Department of Transportation April 2006 – Federal Register Recent Federal Regulation Documents

Results 101 - 150 of 253
Establishment of Class D Airspace; Bay St. Louis, MS
Document Number: 06-3622
Type: Rule
Date: 2006-04-17
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class D airspace at Bay St. Louis, MS. A Federal contract tower with a weather reporting system is being constructed at the Stennis International Airport. Therefore, the airport will meet the criteria for establishment of Class D airspace. Class D surface area airspace is required when the control tower is open to contain existing Standard Instrument Approach Procedures (SIAPs) and other Instrument Flight Rules (IFR) operations at the airport. This action will establish Class D airspace extending upward from the surface, to and including 2,500 feet MSL, within a 4.2-mile radius of the airport.
Airworthiness Directives; General Electric Company Aircraft Engines (GEAE) CT7-8A Turboshaft Engines
Document Number: 06-3616
Type: Rule
Date: 2006-04-17
Agency: Federal Aviation Administration, Department of Transportation
This document publishes in the Federal Register an amendment adopting emergency airworthiness directive (EAD) 2006-06-51 that we sent previously to all known U.S. owners and operators of GEAE CT7-8A turboshaft engines installed on Sikorsky S92 helicopters. This AD requires initial and repetitive inspections of the electrical chip detectors for the No. 3 bearing. This AD results from two failures of the No. 3 bearing in GEAE CT7-8A engines. We are issuing this AD to prevent failures of the No. 3 bearings and possible dual in-flight shutdowns of the engines.
Airworthiness Directives; Air Tractor, Inc. Model AT-501 Airplanes
Document Number: 06-3614
Type: Rule
Date: 2006-04-17
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) to revise AD 2002-11-05, which applies to certain Air Tractor, Inc. (Air Tractor) AT-400 series and Models AT-501, AT-802, and AT-802A airplanes. AD 2002-11-05 establishes a safe life for the wing lower spar cap. Since we issued AD 2002-11-05, we have received reports of cracks found prior to the established safe life on AT-400 series airplanes and on Model AT-802A airplanes. We are issuing separate AD actions for AT-400 series and Models AT-802 and AT-802A airplanes to address the unsafe condition of those airplanes. This AD retains the actions required in AD 2002-11-05 for Model AT-501 airplanes and removes AT-400 series and Models AT-802 and AT-802A airplanes from the applicability of AD 2002-11-05.
Standard Instrument Approach Procedures; Miscellaneous Amendments
Document Number: 06-3561
Type: Rule
Date: 2006-04-17
Agency: Federal Aviation Administration, Department of Transportation
This amendment amends Standard Instrument Approach Procedures (SIAPs) for operations at certain airports. These regulatory actions are needed because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, addition of new obstacles, or changes in air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Standard Instrument Approach Procedures, Weather Takeoff Minimums; Miscellaneous Amendments
Document Number: 06-3560
Type: Rule
Date: 2006-04-17
Agency: Federal Aviation Administration, Department of Transportation
This amendment establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and/or Weather Takeoff Minimums for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, addition of new obstacles, or changes in air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Airworthiness Directives; Brantly International, Inc. Model B-2, B-2A, and B-2B Helicopters
Document Number: 06-3536
Type: Rule
Date: 2006-04-17
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD) for the specified Brantly International, Inc. (Brantly) model helicopters. This action requires certain inspections and measurements of the upper tail rotor vertical gearbox (gearbox), vertical shaft (shaft) and shaft housing (housing) and their associated parts; and of the intermediate gear box bushing (bushing). This amendment is prompted by an accident and an incident report of fatigue cracking of a shaft. The actions specified in this AD are intended to prevent fatigue cracking of a shaft, failure of a shaft, and subsequent loss of control of the helicopter.
TIFIA Program Public Meeting
Document Number: E6-5594
Type: Notice
Date: 2006-04-14
Agency: Federal Highway Administration, Department of Transportation
The DOT seeks views on regulatory implementation of changes made by SAFETEA-LU to the TIFIA statute. All interested persons are invited to offer views at two public meetings.
Qualification of Drivers; Exemption Applications; Vision
Document Number: E6-5593
Type: Notice
Date: 2006-04-14
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces its decision to renew the exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations for 18 individuals. FMCSA has statutory authority to exempt individuals from its vision standards if the exemptions granted will not compromise safety. The exemptions will enable these individuals to operate commercial motor vehicles (CMVs) in interstate commerce without meeting the vision standard prescribed in 49 CFR 391.41(b)(10). The Agency has concluded that granting these exemptions will provide a level of safety that is equivalent to, or greater than, the level of safety maintained without the exemptions for these commercial motor vehicle (CMV) drivers.
Qualification of Drivers; Exemption Applications; Vision
Document Number: E6-5592
Type: Notice
Date: 2006-04-14
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces its decision to exempt 19 individuals from the vision requirement in the Federal Motor Carrier Safety Regulations (FMCSR). The exemptions will enable these individuals to operate commercial motor vehicles (CMVs) in interstate commerce without meeting the vision standard prescribed in 49 CFR 391.41(b)(10). The Agency has concluded that granting these exemptions will provide a level of safety that is equivalent to, or greater than, the level of safety maintained without the exemptions for these CMV drivers.
Demonstration of Enhanced Human Service Transportation Models: Phase 1-System Development and Design
Document Number: E6-5588
Type: Notice
Date: 2006-04-14
Agency: Federal Transit Administration, Department of Transportation
This notice is a request for proposals (RFP) for system development and design of enhanced human service transportation models. The USDOT seeks up to 10 local communities to carry out detailed development and design of coordinated human service transportation systems that utilize Intelligent Transportation Systems capabilities. The expected results from Phase 1 include up to 10 ``deployment- ready,'' replicable and scalable system detailed designs for enhanced human service transportation delivery models in communities representing a variety of operational environments and scenarios.
Proposed Cancellation of the Air Taxi Authority of Aero Leasings, Inc. D/B/A Air Florida Airlines
Document Number: E6-5552
Type: Notice
Date: 2006-04-14
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 (1) finding that Aero Leasings, Inc. d/b/a Air Florida Airlines lacks the compliance disposition to hold part 298 exemption authority (2) proposing to cancel its part 298 exemption authority.
BNSF Railway Company-Abandonment Exemption-in Thurston County, WA
Document Number: E6-5546
Type: Notice
Date: 2006-04-14
Agency: Surface Transportation Board, Department of Transportation
BNSF Railway Company-Abandonment Exemption-in Morrison County, MN
Document Number: E6-5491
Type: Notice
Date: 2006-04-14
Agency: Surface Transportation Board, Department of Transportation
National Fuel Cell Bus Technology Development Program
Document Number: 06-3606
Type: Notice
Date: 2006-04-14
Agency: Department of Transportation, Federal Transit Administration Federal Register Notice, Federal Transit Administration
This competitive solicitation is for fiscal year 2006-2009 funding, subject to congressional appropriations action, for the new National Fuel Cell Bus Technology Development Program (NFCBP), administered by the Federal Transit Administration. The purpose of the program is to facilitate the development of commercially viable fuel cell bus technology and related infrastructure. FTA intends to enter into grants, contracts, and cooperative agreements with no more than 3 geographically diverse nonprofit organizations and recipients under chapter 53 of title 49, United States Code, to conduct fuel cell bus technology and infrastructure projects under the program. Regional consortia in partnership with transit agencies are encouraged to apply. The Federal share of the cost of a project carried out under this Program shall not exceed 50 percent of such cost.
Office of Hazardous Materials Safety; Notice of Applications for Modification of Special Permit
Document Number: 06-3589
Type: Notice
Date: 2006-04-14
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
In accordance with the procedures governing the application for, and the processing of, special permits from the Department of Transportation's Hazardous Material Regulations (49 CFR part 107, subpart B), notice is hereby given that the Office of Hazardous Materials Safety has received the application described herein. This notice is abbreviated to expedite docketing and public notice. Because the sections affected, modes of transportation, and the nature of application have been shown in earlier Federal Register publications, they are not repeated here. Request of modifications of special permits (e.g. to provide for additional hazardous materials, packaging design changes, additional mode of transportation, etc.) are described in footnotes to the application number. Application numbers with the suffic ``M'' denote a modification request. These applications have been separated from the new applications for special permits to facilitate processing.
Office of Hazardous Materials Safety; Notice of Application for Special Permits
Document Number: 06-3588
Type: Notice
Date: 2006-04-14
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
In accordance with the procedures governing the application for, and the processing of, special permits from the Department of Transportation's Hazardous Material Regulations (49 CFR Part 107, Subpart B), notice is hereby given that the Office of Hazardous Materials Safety has received the application described herein. Each mode of transportation for which a particular special permit is requested is indicated by a number in the ``Nature of Application'' portion of the table below as follows: 1Motor vehicle, 2Rail freight, 3Cargo vessel, 4Cargo aircraft only, 5Passenger-carrying aircraft.
Qualification of Drivers; Exemption Applications; Vision
Document Number: 06-3587
Type: Notice
Date: 2006-04-14
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces its decision to exempt 14 individuals from the vision requirement in the Federal Motor Carrier Safety Regulations (FMCSR). The exemptions will enable these individuals to operate commercial motor vehicles (CMVs) in interstate commerce without meeting the vision standard prescribed in 49 CFR 391.41(b)(10). The Agency has concluded that granting these exemptions will provide a level of safety that is equivalent to, or greater than, the level of safety maintained without the exemptions for these CMV drivers.
Environmental Impact Statement: Grant, Hardy, Hampshire, and Mineral Counties in WV; and, Allegany County, MD
Document Number: 06-3576
Type: Notice
Date: 2006-04-14
Agency: Federal Highway Administration, Department of Transportation
The FHWA is issuing this notice to advise the public that a Tier I Environmental Impact Statement (EIS) will be prepared to review improvements in the existing transportation system between Interstate 68 in Western Maryland and Appalachian Corridor H in the West Virginia Potomac Highlands. The study area generally parallels the existing U.S. 220 highway corridor.
Average Fuel Economy Standards for Light Trucks Model Years 2008-2011
Document Number: 06-3533
Type: Rule
Date: 2006-04-14
Agency: National Highway Traffic Safety Administration, Department of Transportation
The National Highway Traffic Safety Administration published in the Federal Register of April 6, 2006, a final rule establishing Corporate Average Fuel Economy (CAFE) standards for light trucks manufactured in model years 2008 through 2011. Inadvertently, the document had the wrong docket number; footprint and target fuel economy values provided in example calculations did not have the correct number of decimal places; the definition of ``footprint'' in the regulatory text was incorrect; and Figure 1 of the regulatory text incorrectly referenced ``model,'' as opposed to ``model type.'' Additionally, there was a typographical error in the regulatory text regarding the flat floor provision. This document makes the appropriate corrections.
Proposed Modification of Control 1234L Offshore Airspace Area; AK
Document Number: E6-5523
Type: Proposed Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend Control 1234L, Offshore Airspace Area in Alaska. Specifically, this action proposes to modify Control 1234L in the immediate vicinity of the Saint Paul Island Airport, AK, by lowering the airspace floor from 2,000 feet above ground level (AGL) to 700 AGL. Additionally, outside the vicinity of the airport this proposal lowers the airspace floor from 2,000 AGL to 1,200 feet AGL within a 73-mile radius of the St. Paul Island Airport. The FAA is proposing this action to provide additional controlled airspace for aircraft instrument operations (IFR) at the St. Paul Island Airport.
Notice of National Grain Car Council Meeting
Document Number: E6-5505
Type: Notice
Date: 2006-04-13
Agency: Surface Transportation Board, Department of Transportation
Notice is hereby given of a meeting of the National Grain Car Council (NGCC), pursuant to section 10(a)(2) of the Federal Advisory Committee Act, Public Law No. 92-463, as amended (5 U.S.C., App. 2).
Released Rates of Motor Common Carriers of Household Goods
Document Number: E6-5503
Type: Notice
Date: 2006-04-13
Agency: Surface Transportation Board, Department of Transportation
The Household Goods Carriers' Bureau Committee (Committee), on behalf of its member motor carriers, seeks authority to amend Released Rates Decision No. MC-999 by changing the index used for annual adjustments to the minimum per-pound valuation and to the charges for protecting the full value of shipments of household goods.
North Central Railway Association, Inc.-Abandonment Exemption-in Hardin County, IA
Document Number: E6-5487
Type: Notice
Date: 2006-04-13
Agency: Surface Transportation Board, Department of Transportation
Airworthiness Directives; Airbus Model A319, A320, and A321 Airplanes
Document Number: E6-5476
Type: Proposed Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A319, A320, and A321 airplanes. This proposed AD would require a detailed inspection for cracks and marks on the carbon blades of the ram air turbine (RAT), and replacement of the RAT with a new or serviceable RAT if necessary. This proposed AD results from a report of three chord-wise cracks on the aft side of one carbon blade of a certain RAT. We are proposing this AD to detect and correct cracks and/or marks on the RAT carbon blades, which could result in reduced structural integrity of the carbon blade, and consequent loss of the RAT as a source of hydraulic and electrical power in an emergency.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145XR Airplanes
Document Number: E6-5474
Type: Proposed Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain EMBRAER Model EMB-145XR airplanes. This proposed AD would require modification of the flap system interface wiring. This proposed AD results from a finding that the aural and visual warnings, which should be activated when the flaps are set to 22 degrees during takeoff, were not enabled during the manufacture of certain Model EMB- 145XR airplanes. We are proposing this AD to prevent overrunning the runway during takeoff.
Airworthiness Directives; McDonnell Douglas Model DC-9-31, DC-9-32, DC-9-32F, DC-9-33F, DC-9-34, and DC-9-34F Airplanes; and Model DC-9-40 and DC-9-50 Series Airplanes
Document Number: E6-5472
Type: Proposed Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain transport category airplanes, identified above. This proposed AD would require installing a bonding jumper from the boost pump volute to the fuel tank structure, and related investigative/ corrective actions. This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent point-contact arcing or filament heating in the fuel tank, which, in the event of a short or ground fault inside the fuel tank, could result in a fuel tank explosion and consequent loss of the airplane.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145XR Airplanes
Document Number: E6-5470
Type: Proposed Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain EMBRAER Model EMB-145XR airplanes. This proposed AD would require replacement of certain segments of the passenger seat tracks with new, improved seat tracks. This proposed AD results from instances where the shear plungers of the passenger seat legs were not adequately fastened. We are proposing this AD to prevent inadequate fastening of the seat leg shear plungers, which could result in failure of the passenger seat tracks during emergency landing conditions and consequent injury to passengers.
Airworthiness Directives; Boeing Model 737-100, -200, and -200C Series Airplanes
Document Number: E6-5469
Type: Proposed Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Boeing Model 737 series airplanes. The existing AD currently requires inspection of the elevator tab inboard hinge support structure to detect fatigue cracking and corrective action if necessary. That AD also provides an optional terminating action. This proposed AD would add airplanes to the applicability and would require new repetitive inspections. For airplanes having elevators with laminated rear spars, this proposed AD would require repetitive inspections for interlaminar corrosion, delamination, or disbonding in the rear spar, repetitive inspections for cracking in the spar web, and repair including related investigative/corrective actions if necessary. For airplanes having elevators with solid rear spars, this proposed AD would require repetitive inspections for cracking in the spar web and repair including related investigative/corrective actions if necessary. This proposed AD results from reports of cracks in the elevator rear spar web at the tab hinge bracket locations. We are proposing this AD to detect and correct cracking, corrosion, interlaminar corrosion, delamination, and disbonding in the elevator rear spar, which may reduce elevator stiffness and lead to in-flight vibration. In-flight vibration may lead to elevator and horizontal stabilizer damage and reduced controllability of the airplane.
Grade Crossing Signal System
Document Number: 06-55514
Type: Rule
Date: 2006-04-13
Agency: Federal Railroad Administration, Department of Transportation
Notice of Availability of a Record of Decision (ROD) and a Written Reevaluation for the Evaluation of New Information Regarding Departure Procedures at Hartsfield-Jackson Atlanta International Airport, Atlanta, GA
Document Number: 06-3581
Type: Notice
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) is making available a ROD and a Written Reevaluation for new information concerning departure procedures at Hartsfield-Jackson Atlanta International Airport, Atlanta, Georgia. Point of Contact: Mr. Steve Kelley, Acting Manager, FAA Eastern Terminal Service, Airspace and Procedures, 1 Aviation Plaza, Jamaica, NY 11434-4809, (718) 553-4558.
Establishment of Area Navigation Instrument Flight Rules Terminal Transition Route (RITTR); T-210; Jacksonville, FL
Document Number: 06-3559
Type: Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
This action corrects an error in the geographic coordinates of a waypoint (WP) listed in the description of route T-210 in a final rule published in the Federal Register on March 27, 2006 (71 FR 15027), Airspace Docket No. 05-ASO-10. This action also makes an editorial change to the order of the points listed in the route description.
Office of Hazardous Materials Safety; Notice of Delays in Processing of Special Permits Applications
Document Number: 06-3558
Type: Notice
Date: 2006-04-13
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
In accordance with the requirements of 49 U.S.C. 5117(c), PHMSA is publishing the following list of special permit applications that have been in process for 180 days or more. The reason(s) for delay and the expected completion date for action on each application is provided in association with each identified application.
Lightning Direct Effects Compliance
Document Number: 06-3557
Type: Notice
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces the availability of final policy on Lightning Direct Effects Compliance.
Airworthiness Directives; Gulfstream Model GIV-X and GV-SP Series Airplanes
Document Number: 06-3540
Type: Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an existing airworthiness directive (AD), which applies to certain Gulfstream Model GIV-X and GV-SP series airplanes. That AD currently requires revising the Limitations section of the airplane flight manual (AFM) by incorporating new procedures to follow in the event that the cockpit displays go blank or malfunction. This AD allows for the use of alternative AFM revisions for a certain subset of the existing applicability. This AD results from a report that all four of the cockpit flight panel display units simultaneously went blank during flight. We are issuing this AD to ensure that the flightcrew is advised of the appropriate procedures to follow in the event that the cockpit displays go blank or malfunction, which could result in a reduction of the flightcrew's situational awareness and possible loss of control of the airplane.
Airworthiness Directives; Eurocopter France Model SA-360C, SA-365C, SA-365C1, and SA-365C2 Helicopters
Document Number: 06-3535
Type: Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model SA-360C, SA-365C, SA-365C1, and SA-365C2 helicopters. This action requires inspecting the main gearbox (MGB) base plate for a crack and replacing the MGB if a crack is found. This amendment is prompted by the discovery of a crack in a MGB base plate. The actions specified in this AD are intended to detect a crack in a MGB base plate and prevent failure of one of the MGB attachment points to the frame, which could result in severe vibration and subsequent loss of control of the helicopter.
Airworthiness Directives; Fokker Model F.28 Mark 0100 Airplanes
Document Number: 06-3480
Type: Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Fokker Model F.28 Mark 0100 airplanes. This AD requires reinforcing the fuselage at the emergency locator transmitter system's antenna area. This AD results from a report that certain structural provisions for an optional antenna are of insufficient strength. We are issuing this AD to prevent reduced structural integrity of the airplane.
Airworthiness Directives; Sicma Aero Seat (Formerly Farner); Cabin Attendant Seats Series 150 Type FN and Series 151 Type WN
Document Number: 06-3479
Type: Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Sicma Aero Seat (formerly Farner) cabin attendant seats series 150 type FN and series 151 type WN. This AD requires installing two protection fairings over the upper seat structure to cover the gap between the upper and lower seats and prevent any contact with the bottom seat folding mechanisms. This AD results from a child catching its fingers in the folding mechanism of the bottom of the attendant seat. We are issuing this AD to prevent injury resulting from contact with the bottom folding mechanism.
Airworthiness Directives; Boeing Model 767 Airplanes
Document Number: 06-3478
Type: Rule
Date: 2006-04-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 767 airplanes. This AD requires performing a test of the bonding resistance between the engine fuel feed tube fitting and the front spar, applying sealant on a hex nut inside the dry bay, and performing any applicable corrective actions. This AD results from a report that the engine fuel feed tubes were found not electrically bonded to the front spar. We are issuing this AD to prevent an ignition source from entering the fuel tank during a lightning strike event, which could cause a fuel tank explosion.
Agency Information Collection Activities; Request for Comment; Approval of a New Information Collection: Letter of Confirmation and Carrier Contact Information Sheets
Document Number: E6-5434
Type: Notice
Date: 2006-04-12
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA invites public comment on its plan to request the Office of Management and Budget's (OMB) approval to collect information on new forms entitled ``Carrier Contact Information Sheets.'' The information will be collected from United States and Canada-based motor carriers through the use forms, and used by FMCSA Safety Auditors and Safety Investigators to prepare in advance for Compliance Reviews (CRs) and New Entrant Program Safety Audits (NEPSAs); Pre-authority Safety Audits (PASAs) and CRs of certain Mexico-domiciled motor carriers; and NEPSAs and CRs of Non-North American motor carriers. FMCSA conducts CRs to determine motor carrier compliance with the Federal Motor Carrier Safety Regulations (FMCSRs) and other regulations overseen by FMCSA. In accordance with section 350 of the 2002 DOT Appropriations Act and the Agency's regulations, all Mexico-domiciled long-haul carriers must successfully complete a PASA before receiving authority to operate in the United States and must receive a CR within their first 18 months of operations in the United States. All other motor carriers receive CRs to determine their safety fitness. FMCSA conducts NEPSAs in accordance with section 210 of the Motor Carrier Safety Improvement Act of 1999, which requires safety reviews of all new entrants during their first 18 months of operations. The information collected from motor carriers will be used to assist safety investigators to become familiar with the motor carrier's operation prior to visiting the carrier's place of business. The information collected will include, but is not limited to, company information and contact persons, business type, insurance, type of cargo transported, vehicle and driver information and controlled substance testing information. Additional information will be collected from carriers who transport hazardous materials, household goods, and passengers or are domiciled in Mexico. This notice is required by the Paperwork Reduction Act of 1995.
Airworthiness Directives; Short Brothers Model SD3 Airplanes
Document Number: E6-5357
Type: Proposed Rule
Date: 2006-04-12
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to all Short Brothers Model SD3 airplanes. The original NPRM would have required installing additional fuel tank bonding jumpers, performing an in-place resistance check of the float switches, inspecting certain internal components of the fuel tanks, and performing related corrective actions if necessary. The original NPRM would have also required revisions to the Airworthiness Limitations section of the Instructions for Continued Airworthiness, and to the airplane flight manual procedures for operation during icing conditions and fuel system failures. The original NPRM resulted from fuel system reviews conducted by the manufacturer. This action revises the original NPRM by adding service information. We are proposing this supplemental NPRM to prevent ignition sources inside the fuel tanks, which could lead to fire or explosion.
Federal Motor Vehicle Safety Standards; Power-Operated Window, Partition, and Roof Panel Systems
Document Number: 06-3505
Type: Rule
Date: 2006-04-12
Agency: National Highway Traffic Safety Administration, Department of Transportation
This document responds to two petitions for reconsideration of our September 2004 final rule amending the Federal motor vehicle safety standard for power-operated windows, partitions, and roof panel systems. The amendments required that switches for these windows and other items in new motor vehicles be resistant to accidental actuation that causes those items to begin to close. The purpose of the amendments was to reduce the number of injuries and fatalities to people, especially children, that occur when they unintentionally close the power-operated items on themselves by accidentally leaning against or kneeling or standing on the switch or when other occupants accidentally actuate the switch in that manner. The petitions for reconsideration requested that the agency adopt additional amendments. The petitions are granted in part and denied in part. In responding to the petitions' request to require ``pull-up-to- close'' power window switches, we are simultaneously implementing a congressional mandate to require such switches. In addition, through this document, we are amending the standard to make a number of technical amendments.
Airworthiness Directives; Boeing Model 747-200C and -200F Series Airplanes
Document Number: 06-3432
Type: Rule
Date: 2006-04-12
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 747-200C and -200F series airplanes. That AD currently requires repetitive inspections to find fatigue cracking in the upper chord of the upper deck floor beams, and repair if necessary. For certain airplanes, the existing AD also provides an optional repair/modification, which extends certain repetitive inspection intervals. This new AD reduces the compliance time for all initial inspections and reduces the repetitive interval for a certain inspection. This AD results from new reports of cracks in the upper deck floor beams occurring at lower flight cycles. We are issuing this AD to find and fix cracking in certain upper deck floor beams. Such cracking could extend and sever floor beams at a floor panel attachment hole location and could result in rapid decompression and loss of controllability of the airplane.
Union Pacific Railroad Company-Trackage Rights Exemption-BNSF Railway Company
Document Number: E6-5335
Type: Notice
Date: 2006-04-11
Agency: Surface Transportation Board, Department of Transportation
Illinois Central Railroad Company-Abandonment Exemption-in Madison County, MS
Document Number: E6-5333
Type: Notice
Date: 2006-04-11
Agency: Surface Transportation Board, Department of Transportation
Fire Penetration Resistance of Thermal Acoustic Insulation Installed on Transport Category Airplanes
Document Number: E6-5330
Type: Proposed Rule
Date: 2006-04-11
Agency: Federal Aviation Administration, Department of Transportation
This document makes a correction to the Notice of Proposed Rulemaking (NPRM) published in the Federal Register on April 3, 2006 by changing the amendment number to a notice number. The NPRM proposed to extend, by 12 months, the date for operators to comply with the fire penetration resistance requirements of thermal/acoustic insulation used in transport category airplanes manufactured after September 2, 2007.
Airworthiness Directives; Gulfstream Model GV-SP Series Airplanes
Document Number: E6-5253
Type: Proposed Rule
Date: 2006-04-11
Agency: Federal Aviation Administration, Department of Transportation
The FAA withdraws a notice of proposed rulemaking (NPRM) that proposed a new airworthiness directive (AD) for certain Gulfstream Model GV-SP series airplanes. The proposed AD would have required an inspection to determine the serial number of the anti-skid control unit (ACU) in the right electronics equipment rack, and replacement of the ACU with a new or serviceable ACU if necessary. Since the proposed AD was issued, we have received new data that indicate the identified unsafe condition has been corrected on all airplanes that would have been affected by the NPRM, and on all ACUs in the affected range of serial numbers. Accordingly, the proposed AD is withdrawn.
Airworthiness Directives; Airbus Model A300 F4-600R Series Airplanes and Model A300 C4-605R Variant F Airplanes
Document Number: E6-5246
Type: Proposed Rule
Date: 2006-04-11
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A300 F4-600R series airplanes and Model A300 C4-605R Variant F airplanes. This proposed AD would require modifying certain structure in the fuselage zone at the lavatory venturi installation in the nose section, and performing a related investigative action and corrective action if necessary. This proposed AD results from an analysis that revealed that airplanes equipped with Airbus Modification 08909 had a concentration of loads higher than expected in the fuselage zone (high stress) at the lavatory venturi installation in the nose section, which could be the origin of cracks that developed in the fuselage skin and propagated from the edge of the air vent hole. We are proposing this AD to prevent fatigue cracking of the fuselage skin, which could result in loss of the structural integrity of the fuselage and consequent rapid depressurization of the airplane.
Special Conditions: Airbus Model A380-800 Airplane, Reinforced Flightdeck Bulkhead
Document Number: E6-5240
Type: Proposed Rule
Date: 2006-04-11
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes special conditions for the Airbus A380- 800 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. Many of these novel or unusual design features are associated with the complex systems and the configuration of the airplane, including its full- length double deck. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding a reinforced flightdeck bulkhead. These proposed special conditions contain the additional safety standards that the Administrator considers necessary to establish an appropriate level of safety for a reinforced flightdeck bulkhead and are equivalent to the standards established by existing airworthiness regulations for the flightdeck door. Additional special conditions will be issued for other novel or unusual design features of the Airbus Model A380-800 airplane.
This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.