Department of Transportation November 2, 2006 – Federal Register Recent Federal Regulation Documents
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Neptune L.L.C., Liquefied Natural Gas Deepwater Port License Application; Final Application Public Hearings and Final Environmental Impact Statement
The Maritime Administration (MARAD) and the U.S. Coast Guard (USCG) announce the availability of the Final Environmental Impact Statement (FEIS) for the Neptune LNG LLC, Liquefied Natural Gas Deepwater Port license application. Also, public hearings will be held on matters relevant to the approval or denial of the license application. The application describes a project that would be located in Federal waters of Massachusetts Bay, in Block 125, approximately 8 miles southeast of Gloucester, MA and 22 miles northeast of Boston, MA. The Coast Guard and MARAD request public comments on the FEIS and application. Publication of this notice begins a 30 day comment period and provides information on how to participate in the process. As a point of clarification, there is another deepwater port application by Northeast Gateway Energy Bridge, L.L.C. in the same vicinity. These applications are being processed and reviewed independently. The Northeast Gateway Energy Bridge, L.L.C. FEIS was noticed on an earlier date and is available on the Docket at USCG-2005- 22219.
Disadvantaged Business Enterprise
In accordance with the Paperwork Reduction Act of 1995 (44 U.S.C. Chapter 35, as amended) this notice announces the Department of Transportation's (DOT) intention to request extension for a currently approved information collection.
Airworthiness Directives; Bell Helicopter Textron Model 204B, 205A, 205A-1, 205B, 210, 212, 412, 412CF, and 412EP Helicopters
This document proposes adopting a new airworthiness directive (AD) for Bell Helicopter Textron (Bell) Model 204B, 205A, 205A-1, 205B, 210, 212, 412, 412CF, and 412EP helicopters. The AD would require certain checks and inspections of each tail rotor blade assembly (T/R blade) at specified intervals and repairing or replacing, as applicable, any unairworthy T/R blade. This proposal is prompted by eight reports of T/R blade failures. The actions specified by the proposed AD are intended to prevent failure of a T/R blade and subsequent loss of control of the helicopter.
Airworthiness Directives; Bombardier Model DHC-8-400 Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier Model DHC-8-400 series airplanes. This proposed AD would require revising the Airworthiness Limitations Items (ALI) of the maintenance requirements manual to require additional inspection requirements of the maintenance requirements manual for certain principal structural elements (PSEs) related to fuselage cutouts and to reduce an inspection threshold for an existing ALI task on the aft entry door. This proposed AD results from data obtained from the manufacturer's fatigue testing. We are proposing this AD to detect and correct fatigue cracking of certain PSEs, which could result in reduced structural integrity of the airplane.
Federal Motor Vehicle Safety Standards; Glazing Materials; Correction
In July 2003, the agency published a final rule updating our Federal motor vehicle safety standard on glazing materials. As part of that rulemaking, boundaries were established for shade bands on vehicle windshields in order to limit their potential encroachment on the driver's field of view. As part of the new shade band requirements, the Society of Automotive Engineers (SAE) Recommended Practice J100 (rev. June 1995), ``Class `A' Vehicle Glazing Shade Bands,'' was incorporated by reference into the standard. However, in a July 2005 final rule responding to petitions for reconsideration of that earlier rulemaking, the standard's provisions related to shade bands requirements were amended, and as a result, a later but substantively identical version of SAE J100 (i.e., the November 1999 revision) was inadvertently included in the standard. The July 2005 final rule should have referenced SAE J100 (rev. June 1995), the document properly incorporated by reference into the safety standard. This document corrects this inconsistency resulting from administrative error.
Airworthiness Directives; Pratt & Whitney PW4074, PW4074D, PW4077, PW4077D, PW4084D, PW4090, PW4090-3, and PW4098 Turbofan Engines
The FAA is adopting a new airworthiness directive (AD) for Pratt & Whitney PW4074, PW4074D, PW4077, PW4077D, PW4084D, PW4090, PW4090-3, and PW4098 turbofan engines, with certain front turbine hub part numbers installed. This AD requires a onetime visual inspection of the anti-rotation slots in the front turbine hub, for a machining nonconformance, and its replacement if the inspection failed. This AD results from a report of a crack found in an anti-rotation slot of a front turbine hub, during overhaul shop inspection. The anti-rotation slot geometry was not machined in conformance with the design drawing during manufacture. We are issuing this AD to prevent uncontained engine failure, damage to the airplane, and injury to passengers.
Special Conditions: Boeing Commercial Airplane Group, Boeing Model 777 Series Airplane; Overhead Cross Aisle Stowage Compartments
The FAA amends and supersedes proposed special conditions for the Boeing Model 777 series airplanes. The previous notice (Notice No. 25-06-09-SC) published on October 18, 2006 (71 FR 61432), did not reflect the final FAA position on the novel design feature, and was thus in error. This airplane, modified by Boeing Commercial Airplane Group, will have novel or unusual design features associated with overhead cross aisle stowage compartments. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. These amended proposed special conditions contain the additional safety standards the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Agency Information Collection Activity Seeking OMB Approval
The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) revision of a current information collection. The Federal Register notice with a 60-day comment period soliciting comments on the following collection of information was published on June 28, 2006, vol. 71, no. 124, page 36869. The FAA Aviation Research and Development Grants Program establishes uniform policies and procedures for the award and administration of research grants to colleges, universities, and not for profit organizations.
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