Department of Transportation January 2011 – Federal Register Recent Federal Regulation Documents
Results 51 - 100 of 232
Operating Certain Railroad Tank Cars in Excess of 263,000 Pounds Gross Rail Load; Approval
On May 14, 2010, the Pipeline and Hazardous Materials Safety Administration (PHMSA) published a final rule amending the Hazardous Materials Regulations (HMR) to incorporate provisions contained in several widely used or longstanding special permits that have an established safety record. 75 FR 27205 (Final Rule). The Final Rule titled, Hazardous Materials: Incorporation of Special Permits into Regulations, in part, amended the HMR to allow certain rail tank cars, transporting hazardous materials, to exceed the gross weight on rail limitation of 263,000 pounds upon approval of the Federal Railroad Administration (FRA). This document provides notice of FRA's approval pursuant to the Final Rule of the operation of certain tank cars in hazardous materials service that exceed 263,000 pounds and weigh up to 286,000 pounds gross rail load (GRL).
Notice of Intent To Rule on Application 10-06-C-00-BOS To Impose and Use the Revenue From a Passenger Facility Charge (PFC) at General Edward Lawrence Logan International Airport, East Boston, MA
This document requests public comment on the supplementary material provided by the applicant, Massachusetts Port Authority (Massport), in response to the FAA's requests for clarification of its application to impose and use a PFC at General Edward Lawrence Logan International Airport, East Boston, Massachusetts. The FAA received additional documentation and information in support of Massport's PFC application, received April 15, 2010. The FAA is soliciting public comment on this supplementary material. Once received and following the FAA's review of any comments submitted pursuant to this notice, a Final Agency Decision is anticipated either approving or disapproving the application, in whole or in part, within 60 days of the date of this Notice. The ruling will be issued under the provisions of the 49 U.S.C. 40117 and 14 Code of Federal Regulations part 158 (14 CFR part 158).
Commercial Space Transportation Advisory Committee-Closed Session
Pursuant to Section 10(a)(2) of the Federal Advisory Committee Act (Pub. L. 92-463, 5 U.S.C. App. 2), and Title 41 of the Code of Federal Regulations, section 102-3.160, notice is hereby given of a special closed session of the Commercial Space Transportation Advisory Committee (COMSTAC). The special closed session will be an administrative session for the Committee members to review the structure of COMSTAC's public meetings and discuss if the current structure is the most desirable arrangement of activities. The meeting will take place on Thursday, February 10, 2010, at the Washington Convention Center, 801 Mount Vernon Place NW., Washington, DC 20001, from 8 a.m. until 8:45 a.m.
Airworthiness Directives; Airbus Model A330-200 Series Airplanes; Model A330-300 Series Airplanes; Model A340-200 Series Airplanes; and Model A340-300 Series 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; Aircraft Industries a.s. Model L 23 Super Blanik Sailplanes
We are adopting a new airworthiness directive (AD) for the products listed above. 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:
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
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.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
This 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.
Notice of Limitation on Claims Against Proposed Public Transportation Projects
This notice announces final environmental actions taken by the Federal Transit Administration (FTA) for the following project: Honolulu High Capacity Transit Corridor Project, City and County of Honolulu Department of Transportation Services, Honolulu, HI. The purpose of this notice is to announce publicly the environmental decisions by FTA on the subject project and to activate the limitation on any claims that may challenge these final environmental actions.
National Emergency Medical Services Advisory Council Teleconference Meeting
The NHTSA announces a teleconference meeting of the NEMSAC to be held on February 9, 2011. This notice announces the date, time and call-in information for the meeting, which will be open to the public. The purpose of NEMSAC is to serve as a nationally recognized council of emergency medical services representatives and consumers to provide advice and recommendations regarding Emergency Medical Services (EMS) to the U.S. DOT's NHTSA.
Reports, Forms and Recordkeeping Requirements; Agency Information Collection Activity Under OMB Review
In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Request (ICR) abstracted below has been forwarded to the Office of Management and Budget (OMB) for review and comment. The ICR describes the nature of the information collections and their expected burden. The Federal Register Notice with a 60-day comment period was published on April 23, 2010 (75 FR 21385-21386).
Notice of Establishment of Emergency Relief Docket for Calendar Year 2011
The Federal Transit Administration (FTA) is establishing an Emergency Relief Docket for calendar year 2011 so grantees and subgrantees affected by national or regional emergencies may request relief from FTA administrative requirements set forth in FTA policy statements, circulars, guidance documents, and regulations. By this notice, FTA is establishing an Emergency Relief Docket for calendar year 2011.
Notice of Opportunity for Public Comment on Surplus Property Release at Brunswick-Golden Isles Airport, Brunswick, GA
Under the provisions of Title 49, U.S.C. Section 47153(c), notice is being given that the FAA is considering a request from the Glynn county Airport Commission to waive the requirement that a 16.84- acre parcel of surplus property, located on Glynn County Airport owned and operated land adjacent to, but separated by a public roadway, Brunswick-Golden Isles Airport, be used for aeronautical purposes.
Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This emergency AD was sent previously to all known U.S. owners and operators of these airplanes. This AD supersedes Emergency AD 2011-01-51, requires an immediate functional test of the fuselage drain holes, and requires sending a report of the results to the FAA. This AD also allows, with noted exceptions, for the return/ position of the airplane to a home base, hangar, maintenance facility, etc. This AD was prompted by reports of water accumulation in the belly of the fuselage that froze and caused the flight controls to jam. We are issuing this AD to prevent water or fluid from accumulating in the belly of the fuselage and freezing when the aircraft reaches and holds altitudes where the temperature is below the freezing point. This condition could cause the flight controls to jam with consequent loss of control.
Fifty-Third Meeting: RTCA Special Committee 186: Automatic Dependent Surveillance-Broadcast (ADS-B)
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 186: Automatic Dependent SurveillanceBroadcast (ADS-B).
Fourth Meeting: RTCA Special Committee 224: Airport Security Access Control Systems
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 224: Airport Security Access Control Systems.
Second Meeting RTCA NextGen Advisory Committee (NAC)
The FAA is issuing this notice to advise the public of a meeting of RTCA NextGen Advisory Committee (NAC).
Airworthiness Directives; The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This proposed AD would result in all airplanes having new relays with a ground fault interrupter (GFI) feature. This proposed AD would require, depending on airplane configuration, doing certain wiring changes, replacing the fuel pump power control relays for the main, center and auxiliary tanks, as applicable, with new relays having a GFI feature, performing certain bonding resistance measurements, and modifying relay module assemblies. The proposed AD also would require revising the maintenance program to incorporate Airworthiness Limitations (AWLs) 28-AWL-23 (for Model 737-100, 737-200, and 737-200C series airplanes), and 28-AWL-22 (for Model 737-300, 737-400, and 737- 500 series airplanes). This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent damage to the fuel pumps caused by electrical arcing that could introduce an ignition source in the fuel tank, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
Airworthiness Directives; REIMS AVIATION S.A. Model F406 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:
Crew Resource Management Training for Crewmembers in Part 135 Operations
This final rule requires all certificate holders conducting operations under part 135 to include in their training programs crew resource management training for crewmembers, including pilots and flight attendants. This final rule is needed to ensure that crewmembers in part 135 operations receive training in the use of crew resource management principles, as appropriate for their operation. This final rule responds to National Transportation Safety Board recommendations, addresses a recommendation from the Part 125/135 Aviation Rulemaking Committee, and codifies current FAA guidance. The intended effect of this final rule is to reduce the frequency and severity of errors that are crew based, which will reduce the frequency of accidents and incidents within the scope of part 135 operations.
Reports, Forms, and Recordkeeping Requirements; Agency Information Collection Activity Under OMB Review
In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Request (ICR) abstracted below has been forwarded to the Office of Management and Budget (OMB) for review and comment. The ICR describes the nature of the information collection and the expected burden. The Federal Register Notice with a 60-day comment period was published on August 16, 2010 (75 FR 50034-50036).
Agency Information Collection Activities: Notice of Request for Renewal of a Previously Approved Information Collection
The FHWA has forwarded the information collection request described in this notice to the Office of Management and Budget (OMB) to renew an information collection. We published a Federal Register Notice with a 60-day public comment period on this information collection on August 19, 2010. We are required to publish this notice in the Federal Register by the Paperwork Reduction Act of 1995.
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.
Environmental Impact Statement: Interstate 64 Corridor, Virginia
The Federal Highway Administration is issuing this notice to advise the public of its intent to prepare an Environmental Impact Statement (EIS) in cooperation with the Virginia Department of Transportation for potential transportation improvements along the Interstate 64 corridor in Virginia.
Airworthiness Directives; The Boeing Company Model 777-200 and -300 Series Airplanes Equipped with Rolls-Royce RB211 Trent 800 Engines
We propose to adopt a new airworthiness directive (AD) for certain Model 777-200 and -300 series airplanes. This proposed AD would require repetitive inspections of all thrust reverser (T/R) structure and sealant for degradation, and related investigative and corrective actions if necessary. This proposed AD results from reports of thrust reverser events related to thermal damage of the thrust reverser inner wall. We are proposing this AD to detect and correct a degraded T/R inner wall panel, which could lead to failure of a T/R and adjacent components and their consequent separation from the airplane, which could result in a rejected takeoff (RTO) and cause asymmetric thrust and consequent loss of control of the airplane during reverse thrust operation. If a T/R inner wall overheats, separated components could cause structural damage to the airplane, damage to other airplanes, or possible injury to people on the ground.
Airworthiness Directives; The Boeing Company Model 777-200 and -300 Series Airplanes Equipped With Pratt and Whitney Engines
We propose to adopt a new airworthiness directive (AD) for certain Model 777-200 and -300 series airplanes. This proposed AD would require repetitive inspections for hydraulic fluid contamination of the interior of the strut disconnect assembly; repetitive inspections for discrepancies of the interior of the strut disconnect assembly, if necessary; repetitive inspections of the exterior of the strut disconnect assembly for cracks, if necessary; and corrective action if necessary. This proposed AD also provides an optional terminating action for the inspections. This proposed AD results from reports of system disconnect boxes that have been contaminated with hydraulic fluid and, in one incident, led to subsequent cracking of titanium parts in the system disconnect assembly. We are proposing this AD to detect and correct hydraulic fluid contamination, which can cause cracking of titanium parts in the system disconnect assembly, resulting in compromise of the engine firewall. A cracked firewall can allow fire in the engine area to enter the strut and can lead to an uncontained engine strut fire if flammable fluid is present. Cracking of the disconnect box may also reduce the effectiveness of the fire extinguishing system in the engine compartment and could contribute to an uncontained engine fire. In addition, a cracked disconnect box can leak flammable fluids into the engine core, which can initiate an engine fire, and lead to one or both fire conditions discussed above.
Airworthiness Directives; Saab AB, Saab Aerosystems Model SAAB 340A (SAAB/SF340A) and SAAB 340B Airplanes Modified in Accordance With Supplemental Type Certificate (STC) ST00224WI-D, ST00146WI-D, or SA984GL-D
We are revising an earlier proposed airworthiness directive (AD) for certain Saab AB, Saab Aerosystems Model SAAB 340A (SAAB/ SF340A) and SAAB 340B airplanes. The first supplemental NPRM would have required inspecting the fuselage surface for corrosion and cracking behind the external adapter plate of the antennae installation, and repair if necessary. The first supplemental NPRM resulted from a report of a crack found behind the external adapter plate of the antennae during inspection. Similar cracking was found on two additional airplanes, and extensive corrosion was found on one airplane. This action revises the first supplemental NPRM by correcting an STC number, which would expand the applicability of the first supplemental NPRM. We are proposing this second supplemental NPRM to detect and correct corrosion and cracking behind the external adapter plate of the antennae of certain damage- tolerant structure, which could result in reduced structural integrity and consequent rapid depressurization of the airplane.
Proposed Establishment of Class E Airspace; Kahului, HI
This action proposes to establish Class E airspace at Kahului Airport, Kahului, HI. Controlled airspace is necessary to accommodate aircraft using the Instrument Landing System (ILS) standard instrument approach procedures at Kahului Airport, Kahului, HI. The FAA is proposing this action to enhance the safety and management of aircraft operations at the airport.
Proposed Amendment of Class E Airspace; Taylor, AZ
This action proposes to modify Class E airspace at Taylor Airport, Taylor, AZ. Controlled airspace is necessary to accommodate aircraft using the CAMBO One Departure Area Navigation (RNAV) out of Taylor Airport. The FAA is proposing this action to enhance the safety and management of aircraft operations at Taylor Airport, Taylor, AZ.
Proposed Amendment of Class E Airspace; West Yellowstone, MT
This action proposes to modify Class E airspace at Yellowstone Airport, West Yellowstone, MT, to accommodate aircraft using the Instrument Landing System (ILS) Localizer (LOC) standard instrument approach procedures at Yellowstone Airport, West Yellowstone, MT. The FAA is proposing this action to enhance the safety and management of aircraft operations at Yellowstone Airport.
Public Notice for Waiver of Aeronautical Land-Use Assurance Viroqua Municipal Airport; Viroqua, WI
The Federal Aviation Administration (FAA) is considering a proposal to authorize the release of 0.93 acres of the airport property at the Viroqua Municipal Airport, Viroqua, WI. The Wisconsin Department of Transportation (WisDOT) is seeking airport property for right of way along U.S. Highway 14/61. The FAA issued a categorical exclusion on December 23, 2010. The acreage being released is not needed for aeronautical use as currently identified on the Airport Layout Plan. The acreage comprising this parcel was originally acquired with local funds by the City of Viroqua. The airport will receive the appraised fair market value of $495,909 for the land. 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.
Notice to Rescind a Notice of Intent to Prepare a Supplemental Environmental Impact Statement: State Route 374 From State Route 149 West of River Road to State Route 76 in Clarksville, Montgomery County, TN
The FHWA is issuing this notice to advise the public that the Notice of Intent published on April 21, 2010, at 75 FR 20879, to prepare a Supplemental EIS for the extension of SR 374 from SR 149 west of River Road to SR 76 in Clarksville, Montgomery County, Tennessee, is being rescinded.
Establishment of Class E Airspace; Port Clarence, AK
This action changes the effective date for the establishment of Class E airspace at Port Clarence Coast Guard Station (CGS) Airport, Port Clarence, AK. The charting of this airspace has been delayed; therefore the effective date of the establishment of the Class E airspace area also must be delayed. A minor correction to a geographic coordinate also will be made.
Notice of Funding Availability for Applications for Credit Assistance Under the Transportation Infrastructure Finance and Innovation Act (TIFIA) Program
The DOT's TIFIA Joint Program Office (JPO) announces the availability of funding to support new applications for credit assistance. Under TIFIA, the DOT provides secured (direct) loans, lines of credit, and loan guarantees to public and private applicants for eligible surface transportation projects of regional or national significance. Projects must meet statutorily specified criteria to be selected for credit assistance. Because demand for the TIFIA program can exceed budgetary resources, the DOT is utilizing periodic fixed-date solicitations that will establish a competitive group of projects to be evaluated against the program objectives. This notice outlines the process that applicants must follow.
Federal Motor Vehicle Safety Standards, Ejection Mitigation; Phase-In Reporting Requirements; Incorporation by Reference
This final rule establishes a new Federal Motor Vehicle Safety Standard No. 226, ``Ejection Mitigation,'' to reduce the partial and complete ejection of vehicle occupants through side windows in crashes, particularly rollover crashes. The standard applies to the side windows next to the first three rows of seats, and to a portion of the cargo area behind the first or second rows, in motor vehicles with a gross vehicle weight rating (GVWR) of 4,536 kilogram (kg) or less (10,000 pounds (lb) or less). To assess compliance, the agency is adopting a test in which an impactor is propelled from inside a test vehicle toward the windows. The ejection mitigation safety system is required to prevent the impactor from moving more than a specified distance beyond the plane of a window. To ensure that the systems cover the entire opening of each window for the duration of a rollover, each side window will be impacted at up to four locations around its perimeter at two time intervals following deployment. The agency anticipates that manufacturers will meet the standard by modifying existing side impact air bag curtains, and possibly supplementing them with advanced glazing. The curtains will be made larger so that they cover more of the window opening, made more robust to remain inflated longer, and made to deploy in both side impacts and in rollovers. In addition, after deployment the curtains will be tethered near the base of the vehicle's pillars or otherwise designed to keep the impactor within the boundaries established by the performance test. This final rule adopts a phase-in of the new requirements, starting September 1, 2013. This final rule advances NHTSA's initiatives in rollover safety and also responds to Section 10301 of the Safe, Accountable, Flexible, Efficient Transportation Equity Act: A Legacy for Users (SAFETEA-LU). That section directs NHTSA to initiate and complete rulemaking to reduce complete and partial ejections of vehicle occupants from outboard seating positions, considering various ejection mitigation systems.
Value Pricing Pilot Program Participation, Fiscal Years 2010 and 2011
The FHWA is extending the deadline for formal grant applications for the Value Pricing Pilot (VPP) program, which was published on October 19, 2010, at 75 FR 64397. The original deadline for formal grant applications was January 18, 2011. This notice extends the deadline by 15 calendar days to February 2, 2011.
Airworthiness Directives; The Boeing Company Model 777 Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD would require revising the maintenance program to update inspection requirements to detect fatigue cracking of principal structural elements (PSEs). This proposed AD was prompted by a new revision to the airworthiness limitations of the maintenance planning document. We are proposing this AD to ensure that fatigue cracking of various PSEs is detected and corrected; such fatigue cracking could adversely affect the structural integrity of these airplanes.
Hazardous Materials: Harmonization With the United Nations Recommendations, International Maritime Dangerous Goods Code, and the International Civil Aviation Organization Technical Instructions for the Safe Transport of Dangerous Goods by Air
PHMSA is amending the Hazardous Materials Regulations to maintain alignment with international standards by incorporating various amendments, including changes to proper shipping names, hazard classes, packing groups, special provisions, packaging authorizations, air transport limited quantities, and vessel stowage requirements. These revisions are necessary to harmonize the Hazardous Materials Regulations with recent changes made to the International Maritime Dangerous Goods Code, the International Civil Aviation Organization's Technical Instructions for the Safe Transport of Dangerous Goods by Air, and the United Nations Recommendations on the Transport of Dangerous GoodsModel Regulations.
Airworthiness Directives; The Boeing Company Model 757 Airplanes
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Model 757 airplanes. The existing AD currently requires inspecting certain power feeder wire bundles for damage, inspecting the support clamps for these wire bundles to determine whether the clamps are properly installed, and performing corrective actions if necessary. This proposed AD would require additional inspections for certain airplanes. This proposed AD results from a report that a power feeder wire bundle chafed against the number six auxiliary slat track, causing electrical wires in the bundle to arc, which damaged both the auxiliary slat track and power feeder wires. We are proposing this AD to prevent arcing that could be a possible ignition source for leaked flammable fluids, which could result in a fire. Arcing could also result in a loss of power from the generator connected to the power feeder wire bundle, and consequent loss of systems, which could reduce controllability of the airplane.
Airworthiness Directives; The Boeing Company Model 777-200, -200LR, -300, and -300ER Series Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD would require installing foreign object debris (FOD) rubber shields over the primary and secondary external power connectors for certain airplanes, and wrapping fire-resistant silicone tape around the hydraulic tube for certain other airplanes. This proposed AD was prompted by a report of a fire in the main equipment center due to failure of an external power connector, which caused high-temperature arcing and subsequent splatter of molten copper on an adjacent hydraulic tube, creating a hole in the tube and spraying hydraulic fluid into the power connector, resulting in a fire. In addition there were several reports of overheating or arcing of external power connectors, and one report of a fire due to arcing caused by FOD. We are proposing this AD to prevent FOD from entering the primary and secondary external power connectors, which could result in overheating or arcing and consequent fire in the main equipment center.
Notice of Final Federal Agency Actions on Proposed Highway in California
The FHWA, on behalf of Caltrans, is issuing this notice to announce actions taken by Caltrans, that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to a proposed highway project along Interstate 805, San Diego, CA, PM: 23.3-27.7 in the County of San Diego, State of California. Those actions grant licenses, permits, and approvals for the project.
Notice of Final Federal Agency Actions on Proposed Project in Washington
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 project, the SR 520 Pontoon Construction Project in the State of Washington. Those actions grant approval for the project.
Safe, Efficient Use and Preservation of the Navigable Airspace; Correction
The FAA is correcting the regulation addressing the effective date of FAA determinations issued under 14 CFR part 77. The FAA amended this regulation by final rule published on July 21, 2010. The purpose of the final rule was to update the regulations governing objects that may affect the navigable airspace, to incorporate case law and legislative action, and to simplify the rule language. In one section of the regulations, we inadvertently state that the effective date of all determinations is 40 days from the date of issuance. However, only FAA determinations subject to the discretionary review process are effective 40 days from the date of issuance. All other FAA determinations are effective upon issuance. This document corrects that error.
Airworthiness Directives; The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER Series Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This proposed AD would require inspecting to determine the clearance and any wire bundle damage between wire bundle W443 and the left forward rudder quadrant, followed by adjusting the minimum clearance between the wire bundle and the left forward rudder quadrant, and repairing any wire bundle damage. This proposed AD results from reports of contact between wire bundle W443 and the left forward rudder quadrant. We are proposing this AD to detect and correct contact between the wire bundle and the left forward rudder quadrant. Damage to the wire bundle could result in uncommanded stabilizer trim and autopilot disconnects due to shorted wires from contact between the wire bundle and the left forward rudder quadrant, potentially affecting the capability of the flight crew during high work load and consequently reducing control of the airplane. Restricted free movement of the rudder quadrant at full right rudder travel would reduce controllability of the airplane.
Notice of Limitation on Claims Against Proposed Public Transportation Projects
This notice announces final environmental actions taken by the Federal Transit Administration (FTA) for the following projects: (1) New Orleans Union Passenger Terminal (NOUPT)/Loyola Avenue Streetcar Project, New Orleans Regional Transit Authority, New Orleans, LA; (2) South Corridor: Portland-Milwaukie Light Rail Project, Tri-County Metropolitan Transportation District of Oregon (TriMet), Clackamas, and Portland, Oregon; and (3) Second Avenue Subway Project, Metropolitan Transportation Authority, New York, NY. The purpose of this notice is to announce publicly the environmental decisions by FTA on the subject projects and to activate the limitation on any claims that may challenge these final environmental actions.
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