Department of Transportation March 2005 – Federal Register Recent Federal Regulation Documents

Results 301 - 324 of 324
Georgia Central Railway, L.P.-Acquisition and Operation Exemption-Rail line of CSX Transportation, Inc.
Document Number: 05-4101
Type: Notice
Date: 2005-03-03
Agency: Surface Transportation Board, Department of Transportation
Columbia Basin Railroad Company, Inc.-Lease and Operation Exemption-Clark County, WA
Document Number: 05-4100
Type: Notice
Date: 2005-03-03
Agency: Surface Transportation Board, Department of Transportation
Airworthiness Directives; Boeing Model 757-200, -200PF, and -300 Series Airplanes
Document Number: 05-4080
Type: Proposed Rule
Date: 2005-03-03
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 757-200, -200PF, and -300 series airplanes. This proposed AD would require inspecting for damage of the ground brackets, ground wires, and terminal lugs of the auxiliary power unit (APU) battery and the APU start transformer rectifier unit (TRU) as applicable; and corrective and related investigative actions. This proposed AD is prompted by reports indicating that, during inspections on two airplanes, the ground brackets for the APU battery were found damaged. We are proposing this AD to detect and correct a damaged electrical bonding surface of the APU battery and APU start TRU ground connections, which could cause overheating of the ground connections and lead to possible consequent ignition of the adjacent insulating blankets.
Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Series Airplanes
Document Number: 05-4079
Type: Proposed Rule
Date: 2005-03-03
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A318, A319, A320, and A321 series airplanes. This proposed AD would require replacing the water drain valves in the forward and aft cargo doors with new valves. This proposed AD is prompted by a report indicating that, during a test of the fire extinguishing system, air leakage through the water drain valves in the forward and aft cargo doors reduced the concentration of fire extinguishing agent to below the level required to suppress a fire. We are proposing this AD to prevent air leakage through the water drain valves, which, in the event of a fire in the forward or aft cargo compartment, could result in an insufficient concentration of fire extinguishing agent and consequent inability of the fire extinguishing system to suppress the fire.
Airworthiness Directives; Airbus Model A300 B2-203 and B4-203 Series Airplanes; Model A310 Series Airplanes; Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600)
Document Number: 05-4078
Type: Proposed Rule
Date: 2005-03-03
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus transport category airplanes. This proposed AD would require an inspection to determine if the suspect part numbers (P/N) and serial numbers of certain Thales Avionics equipment is installed, and replacement of any suspect part with a modified part having a new P/N. This proposed AD is prompted by reports of loss of the digital distance radio magnetic indicator and subsequent loss of both very high frequency omnidirectional range indicators, both distance measuring equipment, and one centralized maintenance computer. We are proposing this AD to prevent loss of navigation indications on the primary flight display requiring continuation of the flight on emergency instruments, which could lead to reduced ability to control the airplane in adverse conditions.
Airworthiness Directives; Boeing Model 777-200, -200ER, and -300 Series Airplanes
Document Number: 05-4073
Type: Proposed Rule
Date: 2005-03-03
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 777-200, -200ER, and -300 series airplanes. This proposed AD would require modification of the splice plate assemblies installed under the floor panels at the forward and aft edges of the cabin aisle. This proposed AD is prompted by reports of cracking of the aluminum splice plates under the floor panels in the cabin aisle. We are proposing this AD to prevent loss of the capability of the cabin floor and seat track structure to support the airplane interior inertia loads under emergency landing conditions. Loss of this support could lead to galley or seat separation from attached restraints, which could result in blocking of the emergency exits and consequent injury to passengers and crew.
Workhorse Custom Chassis, Receipt of Petition for Decision of Inconsequential Noncompliance
Document Number: 05-3991
Type: Notice
Date: 2005-03-02
Agency: National Highway Traffic Safety Administration, Department of Transportation
Unified Marine, Inc., Denial of Petition for Decision of Inconsequential Noncompliance
Document Number: 05-3990
Type: Notice
Date: 2005-03-02
Agency: National Highway Traffic Safety Administration, Department of Transportation
Coupled Products, Inc., Notice of Appeal of Denial of Petition for Decision of Inconsequential Noncompliance
Document Number: 05-3989
Type: Notice
Date: 2005-03-02
Agency: National Highway Traffic Safety Administration, Department of Transportation
Michelin North America, Inc.; Grant of Application for Decision That a Noncompliance Is Inconsequential to Motor Vehicle Safety
Document Number: 05-3988
Type: Notice
Date: 2005-03-02
Agency: National Highway Traffic Safety Administration, Department of Transportation
Preliminary Theft Data; Motor Vehicle Theft Prevention Standard
Document Number: 05-3987
Type: Proposed Rule
Date: 2005-03-02
Agency: National Highway Traffic Safety Administration, Department of Transportation
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)
Document Number: 05-3986
Type: Notice
Date: 2005-03-02
Agency: National Highway Traffic Safety Administration, Department of Transportation
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.
San Diego & Imperial Valley Railroad Company, Inc.-Lease and Operation Exemption-BNSF Railway Company 1
Document Number: 05-3985
Type: Notice
Date: 2005-03-02
Agency: Surface Transportation Board, Department of Transportation
Airworthiness Directives; Aerospatiale Model ATR 42-200, -300, and -320 Series Airplanes
Document Number: 05-3787
Type: Rule
Date: 2005-03-02
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: 05-3786
Type: Rule
Date: 2005-03-02
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: 05-3785
Type: Rule
Date: 2005-03-02
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: 05-3784
Type: Rule
Date: 2005-03-02
Agency: Federal Aviation Administration, Department of Transportation
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.
Notice of Request for Comments on Renewing Approval of an Information Collection: OMB Control No. 2126-0015 (Designation of Agents, Motor Carriers, Brokers and Freight Forwarders)
Document Number: 05-3953
Type: Notice
Date: 2005-03-01
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
The FMCSA announces that the Information Collection Request (ICR) described in this notice is being sent to the Office of Management and Budget (OMB) for review and approval. This information collection allows registered motor carriers, property brokers and freight forwarders a means of meeting process agent requirements. On September 14, 2004, the agency published a Federal Register notice announcing a 60-day comment period on this information collection (69 FR 55490). We are required to send ICRs to OMB under the Paperwork Reduction Act.
Licensing and Safety Requirements for Launch
Document Number: 05-3916
Type: Proposed Rule
Date: 2005-03-01
Agency: Federal Aviation Administration, Department of Transportation
The FAA is making available a draft of changes to the commercial space transportation regulations governing licensing and safety requirements for launch. We intend the changes to identify, codify, and maintain the successful safety measures that have been implemented at the federal launch ranges belonging to the Department of Defense and NASA. We are also establishing clear safety requirements for launches from non-federal launch sites. We will hold a public meeting on March 29-31, 2005, to give stakeholders an opportunity to get information about, and provide comments on, the draft regulatory language.
Keokuk Junction Railway Co.-Trackage Rights Exemption-Union Pacific Railroad Company
Document Number: 05-3885
Type: Notice
Date: 2005-03-01
Agency: Surface Transportation Board, Department of Transportation
Union Pacific Railroad Company-Temporary Trackage Rights Exemption-BNSF Railway Company 1
Document Number: 05-3884
Type: Notice
Date: 2005-03-01
Agency: Surface Transportation Board, Department of Transportation
The Board, under 49 U.S.C. 10502, revokes the class exemption as it pertains to the modified trackage rights described in STB Finance Docket No. 34417 (Sub-No. 2) \2\ to permit the trackage rights to expire on or about May 16, 2005, in accordance with the agreement of the parties,\3\ subject to the employee protective conditions set forth in Oregon Short Line R. Co.AbandonmentGoshen, 360 I.C.C. 91 (1979).
Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes
Document Number: 05-3634
Type: Rule
Date: 2005-03-01
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 airplanes. This AD requires you to do a one-time inspection of the windshield de-ice wiring system for heat damage and incorrect wire sizes and to replace any wires that are damaged or the incorrect size. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. We are issuing this AD to detect and replace windshield de-ice wiring of the incorrect size, which could result in heat damage of the windshield de-ice wiring. This failure could lead to possible fire in the overhead panel of the flight compartment.
Airworthiness Directives; Dassault Model Falcon 2000EX and 900EX Series Airplanes
Document Number: 05-3559
Type: Rule
Date: 2005-03-01
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Dassault Model Falcon 2000EX and 900EX series airplanes. This AD requires prohibiting dispatch with certain equipment inoperative; and revising the airplane flight manual to facilitate recovery of the cockpit display units in the event of an avionics standard communication bus (ASCB) failure and to inform the flightcrew what equipment is inoperative during an ASCB failure. This AD also requires doing an integrity check of the ASCB for any faults and corrective action if necessary, and installing an avionics software update to the Honeywell Primus Epic system. This AD is prompted by a report that an analysis and tests of the Honeywell Primus Epic systems installed on the Model Falcon 2000EX and 900EX series airplanes revealed that all information displayed on the cockpit display units could become invalid during flight. We are issuing this AD to prevent a loss of data from all four of the cockpit display units, and loss of all radio communications (with the exception of VHF emergency frequency and last frequency used), primary navigation instruments, autopilot, auto- throttle, central alerting system, aural alarms, and normal braking (on Model Falcon 2000EX series airplanes only). These losses could reduce the flightcrew's situational awareness, increase flightcrew workload, and consequently reduce the ability to maintain safe flight and landing of the airplane.
Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes; A300 B4-600, B4-600R and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600); and A310 Series Airplanes
Document Number: 05-3279
Type: Rule
Date: 2005-03-01
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to all Airbus Model A300 B2 and B4, A300-600, and A310 series airplanes. That AD currently requires identification of the part number and serial number of the parking brake operated valve (PBOV); and, if necessary, inspections of the PBOV, including a functional check of the PBOV, and follow-on and corrective actions. That AD also provides for optional terminating action for the requirements of that AD. This new AD requires modification of all affected PBOVs, or replacement with new, non-affected PBOVs, which would terminate the requirements of the existing AD. This AD is prompted by a decision by the FAA and a civil airworthiness authority to require modification or replacement of all affected PBOVs. We are issuing this AD to prevent loss of the yellow hydraulic system, which provides all the hydraulics for certain spoilers; elements of the hydraulics for flaps, stabilizer, pitch and yaw feel systems, pitch and yaw autopilot, and yaw damper; and elevator, rudder, and aileron.
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