Department of Transportation 2005 – Federal Register Recent Federal Regulation Documents

Results 551 - 600 of 3,378
Aviation Proceedings, Agreements Filed the Week Ending September 30, 2005
Document Number: 05-21453
Type: Notice
Date: 2005-10-27
Agency: Office of the Secretary, Department of Transportation
Airworthiness Directives; Raytheon Model Hawker 800XP Airplanes
Document Number: 05-21438
Type: Proposed Rule
Date: 2005-10-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Raytheon Model Hawker 800XP airplanes. This proposed AD would require inspecting to determine if the correct fuse is installed on the hydraulic over-temperature switch on panel ZK in the rear equipment bay, and replacing the existing fuse if necessary. This proposed AD results from a report of the installation of an incorrect fuse on the over-temperature switch on panel ZK in the rear equipment bay during airplane maintenance. We are proposing this AD to prevent a short circuit in the fuse and consequent heat damage to associated wiring and surrounding equipment, which could result in smoke or fire on the airplane.
Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146-100A and -200A Series Airplanes
Document Number: 05-21437
Type: Proposed Rule
Date: 2005-10-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all BAE Systems (Operations) Limited Model BAe 146-100A and -200A series airplanes. This proposed AD would require inspecting the nose landing gear (NLG) assembly to determine the part number of the NLG main fitting subassembly. For subject NLG main fitting subassemblies, this proposed AD would also require determining the total number of accumulated landings on a subject NLG main fitting subassembly, and eventually replacing the NLG assembly. This proposed AD results from a report indicating that the airplane maintenance manual contains incorrect safe-life limit information for certain NLG assemblies. We are proposing this AD to ensure that affected NLG fitting subassemblies are removed from service before they reach their approved safe-life limit. Operating with an NLG fitting subassembly that is beyond its approved safe-life limit could result in failure of the NLG and consequent loss of directional control on the ground and major structural damage to the airplane.
Airworthiness Directives; BAE Systems (Operations) Limited Model Avro 146-RJ Airplanes
Document Number: 05-21436
Type: Proposed Rule
Date: 2005-10-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all BAE Systems (Operations) Limited Model Avro 146-RJ airplanes. This proposed AD would require reviewing the airplane's maintenance records to determine if certain tasks of the Bae146/Avro RJ Maintenance Planning Document have been accomplished. This proposed AD would also require doing repetitive detailed inspections of the external fuselage skin adjacent to the longeron at rib 0 from frame 29 to frame 31 and repairing any damage if necessary. This proposed AD results from issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. We are proposing this AD to detect and correct cracking of the fuselage skin, which could result in structural failure of the fuselage.
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Document Number: 05-21435
Type: Proposed Rule
Date: 2005-10-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This proposed AD would require replacing the Gask-O- Seal in the coupling of the refuel/defuel shut-off valves. This proposed AD results from a report that Gask-O-Seals that did not incorporate an integral restrictor to limit fuel flow rate and fuel pressure during refueling were installed on certain airplanes. We are proposing this AD to prevent a buildup of excessive static charge, which could create an ignition source inside the fuel tank.
Airworthiness Directives; Airbus Model A318-100 and A319-100 Series Airplanes; Model A320-111 Airplanes; and Model A320-200, A321-100, and A321-200 Series Airplanes
Document Number: 05-21434
Type: Proposed Rule
Date: 2005-10-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Model A318-100 and A319-100 series airplanes; Model A320-111 airplanes; and Model A320-200, A321-100, and A321-200 series airplanes. This proposed AD would require repetitive detailed inspections of the trimmable horizontal stabilizer actuator (THSA) attachments for proper clearances, and any crack, damage, or metallic particles; related corrective actions if necessary; and a report of the inspection results to the manufacturer. This proposed AD results from a report that during lab testing to verify the performance of the THSA's secondary load path with a simulated failure of the THSA's primary load path, the secondary load path's nut did not jam (as it was supposed to do.) We are proposing this AD to ensure the integrity of the THSA's primary load path, which if failed, could result in latent (undetected) loading and eventual failure of the THSA's secondary load path and consequent uncontrolled movement of the horizontal stabilizer and loss of control of the airplane.
Airworthiness Directives; Airbus Model A330-200, A330-300, A340-200, and A340-300 Series Airplanes
Document Number: 05-21429
Type: Proposed Rule
Date: 2005-10-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A330-200, A330-300, A340-200, and A340-300 series airplanes. This proposed AD would require repetitive detailed inspections for cracking in the aft web of support rib 6 between certain bottom skin stringers on both wings; high frequency eddy current inspections for cracking of the attachment holes of the fuel pipes, and repair if necessary. This proposed AD would also provide for an optional modification, which would extend a certain inspection threshold. This proposed AD results from a report of significant cracking found in the aft web of support rib 6 on both wings. We are proposing this AD to prevent cracking in the aft web of support rib 6, which could result in overloading of adjacent ribs and the surrounding wing structure and consequent reduced structural integrity of the wing.
Airworthiness Directives; Airbus Model A310-203, -204, and -222 Airplanes, and Model A310-300 Series Airplanes
Document Number: 05-21428
Type: Proposed Rule
Date: 2005-10-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A310-203, -204, and -222 airplanes, and Model A310-300 series airplanes. This proposed AD would require a one-time rototest inspection for cracking of the frame foot and adjacent frames and skin in the area surrounding the frame foot run-outs from fuselage frames (FR) 43 through FR 46, and repair if necessary. The proposed AD also requires modification of certain fastener holes. This proposed AD results from a structural evaluation of Model A310 airplanes for widespread fatigue damage of the frame foot run-outs from FR 43 through FR 46. The evaluation revealed that, on in-service airplanes, undetected cracking in this area can lead to the rupture of the frame foot and subsequent cracking of the adjacent frames and fuselage skin. We are proposing this AD to prevent fatigue cracking of the frame foot run-outs, which could lead to rupture of the frame foot and cracking in adjacent frames and skin, and result in reduced structural integrity of the fuselage.
Modification of the Los Angeles Class B Airspace Area; CA
Document Number: C5-15855
Type: Rule
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
Marquette Rail, LLC-Lease and Operation Exemption-CSX Transportation, Inc.
Document Number: 05-21410
Type: Notice
Date: 2005-10-26
Agency: Surface Transportation Board, Department of Transportation
Watco Companies, Inc.-Continuance in Control Exemption-Arkansas Southern Railroad, Inc.
Document Number: 05-21409
Type: Notice
Date: 2005-10-26
Agency: Surface Transportation Board, Department of Transportation
Arkansas Southern Railroad, Inc.-Lease Exemption-The Kansas City Southern Railway Company
Document Number: 05-21402
Type: Notice
Date: 2005-10-26
Agency: Surface Transportation Board, Department of Transportation
Agency Information Collection Activities; Request for Comment; Clearance of a New Information Collection: Commercial Driver's License Policies and Practices Among the 51 Jurisdictions
Document Number: 05-21397
Type: Notice
Date: 2005-10-26
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
This notice advises the public about FMCSA's intention to request Office of Management and Budget (OMB) approval for a new information collection concerning the Commercial Driver's License (CDL) policies and practices among the 50 States and the District of Columbia (referred to as the 51 jurisdictions). This information is needed to identify where problems exist within the CDL Program and how to address those problems through new or revised safety initiatives. This notice is required by the Paperwork Reduction Act of 1995.
Public Notice For Waiver of Aeronautical Land-Use Assurance, Delta County Airport, Escanaba, MI
Document Number: 05-21392
Type: Notice
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of the airport from aeronautical use to non-aeronautical use and to authorize the lease of the airport property. The proposal consists of 1 parcel of land, totaling approximately 37 acres. Current use and present condition is undeveloped land compatible with local commercial/industrial zoning classification. The land was acquired under part of the property from the City of Escanaba deeded to Delta County for airport use. There are no impacts to the airport by allowing the airport to lease of the property. Subject land may provide good commercial/industrial development opportunities for the community and are well outside airport perimeter fence limits. Approval does not constitute a commitment by the FAA to financially assist in the lease of the subject airport property nor a determination of eligibility for grant-in-aid funding from the FAA. The disposition of proceeds from the lease of the airport property will be in accordance FAA's Policy and Procedures Concerning the Use of Airport Revenue, published in the Federal Register on February 16, 1999. In accordance with section 34107(h) of title 49, United States Code, this notice is required to be published in the Federal Register 30 days before modifying the land-use assurance that requires the property to be used for an aeronautical purpose.
Public Notice for Waiver of Aeronautical Land-Use Assurance Delta County Airport Escanaba, MI
Document Number: 05-21391
Type: Notice
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of the airport from aeronautical use to non-aeronautical use and to authorize the lease of the airport property. The proposal consists of 1 parcel of land, totaling approximately 3.6 acres. Current use and present condition is undeveloped land compatible with local commercial/industrial zoning classification. The land was acquired under part of the property from the City of Escanaba deeded to Delta County for airport use. There are no impacts to the airport by allowing the airport to lease of the property. Subject land may provide good commercial/industrial development opportunities for the community and are well outside airport perimeter fence limits. Approval does not constitute a commitment by the FAA to financially assist in the lease of the subject airport property nor a determination of eligibility for grant-in-aid funding from the FAA. The disposition of proceeds from the lease of the airport property will be in accordance FAA's Policy and Procedures Concerning the Use of Airport Revenue, published in the Federal Register on February 16, 1999. In accordance with section 47107(h) of title 49, United States Code, this notice is required to be published in the Federal Register 30 days before modifying the land-use assurance that requires the property to be used for an aeronautical purpose.
Amendment of Class E Airspace; Cortland, NY; Ithaca, NY; Elmira, NY; Endicott, NY; Sayre, PA
Document Number: 05-21321
Type: Rule
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
This action removes the description of the Class E airspace designated for Cortland, NY, Cortland County-Chase Field Airport (N03); Ithaca, NY, Tompkins County Airport (ITH); Elmira, NY, Elmira/Corning Regional Airport (ELM); Endicott, NY, Tri-Cities Airport (CZG); and Sayre, PA, Robert Parker Hospital Heliport. The affected Class E-5 airspace for the airports included in these descriptions will be consolidated into the amended Binghamton, NY airspace description contained in Docket No. FAA-2005-22100, Airspace Docket No. 05-AEA-16, effective February 16, 2006.
Amendment of Class E Airspace; Binghamton, NY
Document Number: 05-21320
Type: Rule
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E airspace at Binghamton, NY. The development of multiple area navigation (RNAV) Standard Instrument Approach Procedures (SIAP) for numerous airports within the Binghamton, NY geographical area with approved Instrument Flight Rules (IFR) operations and the resulting overlap of designated Class E-5 airspace have made this action necessary. This action consolidates the Class E-5 airspace designations for five airspace and one heliport and results in the rescission of the five Class E-5 descriptions through separate rulemaking action. The area will be depicted on aeronautical charts for pilot reference.
Establishment of Area Navigation Instrument Flight Rules Terminal Transition Routes (RITTR); Cincinnati, OH
Document Number: 05-21318
Type: Rule
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
This action establishes three Area Navigation Instrument Flight Rules Terminal Transition Routes (RITTR) in the Cincinnati, OH, terminal area. The FAA originally proposed to establish four routes as part of this action, but one route (T-212) was deleted because it did not meet RITTR design criteria and its short length would provide limited benefits. RITTR's are low altitude Air Traffic Service (ATS) routes, based on Area Navigation (RNAV), for use by aircraft having Instrument Flight Rules (IFR)-approved Global Positioning System (GPS)/ Global Navigation Satellite System (GNSS) equipment. The FAA is taking this action to enhance safety and facilitate the more flexible and efficient use of the navigable airspace in the Cincinnati terminal area.
Airworthiness Directives; Airbus Model A320-111, -211, -212, and -231 Airplanes
Document Number: 05-21312
Type: Rule
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A320-111, -211, -212, and -231 airplanes. This AD requires, for certain airplanes, modifying the cables and access holes to the inner tank fuel pumps; and, for certain other airplanes, inspecting the fuel pump access holes and modifying the access holes, if necessary. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent chafing of the fuel pump cables, which could result in electrical arcing and possible ignition of fuel vapors and consequent explosion of the fuel tank.
Airworthiness Directives; Boeing Model 757-200, -200PF, and -300 Series Airplanes
Document Number: 05-21311
Type: Rule
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 757-200, -200PF, and -300 series airplanes. This AD requires 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 AD results from reports indicating that during inspections on two airplanes, the ground brackets for the APU battery were found damaged. We are issuing 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; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135BJ, -135ER, -135KE, -135KL, -135LR, -145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes
Document Number: 05-21310
Type: Rule
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain EMBRAER airplane models as identified above. This AD requires modifying the total air temperature (TAT) sensor heating system. This AD also allows replacing the fully automated digital electronic control (FADEC) assemblies with new or modified assemblies as an additional means of compliance. This AD results from a report indicating that the FADEC unit failed to compensate for ice accretion on the engine fan blades due to a false temperature signal from the TAT sensor to the FADEC. We are issuing this AD to prevent failure of the TAT sensor, which could result in insufficient thrust to take off or (if coupled with the loss of an engine during takeoff) to abort the takeoff in a safe manner, and consequent reduced controllability of the airplane.
Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP Series Airplanes
Document Number: 05-21293
Type: Rule
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747- 200C, 747-200F, 747-300, 747SR, and 747SP series airplanes. This AD requires doing a one-time high-frequency eddy current inspection and repetitive detailed inspections for cracks in the frame web of main entry door number 1; and repairing the door frame web if necessary. This AD also provides for optional terminating action for the repetitive inspections. This AD is prompted by reports of cracking at the upper aft corner of the cutout for main entry door number 1 in the station 488 frame web. We are issuing this AD to detect and correct cracks in the frame web. These cracks could cause the frame to break and lead to rapid decompression of the airplane.
Hazardous Materials Regulations: Aluminum Cylinders Manufactured of Aluminum Alloy 6351-T6 Used in SCUBA, SCBA, Carbon Dioxide, and Oxygen Service-Revised Requalification and Use Criteria
Document Number: 05-21273
Type: Proposed Rule
Date: 2005-10-26
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
On September 10, 2003, the Research and Special Programs Administrationthe predecessor agency to the Pipeline and Hazardous Materials Safety Administration published a notice of proposed rulemaking (NPRM) to propose an inspection and testing program for early detection of sustained load cracking in certain cylinders manufactured with aluminum alloy 6351-T6. Based on comments received in response to that NPRM, we are proposing to adopt a maximum service life for cylinders manufactured with aluminum alloy 6351-T6 and to prohibit the use of these cylinders after the expiration of their maximum service life.
Airworthiness Directives; Sikorsky Aircraft Corporation Model S-76A, B, and C Helicopters
Document Number: 05-21256
Type: Rule
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD) for the Sikorsky Aircraft Corporation (Sikorsky) Model S-76A, B, and C helicopters. This action requires certain inspections of the main rotor lower bifilar arm assembly in the attachment area around the lower bifilar lugs for a crack. If a crack is found on any bifilar lug, this AD requires replacing the bifilar arm assembly with an airworthy bifilar arm assembly. If no crack is found, this AD requires a one-time test for the required torque on the lug nuts and, if necessary, applying the required torque and conducting the torque stabilization tests. This amendment is prompted by four reports of cracked bifilars. The actions specified in this AD are intended to prevent failure of a bifilar lug, damage to the main rotor control system, and subsequent loss of control of the helicopter.
Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes
Document Number: 05-21255
Type: Rule
Date: 2005-10-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA adopts a new airworthiness directive (AD) for certain Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC-12/45 airplanes. This AD requires you to determine (maintenance records check and/or inspection) whether certain nose landing gear (NLG), main landing gear (MLG), and MLG shock absorber assemblies with a serial number beginning with ``AM'' are installed, and, if installed, would require you to replace them with ones without the ``AM.'' This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. We are issuing this AD to detect and correct the NLG, MLG, and MLG shock absorber assemblies that are affected by hydrogen embrittlement, which could result in failure of the landing gear. This failure could lead to nose or main landing gear collapse during operation with consequent loss of airplane control.
Pipeline Safety: Meetings of the Pipeline Safety Advisory Committees
Document Number: 05-21346
Type: Notice
Date: 2005-10-25
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
This notice announces public meetings of PHMSA's Technical Pipeline Safety Standards Committee (TPSSC) and Technical Hazardous Liquid Pipeline Safety Standards Committee (THLPSSC) to discuss regulatory issues.
Airworthiness Directives; Cessna Model 500, 501, 550, S550, 551, and 560 Airplanes
Document Number: 05-21309
Type: Proposed Rule
Date: 2005-10-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier proposed airworthiness directive (AD) for certain Cessna Model 500, 501, 550, S550, 551, and 560 airplanes. The original NPRM would have required revising the airplane flight manual (AFM) to prohibit use of the wing fuel boost pumps for defueling under certain conditions; installing a placard; doing other specified investigative and corrective actions as necessary; and modifying the boost pumps. The original NPRM also would have required the subsequent removal of the AFM revision and placard. The original NPRM resulted from a report of a chafed electrical wiring harness, which was arcing inside the fuel tank. This action revises the original NPRM by identifying certain service information not identified in the original NPRM. We are proposing this supplemental NPRM to prevent potential fuel vapor ignition in a fuel tank, which could result in explosion and loss of the airplane.
Release of Waybill Data
Document Number: 05-21304
Type: Notice
Date: 2005-10-25
Agency: Surface Transportation Board, Department of Transportation
Requested Administrative Waiver of the Coastwise Trade Laws
Document Number: 05-21239
Type: Notice
Date: 2005-10-25
Agency: Maritime Administration, Department of Transportation
As authorized by Public Law 105-383 and Public Law 107-295, the Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.- build requirement of the coastwise laws under certain circumstances. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below. The complete application is given in DOT docket 2005-22783 at https:// dms.dot.gov. Interested parties may comment on the effect this action may have on U.S. vessel builders or businesses in the U.S. that use U.S.-flag vessels. If MARAD determines, in accordance with Public Law 105-383 and MARAD's regulations at 46 CFR part 388 (68 FR 23084; April 30, 2003), that the issuance of the waiver will have an unduly adverse effect on a U.S.-vessel builder or a business that uses U.S.-flag vessels in that business, a waiver will not be granted. Comments should refer to the docket number of this notice and the vessel name in order for MARAD to properly consider the comments. Comments should also state the commenter's interest in the waiver application, and address the waiver criteria given in Sec. 388.4 of MARAD's regulations at 46 CFR part 388.
Requested Administrative Waiver of the Coastwise Trade Laws
Document Number: 05-21238
Type: Notice
Date: 2005-10-25
Agency: Maritime Administration, Department of Transportation
As authorized by Public Law 105-383 and Public Law 107-295, the Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.- build requirement of the coastwise laws under certain circumstances. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below. The complete application is given in DOT docket 2005-22784 at https:// dms.dot.gov. Interested parties may comment on the effect this action may have on U.S. vessel builders or businesses in the U.S. that use U.S.-flag vessels. If MARAD determines, in accordance with Public Law 105-383 and MARAD's regulations at 46 CFR part 388 (68 FR 23084; April 30, 2003), that the issuance of the waiver will have an unduly adverse effect on a U.S.-vessel builder or a business that uses U.S.-flag vessels in that business, a waiver will not be granted. Comments should refer to the docket number of this notice and the vessel name in order for MARAD to properly consider the comments. Comments should also state the commenter's interest in the waiver application, and address the waiver criteria given in Sec. 388.4 of MARAD's regulations at 46 CFR part 388.
Preparation of Environmental Impact Statement for the Downtown Birmingham/University of Alabama Birmingham Activity Centers (a.k.a. In-town Transit Partnership Project)
Document Number: 05-21237
Type: Notice
Date: 2005-10-25
Agency: Federal Transit Administration, Department of Transportation
The Federal Transit Administration and the Regional Planning Commission of Greater Birmingham are conducting an alternatives analysis and preparing a Draft Environmental Impact Statement (DEIS) for transit improvements in the Downtown Birmingham/University of Alabama Birmingham Activity Centers. The FTA is the lead federal agency and the DEIS will be prepared in accordance with National Environmental Policy Act (NEPA) and the applicable regulations for implementing NEPA, as set forth in 23 CFR part 771 and 40 CFR parts 1500-1508, as well as applicable laws and regulations including section 4(f) of the Department of Transportation Act of 1966, the Clean Air Act, and Executive Order 12898 on Environmental Justice. The project will consider the following alternatives: (1) A No- Build Alternative consisting of improvements included in the Birmingham MPO 2030 Long Range Transportation Plan; (2) Transportation System Management (TSM) Alternative that includes all reasonable cost- effective transit service improvements in the study area short of the major investment in a New starts project; (3) Build Alternative: Bus Rapid Transit (BRT) project using rubber tired vehicles operating either in mixed traffic or along an exclusive right-of-way; and (4) Build Alternative: Streetcar using light rail technology operating along tracks embedded in the pavement operating in either mixed traffic or along an exclusive right-of-way. The type, location, and need for ancillary facilities such as maintenance facilities will also be considered for each alternative. In addition, alternatives that are identified during the scoping process will be evaluated in the AA. Scoping will be accomplished through correspondence and discussions with interested persons; organizations; and Federal, State, and local agencies; and through public and agency meetings. Depending on the outcome of the scoping process and the analysis of a range of transit alternatives in the DEIS, a Locally Preferred Alternative (LPA) will be selected and addressed in the Final EIS (FEIS). The FEIS will address the potential impacts of the selected investment strategy and a No- Build Alternative.
Executive Committee of the Aviation Rulemaking Advisory Committee; Meeting
Document Number: 05-21234
Type: Notice
Date: 2005-10-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of a meeting of the Executive Committee of the Aviation Rulemaking Advisory Committee.
Pipeline Safety: Standards for Direct Assessment of Gas and Hazardous Liquid Pipelines
Document Number: 05-21233
Type: Rule
Date: 2005-10-25
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
Under current regulations governing integrity management of gas transmission lines, if an operator uses direct assessment to evaluate corrosion risks, it must carry out the direct assessment according to PHMSA standards. In response to a statutory directive, this Final Rule prescribes similar standards operators must meet when they use direct assessment on certain other onshore gas, hazardous liquid, and carbon dioxide pipelines. PHMSA believes broader application of direct assessment standards will enhance public confidence in the use of direct assessment to assure pipeline safety.
Proposed Establishment of Class E Airspace; Tok Junction, AK
Document Number: 05-21232
Type: Proposed Rule
Date: 2005-10-25
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish new Class E airspace at Tok Junction, AK. Two new Standard Instrument Approach Procedures (SIAPs) are being published for the Tok Junction Airport. There is no existing Class E airspace to contain aircraft executing the new instrument procedures at Tok Junction, AK. Adoption of this proposal would result in the establishment of Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Tok Junction, AK.
Establishment of Class E Airspace; Deering, AK
Document Number: 05-21231
Type: Rule
Date: 2005-10-25
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Deering, AK to provide adequate controlled airspace to contain aircraft executing four new Standard Instrument Approach Procedures (SIAPs). This rule results in new Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Deering, AK.
Proposed Establishment of Class E Airspace; Nondalton, AK
Document Number: 05-21230
Type: Proposed Rule
Date: 2005-10-25
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish new Class E airspace at Nondalton, AK. One new Standard Instrument Approach Procedure (SIAPs) and one Departure Procedure (DP) are being published for the Nondalton Airport. There is no existing Class E airspace to contain aircraft executing the new instrument procedures at Nondalton, AK. Adoption of this proposal would result in the establishment of Class E airspace upward from 700 feet (ft.) above the surface at Nondalton, AK.
Proposed Establishment of Class E Airspace; New Stuyahok, AK
Document Number: 05-21229
Type: Proposed Rule
Date: 2005-10-25
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish new Class E airspace at New Stuyahok, AK. Two new Standard Instrument Approach Procedures (SIAPs) are being published for the New Stuyahok Airport. There is no existing Class E airspace to contain aircraft executing the new instrument procedures at New Stuyahok, AK. Adoption of this proposal would result in the establishment of Class E airspace upward from 700 feet (ft.) above the surface at New Stuyahok, AK.
Proposed Revision of Class E Airspace; Koliganek, AK
Document Number: 05-21228
Type: Proposed Rule
Date: 2005-10-25
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to revise Class E airspace at Koliganek, AK. Two new Standard Instrument Approach Procedures (SIAPs) are being published for the Koliganek Airport. Additional Class E Airspace is needed to contain aircraft executing instrument approaches at Koliganek Airport. Adoption of this proposal would result in additional Class E airspace upward from 1,200 feet (ft.) above the surface at Koliganek, AK.
Notice of Intent To Rule on Application 05-05-C-00-MCI To Impose a Passenger Facility Charge (PFC) at Kansas City International Airport (MCI) for Use at MCI and Charles B. Wheeler Downtown Airport (MKC), Kansas City, MO
Document Number: 05-21227
Type: Notice
Date: 2005-10-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invites public comment on the application to impose a PFC at MCI for use at MCI and MKC under the provisions of the 49 U.S.C. 40117 and Part 158 of the Federal Aviation Regulations (14 CFR Part 158).
Wet Lease Policy Guidance
Document Number: 05-21226
Type: Notice
Date: 2005-10-25
Agency: Federal Aviation Administration, Department of Transportation
It has long been contrary to Federal Aviation Regulations for an air carrier to ``wet lease'' an aircraft from an individual or entity that is not separately authorized to engage in common carriage. By this notice, the Federal Aviation Administration (FAA) seeks comment on proposed policy guidance identifying those commercial arrangements that would be considered to be unlawful wet lease arrangements under these regulations as well as those that would be permissible. Additionally, we seek comment on our proposed treatment of certain other commercial arrangements between air carriers and aircraft owners thatwhile not amounting to illegal wet leasescould nevertheless result in the air carrier impermissibly ceding operational control of flight to non-certificated entities.
Mohall Central Railroad, Inc.-Acquisition and Operation Exemption-Rail Line of BNSF Railway Company
Document Number: 05-21209
Type: Notice
Date: 2005-10-25
Agency: Surface Transportation Board, Department of Transportation
Airworthiness Directives; Gippsland Aeronautics Pty. Ltd. Model GA8 Airplanes
Document Number: 05-21176
Type: Rule
Date: 2005-10-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Gippsland Aeronautics Pty. Ltd. (Gippsland) Model GA8 airplanes. This AD requires you to repetitively inspect the upper and lower grooves of the forward cargo door slide for cracks, excessive wear, and excessive width. This AD also requires you to replace the forward cargo door slide if any of the above conditions are found during any inspection. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Australia. We are issuing this AD to prevent failure of the forward cargo door slide caused by cracks, excessive wear, or excessive width. This failure could result in the cargo door detaching from the airplane in flight, potentially causing damage by hitting the back end of the airplane.
Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 501-D22A, 501-D22C, and 501-D22G Turboprop Engines
Document Number: 05-21173
Type: Rule
Date: 2005-10-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce Corporation (RRC) (formerly Allison Engine Company) 501- D22A, 501-D22C, and 501-D22G turboprop engines. This AD requires a onetime inspection for proper metal hardness of certain 1st stage, 2nd stage, 3rd stage, and 4th stage turbine wheels. This AD results from a report of a turbine wheel found to be over dimensional limits, caused by improper metal hardness. We are issuing this AD to prevent uncontained turbine wheel failure, leading to damage of the airplane and total loss of engine power.
Emergency Order Requiring Special Handling, Instruction and Testing of Railroad Operating Rules Pertaining to Hand-Operated Main Track Switches
Document Number: 05-21253
Type: Notice
Date: 2005-10-24
Agency: Federal Railroad Administration, Department of Transportation
The Federal Railroad Administration (FRA) of the United States Department of Transportation (DOT) has determined that public safety compels issuance of this Emergency Order (EO) requiring railroads to modify their operating rules and take certain other actions necessary to ensure that railroad employees who dispatch non-signaled territory or who operate hand-operated main track switches (switches) in non- signaled territory, ensure the switches are restored to their proper (normal) position after use. For purposes of this EO, ``employee'' means an individual who is engaged or compensated by a railroad or by a contractor to a railroad to perform any of the duties defined in this EO. This EO is intended to reduce the risk of serious injury or death both to railroad employees and the general public.
Agency Request for Emergency Processing of Collection of Information by the Office of Management and Budget
Document Number: 05-21250
Type: Notice
Date: 2005-10-24
Agency: Federal Railroad Administration, Department of Transportation
FRA hereby gives notice that it has submitted the following information collection request (ICR) to the Office of Management and Budget (OMB) for emergency processing under the Paperwork Reduction Act of 1995 (Pub. L. 104-13, 44 U.S.C. Chapter 35). FRA requests that OMB authorize the collection of information identified below on or before October 31, 2005, for a period of 180 days after the date of issuance of this notice in the Federal Register. A copy of this individual ICR, with applicable supporting documentation, may be obtained by calling FRA's clearance officers, Robert Brogan (telephone number (202) 493- 6292) or Victor Angelo (telephone number (202) 493-6470; these numbers are not toll-free), or by contacting Mr. Brogan via facsimile at (202) 493-6270 or Mr. Angelo via facsimile at (202) 493-6170, or via e-mail by contacting Mr. Brogan at robert.brogan@fra.dot.gov. or by contacting Mr. Angelo at victor.angelo@fra.dot.gov. Comments and questions about the ICR identified below should be directed to the Office of Information and Regulatory Affairs, Attn: OMB Desk Officer for FRA. Title: FRA Emergency Order No. 24, Notice No. 1.
Qualification of Drivers; Exemption Applications; Vision
Document Number: 05-21203
Type: Notice
Date: 2005-10-24
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
The FMCSA announces its decision to grant exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations (FMCSRs) for 40 individuals. The exemptions will enable these individuals to qualify as drivers of commercial motor vehicles (CMVs) in interstate commerce without meeting the vision standard prescribed in 49 CFR 391.41(b)(10).
Agency Information Activities; Clearance of a New Information Collection: Assessing the Effectiveness of the Arbitration Program as a Means of Settling Household Goods Disputes
Document Number: 05-21202
Type: Notice
Date: 2005-10-24
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
This notice seeks comments from the public regarding the need for FMCSA to collect information by using three new surveys to assess how household goods (HHGs) carriers and shippers (persons who arrange for the transportation of, or those who move, household goods) are satisfied with current arbitration dispute resolution procedures. The information collection (IC) meets the statutory requirements of the Interstate Commerce Commission Termination Act of 1995 (ICCTA). This notice is published (pursuant to the Paperwork Reduction Act of 1995) to measure the need for the proposed information collection, to find ways to minimize the burden on household goods shippers and carriers, to find ways to enhance the quality of information collected, and to verify the accuracy of the agency's estimate of the burden (measured in work hours) on household goods shippers and carriers.
Application of U.S. Helicopter Corporation for Certificate Authority
Document Number: 05-21200
Type: Notice
Date: 2005-10-24
Agency: Office of the Secretary, Department of Transportation
The Department of Transportation is directing all interested persons to show cause why it should not issue an order finding U.S. Helicopter Corporation fit, willing, and able, and awarding it a certificate of public convenience and necessity to engage in interstate scheduled air transportation of persons, property, and mail.
Applications of Platinum Airlines, Inc. for Certificate Authority
Document Number: 05-21199
Type: Notice
Date: 2005-10-24
Agency: Office of the Secretary, Department of Transportation
The Department of Transportation is directing all interested persons to show cause why it should not issue orders finding Platinum Airlines, Inc. fit, willing, and able, and awarding it certificates of public convenience and necessity to engage in interstate and foreign charter air transportation of persons, property and mail.
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