Department of Transportation May 2015 – Federal Register Recent Federal Regulation Documents

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.

This notice contains a summary of a petition seeking relief from specified requirements of Title 14 of the Code of Federal Regulations. The purpose of this notice is to improve the public's awareness of, and participation in, the FAA's exemption process. 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.

The FAA is withdrawing a previously published direct final rule that would have prohibited fixed-wing special visual flight rules operations at Washington-Dulles International Airport. The FAA is withdrawing this action because it has received an adverse comment.

This action modifies the Class D and Class E airspace at Tri- Cities Airport, Pasco, WA. Controlled airspace is necessary to accommodate the new Area Navigation (RNAV) Global Positioning System (GPS) standard instrument approach procedures at the airport. This action, initiated by the biennial review of the Pasco, WA, enhances the safety and management of IFR operations at the airport.

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.

This notice provides information regarding FHWA's finding that a Buy America waiver is appropriate for the use of non-domestic steel cable nets for truck escape ramps used in a dragnet impact absorption system on State route (SR) 431, US550, and SR163 in the State of Nevada.

This notice contains a summary of a petition seeking relief from specified requirements of Title 14 of the Code of Federal Regulations. The purpose of this notice is to improve the public's awareness of, and participation in, the FAA's exemption process. 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.

We are publishing a new airworthiness directive (AD) for Enstrom Helicopter Corporation (Enstrom) Model F-28A, 280, F-28C, F- 28C-2, F-28C-2R, 280C, F-28F, F-28F-R, 280F, 280FX, and 480 helicopters. This AD was sent previously to all known U.S. owners and operators of these helicopters and supersedes Emergency AD (EAD) 2015- 04-51, dated February 12, 2015. This AD requires inspecting certain main rotor spindles (spindles) for cracks and reporting the inspection results to the FAA. This AD is prompted by a fatal accident and reports of spindles with cracks. The actions specified in this AD are intended to detect a crack in a spindle and prevent loss of a main rotor blade and subsequent loss of control of the helicopter.

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.

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.

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.

This document provides a statement of FAA policy concerning the required use of the Aviation Environmental Design Tool version 2b (AEDT 2b) to analyze noise, fuel burn, and emissions for FAA actions. The policy statement is intended to ensure consistency and quality of analysis performed to assess noise, fuel burn, and emissions impacts of such actions under the National Environmental Policy Act of 1969 (NEPA), as amended, 42 U.S.C. 4321 et seq.

The Federal Aviation Administration (FAA) proposes to fund, construct, and operate a new Airport Traffic Control Tower (ATCT) and Base Building at the General Wayne A. DowningPeoria International Airport (PIA), Peoria, Illinois. The FAA's preferred alternative is to construct the ATCT at a location approximately 1,000 feet east of the PIA terminal building. The purpose of the proposed project is to improve operational efficiency, meet existing and future operational and administrative expansion requirements, and accommodate state-of-the-art equipment upgrades. The need for the project is to provide a replacement ATCT, as the existing ATCT was constructed as part of the original terminal building, which is planned to be demolished. A new ATCT and Base Building at PIA would be able to meet these needs. The FAA has prepared a Draft Environmental Assessment (DEA) in conformance with the requirements of the National Environmental Policy Act of 1969 (NEPA) and FAA Order 1050.1E, Environmental Impacts: Policies and Procedures. The DEA analyzes the potential environmental impacts that may result from construction and operation of the proposed new ATCT and Base Building at the proposed site, as well as the no action alternative (i.e., not constructing and operating the new ATCT).

In accordance with the Paperwork Reduction Act of 1995, PHMSA invites comments on its intention to revise an information collection under Office of Management and Budget (OMB) Control Number 2137-0628, ``Flammable Hazardous Materials by Rail Transportation''. This reporting requirement would require tank car owners to report their progress in the retrofitting of tank cars to the Department of Transportation (DOT).

We propose to supersede airworthiness directive (AD) 2002-13- 11 for Eurocopter France (now Airbus Helicopters) Model EC120B helicopters. AD 2002-13-11 currently requires installing front and side covers on the cabin floor to protect the yaw control at both the pilot and co-pilot stations. Since we issued AD 2002-13-11, we have determined that the required actions should apply only to the cabin's right-hand pilot station. This proposed AD would retain the requirements of AD 2002-13-11 but for only the pilot station. These proposed actions are intended to prevent an object from sliding between the canopy and the cabin floor, loss of yaw control, and subsequent loss of helicopter control.

We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 777 airplanes. This proposed AD was prompted by reports of unreliable performance of the fuel scavenge system. This proposed AD would require changing the main fuel tank water scavenge system, center fuel tank fuel scavenge system, certain electrical panels; related investigative actions, and corrective actions if necessary; and for certain airplanes, changing to give redundant control of the center override/jettison fuel pumps and main jettison fuel pumps. We are proposing this AD to prevent fuel exhaustion and subsequent power loss of all engines due to loss of capability to scavenge fuel in the center fuel tank.

The Surface Transportation Board (Board) will hold a public hearing on June 10, 2015, at its offices in Washington, DC, to further examine issues related to the accessibility of rate complaint procedures for grain shippers.

In compliance with the Paperwork Reduction Act of 1995, this notice announces that the Information Collection Requests (ICRs) abstracted below are being forwarded to the Office of Management and Budget (OMB) for review and comment. The ICRs describes the nature of the information collections and their expected burdens. The Federal Register notice with a 60-day comment period soliciting comments on the following collections of information was published on March 3, 2015 (80 FR 11518).

We propose to adopt a new airworthiness directive (AD) for certain ATR-GIE Avions de Transport R[eacute]gional Model ATR42-500 airplanes, and Model ATR72-102, -202, -212, and -212A airplanes. This proposed AD was prompted by a report of chafed wires between electrical harnesses. This proposed AD would require inspections for wiring discrepancies, and corrective actions if necessary. We are proposing this AD to detect and correct damaged wiring and incorrect installation of the wiring harness and adjacent air ducts, which could lead to wire harness chafing and arcing, possibly resulting in an on-board fire.

We are superseding Airworthiness Directive (AD) 2004-07-11 for all The Boeing Company Model 767-400ER series airplanes. AD 2004-07-11 requires repetitive high frequency eddy current (HFEC) inspections of the aft lower lugs of the deflection control track of the outboard flap for cracks, and replacement of any cracked deflection control track with a new track assembly. This AD retains those requirements, provides optional terminating action for the repetitive inspections, and adds airplane models to the applicability. This AD was prompted by our determination that additional airplane models require repetitive HFEC inspections of the aft lower lugs of the deflection control track of the outboard flap for cracks, and replacement of any cracked deflection control track with a new track assembly. We are issuing this AD to detect and correct fatigue cracking in the aft lower lug run-out region of the deflection control track, which could result in the loss of the secondary load path for the outboard flap, resulting in the loss of the outboard flap and consequent reduced controllability of the airplane in the event that the primary load path also fails.

We are superseding Airworthiness Directive (AD) 2014-26-04 for certain GROB-WERKE Models G115EG and G120A 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 a defective starter solenoid. We are issuing this AD to require actions to address the unsafe condition on these products.