Department of Transportation 2016 – Federal Register Recent Federal Regulation Documents
Results 2,151 - 2,200 of 3,058
Notice of Buy America Waiver for a Radio Communications System
In response to the request of the Kansas City Area Transportation Authority (KCATA) for a Buy America waiver for a DMR Tier III Trunked UHF Voice radio system that is compatible with its current system, the Federal Transit Administration (FTA) hereby waives its Buy America requirements finding that the materials for which a waiver is requested are not produced in the United States in sufficient and reasonably available quantities and of a satisfactory quality. This waiver is limited to a single procurement by KCATA for the DMR Tier III Trunked UHF Voice radio system.
Notice of Buy America Waiver for Special Trackwork Turnout Switch Components.
In response to the request of the Detroit Transportation Corporation (DTC) for a Buy America non-availability waiver for the procurement of two special trackwork turnout switch components (switch), the Federal Transit Administration (FTA) hereby waives its Buy America requirements, finding that the materials for which the waiver is requested are not produced in the United States in sufficient and reasonably available quantities and of satisfactory quality. This waiver is limited to the procurement by DTC for the switch.
Notice of Buy America Waiver for Ductless Mini-Split Air Conditioning Systems
In response to requests received from the Indianapolis Public Transportation Corporation (IPTC) for a Buy America non-availability waiver for the procurement of an inverter-driven ductless mini-split system air conditioner; the York Adams Transportation Authority (YATA) for ductless split system air conditioning units; the Key West Transit (KWT) for a ductless mini-split mechanical system for the City of Key West Public Transportation Facility; and the Springfield Redevelopment Authority (SRA) for ductless mini-split air conditioners for the Union Station Regional Intermodal Transportation Center in Springfield, Massachusetts, the Federal Transit Administration (FTA) hereby waives its Buy America requirements, finding that the materials for which the waivers are requested are not produced in the United States in sufficient and reasonable quantities and of satisfactory quality. This waiver is limited to the specific procurements identified herein.
Notice of Buy America Waiver for Steel Excavator With a Continuous Wield Platform
In response to the request of Metro North Railroad (MNR) for a Buy America non-availability waiver for the procurement of a steel excavator with a continuous wield platform (CWP), the Federal Transit Administration (FTA) hereby waives its Buy America requirements, finding that the materials for which the waiver is requested are not produced in the United States in sufficient and reasonably available quantities and of satisfactory quality. This waiver is limited to a single procurement by MNR for the CWP.
Marine Highway Projects Open Season
The U.S. Department of Transportation (DOT) and Maritime Administration (MARAD) announce that the period for Marine Highway project submissions is being extended to December 31, 2018 (Open Season). The purpose of this notice is to extend the invitation to interested organizations to submit Marine Highway project applications to DOT for review and consideration.
Notice of Request To Release Airport Property
The FAA proposes to rule and invites public comment on the release of land at the Hebron Municipal Airport (HJH), Hebron, Nebraska, under the provisions of 49 U.S.C. 47107(h)(2).
Denial of Motor Vehicle Defect Petition
This notice sets forth the reasons for the denial of a petition submitted to NHTSA under 49 U.S.C. 30162, requesting that the agency commence a proceeding to determine the existence of a defect related to motor vehicle safety in 2015 Volvo VNL 780 vehicles. After a review of the petition and other information, NHTSA has concluded that further expenditure of the agency's investigative resources on the issues raised by the petition does not appear warranted. The agency accordingly has denied the petition. The petition is hereinafter identified as DP15-006.
Request for Information
Section 24105 of the Fixing America's Surface Transportation (FAST) Act, Public Law 114-94 (2015), requires NHTSA to implement a two-year pilot program to evaluate the feasibility and effectiveness of a State process for informing consumers of open motor vehicle recalls at the time of motor vehicle registration. This notice requests information from interested parties to help inform the agency's approach as it moves forward to implement the pilot program.
Federal Aviation Administration
The FAA proposes to rule and invites public comment on the release of land at The Des Moines International Airport, Des Moines, Iowa, under the provisions of 49 U.S.C. 47107(h)(2).
Deadline for Notification of Intent To Use the Airport Improvement Program (AIP) Primary, Cargo, and Nonprimary Entitlement Funds Available to Date for Fiscal Year 2016
The Federal Aviation Administration (FAA) announces May 2, 2016, as the deadline for each airport sponsor to notify the FAA whether or not it will use its fiscal year 2016 entitlement funds available under Section 47114 of Title 49, United States Code, to accomplish Airport Improvement Program (AIP) eligible projects that the airport sponsor previously identified through the Airports Capital Improvement Plan (ACIP) process during the preceding year. The airport sponsor's notification must address all entitlement funds available to date for fiscal year 2016, as well as any entitlement funds not obligated from prior years. After Friday, July 1, 2016, the FAA will carry-over the remainder of currently available entitlement funds, and these funds will not be available again until at least the beginning of fiscal year 2017. Currently, the AIP has 79 percent of the entitlements available through July 15, 2016. If congressional action is taken on future extensions which provide for additional current year and protected entitlements (the remaining 21 percent), the FAA will then work with airport sponsors to adjust accordingly. This notification requirement does not apply to non- primary airports covered by the block-grant program.
Office of Commercial Space Transportation; Notice of Availability of the Final Environmental Assessment (Final EA), Finding of No Significant Impact (FONSI)/Record of Decision (ROD) for the Kodiak Launch Complex Launch Pad 3, Kodiak Island, Alaska
In accordance with the National Environmental Policy Act of 1969, as amended (NEPA; 42 United States Code 4321 et seq.), Council on Environmental Quality NEPA implementing regulations (40 CFR parts 1500 to 1508), and FAA Order 1050.1E, Change 1, Environmental Impacts: Policies and Procedures, the FAA is announcing the availability of the Final EA and FONSI/ROD for the Kodiak Launch Complex Launch Pad 3.
Guidelines for the Safe Deployment and Operation of Automated Vehicle Safety Technologies
NHTSA is announcing a second public meeting to seek input on planned guidelines for the safe deployment and operation of automated vehicles. NHTSA held its first public meeting on this topic on April 8, 2016, in Washington, DC. The intent of the operational guidelines is to encourage innovative and safe deployment of automated vehicle technologies. At this meeting, NHTSA is seeking public input on those aspects of automated vehicle (AV) systems that would benefit from operational guidelines. For example, of high importance to the Agency is information on the roadway scenarios and operational environments highly automated vehicles will need to address and the associated design and evaluation processes and methods needed to ensure that AV systems can detect and appropriately react to these scenarios such that a high level of safety is assured when these systems are deployed on US roadways. Also of interest to the Agency is input on aspects of automated vehicle technology that may not be suitable or ready for guidelines. For these areas, information would be useful on alternative approaches to assure safety.
Transit-Oriented Development Planning Pilot Program
The Federal Transit Administration (FTA) announces the availability of $20.49 million of Fiscal Year (FY) 2014, FY 2015 and FY 2016 funds under the Pilot Program for Transit-Oriented Development (TOD) Planning as authorized under Section 20005(b) of the Moving Ahead for Progress in the 21st Century Act (MAP-21), Public Law 112-141, July 6, 2012, with funding provided under 49 U.S.C. 5338(a)(2)(B), as amended by the Fixing America's Surface Transportation (FAST) Act. The program augments FTA's Fixed Guideway Capital Investment Grants (CIG) Program by supporting comprehensive planning associated with new fixed guideway and core capacity improvement projects. This notice solicits proposals to compete for FY 2014, FY 2015 and FY 2016 funding under the Pilot Program for TOD Planning and may include additional funds made available under future appropriations. It outlines the process to apply for funding, identifies FTA's priorities for these competitive funds, and establishes the criteria FTA will use to identify meritorious projects for funding. This announcement is available on the FTA Web site at: https://www.fta.dot.gov. FTA may announce final selections on the Web site and in the Federal Register. Additionally, a synopsis of this funding opportunity will be posted in the FIND module of the government-wide electronic grants (GRANTS.GOV) Web site at https://www.grants.gov.
Limitation on Claims Against Proposed Public Transportation Projects
This notice announces final environmental actions taken by the Federal Transit Administration (FTA) for projects in New York, NY; North Brunswick Township and City of New Brunswick, NJ; and Cobb and Fulton Counties, GA. 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.
Airworthiness Directives; Bombardier Inc. Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440), CL-600-2C10 (Regional Jet Series 700, 701, & 702), CL-600-2D15 (Regional Jet Series 705), CL-600-2D24 (Regional Jet Series 900), and CL-600-2E25 (Regional Jet Series 1000) airplanes. This proposed AD was prompted by reports of undesirable changes in the Reference Airspeed (RAS) Bug, occurring during flight without pilot input. This proposed AD would require replacing the flight control computer (FCC). We are proposing this AD to prevent uncommanded pitch changes, which could result in deviation from a safe flight path.
Research, Engineering and Development Advisory Committee Meeting
The FAA is issuing this notice to advise the public of the Research, Engineering and Development Advisory Committee meeting. The notice was previously published (81 FR 18933) in the April 1, 2016 issue of the Federal Register.
Airworthiness Directives; Airbus Airplanes
We propose to supersede Airworthiness Directive (AD) 2012-20- 07, for certain Airbus Model A318, A319, A320, and A321 series airplanes. AD 2012-20-07 currently requires revising the airworthiness limitations section (ALS) of the instructions for continued airworthiness (ICA) to incorporate new limitations for fuel tank systems, and revising the maintenance program to incorporate revised fuel maintenance and inspection tasks. Since we issued AD 2012-20-07, Airbus has issued more restrictive maintenance requirements and/or airworthiness limitations. This proposed AD would require revising the maintenance or inspection program to incorporate revised fuel airworthiness limitations. We are proposing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
Hazardous Materials: Notice of Applications for Special Permits
In accordance with the procedures governing the application for, and the processing of, special permits from the Department of Transportation's Hazardous Material Regulations (49 CFR part 107, subpart B), notice is hereby given that the Office of Hazardous Materials Safety has received the application described herein. Each mode of transportation for which a particular special permit is requested is indicated by a number in the ``Nature of Application'' portion of the table below as follows: 1Motor vehicle, 2Rail freight, 3Cargo vessel, 4Cargo aircraft only, 5Passenger-carrying aircraft.
Notice of Request To Release Airport Property
The FAA proposes to rule and invites public comment on the release of land at the Humboldt Municipal, Humboldt, Iowa, under the provisions of 49 U.S.C. 47107(h)(2).
Developing Evidence Based Fatigue Risk Management Guidelines for Emergency Medical Services: First Expert Panel Meeting
The National Highway Traffic Safety Administration (NHTSA) is announcing the first in a series of expert panel meetings to develop evidence based guidelines for fatigue management in the Emergency Medical Services (EMS) community. This meeting will focus on generating research questions germane to fatigue mitigation in EMS settings as well as inclusion criteria for the evidence based guideline literature review. Members of the public are encouraged to attend the meeting and make comments about the topic during times set aside specifically for this purpose. Due to space limitations, attendance at the meeting is limited to invited participants and those who register in advance at www.emsfatigue.org. Written comments can also be made on https:// www.regulations.gov (Docket No. NHTSA-2015-0121).
Airworthiness Directives; International Aero Engines AG Turbofan Engines
We propose to adopt a new airworthiness directive (AD) for certain International Aero Engines AG (IAE) V2500-A1 turbofan engines. This proposed AD was prompted by a report of an uncontainment caused by a high-pressure turbine (HPT) seal release. This proposed AD would require removing from service the HPT No. 4 bearing front seal seat, part numbers (P/Ns) 2A0066, 2A1998, and 2A3432, and the HPT No. 4 bearing rear seal seat, P/Ns 2A0067, 2A1999, and 2A3433, and replacement with parts eligible for installation. This proposed AD would also require inspecting the HPT rotor and stator assembly, and, if necessary, their replacement with parts that are eligible for installation. We are proposing this AD to prevent failure of the HPT stage 2 seals, uncontained HPT seal release, damage to the engine, and damage to the airplane.
Notice To Rescind a Notice of Intent for an Environmental Impact Statement for the Kake Access Project in Southeast Alaska
A Notice of Intent (NOI) to prepare an Environmental Impact Statement (EIS) was published in the Federal Register on January 22, 2013. The FHWA is issuing this notice to advise the public that FHWA and the Alaska Department of Transportation and Public Facilities (ADOT&PF) will no longer prepare an EIS for the Kake Access project. The purpose of the Kake Access project was to provide Kake residents with more frequent, faster and cost effective surface transportation access to medical facilities, goods and services, education facilities, and economic opportunities not available in Kake.
Aerospace Fuel, Engine Oil, and Hydraulic Hose Assemblies
This notice announces the Federal Aviation Administration's (FAA) intent to cancel the following Technical Standard Orders (TSOs): -C42, Propeller Feathering Hose Assemblies; -C53c, Fuel and Engine Oil System Hose Assemblies; and -C75, Hydraulic Hose Assemblies. The intent is to combine the updated requirements of the aforementioned TSOs into TSO-C140, Aerospace Fuel, Engine Oil, and Hydraulic Hose Assemblies. The impact of cancelling these TSOs will not affect current design or production approvals for an existing TSO-C42, -C53c, or -C75 authorization (TSOA). However, modifications to TSO-C42, -C53c, and - C75 TSOAs will no longer be accepted after the effective cancellation date. Generally, we will not accept applications for the previous revisions after the cancellation date of these TSOs. We may do so, however, up to six months after publication of this cancellation notice if we know that work was being done against the prior minimum performance standard before the cancellations became effective. Articles approved under those cancelled TSOAs may continue to be produced under the provisions of their original approvals.
Reports, Forms and Record Keeping Requirements; Agency Information Collection Activity Under OMB Review
This document corrects the docket number in a Federal Register notice published on Friday, December 4, 2015, that announced a request for public comment on proposed collection of information.
Establishment of Class E Airspace, South Bend, WA
This action corrects administrative errors in a final rule published in the Federal Register of March 8, 2016, that establishes Class E airspace at Willapa Harbor Heliport, South Bend, WA, by amending the assigned paragraph for rule incorporation within FAA Order 7400.9Z, by correcting format errors in the text header of the airspace legal description, and by correcting inconsistent airport name information in the airspace legal description. These changes do not affect the boundaries or operating requirements of the airspace.
Proposed Amendment of Class D and E Airspace and Revocation of Class E Airspace; Sioux City, IA
This action proposes to amend Class D and E airspace at Sioux Gateway/Col. Bud Day Field, Sioux City, IA, due to the decommissioning of the Gateway non-directional radio beacon (NDB) and cancellation of the NDB approaches at the airport. The Class E airspace area designated as an extension would be removed as it is no longer needed. Advances in Global Positioning System (GPS) capabilities have made this action necessary for the safety and management of Instrument Flight Rules (IFR) operations at the airport. This action also would update the geographic coordinates for Martin Field, NE, to coincide with the FAA's aeronautical database.
Proposed Amendment of Class E Airspace for the Following Louisiana Towns; De Quincy, LA; Minden, LA; Slidell, LA; and Revocation of Class E Airspace; Homer, LA
This action proposes to modify Class E airspace extending upward from 700 feet above the surface at De Quincy Industrial Airpark, De Quincy, LA; Minden-Webster Airport, Minden, LA; and Slidell, Airport, Slidell, LA. Decommissioning of non-directional radio beacon (NDB), cancellation of NDB approaches, and implementation of area navigation (RNAV) procedures have made this action necessary for the safety and management of Instrument Flight Rules (IFR) operations at the above airports. This action also proposes to remove Class E airspace extending upward from 700 feet above the surface at Homer Municipal Airport, Homer, LA, as controlled airspace is no longer needed. Additionally, the geographic coordinates at De Quincy Industrial Airpark, Minden-Webster Airport, and Slidell Airport would be adjusted to coincide with the FAA's aeronautical database.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for certain Airbus Model A330-223F and -243F airplanes. This AD was prompted by a report of missing fasteners in certain locations of the fuselage during production. This AD would require inspecting for missing, damaged, or incorrectly installed fasteners; and corrective actions if necessary. We are issuing this AD to detect and correct cracking of the fuselage due to missing, damaged, or incorrectly installed fasteners, which could result in reduced structural integrity of the fuselage.
Airworthiness Directives; The Boeing Company Airplanes
We are revising an earlier proposed airworthiness directive (AD) for certain The Boeing Company Model 767-200, -300, and -400ER series airplanes. The NPRM proposed an inspection for plastic couplings, corrective actions if necessary, and installation of new spray shrouds. The NPRM was prompted by a report of the engine indication and crew alerting system (EICAS) display system malfunctioning during flight. This action revises the NPRM by adding, for certain airplanes, a general visual inspection of the spray shield and related investigative and corrective actions if necessary. We are proposing this supplemental NPRM (SNPRM) to prevent an uncontrolled water leak from a defective potable water system coupling, which could cause the main equipment center (MEC) line replaceable units (LRUs) to become wet, resulting in an electrical short and potential loss of several functions essential for safe flight. Since these actions impose an additional burden over that proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.
Airworthiness Directives; The Boeing Company Airplanes
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 777-200, -200LR, -300, and -300ER series airplanes. This AD was prompted by reports of fractured forward attach fittings of the inboard flap outboard aft flap track. The fractured fittings were determined to be the result of corrosion pits forming on the inside diameter of the fittings. This AD requires an inspection for the affected part number and serial number of the main flap; various additional repetitive inspections of the fitting, if necessary; and replacement of the fitting or nested bushing installation, if necessary, which would terminate the inspections. This AD also provides an optional terminating action for the repetitive inspections. We are issuing this AD to detect and correct fracture of the fitting, which could result in the loss of the inboard aft flap and could lead to a punctured fuselage, causing injury to the flightcrew and passengers, and damage to the airplane.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for certain Airbus Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300- 600 series airplanes), modified by a particular supplemental type certificate (STC). This AD was prompted by a report of chafing found on the overflow sensor harness of the surge tank, and subsequent contact between the electrical wiring and fuel tank structure. This AD requires a one-time inspection for damage of the outer tank overflow sensor harness, and repair if necessary. This AD also requires modification of the sensor harness. We are issuing this AD to prevent chafing of the harness and subsequent contact between the electrical wiring and fuel tank structure, which could result in electrical arcing and a fuel tank explosion.
Airworthiness Directives; Dassault Aviation
We propose to adopt a new airworthiness directive (AD) for certain Dassault Aviation Model FALCON 7X airplanes. This proposed AD was prompted by investigation results that determined that a certain thickness of the fuel tank panels is insufficient to meet the certification requirements. This proposed AD would require inspecting the thickness of the fuel tank panels, and repair if necessary. We are proposing this AD to detect and correct improper thickness of the fuel tank panels. Improper thickness increases the risk of damaging and puncturing a fuel tank wall panel as a result of a high energy lightning strike, which could lead to loss of electrical power and/or other essential functions, possibly resulting in reduced control of the airplane or ignition of a fuel tank.
Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes
We propose to adopt a new airworthiness directive (AD) for all Airbus Defense and Space S.A. Model CN-235, CN-235-200, and CN-235-300 airplanes. This proposed AD was prompted by reports of main landing gear (MLG) access doors detaching from the airplane as a result of excessive vibration and metal fatigue in the attach fittings. This proposed AD would require modification of the MLG access door by replacing seals in the MLG fairing and, for certain airplanes, adding an additional bolt. We are proposing this AD to prevent a fracture in the MLG access door associated with excessive vibration and metal fatigue in the attach fittings. This condition could lead to MLG access door detachment and consequent impact of flight controls, resulting in reduced control of an airplane.
Airworthiness Directives; Bombardier, Inc. Airplanes
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes, Model CL-600-2D15 (Regional Jet Series 705) airplanes, Model CL-600-2D24 (Regional Jet Series 900) airplanes, and Model CL- 600-2E25 (Regional Jet Series 1000) airplanes. This AD was prompted by the discovery of a number of incorrectly calibrated angle of attack (AOA) transducers installed in the stall protection system. This AD requires replacement of affected AOA transducers. We are issuing this AD to detect and replace incorrectly calibrated AOA transducers; incorrect calibration of the transducers could result in late activation of the stick pusher.
Airworthiness Directives; The Boeing Company Airplanes
We are superseding Airworthiness Directive (AD) 2013-22-11 for certain The Boeing Company Model 747-400 and -400D series airplanes. AD 2013-22-11 required repetitive inspections to detect cracks in the floor panel attachment fastener holes of certain upper deck floor beam upper chords, repetitive inspections, corrective actions if necessary, and replacement of the upper deck floor beam upper chords. Since we issued AD 2013-22-11, we received a report that certain fastener holes in the upper deck floor beam upper chords may not have been inspected in accordance with AD 2013-22-11. This AD adds additional repetitive inspections for cracks for certain airplanes, and corrective actions if necessary. We are issuing this AD to detect and correct fatigue cracking in certain upper chords of the upper deck floor beam. Such cracks could become large and cause the floor beams to become severed and result in rapid decompression or reduced controllability of the airplane.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for all Airbus Model A330-200, -200 Freighter, and -300 series airplanes, and all Airbus Model A340-200, -300, -500, and -600 series airplanes. This AD was prompted by a report of blockage of Angle of Attack (AOA) probes during climb, leading to activation of the Alpha Protection (Alpha Prot) while the Mach number increased. This activation could cause a continuous nose-down pitch rate that cannot be stopped with backward sidestick input, even in the full backward position. For certain airplanes, this AD requires replacing certain AOA sensors (probes) with certain new AOA sensors. For certain other airplanes, this AD also requires inspections and functional heat testing of certain AOA sensors for discrepancies, and replacement if necessary. We are issuing this AD to prevent erroneous AOA information and Alpha Prot activation due to blocked AOA probes, which could result in a continuous nose-down command and loss of control of the airplane.
Airworthiness Directives; SOCATA Airplanes
We are superseding airworthiness directive (AD) 92-06-10 for SOCATA Models MS 880B, MS 885, MS 892A-150, MS 892E-150, MS 893A, MS 893E, MS 894A, MS 894E, Rallye 100S, Rallye 150ST, Rallye 150T, Rallye 235E, and Rallye 235C 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 fatigue failure of the nose landing gear wheel axle. We are issuing this AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; Airbus Helicopters (formerly Eurocopter France)
We are adopting a new airworthiness directive (AD) for Airbus Helicopters Model SA341G and SA342J helicopters. This AD requires repetitive inspections of a certain part-numbered main rotor hub torsion bar (torsion bar). This AD was prompted by several cases of corrosion in the metal strands of the torsion bar. The actions of this AD are intended to detect corrosion and prevent failure of the torsion bar, loss of a main rotor blade, and subsequent loss of control of the helicopter.
Airworthiness Directives; The Boeing Company Airplanes
We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787-8 airplanes. This AD was prompted by reports indicating that the ram air turbine (RAT) assembly may fail to operate if deployed at low airspeeds. This AD requires replacing either the RAT pump and control module assembly or the entire RAT assembly. We are issuing this AD to prevent failure of the RAT assembly to operate at low air speeds. The volume fuse on the RAT assembly may be activated in-flight before the RAT is deployed. This may lead to improper pump hydraulic pressure offloading when the RAT is needed. Failure of the RAT to operate in an all engine out event would result in loss of control of the airplane.
Aviation Training Device Credit for Pilot Certification
This rulemaking relieves burdens on pilots seeking to obtain aeronautical experience, training, and certification by increasing the allowed use of aviation training devices. These actions are necessary to bring the regulations in line with the current capabilities of aviation training devices and the needs and activities of the general aviation training community and pilots.
Continental Tire the Americas, LLC, Grant of Petition for Decision of Inconsequential Noncompliance
Continental Tire the Americas, LLC (CTA), has determined that certain Continental Tire brand T-type spare tires do not fully comply with paragraph S4.3(a) of Federal Motor Vehicle Safety Standard (FMVSS) No. 109, New Pneumatic and Certain Specialty Tires. CTA has filed a report dated August 25, 2015 and amended on October 1, 2015, pursuant to 49 CFR part 573, Defect and Noncompliance Responsibility and Reports.
Mercedes-Benz USA LLC, Denial of Petition for Decision of Inconsequential Noncompliance
Mercedes-Benz USA LLC (MBUSA), on behalf of itself and its parent company Daimler AG (DAG), collectively referred to as ``Mercedes'' has determined that certain model year (MY) 2015 Mercedes- Benz C-Class (205 Platform) passenger cars do not fully comply with paragraph S10.18.4 of Federal Motor Vehicle Safety Standard (FMVSS) No. 108, Lamps, Reflective Devices, and Associated Equipment. Mercedes has filed a report dated February 9, 2015, pursuant to 49 CFR part 573, Defect and Noncompliance Responsibility and Reports. Mercedes then petitioned NHTSA under 49 CFR part 556 requesting a decision that the subject noncompliance is inconsequential to motor vehicle safety.
Morgan 3 Wheeler Limited, Denial of Petition for Decision of Inconsequential Noncompliance
Morgan 3 Wheeler Limited (Morgan) has determined that certain model year (MY) 2012 and 2013 Morgan model M3W three-wheeled motorcycles do not comply with all of the requirements of Federal Motor Vehicle Safety Standard (FMVSS) No. 108, Lamps, reflective devices, and associated equipment. Specifically, the vehicles' headlamps are spaced further apart than permitted, and do not have the required ``DOT'' marking. Morgan has petitioned for an exemption from the recall notification and remedy requirements of 49 U.S.C. Chapter 301``Motor Vehicle Safety'' (Vehicle Safety Act) on the grounds that the noncompliances are inconsequential to motor vehicle safety. This notice announces and explains NHTSA's denial of Morgan's petition.
Qualification of Drivers; Exemption Applications; Vision
FMCSA announces receipt of applications from 11 individuals for exemption from the vision requirement in the Federal Motor Carrier Safety Regulations. They are unable to meet the vision requirement in one eye for various reasons. The exemptions will enable these individuals to operate commercial motor vehicles (CMVs) in interstate commerce without meeting the prescribed vision requirement in one eye. If granted, the exemptions would enable these individuals to qualify as drivers of commercial motor vehicles (CMVs) in interstate commerce.
Qualification of Drivers; Exemption Applications; Diabetes Mellitus
FMCSA announces receipt of applications from 46 individuals for exemption from the prohibition against persons with insulin-treated diabetes mellitus (ITDM) operating commercial motor vehicles (CMVs) in interstate commerce. If granted, the exemptions would enable these individuals with ITDM to operate CMVs in interstate commerce.
Qualification of Drivers; Exemption Applications; Vision
FMCSA announces receipt of applications from 25 individuals for exemption from the vision requirement in the Federal Motor Carrier Safety Regulations. They are unable to meet the vision requirement in one eye for various reasons. The exemptions will enable these individuals to operate commercial motor vehicles (CMVs) in interstate commerce without meeting the prescribed vision requirement in one eye. If granted, the exemptions would enable these individuals to qualify as drivers of commercial motor vehicles (CMVs) in interstate commerce.
Stop Signal Overruns
The Federal Transit Administration (FTA) issued Safety Advisory 16-1 regarding stop signal overruns on rail fixed guideway public transportation systems, and an accompanying letter to the State Safety Oversight (SSO) program managers and the chief safety officers of rail transit systems, seeking data and information on stop signal overruns during 2015. Safety Advisory 16-1 and the accompanying letter are available in their entirety on the FTA public Web site at https://www.fta.dot.gov/tso.html.
Airworthiness Directives; The Boeing Company Airplanes
We propose to adopt a new airworthiness directive (AD) for all The Boeing Company Model 737-600, -700, -700C, -800, and -900 series airplanes. This proposed AD was prompted by reports of paint deterioration on the surface of the main landing gear (MLG) and the early onset of corrosion in the trunnion bore of the MLG outer cylinder. This proposed AD would require identifying affected parts, repetitive external surface detailed inspection for damage of affected parts, and related investigative and corrective actions if necessary. For certain airplanes, this AD also would require a detailed inspection and bushing replacement of the trunnion bore, and related investigative and corrective action if necessary. We are proposing this AD to prevent stress corrosion cracking of the external surfaces of the MLG, which could result in a fracture of the MLG and consequent MLG collapse.
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