Department of Transportation November 2011 – Federal Register Recent Federal Regulation Documents

Results 201 - 243 of 243
Railroad Revenue Adequacy-2010 Determination
Document Number: 2011-28748
Type: Notice
Date: 2011-11-07
Agency: Surface Transportation Board, Department of Transportation
On November 3, 2011, the Board served a decision announcing the 2010 revenue adequacy determinations for the Nation's Class I railroads. One carrier, Union Pacific Railroad Company, was found to be revenue adequate.
Notice of Final Federal Agency Actions on Farm-to-Market 1626 in Texas
Document Number: 2011-28686
Type: Notice
Date: 2011-11-07
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 a proposed highway project, Farm-to-Market (FM) 1626, from Ranch-to-Market (RM) 967 to Brodie Lane in Hays and Travis Counties, Texas. Those actions grant licenses, permits, and approvals for the project.
Airworthiness Directives; Rolls-Royce plc (RR) RB211-Trent 800 Series Turbofan Engines
Document Number: 2011-28678
Type: Proposed Rule
Date: 2011-11-07
Agency: Federal Aviation Administration, Department of Transportation
We are revising an earlier proposed airworthiness directive (AD) for RR RB211-Trent 800 series turbofan engines. That NPRM proposed to revise the Trent 800 Time Limits Manual (TLM) of the Trent 800 engine maintenance manuals (EMMs). That NPRM was prompted by RR reducing the life limits of certain critical engine parts. This action revises that NPRM by proposing to supersede an existing AD to prohibit installation of one certain critical part and to increase the life of another critical part whose lives were previously reduced by that existing AD. We are proposing this supplemental NPRM to prevent the failure of critical rotating parts, which could result in uncontained failure of the engine and damage to the airplane. Because of the extensive changes since the NPRM was issued, we are reopening the comment period to allow the public the chance to comment on these proposed changes.
Airworthiness Directives; Turbomeca S.A. Arriel 2B and 2B1 Turboshaft Engines
Document Number: 2011-28677
Type: Proposed Rule
Date: 2011-11-07
Agency: Federal Aviation Administration, Department of Transportation
We propose to supersede an existing airworthiness directive (AD) that applies to all Turbomeca S.A. Arriel 2B and 2B1 turboshaft engines. The existing AD currently requires checking the transmissible torque between the low-pressure (LP) pump impeller and the high- pressure (HP) pump shaft on HP/LP pump hydro-mechanical metering units (HMUs) that do not incorporate Modification TU 147. Since we issued that AD, EASA issued a new AD. This proposed AD would require inspection and possible replacement of the HMU. We are proposing this AD to prevent reduced engine power or, at worst, an uncommanded in- flight shutdown (IFSD), which can result in a forced autorotation landing or accident.
Airworthiness Directives; Pratt & Whitney Division (PW) PW4000 Series Turbofan Engines
Document Number: 2011-28676
Type: Proposed Rule
Date: 2011-11-07
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for PW4000 series turbofan engines. This proposed AD would require replacing the fuel metering unit (FMU), part number (P/N) 50U150, at the next shop visit after the effective date of this proposed AD. This proposed AD was prompted by an engine overspeed event that occurred during taxi and resulted in a high-pressure compressor (HPC) surge and tailpipe fire. We are proposing this AD to prevent engine overspeed on these engines, which could result in an uncontained engine failure and damage to the airplane.
Airworthiness Directives; Thielert Aircraft Engines GmbH (TAE) Reciprocating Engines
Document Number: 2011-28672
Type: Rule
Date: 2011-11-07
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for Thielert Aircraft Engines GmbH (TAE) Models TAE 125-01 and TAE 125- 02-99 reciprocating engines. That AD currently requires replacement of certain part numbers (P/Ns) and serial numbers (S/Ns) of clutch assemblies due to clutch failure. The failures identified above could lead to engine in-flight shutdown and loss of control of the airplane. This AD requires the same actions, but applies the corrective action to an additional 244 affected clutch assemblies. This AD was prompted by TAE identifying additional clutch assemblies with nonconforming disc springs. We are issuing this AD to correct the unsafe condition on these products.
Airworthiness Directives; General Electric Company (GE) CF6 Turbofan Engines
Document Number: 2011-28671
Type: Rule
Date: 2011-11-07
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for the engines identified above. That AD currently requires initial and repetitive visual inspections of the forward engine mount assembly side links for cracks, stripping and reapplying the Sermetel W coating on the side links at every exposure of the side link. This new AD requires those same inspections, stripping and reapplying the Sermetel W coating, and adds two part numbers to the applicability. This AD was prompted by a review of the inspection program, which revealed that GE had omitted two affected side link part numbers from the applicability. We are issuing this AD to prevent failure of the side links and possible engine separation from the airplane.
Proposed Amendment of VOR Federal Airways V-320 and V-440; Alaska
Document Number: 2011-28614
Type: Proposed Rule
Date: 2011-11-07
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend two VHF Omnidirectional Range (VOR) Federal airways in Alaska, V-320 and V-440, due to the relocation of the Anchorage VOR navigation aid. This action is necessary for the continued safe and efficient management of Instrument Flight Rules (IFR) operations within the National Airspace System.
Utah Southern Railroad Company, LLC-Change in Operators Exemption-Iron Bull Railroad Company, LLC
Document Number: 2011-28642
Type: Notice
Date: 2011-11-04
Agency: Surface Transportation Board, Department of Transportation
Airworthiness Directives; DASSAULT AVIATION Model MYSTERE-FALCON 900 Airplanes
Document Number: 2011-28578
Type: Proposed Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all DASSAULT AVIATION Model MYSTERE-FALCON 900 airplanes. 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; The Boeing Company Model 777-200 and -300 Series Airplanes
Document Number: 2011-28568
Type: Proposed Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 777-200 and -300 series airplanes. This proposed AD would require replacing certain single-tabbed bonding brackets in the airplane empennage with two-tabbed bonding brackets. This proposed AD would also require, for certain airplanes, installing new bonding jumpers, and measuring the resistance of the modified installation to verify resistance is within specified limits. This proposed AD was prompted by reports of two failures of the single- tabbed bracket on the rudder. We are proposing this AD to prevent failure of the bonding jumper bracket, which could result in loss of lightning protection ground path, which could lead to increased lightning-induced currents and subsequent damage to composite structures, hydraulic tubes, and actuator control electronics. In the event of a lightning strike, loss of lightning ground protection could result in the loss of control of the airplane.
Commercial Driver's License Information System State Procedures Manual, Release 5.2.0
Document Number: 2011-28517
Type: Rule
Date: 2011-11-04
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA amends the Federal Motor Carrier Safety Regulations (FMCSRs) to incorporate by reference the most recent edition of the American Association of Motor Vehicle Administrators, Inc.'s (AAMVA) Commercial Driver's License Information System (CDLIS) State Procedures Manual (the Manual) (Release 5.2.0). This final rule requires all State driver licensing agencies (SDLAs) to use this recent edition of the Manual to develop the process required to transmit, receive, record, and update information on a CDLIS driver record. This information includes, but is not limited to, the commercial driver's license (CDL) holder's physical description, commercial and noncommercial driving status, medical certification status, convictions, disqualifications and accidents. This final rule is intended to ensure the uniform application of CDLIS procedures among all States.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2011-28360
Type: Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Bombardier, Inc. 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. 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; Sicma Aero Seat Passenger Seat Assemblies, Installed on, But Not Limited to, ATR-GIE Avions de Transport Régional Airplanes
Document Number: 2011-28357
Type: Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Sicma Aero Seat Model 9401, 9402, 9404, 9405, 9406, 9407, 9408, and 9409 series passenger seat assemblies, installed on, but not limited to, ATR-GIE Avions de Transport R[eacute]gional Model ATR42 and ATR72 airplanes. 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; Bell Helicopter Textron, Inc. (Bell), Model 205A-1, 205B, 210, and 212 Helicopters
Document Number: 2011-28355
Type: Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
This amendment supersedes an existing airworthiness directive (AD) for Bell Model 205B and 212 helicopters with certain main rotor blade (blade) assemblies installed. That AD currently requires washing the upper and lower surfaces of each blade and visually inspecting the grip plates, doublers, and the remaining upper and lower surfaces of the blades in the area between blade stations 24.5 to 40 for an edge void, corrosion, or a crack. This amendment retains the requirements of that AD for the affected part-numbered blades but increases the scope and frequency of the inspections and expands the applicability to include the Model 205A-1 and 210 helicopters, additional blade part numbers, and all helicopter serial numbers for the affected helicopter models. This amendment also requires applying a light coat of preservative oil (C-125) to all surfaces of the blade in addition to the inspection areas as required in the existing AD. This amendment is prompted by an additional report of a fatigue crack on a blade installed on a Model 212 helicopter. The actions specified by this AD are intended to detect an edge void, corrosion, or a crack on a blade, and to prevent loss of a blade and subsequent loss of control of the helicopter.
Agency Information Collection Activities: Request for Comments; Clearance of a New Information Collection; U.S. DOT Mentor Protégé Pilot Program
Document Number: 2011-27916
Type: Notice
Date: 2011-11-04
Agency: Office of the Secretary, Department of Transportation
In accordance with the Paperwork Reduction Act of 1995, Public law 104-13 (44 U.S.C. 3501 et seq) this notice announces the information collection request on Mentor Prot[eacute]g[eacute] Pilot Program annual report form, and the Mentor Prot[eacute]g[eacute] Pilot Program evaluation form. DOT's Mentor-Prot[eacute]g[eacute] Pilot Program enhances the capability of disadvantaged and small business owners to compete more successfully for federal procurement opportunities. The program encourages private-sector relationships and expands DOT's efforts to identify and respond to the developmental needs of small and disadvantaged businesses. The program is administered by the DOT OST Office of Small and Disadvantaged Business Utilization (OSDBU).
Airworthiness Directives; Eurocopter Deutschland GmbH (ECD) Model MBB-BK 117 C-2 Helicopters
Document Number: 2011-27776
Type: Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD) for ECD Model MBB-BK 117 C-2 helicopters. This action requires revising the Rotorcraft Flight Manual (RFM) by inserting certain temporary pages into the Emergency and Performance Data sections of the RFM to alert the operators to monitor the power display when a generator is deactivated and provides appropriate actions. This amendment is prompted by reports of too high a current flow when one generator is deactivated. The actions specified in this AD are intended to prevent failure of the remaining generator when one generator is deactivated, loss of electrical power, loss of systems necessary for flight safety, and subsequent loss of control of the helicopter.
Airworthiness Directives; Agusta S.p.A. (Agusta) Model AB139 and AW139 Helicopters
Document Number: 2011-27772
Type: Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD) for the specified Agusta model helicopters. This action requires inspecting certain modules and related connectors for corrosion. If there is corrosion on the connectors, this AD requires cleaning the connectors before further flight. If there is corrosion on a module, before further flight, this AD requires replacing the module with an airworthy module. This AD also requires modifying the Number 2 Modular Avionic Unit (MAU) ventilation duct. This amendment is prompted by some in- flight emergencies due to internal corrosion of the MAU circuit card assemblies. The actions specified in this AD are intended to detect corrosion of certain modules to prevent the display of misleading data to the flight crew, disengagement of the flight director modes of the autopilot or other alert system, increased workload of the flight crew, and subsequent loss of control of the helicopter.
Letters of Interest for Credit Assistance Under the Transportation Infrastructure Finance and Innovation Act (TIFIA) Program
Document Number: 2011-28584
Type: Notice
Date: 2011-11-03
Agency: Office of the Secretary, Department of Transportation
The DOT's TIFIA Joint Program Office (JPO) announces the availability of a limited amount of funding in Fiscal Year (FY) 2012 to provide 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 exceeds budgetary resources, the DOT is utilizing periodic fixed-date solicitations. This notice outlines the process that project sponsors must follow to compete to secure an invitation for Federal credit assistance for Federal FY 2012.
Petition for Exemption From the Federal Motor Vehicle Theft Prevention Standard; Chrysler
Document Number: 2011-28541
Type: Notice
Date: 2011-11-03
Agency: National Highway Traffic Safety Administration, Department of Transportation
This document grants in full the Chrysler LLC, (Chrysler) petition for exemption of the Chrysler [confidential] vehicle line in accordance with 49 CFR part 543, Exemption from Vehicle Theft Prevention Standard. This petition is granted because the agency has determined that the antitheft device to be placed on the line as standard equipment is likely to be as effective in reducing and deterring motor vehicle theft as compliance with the parts-marking requirements of the Theft Prevention Standard 49 CFR part 541, Federal Motor Vehicle Theft Prevention Standard. Chrysler requested confidential treatment for specific information in its petition. The agency granted Chrysler's request for confidential treatment by letter dated September 14, 2011. Chrysler informed the agency that the nameplate and model year of introduction will be released to the public prior to introduction of the vehicle line.
Aviation Proceedings, Agreements Filed the Week Ending September 10, 2011
Document Number: 2011-28484
Type: Notice
Date: 2011-11-03
Agency: Office of the Secretary, Department of Transportation
Notice of Final Action Under Paperwork Reduction Act
Document Number: 2011-28464
Type: Notice
Date: 2011-11-03
Agency: Surface Transportation Board, Department of Transportation
Pursuant to the Paperwork Reduction Act, 44 U.S.C. 3501 et seq. (PRA) and Office of Management and Budget (OMB) regulations at 5 CFR 1320.10, the Surface Transportation Board has obtained an extension of OMB's approval for the information collection, required under 49 CFR 1114.30(d), 1121.3(d), 1150.33(h), 1150.43(h), and 1180.4(g)(4), of certain agreements that contains rail interchange commitments (OMB Control Number 2140-0016). Unless renewed, OMB approval expires on August 31, 2014. The display of a currently valid OMB control number for this collection is required by law. Under the PRA and 5 CFR 1320.8, an agency may not conduct or sponsor, and a person is not required to respond to, a collection of information unless the collection displays a currently valid OMB control number.
Notice of Public Hearing
Document Number: 2011-28453
Type: Notice
Date: 2011-11-03
Agency: Federal Railroad Administration, Department of Transportation
Availability of Finding of No Significant Impact
Document Number: 2011-28401
Type: Notice
Date: 2011-11-03
Agency: Department of Transportation, U.s. Maritime Administration, Maritime Administration
Notice is hereby given that the Maritime Administration, of the U.S. Department of Transportation (US DOT), has made available to interested parties the Finding of No Significant Impact (FONSI) for the United States Merchant Marine Academy Mallory Pier Replacement project. An environmental assessment (EA) and FONSI have been prepared pursuant to the National Environmental Policy Act (NEPA) (U.S.C. 4231 et seq.) in accordance with the Council on Environmental Quality (CEQ) regulations for implementing the procedural provisions of NEPA (40 CFR 1500-1508). The purpose of the EA is to evaluate the potential environmental impacts from replacement of a 600 foot section of timber pile supported pier with concrete pile supports and decking. The timber pile pier section to be replaced comprises a total area of 13,400 square feet.
National Express Acquisition Corporation-Control-Petermann Partners, Inc.
Document Number: 2011-28408
Type: Notice
Date: 2011-11-02
Agency: Surface Transportation Board, Department of Transportation
National Express Acquisition Corporation (NEAC) and National Express Corporation (NEC), both noncarriers, have filed an application under 49 U.S.C. 14303 for NEAC's acquisition of control of Petermann Partners, Inc. (PPI), a noncarrier, and the passenger motor carriers PPI controls: Beck Bus Transportation Corp. (MC-143528); Petermann Northeast, LLC (MC-723926); Petermann Northwest, LLC (MC-638608); Petermann Southwest, LLC (MC-644996); Petermann STSA, LLC (which has filed for registration in FMCSA Docket No. MC-749360); MV Student Transportation, Inc. (MC-148934); Carrier Management, Inc. (no MC number); and Petermann Ltd. (MC-364668) (collectively, Petermann Carriers). The Board has tentatively approved and authorized the transaction, and, if no opposing comments are timely filed, this notice will be the final Board action. Persons wishing to oppose the application must follow the rules under 49 CFR 1182.5 and 1182.8.
Airworthiness Directives; Cirrus Design Corporation Airplanes
Document Number: 2011-28382
Type: Proposed Rule
Date: 2011-11-02
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Cirrus Design Corporation (Cirrus) Model SR22T airplanes. This proposed AD was prompted by reports of partial loss of engine power due to a dislodged rubber gasket/seal being ingested into the turbocharger. This proposed AD would require inspection and modification of the air box flange welds and slots and installation of induction system air box seals as applicable. We are proposing this AD to correct the unsafe condition on these products.
Airworthiness Directives; Airbus Model A319 and A320 Series Airplanes
Document Number: 2011-28368
Type: Proposed Rule
Date: 2011-11-02
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; Dassault Aviation Model Mystere-Falcon 50 Airplanes
Document Number: 2011-28362
Type: Proposed Rule
Date: 2011-11-02
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; Bell Helicopter Textron, Inc. (Bell) Model 204B, 205A, 205A-1, 205B, and 212 Helicopters
Document Number: 2011-28361
Type: Proposed Rule
Date: 2011-11-02
Agency: Federal Aviation Administration, Department of Transportation
This document proposes superseding four existing airworthiness directives (ADs) for the specified Bell model helicopters. Two of the existing ADs require an initial and repetitive inspection of certain part-numbered main rotor yokes installed on Bell Model 204B, 205A-1, and 212 helicopters. Two other existing ADs also establish a retirement life of 3,600 hours time-in-service (TIS) for certain part-numbered main rotor yokes installed on the Bell Model 204, 205 series, and 212 series helicopters. Those ADs were prompted by reports of cracks in the main rotor yoke (yoke). This action would retain the requirements of the existing ADs and would apply these inspections and retirement lives to additional part-numbered yokes. This action would also increase the inspection frequency for certain yokes installed on a Bell Model 205B or 212 helicopter and would require replacing any unairworthy yoke. This proposal is prompted by the need to expand the applicability to include yokes produced under a Parts Manufacturing Approval (PMA) whose design approval was based on identicality with the affected Bell yoke parts and a recent discovery of a cracked yoke. The actions specified by the proposed AD are intended to prevent cracking of a yoke, failure of the yoke, and subsequent loss of control of the helicopter.
Airworthiness Directives; General Electric Company Turboshaft Engines
Document Number: 2011-28353
Type: Rule
Date: 2011-11-02
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all General Electric Company (GE) CT7-8A, CT7-8A1, CT7-8E, and CT7-8F5 turboshaft engines with a fuel filter differential pressure switch, part number (P/N) TD028VF0H7Y5 (part of the fuel filter assembly, P/N 4110T53P06) installed. This AD requires daily visual inspections of the fuel filter differential pressure switch for fuel leaks and for excessive cracking of the switch mounting flanges due to stress- corrosion. This AD also requires the installation of a collar kit over the fuel filter differential pressure switch as terminating action to the daily inspections. This AD was prompted by reports of 47 fuel filter differential pressure switches found with stress-corrosion cracking of the mounting flanges. We are issuing this AD to prevent unrecoverable in-flight engine shutdown, engine bay fire due to fuel leakage, and forced landing or accident.
Airworthiness Directives; Rolls-Royce Corporation Turbofan Engines
Document Number: 2011-28352
Type: Rule
Date: 2011-11-02
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Rolls- Royce Corporation (RRC) AE 3007A, AE 3007A1/1, AE 3007A1, AE 3007A1/3, AE 3007A1E, AE 3007A1P, and AE 3007A3 turbofan engines. This AD requires initial and repetitive eddy current inspections (ECI) of certain 6th-through-13th stage compressor wheel knife edge seals, and initial and repetitive ECIs of the compressor wheel outer circumference, for cracks. This AD was prompted by reports of low-cycle fatigue cracks found during shop visits, in the 6th-through-13th stage compressor wheels having chrome-carbide coated or uncoated knife edge seals. We are issuing this AD to prevent uncontained failure of the 6th-through-13th stage compressor wheel, leading to damage to the airplane.
Amendment of Class E Airspace; Spearfish, SD
Document Number: 2011-28289
Type: Rule
Date: 2011-11-02
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E airspace at Spearfish, SD, to accommodate new Area Navigation (RNAV) Standard Instrument Approach Procedures at Black Hills AirportClyde Ice Field, and updates the geographic coordinates of the airport. There also is a minor correction to the coordinates of controlled airspace 1,200 feet above the surface, and a minor change in the airport name. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.
Capital Project Management
Document Number: 2011-28300
Type: Proposed Rule
Date: 2011-11-01
Agency: Federal Transit Administration, Department of Transportation
FTA is extending the comment period on its proposed rule for Capital Project Management to December 2, 2011, to allow interested parties time to carefully review the Notice of Proposed Rulemaking (NPRM) issued September 13, 2011. Also, FTA will hold a webinar on November 10, 2011, to enable the public to ask questions and to clarify any misunderstandings regarding the NPRM or the Federal Transit Administrator's Dear Colleague letter of September 30, 2011.
Federal Fiscal Year 2012 Annual List of Certifications and Assurances for Federal Transit Administration Grants and Cooperative Agreements
Document Number: 2011-28293
Type: Notice
Date: 2011-11-01
Agency: Federal Transit Administration, Department of Transportation
The Federal Transit Administration (FTA) has consolidated and updated the various pre-award Certifications and Assurances required for its Federal transit assistance (funding) programs in Federal fiscal year (FY) 2012. We (FTA) are now publishing them at Appendix A of this Notice.
Environmental Impact Statement: Cities of South Lake Tahoe, CA and Stateline, NV
Document Number: 2011-28232
Type: Notice
Date: 2011-11-01
Agency: Federal Highway Administration, Department of Transportation
The FHWA is issuing this notice to advise the public that an Environmental Impact Statement will be prepared for a proposed highway realignment project on US Highway 50 (US 50) in the Cities of South Lake Tahoe, California and Stateline, Nevada.
Airworthiness Directives; The Boeing Company Model 737-300, -400, and -500 Series Airplanes
Document Number: 2011-28053
Type: Rule
Date: 2011-11-01
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for certain Model 737-300, -400, and -500 series airplanes. That AD currently requires repetitive inspections for cracking of the 1.04-inch nominal diameter wire penetration hole, and applicable related investigative and corrective actions. This AD reduces the compliance times for those actions. This AD was prompted by 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; and recent reports of multiple adjacent frame cracking found before the compliance time required by the existing AD. Such cracking 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. We are issuing this AD to correct the unsafe condition on these products.
Requested Administrative Waiver of the Coastwise Trade Laws: Vessel SALLY; Invitation for Public Comments
Document Number: 2011-28023
Type: Notice
Date: 2011-11-01
Agency: Maritime Administration, Department of Transportation
As authorized by 46 U.S.C. 12121, the Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.-build requirement of the coastwise laws under certain circumstances. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below.
Reports, Forms and Recordkeeping Requirements; Agency Information Collection Activity Under OMB Review
Document Number: 2011-27978
Type: Notice
Date: 2011-11-01
Agency: National Highway Traffic Safety Administration, Department of Transportation
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 June 24, 2011 [76 FR 37189].
Airworthiness Directives; SOCATA Airplanes
Document Number: 2011-27949
Type: Rule
Date: 2011-11-01
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain SOCATA Model TBM 700 airplanes. 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; Cessna Aircraft Company Airplanes
Document Number: 2011-27596
Type: Rule
Date: 2011-11-01
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Model 525C airplanes. This emergency AD was sent previously to all known U.S. owners and operators of these airplanes. This AD requires replacing certain lithium-ion batteries installed as the main aircraft battery with either a Ni-Cad or a lead acid battery. This AD was prompted by a report of a battery fire that resulted after an energized ground power unit was connected to one of the affected airplanes equipped with a lithium-ion battery as the main aircraft battery. We are issuing this AD to correct the unsafe condition on these products.
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