Department of Transportation July 6, 2005 – Federal Register Recent Federal Regulation Documents
Results 1 - 20 of 20
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.
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. 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; 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. 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.
Environmental Impact Statement for the East Contra Costa BART Extension, California
The Federal Transit Administration (FTA) and the San Francisco Bay Area Rapid Transit District (BART) intend to prepare a joint Environmental Impact Statement (EIS) pursuant to the National Environmental Policy Act (NEPA) and Environmental Impact Report (EIR) pursuant to the California Environmental Quality Act (CEQA) for proposed transit service to eastern Contra Costa County. The project would extend service from the existing BART terminus station at Pittsburg/BayPoint, through the communities of Pittsburg, Antioch, Brentwood, and Oakley, to a new terminus in Byron. The corridor generally follows State Route 4 through the eastern part of the county. As an extension of BART service into Eastern Contra Costa County, the project, commonly referred to as ``eBART,'' is intended to improve travel in the increasingly congested State Route 4 corridor by providing direct coordinated connections to the BART system. An earlier planning and feasibility study completed in 2002 evaluated a wide range of alternatives and recommended an innovative transit service concept, which employs light-weight, self-propelled rail cars known as Diesel Multiple Units (DMUs) on right-of-way to be acquired from the Union Pacific Railroad. Service with DMUs is intended to provide a seamless connection to the existing BART service but at a much lower cost. The EIS/EIR will evaluate the DMU alternative (the Proposed Action) and will also evaluate a no build alternative, a bus rapid transit alternative, and a conventional BART extension to Hillcrest Avenue in Antioch. Other alternatives may also surface during the scoping process. Based on the presentation of the Proposed Action, project alternatives, and breadth of the environmental analysis described below, please let us know of your views regarding the scope and content of the EIS/EIR. Your suggestions can be communicated at the scoping meeting or via email or letter to the contact person identified below.
Notice of Intent To Request Approval From the Office of Management and Budget (OMB) of One New Public Collection of Information
In compliance with the Paperwork Reduction Act (44 U.S.C. 3501 et seq.), the FAA invites public comment on one public information collection which will be submitted to OMB for review and approval.
Proposed Establishment of Area Navigation Instrument Flight Rules Terminal Transition Routes (RITTR); Cincinnati, OH
This action proposes to establish four Area Navigation Instrument Flight Rules Terminal Transition Routes (RITTR) in the Cincinnati, OH, terminal area. RITTRs are low altitude Air Traffic Service routes, based on area navigation (RNAV), for use by aircraft having instrument flight rules (IFR)-approved Global Positioning (GPS)/ Global Navigation Satellite System (GNSS) equipment. The purpose of RITTR is to expedite the handling of IFR overflight aircraft through busy terminal airspace areas. The FAA is proposing this action to enhance the safe and efficient use of the navigable airspace in the Cincinnati, OH, terminal area.
Spyker Automobielen B.V.; Grant of Application for a Temporary Exemption From Federal Motor Vehicle Safety Standards No. 108, and 208; and Part 581 Bumper Standard
This notice grants the Spyker Automobielen B.V. (``Spyker'') application for a temporary exemption from the requirements of S4.1.5.3 and S14 of Federal Motor Vehicle Safety Standard (FMVSS) No. 208, Occupant crash protection, and Part 581 Bumper Standard. This notice also partially grants the Spyker application for a temporary exemption from FMVSS No. 108, Lamps, reflective devices, and associated equipment. The exemptions apply to the Spyker C8 vehicle line. In accordance with 49 CFR Part 555, the basis for the grant is that compliance would cause substantial economic hardship to a manufacturer that has tried in good faith to comply with the standard.\1\ While the exemption from FMVSS No. 208 and Part 581 will be effective for a period of three years, the exemption from FMVSS No. 108 is limited to the first 10 Spyker C8 vehicles imported and sold in the United States.
Defect and Noncompliance Responsibility and Reports Defect and Noncompliance Notification
This document responds to petitions for reconsideration of the June 23, 2004 dealer notification rule that amended several provisions of agency regulations on notifications by manufacturers of motor vehicles and motor vehicle equipment to dealers and distributors when they or NHTSA decide that vehicles or equipment contain a defect related to motor vehicle safety or do not comply with a Federal motor vehicle safety standard.
Environmental Impact Statement: Sussex County, Delaware
The FHWA is issuing this notice to advise the public that an Environmental Impact Statement (EIS) will be prepared for a proposed highway improvement project in eastern Sussex County, Delaware.
Airworthiness Directives; Bell Helicopter Textron Model 47D1, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1, 47G-3B-2, 47G-3B-2A, 47G-4, 47G-4A, 47G-5, 47G-5A and Coastal Helicopters, Inc. Model OH-13H (Tomcat Mark 5A, 6B, 6C) Helicopters
This document proposes adopting a new airworthiness directive (AD) for Bell Helicopter Textron (Bell) Model 47D1, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1, 47G-3B-2, 47G-3B-2A, 47G-4, 47G-4A, 47G-5, 47G-5A and Coastal Helicopters, Inc. Model OH-13H (Tomcat Mark 5A, 6B, 6C) helicopters that have a certain scissors assembly or weld assembly scissors bracket installed. The AD would require, within 60 days, determining and recording the total hours time-in-service (TIS) for each Parts Manufacturer Approval (PMA)-produced scissors assembly and weld assembly scissors bracket and would establish a life limit for each affected part. This proposal is prompted by the need to establish a life limit on scissors assemblies and weld assembly scissors brackets produced under PMA No. PQ808SW or installed per Supplemental Type Certificate (STC) No. SH2772SW. The actions specified by the proposed AD are intended to establish a life limit to prevent using a scissors assembly or weld assembly scissors bracket past its life limit, which could result in failure of the part and subsequent loss of control of the helicopter.
Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 767-200, -300, and -300F series airplanes. This proposed AD would require replacing the aileron control override quadrant with a modified unit. This proposed AD is prompted by a report of the seizing of the input override mechanism bearings of the lateral central control actuator on affected airplanes. We are proposing this AD to prevent corrosion of the input override mechanism bearings of the lateral central control actuator, which, in the event of a subsequent jam in the pilot's aileron control system, could result in failure of the aileron override system and consequent reduced lateral controllability of the airplane.
Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 777-200 and -300 series airplanes. This AD requires applying an anti-static conductive coating to the fuel access and thermal anti-icing blowout doors at the location of the bonding fasteners on the leading edge of the wings, and performing a resistance test on the new coating to ensure correct ground path resistance. This AD is prompted by a report that an anti-static coating was not applied correctly on doors located within a flammable fluid leakage zone. We are issuing this AD to prevent an uncontrollable fire in the leading edge of the wing, which could damage critical wing structures and cause a fuel tank explosion.
Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 767-200 and -300 series airplanes. This proposed AD would require measuring the turnbuckle gap of the inflation cylinder of the off-wing emergency escape slide; corrective action if necessary; and installing a safety device on the inflation cylinder of the off-wing emergency escape slide. This proposed AD is prompted by a report indicating that the inflation trigger cable may inadvertently disconnect from the inflation turnbuckle of the inflation cylinder of the off-wing emergency escape slide, due to incorrect spacing of the cable insertion gap; and additional reports indicating that the pull force increase mechanism on the off-wing charged cylinder assemblies of the escape slide may be inadvertently disengaged. We are proposing this AD to prevent failed deployment of the emergency escape slide during an emergency, which could impede an evacuation and result in injury to passengers or airplane crewmembers, or inadvertent inflation and loss of an emergency escape slide during flight, which could result in possible structural damage to the airplane.
Airworthiness Directives; Boeing Model 757 Airplanes
The FAA is revising an earlier proposed airworthiness directive (AD) for certain Boeing Model 757 airplanes. The original NPRM would have required inspections of certain wire bundles in the left and right engine-to-wing aft fairings for discrepancies, and related investigative and corrective actions if necessary. The original NPRM was prompted by a report indicating that a circuit breaker for the fuel shutoff valve tripped due to a wire that chafed against the structure in the flammable leakage zone of the aft fairing, causing a short circuit. This action revises the original NPRM by adding a new requirement for installing back-to-back p-clamps between the wire and hydraulic supply tube at the aft end of the right-hand strut only; and associated re-routing of the wire bundles, if necessary; and adding airplanes to the applicability. This action also clarifies the applicability specified in the original NPRM. We are proposing this supplemental NPRM to prevent chafing between the wire bundle and the structure of the aft fairing, which could result in electrical arcing and subsequent ignition of flammable vapors and possible uncontrollable fire.
Proposed Agency Information Collection Activities; Comment Request
In accordance with the Paperwork Reduction Act of 1995 and its implementing regulations, the Federal Railroad Administration (FRA) hereby announces that it is seeking renewal of the following currently approved information collection activities. Before submitting these information collection requirements (ICRs) for clearance by the Office of Management and Budget (OMB), FRA is soliciting public comment on specific aspects of the activities identified below.
Inflation Adjustment of the Ordinary Maximum Civil Monetary Penalty for a Violation of a Federal Railroad Safety Law or Federal Railroad Administration Safety Regulation
FRA is withdrawing its final rule that adjusted from $11,000 to $15,000 the ordinary maximum civil penalty that applies when a civil penalty for a violation of railroad safety statutes and regulations is assessed under its authority, due to an error in the application of the rounding rules found in the applicable statute. The ordinary maximum civil penalty will remain at $11,000.
Airworthiness Directives; Airbus Model A300 B2-203 and B4-203 Airplanes; Model A310-200 and -300 Series Airplanes; and Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model A300 C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)
The FAA is adopting a new airworthiness directive (AD) for certain Airbus transport category airplanes. This AD requires an inspection to determine if suspect part numbers (P/Ns) and serial numbers of certain Thales Avionics equipment are installed, and replacement of any suspect part with a modified part having a new P/N. This 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 issuing 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; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 and EMB-135 Series Airplanes
This amendment adopts a new airworthiness directive (AD), applicable to certain EMBRAER Model EMB-145 and EMB-135 series airplanes, that requires replacement of the engine-driven hydraulic pump. This action is necessary to prevent engine oil leakage at the coupling seal between the hydraulic pump and the engine gearbox from causing low engine oil levels, which could lead to in-flight engine shutdown and consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.
This site is protected by reCAPTCHA and the Google
Privacy Policy and
Terms of Service apply.