Department of Transportation June 10, 2005 – Federal Register Recent Federal Regulation Documents
Results 1 - 6 of 6
Beacon Port Natural Gas Deepwater Port License Application; Preparation of Environmental Impact Statement
The Coast Guard and the Maritime Administration (MARAD) announce that the Coast Guard intends to prepare an environmental impact statement (EIS) as part of the environmental review of this license application. The application describes a project that would be located in the Gulf of Mexico, in lease block High Island Area 27, on the outer Continental Shelf (OCS). The Main Terminal would be located approximately 45 miles South of High Island and 50 miles East-Southeast of Galveston, Texas, with a riser platform in lease block West Cameron 167, approximately 27 miles South of Holly Beach and 29 miles South- Southeast of Johnson?s Bayou, Louisiana. Publication of this notice begins a scoping process that will help identify and determine the scope of environmental issues to be addressed in the EIS. This notice requests public participation in the scoping process and provides information on how to participate.
Notice on Honoring Tickets of Insolvent Airlines Pursuant to the Requirements of Section 145 of the Aviation and Transportation Security Act
The Department is publishing the following notice to provide guidance to the aviation industry regarding the responsibility pursuant to section 145 of the Aviation and Transportation Security Act of certain air carriers to transport under certain conditions the ticketed passengers of a carrier that has ceased operations on a particular route or routes due to bankruptcy or insolvency.
Qualification of Drivers; Exemption Applications; Vision
This notice publishes the FMCSA decision to renew the exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations for 31 individuals. The FMCSA has statutory authority to exempt individuals from vision standards if the exemptions granted will not compromise safety. The agency has concluded that granting these exemptions will provide a level of safety that will be equivalent to, or greater than, the level of safety maintained without the exemptions for these commercial motor vehicle (CMV) drivers.
Airworthiness Directives; Revo, Incorporated Models Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 Airplanes
The FAA is adopting a new airworthiness directive (AD) to supersede Airworthiness Directive (AD) 98-10-12, which applies to all Revo, Incorporated (REVO) (Type Certificate 1A13 formerly held by Colonial Aircraft Company, Lake Aircraft Corporation, Consolidated Aeronautics, Inc., and Global Amphibians LLC) Models Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 airplanes. AD 98-10-12 currently requires you to ensure adequate clearance between the attachment fitting and the horizontal stabilizer rear beam and between the attachment fitting and the stabilizer skin with inspections, possible replacement, and adjustments as necessary. This new AD is the result of several reports of fatigue cracks found in the horizontal stabilizer attachment fitting (part number 2-2200-21) of Model LA-4-200 airplanes that were in compliance with AD 98-10-12. This includes an airplane accident with a fatality attributed to a fatigue crack in the horizontal stabilizer attachment fitting. Consequently, this AD requires either a dye penetrant inspection of the horizontal stabilizer attachment fitting for any evidence of fretting, cracking, or corrosion (with necessary replacement and modification) or replacement of the fittings depending on the number of operational hours on the fitting. The AD also requires you to repetitively replace the fitting every 850 hours time-in-service (TIS), repetitively inspect (visually) the fittings between replacement times, and report to FAA the results of the initial inspection and any cracks found on repetitive inspections. We are issuing this AD to detect, correct, and prevent future cracks in the horizontal stabilizer attachment fitting, which could result in failure of the horizontal stabilizer attachment fitting. This failure could result in loss of control of the airplane.
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