Department of Transportation October 10, 2006 – Federal Register Recent Federal Regulation Documents

Notification of Extension of Comment Period
Document Number: E6-16708
Type: Notice
Date: 2006-10-10
Agency: Federal Railroad Administration, Department of Transportation
Petition for Waiver of Compliance
Document Number: E6-16696
Type: Notice
Date: 2006-10-10
Agency: Federal Railroad Administration, Department of Transportation
Petition for Waiver of Compliance
Document Number: E6-16695
Type: Notice
Date: 2006-10-10
Agency: Federal Railroad Administration, Department of Transportation
Final Theft Data; Motor Vehicle Theft Prevention Standard
Document Number: E6-16687
Type: Rule
Date: 2006-10-10
Agency: National Highway Traffic Safety Administration, Department of Transportation
This document publishes the final data on thefts of model year (MY) 2004 passenger motor vehicles that occurred in calendar year (CY) 2004. The final 2004 theft data indicate a decrease in the vehicle theft rate experienced in CY/MY 2004. The final theft rate for MY 2004 passenger vehicles stolen in calendar year 2004 (1.83 thefts per thousand vehicles) decreased by 0.54 percent from the theft rate for CY/MY 2003 (1.84 thefts per thousand vehicles) when compared to the theft rate experienced in CY/MY 2003. Publication of these data fulfills NHTSA's statutory obligation to periodically obtain accurate and timely theft data and publish the information for review and comment.
NHTSA's Activities Under the United Nations Economic Commission for Europe 1998 Global Agreement
Document Number: E6-16681
Type: Notice
Date: 2006-10-10
Agency: National Highway Traffic Safety Administration, Department of Transportation
NHTSA is publishing this notice to inform the public of the schedule of upcoming meetings of the World Forum for Harmonization of Vehicle Regulations (WP.29) and its working parties of experts for the remainder of calendar year 2006 and the tentative schedule for calendar year 2007. Further, this notice informs the public about the status of activities under the Program of Work of the 1998 Global Agreement and requests comments on various aspects of these activities. Specifically, this notice seeks comment on the recommended Global Technical Regulation (GTR) on motorcycle brake systems that was referred by the Working Party on Brakes and Running Gear (GRRF) to the Executive Committee of the 1998 Global Agreement (AC.3) for a vote at the 140th session of WP.29 in November 2006. Publication of this information is in accordance with NHTSA's Statement of Policy regarding Agency Policy Goals and Public Participation in the Implementation of the 1998 Global Agreement on Global Technical Regulations.
Additional Types of Child Restraint Systems That May Be Furnished and Used on Aircraft; Corrections
Document Number: E6-16622
Type: Rule
Date: 2006-10-10
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration published a final rule in the Federal Register on July 14, 2006 (71 FR 40003). The final rule allowed the use of child restraint systems that the FAA approves under the aviation standards of Technical Standard Order C-100b, Child Restraint Systems, or under its certification regulations regarding the approval of materials, parts, processes, and appliances. That final rule contained two non-substantive typographical errors in the rule text of two sections. This document corrects the final regulations by revising these sections.
Airworthiness Directives; Boeing Model 737 Airplanes
Document Number: E6-16553
Type: Rule
Date: 2006-10-10
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 737 airplanes. This AD requires repetitive measurement of the freeplay of both aileron balance tabs; repetitive lubrication of the aileron balance tab hinge bearings and rod end bearings; and related investigative and corrective actions if necessary. This AD results from reports of freeplay-induced vibration of the aileron balance tab. The potential for vibration of the control surface should be avoided because the point of transition from vibration to divergent flutter is unknown. We are issuing this AD to prevent excessive vibration of the airframe during flight, which could result in loss of control of the airplane.
Airworthiness Directives; Raytheon (Beech) Model 400, 400A, and 400T Series Airplanes; and Raytheon (Mitsubishi) Model MU-300 Airplanes
Document Number: E6-16552
Type: Rule
Date: 2006-10-10
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Raytheon (Beech) Model 400, 400A, and 400T series airplanes; and Raytheon (Mitsubishi) Model MU-300 airplanes. This AD requires revising the airplane flight manual to modify the Operating Limitations, Abnormal Procedures, and Normal Procedures, as applicable, for flight in icing conditions. This AD results from multiple reports of high- altitude, dual-engine flameouts on airplanes operating in certain meteorological conditions. We are issuing this AD to advise the flightcrew that the buildup of ice on certain internal areas of the engine could result in a dual-engine flameout and what action they must take to avoid this hazard.
Airworthiness Directives; Fuji Heavy Industries, Ltd. FA-200 Series Airplanes
Document Number: E6-16354
Type: Rule
Date: 2006-10-10
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 an aviation authority of another country to identify and correct an unsafe condition on an aviation product. We are issuing this AD to require actions that are intended to address the unsafe condition described in the MCAI.
Establishment of Class E Airspace; Kokohanok, AK
Document Number: 06-8523
Type: Rule
Date: 2006-10-10
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Kokohanok, AK to provide adequate controlled airspace to contain aircraft executing new Standard Instrument Approach Procedures (SIAPs) and a new Departure Procedure (DP). This rule results in new Class E airspace established upward from 700 feet (ft) and 1,200 ft. above the surface at Kokohanok, AK.
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