Department of Transportation May 18, 2005 – Federal Register Recent Federal Regulation Documents
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Notice of Availability and Public Comment Period for the Draft Air Quality General Conformity Determination (DGCD) for Proposed New Runways and Associated Development at Chicago O'Hare International Airport, Chicago, IL
The Federal Aviation Administration (FAA) is issuing this notice to advise the public that a Draft Air Quality General Conformity Determination (DGCD) for the O'Hare Modernization Environmental Impact Statement at Chicago O'Hare International Airport has been prepared and is available for public review and comment. In accordance with section 176(c) of the Federal Clean Air Act, FAA has assessed whether the air emissions that would result from FAA's action in approving the proposed projects conform with the Illinois State Implementation Plan (SIP). This assessment is contained in the DGCD. The comment period is open as of the date of this Notice of Availability and closes June 20, 2005. Comments must be sent to Michael W. MacMullen of the FAA at the address shown below, and written comments must be postmarked and emails must be sent by not later than midnight, June 20, 2005.
Revision of Federal Airways V-2, V-257 and V-343; MT
This action revises three Very High Frequency Omnidirectional Range (VOR) Federal airways southeast of Missoula, MT (V-2, V-257, and V-343). These VOR Federal airways are being revised due to the decommissioning of the Drummond VOR. These changes will enhance air safety, simplify routings, and reduce controller workload in Montana.
Notice of Availability of a Draft Environmental Assessment for the Proposed New Air Traffic Control Tower at the St. Louis Downtown Airport in Cahokia, IL
the Federal Aviation Administration (FAA) has prepared and is making available the Draft Environmental Assessment (DEA) for the following proposed action at the St. Louis Downtown Airport: The construction of a new Air Traffic Control Tower, associated support building, parking lot, and access road. The Draft EA is being prepared in accordance with the National Environmental Policy Act (NEPA) of 1969, as amended, FAA Order 1050.1E ``Environmental Impacts: Policies and Procedures'', and FAA Order 5050.4A, ``Airport Environmental Handbook.'' The proposed development action is consistent with the National Airspace System Plan prepared by the U.S. Department of Transportation, Federal Aviation Administration (FAA). A Draft Environmental Assessment will be available for public review and comment at the following locations:
Notice of Intent To Rule on Request To Release Airport Land at Nut Tree Airport, Vacaville, CA
The Federal Aviation Administration (FAA) proposes to rule and invites public comment on the release of Solano County from the conditions and restrictions contained in applicable grant agreements with the United States for approximately 1.9 acres of undeveloped airport land obligated for airport purposes at Nut Tree Airport, Vacaville, California, and which is not needed for airport purposes. The airport land is needed for the realignment and widening of East Monte Vista Avenue, the primary access to the Airport. The improvements to East Monte Vista Avenue represent a compatible land use and will provide better access to the Airport and enhance the value and economic vitality of the Airport. Upon the release of this airport land, the City of Vacaville will acquire the land at appraised fair market value. Solano County will use the sale proceeds for needed airport improvements.
Rules of Practice
FMCSA amends its Rules of Practice for Motor Carrier, Broker, Freight Forwarder, and Hazardous Materials Proceedings. These rules increase the efficiency of the procedures, enhance due process and awareness of the public and regulated community, and accommodate recent programmatic changes. The changes in these rules apply to all motor carriers, other business entities, and individuals involved in motor carrier safety and hazardous materials administrative actions and proceedings with FMCSA.
Public Meeting To Discuss the Establishment of a National Registry of Certified Medical Examiners
FMCSA announces a public meeting concerning a National Registry of Certified Medical Examiners (NRCME). If established, the NRCME would be a database of medical examiners certified by FMCSA (or a third party) to conduct medical examinations of interstate commercial motor vehicle (CMV) drivers and effectively determine their physical qualifications to operate such vehicles in interstate commerce as defined in 49 CFR 391.41. If the NRCME is implemented, the FMCSA would only accept medical examinations conducted by persons listed in the NRCME as proof of the physical qualifications standards for interstate CMV drivers. The meeting is intended to provide a general introduction to the NRCME concept and an opportunity for discussion with subject matter experts.
Notice To Extend Comment Period for an Environmental Impact Statement: St. Louis City and St. Louis County, MO
The FHWA is issuing this notice to advise the public that we are extending the comment period for a final environmental impact statement (EIS) for improvements on I-64 in the City of St. Louis and St. Louis County, Missouri.
Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes; Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600); and Model A310 Series Airplanes
The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to certain Airbus airplane models, as specified above. The original NPRM would have required modifying the thermal insulation system of certain fuselage frames, and modifying the fuselage drainage system. The original NPRM would also have required revising the FAA-approved maintenance inspection program to include inspections for corrosion or cracking in the subject areas. The original NPRM was prompted by reports of corrosion in the lower part of the pressure bulkhead at certain fuselage frames. This action revises the original NPRM by expanding the applicability to include additional airplanes. We are proposing this supplemental NPRM to prevent accumulation of condensation in the insulation blankets of certain fuselage frames, which could cause corrosion that could result in reduced structural integrity of the fuselage and consequent rapid decompression of the airplane.
Airworthiness Directives; Boeing Model 767 Airplanes Equipped with General Electric Model CF6-80C2 Engines
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 767 airplanes. This proposed AD would require modifying a relay installation and associated wiring of the engine cowl anti-ice system and performing a functional test of the thrust reverser system. This proposed AD would also require replacing the operational program software of certain indicating/recording systems. This proposed AD is prompted by numerous operator reports of failures of the lock flexshaft of the thrust reverser actuation system (TRAS) between the upper actuator and the TRAS lock. We are proposing this AD to prevent high power in-flight deployment of a thrust reverser, which could cause high roll force and consequent departure from controlled flight.
Petitions for Exemption; Summary of Petitions Received
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains a summary of certain petitions seeking relief from specified requirements of 14 CFR. On January 13, 2005, a notice was published of a petition seeking relief from the requirements of 14 CFR 25.841(a)(2)(ii). By a letter dated March 4, 2005, the petitioner submitted additional information that indicated that it would also be necessary to obtain exemption from the related requirements of Sec. 25.841(a)(2)(i). The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.
Petitions for Exemption; Dispositions of Petitions Issued
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption, part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains the disposition of certain petitions previously received. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.
Airworthiness Directives; Schweizer Aircraft Corporation Model 269C, C-1, and D Helicopters
This amendment adopts a new airworthiness directive (AD) for the Schweizer Aircraft Corporation (Schweizer) Model 269C, C-1, and D helicopters. This action requires inspecting, modifying, and testing the lateral control trim actuator assembly on certain serial-numbered helicopters. This amendment is prompted by three reported incidents of the inner spring tube separating from the lateral trim control housing resulting in a lateral cyclic control restriction. The actions specified in this AD are intended to prevent separation of the inner spring tube from the lateral trim control housing and the associated loss of trim control, increased local resistance to right cyclic stick movement, and an emergency landing or subsequent loss of control of the helicopter.
Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-B17B, -B17C, -B17D, -B17E, -C20, -C20B, -C20F, -C20J, -C20S, and -C20W Turboprop and Turboshaft Engines
The FAA is adopting a new airworthiness directive (AD) for Rolls- Royce Corporation (RRC) (formerly Allison Engine Company) 250-B17B, - B17C, -B17D, -B17E, -C20, -C20B, -C20F, -C20J, -C20S, and -C20W turboprop and turboshaft engines that do not have turbine energy absorbing ring, RRC part number (P/N) 23035175, or an equivalent FAA- approved serviceable turbine energy absorbing ring, installed. This AD requires installation of a turbine energy absorbing ring in the plane of the 1st stage turbine wheel. This AD results from an unacceptable rate of uncontained 1st stage turbine wheel failures. We are issuing this AD to minimize the risk of uncontained 1st stage turbine wheel fragments from causing damage to the aircraft or damage to the second engine on twin-engine installations, which could lead to loss of control and loss of the aircraft.
Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes
The FAA is superseding an existing airworthiness directive (AD), which applies to all Boeing Model 737-300, -400, and -500 series airplanes. That AD currently requires repetitive inspections of certain connectors located in the main wheel well to detect discrepancies, and corrective action if necessary. This new AD instead mandates a modification. This AD is prompted by the development of a modification intended to address the unsafe condition. We are issuing this AD to prevent discrepancies of certain connectors located in the main wheel well. Those discrepancies could result in electrical arcing of the connectors, uncommanded closure of the engine fuel shut-off valves, and consequent in-flight loss of thrust or engine shutdown from lack of fuel.
Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes); and Model A310 Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Airbus model airplanes, as specified above. This AD requires modifying the electrical bonding points of additional center tanks. This AD is prompted by the results of fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent electrical arcing inside the fuel tank, due to insufficient bonding, which could result in the ignition of fuel vapors with a potential risk of explosion of the fuel tank.
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