Department of Transportation March 2, 2005 – Federal Register Recent Federal Regulation Documents
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Preliminary Theft Data; Motor Vehicle Theft Prevention Standard
This document requests comments on data about passenger motor vehicle thefts that occurred in calendar year (CY) 2003 including theft rates for existing passenger motor vehicle lines manufactured in model year (MY) 2003. The preliminary theft data indicate that the vehicle theft rate for CY/MY 2003 vehicles (1.84 thefts per thousand vehicles) decreased by 26.1 percent from the theft rate for CY/MY 2002 vehicles (2.49 thefts per thousand vehicles). 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.
Insurer Reporting Requirements; Reports Under 49 U.S.C. on Section 33112(c)
This notice announces publication by NHTSA of the annual insurer report on motor vehicle theft for the 1999 reporting year. Section 33112(h) of Title 49 of the U.S. Code, requires this information to be compiled periodically and published by the agency in a form that will be helpful to the public, the law enforcement community, and Congress. As required by section 33112(c), this report provides information on theft and recovery of vehicles; rating rules and plans used by motor vehicle insurers to reduce premiums due to a reduction in motor vehicle thefts; and actions taken by insurers to assist in deterring thefts.
Airworthiness Directives; Aerospatiale Model ATR 42-200, -300, and -320 Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for all Aerospatiale Model ATR 42-200, -300, and -320 series airplanes. This AD requires inspecting to determine the part and serial number of the swinging lever of the main landing gears (MLG) and replacing the swinging lever if necessary. This AD is prompted by a report that, on an airplane lined up for takeoff, the swinging lever of the left MLG collapsed when engine power was applied. We are issuing this AD to prevent fracture of the MLG swinging lever, which could result in collapse of the swinging lever and reduced structural integrity and possible collapse of the MLG during operations on the ground.
Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for all BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ series airplanes. This AD requires repetitive detailed inspections of the center and rear fuselage skin including all the lap joints at stringers 2, 10, 19, and 30, and repair if necessary. This AD is prompted by evidence of cracking due to fatigue along the edges of certain chemi- etched pockets in the rear fuselage upper skin. We are issuing this AD to prevent a possible sudden loss of cabin pressure and consequent injury to passengers and flightcrew.
Airworthiness Directives; McDonnell Douglas Model MD-90-30 Airplanes
The FAA is adopting a new airworthiness directive (AD) for all McDonnell Douglas Model MD-90-30 airplanes. This AD requires a general visual inspection in the electrical/electronics (E/E) compartment for damage of the wire bundle and aft right radio rack structure at station 160.000, and corrective actions if necessary. This AD also requires modifying the radio rack structure and wire bundle routing. This AD is prompted by a report indicating that burnt wiring was discovered in the wire bundle at station 160.000 in the E/E compartment. We are issuing this AD to detect and correct chafing of the wire bundle at station 160.000 against the support bracket located on the aft right radio rack, which could lead to shorted or burnt wires and consequent smoke and fire in the E/E compartment.
Airworthiness Directives; Boeing Model 757 Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 757 series airplanes. This AD requires identification of the part number for the cable assembly for the lower anti-collision light, and related investigative and corrective actions if necessary. This AD is prompted by a report of damage caused by an electrical arc in a connector on the cable assembly for the lower anti-collision light. We are issuing this AD to prevent an electrical arc in the cable assembly for the lower anti-collision light, which could result in a fire in a flammable leakage zone of the airplane.
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