Department of Transportation August 2008 – Federal Register Recent Federal Regulation Documents
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Annual Materials Report on New Bridge Construction and Bridge Rehabilitation
Section 1114 of the Safe, Accountable, Flexible, Efficient Transportation Equity Act: A Legacy for Users (SAFETEA-LU) (Pub. L. 109-59; 119 Stat. 1144) continued the highway bridge program to enable States to improve the condition of their highway bridges over waterways, other topographical barriers, other highways, and railroads. Section 1114(f) amends 23 U.S.C. 144 by adding subsection (r), requiring the Secretary of Transportation (Secretary) to publish in the Federal Register a report describing construction materials used in new Federal-aid bridge construction and bridge rehabilitation projects.
Supplemental Notice for the National Parks Overflights Advisory Group Aviation Rulemaking Committee Meeting
The Federal Aviation Administration (FAA) and the National Park Service (NPS), in accordance with the National Parks Air Tour Management Act of 2000, announce the next meeting of the National Parks Overflights Advisory Group (NPOAG) Aviation Rulemaking Committee (ARC). This notification provides the dates, location, and agenda for the meeting. This notification revises Federal Register notice published on August 19, 2008 (Vol. 73, No. 161, Page 48427-48428) to indicate a change in the time of meetings and that interested persons may attend the meeting.
Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
We are revising an earlier proposed airworthiness directive (AD) for certain Boeing Model 737-100, -200, -200C, -300, -400, and - 500 series airplanes. The original NPRM would have required doing repetitive internal eddy current and detailed inspections to detect cracked stringer tie clips; measuring the fastener spacing and the edge margin if applicable, and doing applicable corrective and related investigative actions. As a temporary alternative to doing the actions described previously, the original NPRM would have required repetitive 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. The original NPRM resulted from a report of several cracked stringer tie clips. This action revises the original NPRM by including repetitive external eddy current sliding probe inspections of the lap joints for cracks and evidence of overload resulting from cracked stringer tie clips. We are proposing this supplemental NPRM to detect and correct multiple adjacent 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; Saab Model SAAB 2000 Airplanes
We are revising an earlier NPRM for the products listed above. This action revises the earlier NPRM by expanding the scope. 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 777 Airplanes
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all Boeing Model 777 airplanes. The existing AD requires, for the drive mechanism of the horizontal stabilizer, repetitive detailed inspections for discrepancies, repetitive lubrication of the ballnut and ballscrew, repetitive measurements of the freeplay between the ballnut and the ballscrew, and corrective action if necessary. This proposed AD would revise the compliance times of the existing AD. This proposed AD results from a report of extensive corrosion of a ballscrew in the drive mechanism of the horizontal stabilizer on a Boeing Model 757 airplane, which is similar in design to the ballscrew on Model 777 airplanes. We are proposing this AD to prevent an undetected failure of the primary load path for the ballscrew in the drive mechanism of the horizontal stabilizer and subsequent wear and failure of the secondary load path, which could lead to loss of control of the horizontal stabilizer and consequent loss of control of the airplane.
Airworthiness Directives; McDonnell Douglas Model DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes; Model DC-8-51, DC-8-52, DC-8-53, and DC-8-55 Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; Model DC-8-61, DC-8-62, and DC-8-63 Airplanes; Model DC-8-61F, DC-8-62F, and DC-8-63F Airplanes; Model DC-8-71, DC-8-72, and DC-8-73 Airplanes; and Model DC-8-71F, DC-8-72F, and DC-8-73F Airplanes
The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to all McDonnell Douglas Model DC-8 airplanes. The original NPRM would have superseded an existing AD that currently requires, among other things, revision of an existing program of structural inspections. The original NPRM proposed to require implementation of a revised program of structural inspections of baseline structure to detect and correct fatigue cracking in order to ensure the continued airworthiness of these airplanes as they approach the manufacturer's original fatigue design life goal. The original NPRM resulted from a significant number of these airplanes approaching or exceeding the design service goal on which the initial type certification approval was predicated. This new action revises the original NPRM by reducing the inspection threshold for certain principal structural elements. We are proposing this supplemental NPRM to detect and correct fatigue cracking that could compromise the structural integrity of these airplanes.
Airworthiness Directives; McDonnell Douglas Model DC-9-30, DC-9-40, and DC-9-50 Series Airplanes, Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) Airplanes, and Model MD-88 and MD-90-30 Airplanes
We propose to adopt a new airworthiness directive (AD) for the McDonnell Douglas airplanes listed above. This proposed AD would require modifying the fuel boost pumps for the center wing, and forward or aft auxiliary fuel tanks. This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent possible sources of ignition in a fuel tank caused by an electrical fault or uncommanded dry operation of the fuel boost pumps. An ignition source in the fuel tank could result in a fire or an explosion and consequent loss of the airplane.
Airworthiness Directives; Dowty Propellers R175/4-30; R184/4-30-4; R193/4-30-4; R.209/4-40-4.5; R212/4-30-4; R.245/4-40-4.5; R251/4-30-4; R257/4-30-4; and R.259/4-40-4.5 Model Propellers
The FAA proposes to supersede an existing airworthiness directive (AD) for all Dowty Rotol propellers. That AD currently requires, for all Dowty Rotol propellers, visual inspections for seizure and for cadmium plating of the blade pitch change operating links and eyebolt fork assemblies. That AD also requires replacement or heat-treatment of the blade pitch change operating links and eyebolt fork assemblies, if necessary. This proposed AD would require the same actions, but only for certain model Dowty Propellers. This proposed AD results from the FAA determining that AD 70-16-02 does not apply to all propellers, since current Dowty Rotol propellers are differently designed. We are proposing this AD supersedure to specify the affected propeller models, and to prevent seizure or embrittlement and cracking of the blade pitch change operating links and eyebolt fork assemblies, which could result in reduced controllability of the airplane.
Decision that Certain Nonconforming Motor Vehicles Are Eligible for Importation
This document announces decisions by NHTSA that certain motor vehicles not originally manufactured to comply with all applicable Federal motor vehicle safety standards (FMVSS) are eligible for importation into the United States because they are substantially similar to vehicles originally manufactured for sale in the United States and certified by their manufacturers as complying with the safety standards, and they are capable of being readily altered to conform to the standards or because they have safety features that comply with, or are capable of being altered to comply with, all applicable FMVSS.
Plan for Evaluating the Effectiveness of Vehicle and Behavioral Programs, 2008-2012
This notice announces the publication by NHTSA of its Evaluation Program Plan for 2008-2012. The report describes the agency's ongoing and planned evaluations of its existing Federal Motor Vehicle Safety Standards [49 CFR part 571] and other vehicle-safety, behavioral-safety and consumer programs. It also summarizes the results of completed evaluations. The agency's evaluation program responds to Executive Order 12866, which provides for Government-wide review of existing significant Federal regulations. This notice solicits public review and comment on the evaluation plan. Comments received will be used to improve the plan.
Qualification and Certification of Locomotive Engineers
FRA is issuing this notice of interpretation to inform interested parties of its application and enforcement of the requirements for each railroad responsible for controlling joint operations territory to maintain a list of person(s) certified as a qualified locomotive engineer for the purposes of the joint operations. FRA has discovered that a number of controlling railroads are not maintaining accurate lists primarily because foreign railroads are not providing the controlling railroads with accurate information and the controlling railroads are not demanding it. If an accurate list is not maintained, a controlling railroad has little chance of preventing an uncertified or unqualified person from operating a locomotive or train in the joint operations territory. This document is intended to inform interested parties of what information is required to be maintained on the required list and provides information as to how often the listings should be updated.
Railroad Safety Advisory Committee (RSAC); Working Group Activity Update
FRA is updating its announcement of RSAC's working group activities to reflect its current status.
Railroad Safety Advisory Committee; Notice of Meeting
FRA announces the 36th meeting of the RSAC, a Federal advisory committee that develops railroad safety regulations through a consensus process. The RSAC meeting topics will include opening remarks from the FRA Administrator, and status reports will be provided by the Passenger Safety, Locomotive Safety Standards, Railroad Bridge, Medical Standards, Railroad Operating Rules, and Track Safety Standards Working Groups. There will be a Committee vote on the acceptance of the report from the Railroad Bridge Working Group and a possible vote on an expanded task statement for the Track Standards Working Group. Accident/incident reporting is on the agenda for discussion by the Committee and there may be a vote on a contingent task statement. This agenda is subject to change.
Final Federal Agency Actions on Proposed Highway in Washington, DC
This notice announces actions taken by the FHWA that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to a proposed highway project, 11th Street Bridges, Anacostia Freeway (I- 295/DC 295) to Southeast/Southwest Freeway (I-695), and Washington, DC. Those actions grant approvals for the project.
Notice of Final Federal Agency Actions on Proposed Highway in Utah
This notice announces actions taken by the FHWA that are final within the meaning of 23 U.S.C. 39(l)(1). The actions relate to a proposed highway project, I-15 Corridor, from the South Payson Interchange in Utah County, to the 12300 South Interchange in Salt Lake County, State of Utah. Those actions grant licenses, permits, and approvals for the project.
Notice of Intent To Rule on Request To Release Airport Property at the Love Field Airport, Dallas, TX
The FAA proposes to rule and invite public comment on the release of land at the Love Field Airport under the provisions of Section 125 of the Wendell H. Ford Aviation Investment Reform Act for the 21st Century (AIR 21).
First Meeting, RTCA/PMC New Special Committee 219: Attitude and Heading Reference Systems (AHRS)
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 219 meeting: Attitude and Heading Reference Systems (AHRS).
Federal Motor Vehicle Safety Standards; Lamps, Reflective Devices, and Associated Equipment
This final rule delays the effective date of an amendment that reorganizes and improves the structure and clarity of the Federal motor vehicle safety standard on lamps, reflective devices, and associated equipment, from September 1, 2008 to December 1, 2009. The final rule reorganizing the lighting standard was published on December 4, 2007.\1\ The agency received fifteen petitions for reconsideration of the final rule, including two that requested a delay in the effective date of the rule, and others which raised concerns that the reorganization of FMVSS No. 108 imposed new requirements. To allow for more time for the agency to analyze the petitions prior to the rule taking effect, the agency is delaying the effective date until December 1, 2009.
Amendment of Class E Airspace; Factoryville, PA
This action amends the Class E airspace area at Factoryville, PA, to provide additional controlled airspace accommodating a new Runway 4 Standard Instrument Approach Procedure (SIAP) developed for Seamans Field, Factoryville, PA. This action increases the radius of the current Class E airspace and includes airspace on each side of the Lake Henry VORTAC 299[deg] radial extending to the VORTAC.
Airworthiness Directives; McDonnell Douglas Model DC-10-10 and DC-10-10F Airplanes, Model DC-10-15 Airplanes, Model DC-10-30 and DC-10-30F (KC-10A and KDC-10) Airplanes, Model DC-10-40 and DC-10-40F Airplanes, Model MD-10-10F and MD-10-30F Airplanes, and Model MD-11 and MD-11F Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain transport category airplanes identified above. This AD requires modifying the fuel boost pumps. This AD results from a fuel boost pump found with blown thermal fuses and a fractured thrust washer. We are issuing this AD to prevent failure of the fuel boost pumps, which could lead to the potential of ignition sources inside fuel tanks. This condition, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
Airworthiness Directives; Boeing Model 747 Airplanes
We are adopting a new airworthiness directive (AD) for all Boeing Model 747 airplanes. This AD requires a one-time inspection of certain fuselage skins at section 41 to find any external doublers that cover the inspection areas and to identify the external doublers that end on a stringer and those that do not, and related investigative and corrective actions if necessary. This AD results from reports of cracks found at fastener locations in the fuselage skins at section 41. We are issuing this AD to detect and correct fuselage skin cracks at fastener locations along the skin-to-stringer attachments, which could join together and become large and consequently result in rapid decompression of the cabin.
Airworthiness Directives; Boeing Model 737-600, -700, -800, and -900 Series Airplanes
We are adopting a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -800, and -900 series airplanes. This AD requires installing hot short protector (HSP) support brackets and equipment for the fuel quantity indicating system (FQIS) fuel densitometer and other specified actions as applicable. This AD also requires revising the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness to incorporate AWL No. 28-AWL- 07. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent the center tank fuel densitometer from overheating and becoming a potential ignition source inside the center fuel tank, which, in combination with flammable fuel vapors, could result in a center fuel tank explosion and consequent loss of the airplane.
Modification of Class E Airspace; Staunton, VA
This action confirms the effective date of a direct final rule published in the Federal Register (73 FR 16751) that modifies the effective time of the Class E Airspace at Staunton, VA. The Shenandoah Valley Regional Airport Commission has requested to change their current Class E2 Airspace from part time (currently 1200 to 0400 Zulu) to full time. This action enhances the safety and management of Instrument Flight Rule (IFR) operations in the area by providing the required controlled airspace to support terminal operations continuously at Staunton, VA.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 Airplanes and Model ERJ 190 Airplanes
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; Airbus Model A318, A319, A320, and A321 Series Airplanes Equipped With Certain Northrop Grumman (Formerly Litton) Air Data Inertial Reference Units
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Airbus Model A319, A320, and A321 series airplanes equipped with certain Litton air data inertial reference units (ADIRUs). That AD currently requires modifying the shelf (floor panel) above ADIRU 3, modifying the polycarbonate guard that covers the ADIRUs for certain airplanes, and modifying the ladder located in the avionics compartment for certain airplanes. This new AD requires those modifications on additional airplanes. This new AD also requires replacing all three ADIRUs with improved ADIRUs. This new AD also adds Model A318 series airplanes to the applicability. This AD results from reports that ``NAV IR FAULT'' messages have occurred during takeoff due to failure of an ADIRU and subsequent analysis showing that the shelf modification has not sufficiently addressed failure of an ADIRU. We are issuing this AD to prevent failure of an ADIRU during flight, which could result in loss of one source of critical attitude and airspeed data and reduce the ability of the flightcrew to control the airplane.
Airworthiness Directives; Boeing Model 727 Airplanes
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 727 series airplanes. That AD currently requires repetitive inspections to detect cracks and loose brackets of the elevator rear spar, and corrective actions if necessary. The existing AD also provides for an optional terminating action for the repetitive inspections. This new AD reduces the repetitive intervals of the inspections, mandates the previously optional terminating action for the repetitive inspections, and no longer allows stop-drilling. This AD results from new reports of cracks, elongated fastener holes, and loose fittings of the elevator rear spar. We are issuing this AD to prevent cracking of the elevator rear spar at the tab hinge locations, which could cause excessive freeplay of the elevator control tab and possible tab flutter, and consequent loss of control of the airplane.
Airworthiness Directives; Boeing Model 707 Airplanes, and Model 720 and 720B Series Airplanes
We are adopting a new airworthiness directive (AD) for certain Boeing Model 707 airplanes, and Model 720 and 720B series airplanes. This AD requires repetitive detailed inspections to detect cracks and corrosion on any existing repairs and at certain body stations of the visible surfaces of the wing to body terminal fittings including the web, flanges, and ribs; and applicable related investigative and corrective actions. This AD results from reports of cracks found in the wing to body terminal fittings during routine inspections. We are issuing this AD to prevent cracks and corrosion in the body terminal fittings, which could cause loss of support for the wing and could adversely affect the structural integrity of the airplane.
Procedures for Transportation Workplace Drug Testing Programs
In response to petitions from certain transportation industry and labor groups, the Department of Transportation is changing the effective date of 49 CFR 40.67(b) from August 25, 2008, to November 1, 2008. The Department is also requesting comments concerning the content of Sec. 40.67(b) for 30 days. This section of the Department's drug testing procedural rule requires employers to ensure that all follow-up and return-to-duty drug tests are directly observed.
Renewal of Approval of Information Collection Requirements
In compliance with the Paperwork Reduction Act of 1995, Public Law 104-13, this notice announces the U.S. Department of Transportation, Office of the Secretary, (DOT) intention to request an extension of the information collection request (ICR) OMB No. 2100- 0019, Americans with Disabilities Act (ADA): Information Collection Requirements for the ADA Rule for Over-the-Road Buses. DOT invites the general public, industry and other governmental parties to comment on the Department's request for the renewal Paperwork Reduction Act approval of the information requirements in Subpart H of 49 CFR Part 37, concerning over-the-road buses. The current request approved by OMB expires on August 31, 2008.
Airworthiness Directives; Bombardier Model CL-600-2C10 (Regional Jet Series 700, 701 & 702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900) Airplanes
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; Airbus Model A330-200, A330-300, A340-300, A340-500, and A340-600 Series Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above that would supersede an existing AD. 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; Airbus Model A310 Series Airplanes
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all Airbus Model A310 series airplanes. The existing AD currently requires repetitive detailed inspections to detect cracks propagating from the fastener holes that attach the left- and right-hand pick-up angles at frame 40 to the wing lower skin and fuselage panel, and corrective actions, if necessary. This proposed AD would revise the intervals for accomplishing the repetitive detailed inspections and would provide for an optional terminating modification for the repetitive inspections. This proposed AD results from mandatory continuing airworthiness information originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. We are proposing this AD to prevent reduced structural integrity of the airplane due to fatigue damage and consequent cracking of the pick-up angles at frame 40.
Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146 and Model Avro 146-RJ Airplanes
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all BAE Systems (Operations) Limited Model BAe 146 and Model Avro 146-RJ airplanes. The existing AD currently requires revising the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate life limits for certain items and inspections to detect fatigue cracking in certain structures. This proposed AD would require revising the ALS of the Instructions for Continued Airworthiness to incorporate new and more restrictive life limits for certain items and new and more restrictive inspections to detect fatigue cracking in certain structures. This proposed AD results from issuance of a later revision to the airworthiness limitations of the BAe/Avro 146 Aircraft Maintenance Manual, which specifies new inspections and compliance times for inspection and replacement actions. We are proposing this AD to ensure that fatigue cracking of certain structural elements is detected and corrected; such fatigue cracking could adversely affect the structural integrity of these airplanes.
Petition for Exemption; Summary of Petition Received
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 the petition or its final disposition.
Petition for Exemption; Summary of Petition Received
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 the petition or its final disposition.
Advance Construction of Federal-Aid Projects
The FHWA is revising its regulation for advance construction of Federal-aid projects by: (a) Removing the restriction that a State must obligate all of its allocated or apportioned funds, or demonstrate that it will use all obligation authority allocated to it for Federal- aid highways and highway safety construction, prior to the approval of advance construction projects; and (b) clarifying that advance construction procedures may be used for all categories of Federal-aid highway funds, and that any available Federal-aid funds for which a project is eligible may be used when a project is converted to a Federal-aid project. These revisions make the regulation consistent with the advance construction statute, which was amended by a provision enacted in the Safe, Accountable, Flexible, Efficient Transportation Equity Act: A Legacy for Users (SAFETEA-LU).
Proposed Modification of the Dallas/Fort Worth, TX Class B Airspace Area; Public Meetings
This notice announces four fact-finding informal airspace meetings to solicit information from airspace users and others concerning a proposal to revise the Class B airspace area at Dallas/ Fort Worth, TX. The purpose of these meetings is to provide interested parties an opportunity to present views, recommendations, and comments on the proposal. All comments received during these meetings will be considered prior to any revision or issuance of a notice of proposed rulemaking.
Motor Carrier Safety Advisory Committee Public Meeting
FMCSA announces that the Motor Carrier Safety Advisory Committee (MCSAC) will hold a committee meeting. The meeting is open to the public.
Commercial Driver's License Standards: Application for Exemption; Isuzu Motors America, Inc. (Isuzu)
FMCSA announces that Isuzu Motors America (Isuzu) has applied for an exemption from the Federal requirement for a driver of a commercial motor vehicle (CMV) to hold a commercial driver's license (CDL). Isuzu requests that the exemption cover 27 of its commercial motor vehicle (CMV) drivers who will test-drive CMVs for Isuzu in the United States. Each of these 27 Isuzu employees holds a valid Japanese CDL but lacks the U.S. residency necessary to obtain a CDL from one of the States of the U.S. Isuzu believes the knowledge and skills tests and training program that drivers undergo to obtain a Japanese CDL ensures that these drivers will achieve a level of safety that is equivalent to, or greater than, the level of safety that would be obtained by complying with the exemption.
Buy America Waiver Notification
This notice provides information regarding the FHWA's finding that a Buy America waiver is appropriate for stainless steel clad reinforcing bars used in certain Federal-aid construction projects in Virginia.
Public Notice for Waiver of Aeronautical Land-Use Assurance; Greater Beardstown Airport, Beardstown, IL
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of airport land from aeronautical use to non-aeronautical use and to authorize the exchange of the property for land needed to protect the transitional surface of Runway 18/36. The proposal consists of a 2.1-acre portion of Parcel 1 in exchange for 9.6 acres of Parcel 3. Presently the 2.1 acres of Parcel 1 is located outside of the fenced in portion of airport property and any protected zone (runway protection zone, object free area, object free zone, etc.) This land is currently being used as residential and has a mobile home located on it. Parcel 1 was acquired in 1986 with Federal participation. It is the intent of the City of Beardstown, as owner and operator of the Greater Beardstown Airport (K06) to exchange the subject portion of Parcel 1 (2.1 Acres) to Ms. Hardwick, Beardstown, IL in exchange for 9.6 acres of land (portion of Parcel 3), which is in the side transition area of Runway 18/36. This notice announces that the FAA is considering the proposal to authorize the exchange of the subject airport property at the Greater Beardstown Airport, Beardstown, IL with a portion of Parcel 3 (9.6 acres). Approval does not constitute a commitment by the FAA to financially assist in disposal of the subject airport property nor a determination that all measures covered by the program are eligible for grant-in-aid funding from the FAA. 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.
Public Notice for Waiver of Aeronautical Land-Use Assurance; Mansfield Lahm International Airport; Mansfield, OH
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 sale of the airport property. The proposal consists of the sale of vacant, much of which is farmed and owned by the City of Mansfield. The Hummel Parcel 35A is approximately 89.86 acres. There are no impacts to the airport by allowing the airport to dispose of the property. The proposed land for release is vacant, not required for future development, safety, or compatible land use. The intended land use is infrastructure development, including roads, utilities, and industrial development. Approval does not constitute a commitment by the FAA to financially assist in the disposal of the subject airport property nor a determination of eligibility for grant-in-aid funding from the FAA. The disposition of proceeds from the disposal 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.
Modification of Area Navigation Route Q-110 and Jet Route J-73; Florida
This action corrects a final rule published in the Federal Register on July 30, 2008; Airspace Docket No. 07-ASO-27, FAA Docket No. FAA-2008-0187. In that rule, an error was made in the navigation aid radials stated in the description for jet route J-73. This action corrects that error. The description of area navigation route Q-110 is correct as published in the rule.
Petition for Exemption; Summary of Petition Received
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 the petition or its final disposition.
Petition for Exemption; Summary of Petition Received
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 the petition or its final disposition.
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