Department of Transportation September 2009 – Federal Register Recent Federal Regulation Documents
Results 151 - 200 of 241
Office of Commercial Space Transportation; Notice of Availability of the Final Programmatic Environmental Impact Statement for Streamlining the Processing of Experimental Permit Applications
In accordance with the National Environmental Policy Act of 1969, as amended (NEPA) (42 U.S.C. 4321 et seq.), Council on Environmental Quality NEPA implementing regulations (40 CFR Parts 1500- 1508), and FAA Order 1050.1E, Change 1, the FAA is announcing the availability of the Final Programmatic Environmental Impact Statement for Streamlining the Processing of Experimental Permit Applications (PEIS). The FAA Office of Commercial Space Transportation is the lead Federal agency for the development of the PEIS. The National Aeronautics and Space Administration and the U.S. Air Force are cooperating agencies.
Notice of Intent To Rule on Request To Release Airport Property at the Upper Cumberland Regional Airport, Sparta, TN
The Federal Aviation Administration is requesting public comment on the release of land at the Upper Cumberland Regional Airport, Sparta, TN.
Airspace Designations; Incorporation by Reference
This action amends Title 14 Code of Federal Regulations (14 CFR) part 71 relating to airspace designations to reflect the approval by the Director of the Federal Register of the incorporation by reference of FAA Order 7400.9T, Airspace Designations and Reporting Points. This action also explains the procedures the FAA will use to amend the listings of Class A, B, C, D, and E airspace areas; air traffic service routes; and reporting points incorporated by reference.
Renewal of Rail Energy Transportation Advisory Committee
In accordance with the Federal Advisory Committee Act, as amended 5 U.S.C., App. (FACA), notice is hereby given that the Surface Transportation Board (Board) intends to renew the charter of the Rail Energy Transportation Advisory Committee (RETAC).
Airworthiness Directives; General Electric Company (GE) CJ610 Series Turbojet Engines and CF700 Series Turbofan Engines
The FAA proposes to adopt a new airworthiness directive (AD) for GE CJ610 series turbojet engines and CF700 turbofan engines with AFT Technologies combustion liners, part number (P/N) AFT-5016T30G02. This proposed AD would require removing from service, AFT Technologies combustion liners, P/N AFT-5016T30G02. This proposed AD results from a report of an AFT Technologies combustion liner that released a large section of the inner combustion liner and reports of six combustion liners with premature cracks. We are proposing this AD to prevent premature cracks in the combustion liner, which could release pieces of the inner combustion liner. A release of pieces of the inner combustion liner could cause an uncontained failure of the engine turbine and damage to the airplane.
Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, -900 and -900ER Series Airplanes
We are adopting a new airworthiness directive (AD) for all Boeing Model 737-600, -700, -700C, -800, -900 and -900ER series airplanes. This AD requires repetitive testing of the rudder pedal forces or repetitive detailed inspections of the inner spring of the rudder feel and centering unit, and corrective actions if necessary. This AD also requires replacement of the spring assembly in the rudder feel and centering unit, which terminates the repetitive tests or inspections. This AD results from reports of low rudder pedal forces that were caused by a broken inner spring in the rudder feel and centering unit; a broken inner spring in conjunction with a broken outer spring would significantly reduce rudder pedal forces. We are issuing this AD to prevent reduced rudder pedal forces, which could result in increased potential for pilot-induced oscillations and reduce the ability of the flightcrew to maintain the safe flight and landing of the airplane.
Airworthiness Directives; Airbus Model A300 B2-1C, B2-203, B2K-3C, B4-103, B4-203, and B4-2C 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 A330-200 and -300 Series Airplanes and Model A340-200 and -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; Airbus Model A330-300, A340-200, and 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:
Excess Risk Estimate for Highway-Rail Grade Crossings Along the Florida East Coast Railway Line
This final rule amends the regulations regarding the use of locomotive horns at public highway-rail grade crossings by establishing an excess risk estimate of 90.9 percent for public highway-rail grade crossings along the Florida East Coast Railway Company (FEC) line. When this final rule is effective, public authorities will be permitted to establish New Quiet Zones along the FEC line, in accordance with the existing regulations, through application of the excess risk estimate provided herein.
Airworthiness Directives; ATR Model ATR42 and ATR72 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 A310-203, -204, -221, -222, -304, -322, -324, and -325 Airplanes
We are superseding an existing 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; 328 Support Services GmbH Dornier Model 328-100 and -300 Airplanes
We are superseding an existing 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; Fokker Model F.28 Mark 0070 and 0100 Airplanes
We are superseding an existing 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; Boeing Model 707 Airplanes, and Model 720 and 720B Series Airplanes
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 707 airplanes, and Model 720 and 720B series airplanes. The existing AD currently requires repetitive detailed inspections to detect cracks and corrosion on any existing repairs and at certain body stations (STA) 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 new AD retains the requirements of the existing AD and requires repetitive ultrasonic inspections to detect any stress corrosion cracks within the outboard flange of the left and right body terminal fittings at STA 820, and related investigative and corrective actions if necessary. This AD also provides an optional terminating action for the repetitive inspections. This AD also adds two airplanes to the applicability. This AD results from reports of cracks found in the wing to body terminal fittings during routine inspections. We are issuing this AD to detect and correct cracks and corrosion in the body terminal fittings above and below the floor, which could cause loss of support for the wing and could adversely affect the structural integrity of the airplane.
Airworthiness Directives; Bombardier Model DHC-8-400 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; Fokker Model F.28 Mark 0070 and 0100 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; Rolls-Royce plc. (RR) RB211 Trent 900 Series Turbofan Engines
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:
Establishment of Low Altitude Area Navigation Route (T-Route); Rockford, IL
This action establishes a low altitude Area Navigation (RNAV) route, designated T-265, in the Chicago/Rockford International Airport, IL, terminal area. This route allows for more effective utilization of airspace and enhances the management of aircraft operations in the Chicago/Rockford International Airport, IL, terminal area west of Chicago, IL.
Notice of Intent To Request Revision From the Office of Management and Budget of a Currently Approved Information Collection Activity, Request for Comments; Flight Operational Quality Assurance (FOQA) Program
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection, FOQA is a voluntary program for the routine collection and analysis of digital flight data from airplane operations.
Notice of Intent To Request Revision From the Office of Management and Budget of a Currently Approved Information Collection Activity, Request for Comments; Fractional Aircraft Ownership Programs
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. Fractional Ownership is a program that offers increased flexibility in aircraft ownership.
Hazardous Materials-Automated Cargo Communication for Efficient and Safe Shipments HM-ACCESS) Initiative; Public Meeting
This notice is to advise interested persons that PHMSA will conduct a public meeting to receive input and guidance for the upcoming Proof-of-Concept Study on the use of electronic data sharing in lieu of paper hazardous materials shipping documents.
Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes
We are revising an existing airworthiness directive (AD) that applies to certain Boeing Model 737-300, -400, and -500 series airplanes. That AD currently requires repetitive high frequency eddy current inspections for cracking of the 1.04-inch nominal diameter wire penetration hole in the frame and frame reinforcement, between stringers S-20 and S-21, on both the left and right sides of the airplane, and related investigative and corrective actions if necessary. This new AD clarifies certain compliance requirements. This AD results from reports of cracking in the frame, or in the frame and frame reinforcement, common to the 1.04-inch nominal diameter wire penetration hole intended for wire routing. We are issuing this AD to detect and correct cracking in the fuselage frames and frame reinforcements, which could reduce the structural capability of the frames to sustain limit loads, and result in cracking in the fuselage skin and subsequent rapid depressurization of the airplane.
Establishment of Class D Airspace; Grand Prairie, TX
This action establishes Class D airspace at Grand Prairie, TX. Establishment of an air traffic control tower at Grand Prairie Municipal Airport has made this action necessary for the safety and management of Instrument Flight Rule (IFR) operations at Grand Prairie Municipal Airport.
Establishment of Class E Airspace; Neligh, NE
This action establishes Class E airspace at Neligh, NE. Controlled airspace is necessary to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAP) at Antelope County Airport, Neligh, NE. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at Antelope County Airport.
Establishment of Class D Airspace; Arlington, TX
This action amends Class E airspace at Arlington, TX. Establishment of an air traffic control tower at Arlington Municipal Airport has made this action necessary for the safety and management of Instrument Flight Rule (IFR) operations at Arlington Municipal Airport.
Succession to the Administrator
This document amends NHTSA's regulation specifying the order of succession to the Administrator. We have determined at the present time that a change in the order of succession better serves the agency's mission.
Design Maneuvering Speed Limitation Statement
The Federal Aviation Administration proposes to amend the airworthiness standards applicable to transport category airplanes to clarify that flying at or below the design maneuvering speed does not allow a pilot to make multiple large control inputs in one airplane axis or single full control inputs in more than one airplane axis at a time without endangering the airplane's structure. This proposed regulation is the result of an accident investigation and responds to a National Transportation Safety Board recommendation. The results of the accident investigation indicate that many pilots might have a general misunderstanding of what the design maneuvering speed (VA) is and the extent of structural protection that exists when an airplane is operated at speeds below its VA. This action is being taken to prevent this misunderstanding from causing or contributing to a future accident.
Twelfth Joint Meeting, RTCA Special Committee 205/EUROCAE WG 71: Software Considerations in Aeronautical Systems
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 205/EUROCAE WG 71: Software Considerations in Aeronautical Systems.
Senior Executive Service Performance Review Boards Membership
DOT publishes the names of the persons selected to serve on the various Departmental PRBs as required by 5 U.S.C. 4314(c)(4).
Distracted Driving Summit; Notice
The U.S. Department of Transportation is providing notice that it intends to hold a Distracted Driving Summit (The Summit) to exchange information and ideas on the best possible methods to reduce the number of crashes and deaths due to distracted driving.
Announcing the Eighteenth Public Meeting of the Crash Injury Research and Engineering Network (CIREN)
This notice announces the Eighteenth Public Meeting of members of the Crash Injury Research and Engineering Network. CIREN is a collaborative effort to conduct research on crashes and injuries at eight Level 1 Trauma Centers across the United States linked by a computer network. Researchers can review data and share expertise, which may lead to a better understanding of crash injury mechanisms and the design of safer vehicles. The eight centers will give presentations on current research based on CIREN data. The agenda will be posted to the CIREN Web site that can be accessed by going to the NHTSA homepage https://www.nhtsa.dot.gov/, click on Vehicle Safety Research on the right side of the top toolbar, then click on Crash Injury Research and Engineering Network (CIREN) in the box on the left. The agenda will be posted two weeks prior to the meeting.
Environmental Impact Statement for the California High Speed Train Project From Palmdale to Bakersfield, CA
This notice is to advise the public that FRA and the California High-Speed Rail Authority (Authority) will jointly prepare a project Environmental Impact Statement (EIS) and project Environmental Impact Report (EIR) for the Palmdale to Bakersfield section of the Authority's proposed California High Speed Train (HST) System in compliance with relevant state and federal laws, in particular the National Environmental Policy Act (NEPA) and the California Environmental Quality Act (CEQA).
Surface Transportation Environment and Planning Cooperative Research Program (STEP)
Section 5207 of the Safe, Accountable, Flexible, Efficient Transportation Equity Act: A Legacy for Users (SAFETEA-LU) established the Surface Transportation Environment and Planning Cooperative Research Program (STEP). The FHWA anticipates that resources for STEP or a similar program to carry out national research on issues related to planning, environment, and realty are likely to be included in future surface transportation legislation even though SAFETEA-LU expires at the end of this fiscal year. Legislation preceding SAFETEA- LUthe Intermodal Surface Transportation Efficiency Act of 1991 (ISTEA) and the Transportation Equity Act for the 21st Century (TEA- 21)provided resources for FHWA to carry out surface transportation research initiatives that included planning, environment, and realty research. SAFETEA-LU continued FHWA's research program funding and established STEP.
Petition for Exemption; Summary of Petition Received
This notice contains a summary of a petition seeking relief from specified requirements of 14 CFR 21.151 and 21.153. 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 21.435 (c). 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.
Airworthiness Directives; Bombardier Model DHC-8-400 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; McDonnell Douglas Model MD-90-30 Airplanes
We propose to adopt a new airworthiness directive (AD) for all McDonnell Douglas Model MD-90-30 airplanes. This proposed AD would require repetitive inspections for cracking of the overwing frames at stations 883, 902, 924, 943, and 962, left and right sides, and corrective actions if necessary. This proposed AD results from reports of cracked overwing frames. We are proposing this AD to detect and correct such cracking, which could sever the frame, increase the loading of adjacent frames, and result in damage to adjacent structure and loss of overall structural integrity of the airplane.
Airworthiness Directives; Bombardier Model DHC-8-400 Series 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 A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 Series Airplanes; and Model A340-211, -212, -213, -311, -312, and -313 Series Airplanes; and A340-541 and -642 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:
Notice of Opportunity To Participate, Criteria Requirements and Application Procedure for Participation in the Military Airport Program (MAP).
In anticipation of Congress enacting a reauthorization of the Airport Improvement Program (AIP) the FAA is publishing this annual notice. This notice announces the criteria, application procedures, and schedule to be applied by the Secretary of Transportation in designating or redesignating, and funding capital development annually for up to 15 current (joint-use) or former military airports seeking designation or redesignation to participate in the MAP. While FAA currently has continuing authority to designate or redesignate airports, FAA does not have authority to issue grants for fiscal year 2010 MAP, and will not have authority until Congress enacts legislation enabling FAA to issue grants.
Airworthiness Directives; Agusta S.p.A. Model AB412 and AB412 EP Helicopters
We are adopting a new airworthiness directive (AD) for the specified Agusta S.p.A. (Agusta) Model AB412 and AB412 EP helicopters. This AD results from mandatory continuing airworthiness information (MCAI) issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community. The MCAI establishes a life limit for certain rescue hoist cable assemblies and introduces the term ``hoist lift'' for determining cable life instead of the term ``hoist cycle.'' The MCAI also establishes a replacement time for each affected rescue hoist cable assembly (hoist cable assembly) for which the accumulated number of ``hoist cycles'' cannot be determined. The actions are intended to prevent failure of a hoist cable and inadvertent loss of a load.
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