Department of Transportation September 26, 2006 – Federal Register Recent Federal Regulation Documents

The Maritime Administration (MARAD) and U.S. Coast Guard announce the availability of the Environmental Assessment (EA) and Draft Finding of No Significant Impact (FONSI) on the Main Pass Energy Hub (MPEH) Deepwater Port Amended License Application. We are also announcing the dates and locations of public hearings for input regarding the approval or denial of the license application. The application and the amendment describe a project that would be located in the Gulf of Mexico in Main Pass Lease Block 299 (MP 299), approximately 16 miles southeast of Venice, Louisiana. Draft and final Environmental Impact Statements (EIS) evaluating the original application were published on June 17, 2005 and March 14, 2006, respectively. The Main Pass Energy Hub Deepwater Port License Application originally proposed the use of ``open-loop'' open rack vaporization (ORV). In the amended application, the applicant is proposing a ``closed-loop'' system using submerged combustion vaporization with selective catalytic reduction (SCV/SCR). Though similar, a more generic SCV/SCR system was analyzed in detail in the Final EIS (FEIS) as an alternative. The amended application provides expanded and refined design information regarding the proposed changes. The EA was prepared to provide analysis of the actual SCV/SCR design now being proposed and to determine if there were any significant impacts resulting from this change in proposed regassification technology in addition to or different from those previously assessed in the FEIS. The original application and environmental analysis contained in the FEIS still apply, including facilities, offshore and onshore pipelines, and salt cavern gas storage. Previous comments on the FEIS and application will continue to be considered in this process and need not be repeated. Based upon the EA, we have determined that the project changes as proposed in this amended application will not have a significant impact on the environment and we are therefore issuing a Draft Finding of No Significant Impact (FONSI) for public review and comment.

The Surface Transportation Board (Board) gives notice of the ``Notification and Federal Employee Antidiscrimination Act of 2002,'' the No FEAR Act, to former and current STB employees and to applicants for STB employment.

In accordance with the Paperwork Reduction Act of 1995 (44 U.S.C. Chapter 35, as amended), this notice announces the U.S. Department of Transportation's (DOT) intention to request renewal of a previously approved information collection.

Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains a summary of certain petitions seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.

This document revises the list of vehicles not originally manufactured to conform to the Federal motor vehicle safety standards (FMVSS) that NHTSA has decided to be eligible for importation. This list is contained in an appendix to the agency's regulations that prescribe procedures for import eligibility decisions. The list has been revised to add all vehicles that NHTSA has decided to be eligible for importation since October 1, 2005, and to remove all previously listed vehicles that are now more than 25 years old and need no longer comply with all applicable FMVSS to be lawfully imported. NHTSA is required by statute to publish this list annually in the Federal Register.

This document makes a correction to the final rule published in the Federal Register on September 1, 2006 (71 FR 52250), which amends regulations for issuing airworthiness certificates to certain new aircraft manufactured in the United States. This action is necessary to add an amendment number to the headings section at the beginning of the final rule. This correction does not make substantive changes to the final rule.

The FAA is revising an earlier proposed airworthiness directive (AD) for certain Boeing Model 747 airplanes. The original NPRM would have required repetitive tests to detect hot air leaking from the trim air diffuser ducts or sidewall riser duct assemblies (collectively referred to in this proposed AD as ``TADDs''), related investigative actions, and corrective actions if necessary. The original NPRM also would have provided an optional terminating action for the repetitive tests. The original NPRM resulted from reports of sealant deteriorating on the outside of the center wing fuel tank and analysis that sealant may deteriorate inside the tank due to excess heat from leaking TADDs. This action revises the original NPRM by referring to improved inspection procedures and extending the repetitive interval for certain related investigative actions. We are proposing this supplemental NPRM to prevent leakage of fuel or fuel vapors into areas where ignition sources may be present, which could result in a fire or explosion.

The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all Airbus Model A300 B2, B4-100, and B4-200 series airplanes. The existing AD currently requires supplemental structural inspections to detect fatigue cracking, and repair of cracked structure. This proposed AD would require revising the maintenance program by incorporating new and revised supplemental structural inspections, inspection intervals, and repairs; and repair of any damaged, cracked, or corroded structure; which would end the existing supplement structural inspections. This proposed AD results from a review of service history and reports received from the current supplemental structural inspection document program. We are proposing this AD to prevent reduced structural integrity of these airplanes due to fatigue cracking.

The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A300 and A310 airplanes; and Model A300 B4- 600, B4-600R, and F4-600R series airplanes, and Model C4-605R Variant F airplanes (collectively called A300-600 series airplanes). This proposed AD would require replacing the pressure limiter of the parking brake system with a new or modified pressure limiter. This proposed AD results from a report indicating that failure of the parking brake system occurred on a Model A300-600 airplane. We are proposing this AD to prevent failure of the parking braking system and interference with emergency use of the brake pedals, which could lead to airplane collision with surrounding objects or departure from the runway.