Department of Transportation March 1, 2005 – Federal Register Recent Federal Regulation Documents

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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