Department of Transportation 2007 – Federal Register Recent Federal Regulation Documents

Results 801 - 850 of 3,086
DOT's Migration to the Federal Docket Management Systems (FDMS)
Document Number: 07-4709
Type: Notice
Date: 2007-09-24
Agency: Office of the Secretary, Department of Transportation
This notice announces a service disruption to DOT's Docket Management System (DMS), which contains the public dockets for all DOT agencies (except for the Surface Transportation Board), the Transportation Security Administration (TSA), and the United States Coast Guard (USCG). (Subsequent references to ``DOT'' in this document also apply to TSA and USCG.) Effective September 30, 2007, DOT's DMS will be replaced by the Federal Docket Management System (FDMS), a government-wide, electronic docket management system. Please note that in preparation for migration, effective Thursday, September 27, 2007 at 5 p.m. DMS will no longer accept electronic comments/submissions. DMS will accept, as well as process, faxed and other paper documents up until 12 noon on Friday, September 28, 2007. If falling due during this transition, due dates for filings in rulemakings and adjudications will be delayed until October 1, 2007, unless otherwise advised by the originating office. On October 1, 2007 FDMS will begin accepting DOT- related electronic submission. At that time, it will display all open DOT dockets. Between October 1 and October 31, the remaining DOT dockets still will be accessible in DMS. By October 31, the full migration of all dockets currently in DMS is expected to be completed. The change in systems will not change any requirements in DOT regulations.
Petition for Exemption; Summary of Petition Received
Document Number: E7-18705
Type: Notice
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
This notice contains a summary of a petition 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.
Aviation Proceedings, Agreements Filed the Week Ending September 14, 2007
Document Number: E7-18695
Type: Notice
Date: 2007-09-21
Agency: Office of the Secretary, Department of Transportation
Aviation Rulemaking Advisory Committee Meeting on Transport Airplane and Engine Issues
Document Number: E7-18693
Type: Notice
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
This notice announces a public meeting of the FAA's Aviation Rulemaking Advisory Committee (ARAC) to discuss transport airplane and engine (TAE) issues.
Aviation Proceedings, Agreements Filed the Week Ending September 7, 2007
Document Number: E7-18677
Type: Notice
Date: 2007-09-21
Agency: Office of the Secretary, Department of Transportation
Agency Information Collection Activities; Revision of an Approved Information Collection: Motor Carrier Safety Assistance Program
Document Number: E7-18637
Type: Notice
Date: 2007-09-21
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
In accordance with the Paperwork Reduction Act of 1995, FMCSA announces its plan to submit the Information Collection Request (ICR) described below to the Office of Management and Budget (OMB) for review and approval and invites public comment. The FMCSA requests approval to revise and renew an ICR entitled, ``Motor Carrier Safety Assistance Program'' (MCSAP). The information required consists of grant application preparation, quarterly reports and electronic data documenting the results of driver/vehicle inspections performed by the States.
Minimum Age for Operating a Commercial Motor Vehicle (CMV) in Interstate Commerce: Jcrane, Inc. (Jcrane), Application for Exemption
Document Number: E7-18628
Type: Notice
Date: 2007-09-21
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
The FMCSA announces that it has received from Jcrane, Inc. (Jcrane) an application for an exemption from provisions of the Federal Motor Carrier Safety Regulations that require an individual who operates a commercial motor vehicle (CMV) of 10,001 or more pounds Gross Vehicle Weight Rating (GVWR) in interstate commerce to be a minimum of 21 years of age. The exemption would allow Jcrane's employees who are not yet 21 years of age to legally operate a CMV in interstate commerce. Jcrane states that the granting of the exemption would allow the company to better train crane operators and therefore increase overall safety. The FMCSA requests public comment on Jcrane's application for exemption.
Notice of Final Federal Agency Actions on Proposed Highways in Utah
Document Number: E7-18620
Type: Notice
Date: 2007-09-21
Agency: Federal Highway Administration, Department of Transportation
This notice announces actions taken by the FHWA and other Federal agencies that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to various proposed highway projects in the State of Utah. Those actions grant licenses, permits, and approvals for the projects.
Voluntary Intermodal Sealift Agreement (VISA)/Joint Planning Advisory Group (JPAG)
Document Number: E7-18571
Type: Notice
Date: 2007-09-21
Agency: Maritime Administration, Department of Transportation
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: E7-18541
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD) that applies to certain Boeing Model 747 series airplanes. The existing AD currently requires repetitive inspections and torque checks of the hanger fittings and strut forward bulkhead of the forward engine mount and adjacent support structure, and corrective actions if necessary. The existing AD also currently requires a terminating action for the repetitive inspections and checks. This new AD requires, among other actions, new repetitive inspections in the existing area and new areas. This new AD also provides for an optional inspection and no longer allows the existing fastener replacement to terminate repetitive inspections. This AD results from new reports of under-torqued or loose fasteners, a cracked bulkhead chord, and a fractured back-up angle after operators accomplished the terminating action required by the existing AD. We are issuing this AD to detect and correct loose fasteners and/or damaged or cracked hanger fittings, back-up angles, and bulkhead of the forward engine mount, which could lead to failure of the hanger fitting and bulkhead and consequent separation of the engine from the airplane.
Airworthiness Directives; Pilatus Aircraft Limited Model PC-6 Series Airplanes
Document Number: E7-18476
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above that would supersede existing ADs. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; McDonnell Douglas Model MD-10-10F and MD-10-30F Airplanes, Model MD-11 and MD-11F Airplanes, and Model 717-200 Airplanes
Document Number: E7-18475
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to all McDonnell Douglas Model MD-10-10F and MD-10- 30F airplanes, Model MD-11 and MD-11F airplanes, and Model 717-200 airplanes. That AD currently requires a revision to the Limitations section of the airplane flight manual (AFM) to prohibit use of the flight management system (FMS) profile (PROF) mode for descent and/or approach operations unless certain conditions are met. This new AD requires, for certain Model 717-200 airplanes, upgrading the versatile integrated avionics (VIA) digital computer with new system software, which would end the need for the AFM revision. This AD results from a report of two violations of the selected flight control panel (FCP) altitude during FMS PROF descents. We are issuing this AD to prevent, under certain conditions during the FMS PROF descent, the uncommanded descent of an airplane below the selected level-off altitude, which could result in an unacceptable reduction in the separation between the airplane and nearby air traffic or terrain.
Airworthiness Directives; DG Flugzeugbau GmbH Model DG-1000T Gliders
Document Number: E7-18474
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; Boeing Model 747 Airplanes
Document Number: E7-18473
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 747 series airplanes. That AD requires a one-time inspection for discrepancies of the potable water and drain lines in the cargo compartments, and corrective action if necessary. This new AD requires that the inspection be repetitively performed using new service information, until terminating action is done. This AD also removes certain airplanes from the applicability. This AD results from a report of a fire in the aft cargo compartment started by a potable water line heater tape. We are issuing this AD to prevent overheating of the heater tape on potable water fill and drain lines, which could ignite accumulated debris or contaminants on or near the potable water fill and drain lines, resulting in a fire in the airplane.
Airworthiness Directives; Boeing Model 747 Airplanes
Document Number: E7-18472
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on July 30, 2007 (72 FR 41438). The error resulted in certain compliance times being mislabeled as units of flight cycles instead of flight hours. This AD applies to all Boeing Model 747 airplanes. This AD requires an inspection of the No. 2 and No. 3 windows on the left and right sides of the airplane to determine their part numbers, and related investigative and corrective actions if necessary.
Airworthiness Directives; McDonnell Douglas Model MD-11, MD-11F, DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, and MD-10-30F Airplanes
Document Number: E7-18459
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all McDonnell Douglas Model MD-11 and MD-11F airplanes and certain Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, and MD-10-30F airplanes. This AD requires rerouting system 3 hydraulic piping, installing new pipe assemblies and unions, and installing redesigned support brackets for the system 3 hydraulic piping. This AD results from a report of damage to the hydraulic system that occurred when pieces of a ruptured tire from the left main landing gear penetrated the wing trailing edge access panel during takeoff. We are issuing this AD to prevent damage to the system 3 hydraulic piping, which could result in loss of the hydraulic system.
Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, -900, and -900ER Series Airplanes
Document Number: E7-18436
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
This document publishes in the Federal Register an amendment adopting airworthiness directive (AD) 2007-18-52 that was sent previously to all known U.S. owners and operators of Boeing Model 737- 600, -700, -700C, -800, -900, and -900ER series airplanes by individual notices. This AD requires repetitive detailed inspections of the slat track downstop assemblies to verify that proper hardware is installed, one-time torquing of the nut and bolt, and corrective actions if necessary. This AD is prompted by reports of parts coming off the main slat track downstop assemblies. We are issuing this AD to detect and correct loose or missing parts from the main slat track downstop assemblies, which could result in a fuel leak and consequent fire.
Airworthiness Directives; Airbus Model A300-600R Series Airplanes; and Model A310-300 Series Airplanes
Document Number: E7-18435
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; Turbomeca S.A. Artouste III B, Artouste III B1, and Artouste III D Turboshaft Engines
Document Number: E7-18434
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD) for Turbomeca Artouste III B, Artouste III B1, and Artouste III D turboshaft engines. That AD currently requires removing certain fuel pumps from service and installing serviceable fuel pumps. This AD requires the same actions and adds to the applicability, additional fuel pumps by serial number (SN). This AD results from Turbomeca identifying a number of fuel pump SNs that they omitted from the original population. We are issuing this AD to prevent reduced engine fuel flow and subsequent loss of control of the helicopter, or an accident.
Airworthiness Directives; SICMA Aero Seat 50XXX Passenger Seats
Document Number: E7-18431
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from Mandatory Continuing Airworthiness Information (MCAI) provided by the aviation authority of France to identify and correct an unsafe condition on SICMA Aero Seat 50XXX Passenger Seats. The MCAI states the following:
Airworthiness Directives; Societe de Motorisations Aeronautiques (SMA) SR305-230 and SR305-230-1 Reciprocating Engines
Document Number: E7-18412
Type: Rule
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from Mandatory Continuing Airworthiness Information (MCAI) provided by the aviation authority of France to identify and correct an unsafe condition on SMA SR305-230 and SR305-230-1 reciprocating engines. The MCAI states the following:
Notice of Intent To Release Certain Properties From All Terms, Conditions, Reservations and Restrictions of a Quitclaim Deed Agreement Between Miami-Dade County and the Federal Aviation Administration for the Opa Locka Executive Airport, Opa-locka, FL
Document Number: 07-4697
Type: Notice
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA hereby provides notice of intent to release certain airport properties 74.273 acres at the Opa Locka Executive Airport, Opa Locka, FL from the conditions, reservations, and restrictions as contained in a Quitclaim Deed agrement between the FAA and Miami-Dade County, dated November 16, 1961. The release of property will allow Miami-Dade County to dispose of the property for other than aeronautical purposes. The property is located in Opa-locka, Miami-Dade County, Florida. The parcels are currently designated as non- aeronautical use. The properties will be disposed of for the purpose of municipal uses. The airport will benefit from these releases through the development of infrastructure serving the airport. Further, the airport will no longer incure the costs associated with maintaining these lands. Documents reflecting the Sponsor's request are available, by appointment only, for inspection at the Opa Locka Executive Airport Manager's Office, and the FAA Airports District Office.
Policy for Diesel (Compression Ignition) Engine Certification
Document Number: 07-4696
Type: Notice
Date: 2007-09-21
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces the final policy for Policy for Diesel (Compression Ignition) Engine Certification.
Intent To Prepare a Revised Environmental Impact Statement for the Silicon Valley Rapid Transit Project in Milpitas, San Jose, and Santa Clara, CA
Document Number: 07-4666
Type: Notice
Date: 2007-09-21
Agency: Federal Transit Administration, Department of Transportation
The Federal Transit Administration (FTA) and the Santa Clara Valley Transportation Authority (VTA) will prepare a Revised Environmental Impact Statement (EIS) for the proposed Silicon Valley Rapid Transit Project (SVRT Project), a 16.1-mile extension of the San Francisco Bay Area Rapid Transit District (BART) system from the planned BART Warm Springs Station in Fremont through Milpitas and San Jose to Santa Clara, California. The Revised EIS will be prepared in accordance with regulations implementing the National Environmental Policy Act (NEPA), as well as the provisions of the Safe, Accountable, Flexible, Efficient Transportation Equity Act: A Legacy for Users. The purpose of this Notice of Intent (NOI) is to inform interested parties of the plan to prepare a Revised EIS, to invite agency and public participation in the EIS process, and to announce public scoping meetings.
Recording of Major Repairs and Major Alterations
Document Number: E7-18584
Type: Rule
Date: 2007-09-20
Agency: Federal Aviation Administration, Department of Transportation
This action amends instructions to aviation maintenance providers regarding submittal of FAA Form 337, Major Repair and Alteration, for either major repair or major alteration; or for extended-range fuel tanks installed within the passenger compartment or a baggage compartment. This change clarifies the mailing instructions when submitting Form 337 to the FAA. The intent of this action is to amend the regulation to ensure mailing requirements are clear and accurate.
Aviation Proceedings, Agreements Filed the Week Ending August 10, 2007
Document Number: E7-18578
Type: Notice
Date: 2007-09-20
Agency: Office of the Secretary, Department of Transportation
Aviation Proceedings, Agreements Filed the Week Ending August 3, 2007
Document Number: E7-18576
Type: Notice
Date: 2007-09-20
Agency: Office of the Secretary, Department of Transportation
Aviation Proceedings, Agreements Filed the Week Ending August 17, 2007
Document Number: E7-18570
Type: Notice
Date: 2007-09-20
Agency: Office of the Secretary, Department of Transportation
Aviation Proceedings, Agreements Filed the Week Ending August 31, 2007
Document Number: E7-18565
Type: Notice
Date: 2007-09-20
Agency: Office of the Secretary, Department of Transportation
Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
Document Number: E7-18554
Type: Proposed Rule
Date: 2007-09-20
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This proposed AD would require doing repetitive internal eddy current and detailed inspections to detect cracked stringer tie clips; doing applicable corrective and related investigative actions, if necessary; and measuring the fastener spacing and the edge margin; as applicable. As a temporary alternative to doing the actions described previously, this proposed AD would require repetitive external general visual inspections of the skin and lap joints for cracks and evidence of overload resulting from cracked stringer tie clips, and applicable corrective actions if necessary. This proposed AD results from a report of several cracked stringer tie clips. We are proposing this AD to prevent multiple cracked stringer tie clips and damaged skin and frames, which could lead to the skin and frame structure developing cracks and consequent decompression of the airplane.
Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes
Document Number: E7-18553
Type: Proposed Rule
Date: 2007-09-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Notice of Final Federal Agency Actions on Proposed Highway in Utah
Document Number: E7-18545
Type: Notice
Date: 2007-09-20
Agency: Federal Highway Administration, Department of Transportation
This notice announces actions taken by the FHWA, USACE, and other Federal agencies that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to a proposed highway project, U.S. Route 6, I-15 in Spanish Fork to I-70 near Green River in the State of Utah. Those actions grant licenses, permits, and approvals for the project.
Airworthiness Directives; Boeing Model 767 Airplanes
Document Number: E7-18544
Type: Proposed Rule
Date: 2007-09-20
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all Boeing Model 767 airplanes. The existing AD currently requires repetitive measurements of the rudder and elevator freeplay, repetitive lubrications of rudder and elevator components, and related investigative/corrective actions if necessary. This proposed AD would instead require revised repetitive measurements of the rudder freeplay and the elevator freeplay for each of the power control actuators (PCAs) that move the rudder and elevator, corrective and related investigative actions if necessary, and repetitive lubrications of the rudder and elevator components. For some airplanes, this proposed AD would also require related concurrent actions. This proposed AD results from reports of freeplay-induced vibration of the rudder and the elevator. The potential for vibration of the control surface should be avoided because the point of transition from vibration to divergent flutter is unknown. We are proposing this AD to prevent excessive vibration of the airframe during flight, which could result in loss of control of the airplane.
Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Series Airplanes
Document Number: E7-18540
Type: Proposed Rule
Date: 2007-09-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Document Number: E7-18539
Type: Proposed Rule
Date: 2007-09-20
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 repetitive detailed inspections for cracking of the left side and right side frame and reinforcement angles at fuselage station (FS) 640 between stringer 9 and stringer 12, and corrective actions if necessary. This proposed AD results from reports that cracks have been discovered on the frame and reinforcement angles at FS 640. We are proposing this AD to detect and correct cracking of the frame, which could lead to failure of the fuselage structure and possible loss of the airplane.
Hazardous Materials: Fuel Cell Cartridges and Systems Transported on Board Passenger Aircraft in Carry-on Baggage
Document Number: E7-18532
Type: Proposed Rule
Date: 2007-09-20
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
PHMSA is proposing to amend the Hazardous Materials Regulations (HMR) to permit certain fuel cell cartridges and fuel cell systems designed for portable electronic devices to be transported by passengers and crew in carry-on baggage on board passenger-carrying aircraft. The proposed rule would cover fuel cells containing certain hazardous materials (flammable liquids, including methanol; formic acid; certain borohydride materials; or butane) and meeting certain performance and consumer use standards, which we are proposing to incorporate by reference into the HMR. We have evaluated the possible transportation safety risks presented by these fuel cell cartridges and systems and have determined they may safely be transported in the cabin of a passenger-carrying aircraft.
Interoperability Requirements, Standards, or Performance Specifications for Automated Toll Collection Systems
Document Number: E7-18529
Type: Proposed Rule
Date: 2007-09-20
Agency: Federal Highway Administration, Department of Transportation
As required under section 1604(b)(6) of the Safe, Accountable, Flexible, Efficient Transportation Equity Act: A Legacy for Users (SAFETEA-LU), this proposed rule specifies the interoperability requirements for automated toll collection systems for the facilities that are tolled under any of the tolling programs contained in section 1604 of SAFETEA-LU. Specifically, this notice proposes to require facilities operating with authority under section 1604 of SAFETEA-LU to use electronic toll collection systems and for these systems to address their interoperability with other toll facilities. Although a nationwide interoperability standard has not yet been established, this proposed rule seeks to accelerate progress toward achieving nationwide interoperability by requiring these facilities to upgrade their electronic toll collection systems to the national standards whenever adopted. This document also provides notice of public meetings on this proposed regulation.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: E7-18374
Type: Rule
Date: 2007-09-20
Agency: Federal Aviation Administration, Department of Transportation
This Rule establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures 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, adding new obstacles, or changing 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.
Buy America Requirements; End Product Analysis and Waiver Procedures
Document Number: E7-18355
Type: Rule
Date: 2007-09-20
Agency: Federal Transit Administration, Department of Transportation
The Safe, Accountable, Flexible, Efficient Transportation Equity Act: A Legacy for Users (SAFETEA-LU) requires the Federal Transit Administration (FTA or the Agency) to make certain changes to the Buy America requirements. This Final Rule creates a new publication process for public interest waivers to provide an opportunity for public comment; clarifies Buy America requirements with respect to microprocessor waivers; issues new provisions to permit post-award waivers; clarifies the definition of ``end products'' with regards to components, subcomponents, and major systems, and provides a representative list of end products; clarifies the requirements for final assembly of rolling stock and provides representative examples of rolling stock components; expands FTA's list of communications, train control, and traction power equipment; and updates debarment and suspension provisions to bring them into conformity with statutory amendments made by SAFETEA-LU.
Standard Instrument Approach Procedures; Miscellaneous Amendments
Document Number: E7-18335
Type: Rule
Date: 2007-09-20
Agency: Federal Aviation Administration, Department of Transportation
This rule amends Standard Instrument Approach Procedures (SIAPs) for operations at certain airports. These regulatory actions are needed because of changes in the National Airspace System, such as the commissioning of new navigational facilities, adding of new obstacles, or changing 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.
Public Notice for Waiver of Aeronautical Land-Use Assurance; Pellston Regional Airport; Pellston, MI
Document Number: 07-4650
Type: Notice
Date: 2007-09-20
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 release of 621.46 acres of vacant airport property for the proposed development of warehouses, training centers, and associated access roads as a component of Sovereign Deed's National Response Center. The land consists of 7 parcels. Parcel 1 was acquired under grant 9-20-048-C905. Parcels 2, 3, 4, 5 and 8 were dedicated as airport property prior to 1946 and have no federal funding involvement. Parcel 7 was acquired under grants 9-2- 048-C905 and 8-26-0076-01. There are no impacts to the airport by allowing the airport to lease the property. The land is not needed for aeronautical use. 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 with 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.
Airworthiness Directives; Saab Model SAAB-Fairchild SF340A (SAAB/SF340A) and SAAB 340B Airplanes
Document Number: E7-18478
Type: Proposed Rule
Date: 2007-09-19
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; Boeing Model 747-100, -100B, -100B SUD, -200B, -200C, -300, -400, and -400D Series Airplanes; and Model 747SR Series Airplanes
Document Number: E7-18449
Type: Proposed Rule
Date: 2007-09-19
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 Boeing Model 747-100, -100B, -100B SUD, -200B, -200C, -300, -400, and -400D series airplanes; and Model 747SR series airplanes. The proposed AD would have required repetitive inspections of the forward corner reveal of the number 3 main entry doors (MEDs) for cracking, and corrective actions if necessary. Since the proposed AD was issued, we have received comments for the NPRM and new data showing other issues related to the unsafe condition. The data include reports that additional airplanes are affected by the identified unsafe condition; and that a ``sharp edge'' detail may be present on certain one-piece machined 6061 aluminum reveals, which could lead to fatigue cracking. We have determined from these data that the corrective actions proposed by the NPRM are inadequate for addressing the identified unsafe condition. We are considering requiring other rulemaking, which provides corrective actions for the identified unsafe condition. Accordingly, the proposed AD is withdrawn.
Airworthiness Directives; Airbus Model A300 Series Airplanes and Model A300-600 Series Airplanes
Document Number: E7-18448
Type: Proposed Rule
Date: 2007-09-19
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to all Airbus Model A300 airplanes; and all Airbus Model A300 B4-601, A300 B4-603, A300 B4-620, A300 B4-622, A300 B4-605R, A300 B4-622R, A300 F4-605R, A300 F4-622R, and A300 C4-605R Variant F airplanes. The original NPRM would have required inspecting to determine the part number of the sliding rods of the main landing gear (MLG) retraction actuators. For MLG retraction actuators equipped with sliding rods having certain part numbers, the original NPRM would also have required inspecting for discrepancies, including but not limited to cracking, of the sliding rod; and performing corrective actions if necessary. The original NPRM resulted from a report of a failure of a sliding rod of the MLG retraction actuator before the actuator reached the life limit established by the manufacturer. This action revises the original NPRM by proposing to require the return of affected sliding rods to the manufacturer. We are proposing this supplemental NPRM to prevent failure of the sliding rod of the MLG retraction actuator, which could result in reduced structural integrity of the MLG.
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