assembly (hub assembly), and a visual inspection at specified intervals of each affected grip and pitch horn assembly for a crack using a 10-power or higher magnifying glass. If a crack is found, the existing AD requires replacing each unairworthy grip or pitch horn with an airworthy part before further flight. This amendment requires those same actions, and also requires an additional inspection of the grip and pitch horn assembly for a crack in the disassembled hub assembly, and replacing any cracked part with an airworthy part. This amendment is prompted by the determination that an additional enhanced inspection is needed to ensure the integrity of the hub assembly. The actions specified by this AD are intended to prevent failure of the grip or pitch horn and subsequent loss of control of the helicopter.
Union Pacific Railroad CompanyTemporary Trackage Rights ExemptionBNSF Railway Company \1\ -
Document Number: 05-2597
Type: Notice
Date: 2005-02-11
Agency: Surface Transportation Board, Department of Transportation
Redesignation of Mountainous Areas in Alaska
Document Number: 05-2594
Type: Rule
Date: 2005-02-11
Agency: Part III, Federal Aviation Administration, Department of Transportation
This final rule updates the designated mountainous areas in the State of Alaska. Regulations currently designating mountainous areas in Alaska were established in 1956. Since that time, we have concluded that areas previously considered non-mountainous should be expanded, and two areas previously designated mountainous should be considered non-mountainous. This final rule will allow aircraft operating in certain non-mountainous areas to fly at altitudes acceptable for the actual topography of the area.
Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes
Document Number: 05-2578
Type: Rule
Date: 2005-02-11
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 767 series airplanes. That AD currently requires repetitive detailed and eddy current inspections of the aft pressure bulkhead for damage and cracking, and repair if necessary. This new AD also requires one-time detailed and high frequency eddy current inspections of any ``oil-can'' located on the aft pressure bulkhead, and related corrective actions if necessary. An ``oil-can'' is an area on a pressure dome web that moves when pushed from the forward side. This AD is prompted by reports of cracking at ``oil-can'' boundaries on the aft pressure bulkhead. We are issuing this AD to detect and correct fatigue cracking of the aft pressure bulkhead, which could result in rapid depressurization of the airplane and possible damage or interference with the airplane control systems that penetrate the bulkhead, and consequent loss of controllability of the airplane.
Federal Motor Vehicle Safety Standards; Low Speed Vehicles; Termination of Rulemaking
Document Number: 05-2471
Type: Proposed Rule
Date: 2005-02-11
Agency: National Highway Traffic Safety Administration, Department of Transportation
The purpose of this document is to announce the termination of a rulemaking in which the agency had considered adding additional conspicuity requirements applicable to low-speed vehicles (LSV), as well as a requirement that LSVs bear a label identifying the safety hazards associated with their operation in mixed traffic. Due to the absence of data showing a conspicuity-related safety problem with current LSV designs, the agency has decided to terminate the rulemaking.
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