Historic Preservation, Advisory Council July 2015 – Federal Register Recent Federal Regulation Documents

The FAA proposes to rule and invite public comment for a change in use from aeronautical to non-aeronautical to provide for the use of an existing facility for manufacturing purposes, at Elmira/ Corning Regional Airport, Horseheads, NY.

The FHWA has forwarded the information collection request described in this notice to the Office of Management and Budget (OMB) for approval of a new information collection. We published a Federal Register Notice with a 60-day public comment period on this information collection on February 19, 2015. We are required to publish this notice in the Federal Register by the Paperwork Reduction Act of 1995.

This document provides the public notice that by a document dated November 21, 2014, Union Pacific Railroad Company (UP) has petitioned the Federal Railroad Administration (FRA) for a waiver of compliance from certain provisions of the Federal railroad safety regulations.

We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model BD-100-1A10 (Challenger 300) airplanes. This proposed AD was prompted by multiple reports of a short circuit between the heater element and the metal sheath of the pitot-static probe heater. This proposed AD would require replacement of the left and right pitot-static probes with newly redesigned left and right pitot-static probes. We are proposing this AD to prevent degradation of the heating ability of the pitot-static probe heater, resulting in erroneous airspeed indication during flight in icing conditions and consequent reduced controllability of the airplane.

This rule establishes, amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures (ODPs) for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System,such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

This notice announces actions taken by Texas Department of Transportation (TxDOT) and Federal agencies that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to a proposed highway project, US 281, from Loop 1604 to Borgfeld Drive in Bexar County in the State of Texas. Those actions grant licenses, permits, and approvals for the project.

FMCSA confirms its decision to exempt 51 individuals from its rule prohibiting persons with insulin-treated diabetes mellitus (ITDM) from operating commercial motor vehicles (CMVs) in interstate commerce. The exemptions enable these individuals to operate CMVs in interstate commerce.

This notice sets forth the reasons for the denial of a petition, DP14-004, submitted by the Center for Auto Safety (the petitioner) to the Administrator of NHTSA by a letter dated August 21, 2014, under 49 CFR part 552. The petition requests the agency to initiate a safety defect investigation into alleged failures of Totally Integrated Power Modules (TIPMs) installed in sport utility vehicles, trucks, and vans built by Chrysler FCA (Chrysler) beginning in the 2007 model year. The petitioner alleges that TIPM defects may result in the following safety defect conditions: Engine stall, airbag non- deployment, failure of fuel pump shutoff resulting in unintended acceleration, and fire. After conducting a technical review of: (1) Consumer complaints and other material submitted by the petitioner; (2) information provided by Chrysler in response to information requests regarding TIPM design, TIPM implementation and the complaints submitted by the petitioner; and (3) Chrysler safety recalls 14V-530 and 15V-115 addressing a fuel pump relay defect condition that may result in engine stall while driving in certain vehicles equipped with TIPM body control modules; and the likelihood that additional investigations would result in a finding that a defect related to motor vehicle safety exists, NHTSA has concluded that further investigation of the issues raised by the petition is not warranted. The agency, accordingly, has denied the petition.

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 January 2, 2015 [80 FR 99].

We propose to supersede Airworthiness Directive (AD) 2012-17- 13, which applies to certain The Boeing Company Model 707 airplanes, and Model 720 and 720B series airplanes. For certain airplanes, AD 2012-17-13 required using redefined flight cycle counts; determining the type of material of the horizontal stabilizer, rear spar, and upper and lower chords on the inboard and outboard ends of the rear spar; repetitively inspecting for cracking of the horizontal stabilizer components; and repairing or replacing the chord, or modifying chord segments made of 7079 aluminum, if necessary. For all airplanes, AD 2012-17-13 required inspecting certain structurally significant items, and repairing discrepancies if necessary. Since we issued AD 2012-17- 13, we have determined that all chord segments made of 7079 aluminum must be replaced with new, improved chord segments made of 7075 aluminum. This proposed AD would add a requirement to replace all chord segments made of 7079 aluminum with new, improved chord segments made of 7075 aluminum. We are proposing this AD to detect and correct stress corrosion and potential early fatigue cracking in the horizontal stabilizer, which could result in reduced structural integrity of the horizontal stabilizer.

We propose to adopt a new airworthiness directive (AD) for all Airbus Model A319-131, -132, and -133 airplanes; Model A320-232 and - 233 airplanes; and Model A321-131, -231, and -232 airplanes. This proposed AD was prompted by reports of forward engine mount attachment pins that were manufactured from discrepant raw material. This proposed AD would require identification and replacement of affected forward engine mount attachment pins. We are proposing this AD to prevent failure of a forward engine mount attachment pin, possible loss of an engine in-flight, and consequent reduced controllability of the airplane.

The Maritime Administration (MARAD), in coordination with the U.S. Coast Guard (USCG), will prepare an environmental impact statement (EIS) as part of the environmental review of the Delfin LNG LLC (Delfin LNG) deepwater port license application. The application proposes the ownership, construction, operation and eventual decommissioning of an offshore liquefied natural gas (LNG) deepwater port export facility that would be located in Federal waters within the Outer Continental Shelf (OCS) West Cameron Area, West Addition Protraction Area (Gulf of Mexico), approximately 37.4 to 40.8 nautical miles off the coast of Cameron Parish, Louisiana, in water depths ranging from approximately 64 to 72 feet (19.5 to 21.9 meters). The deepwater port would consist of four semi-permanently moored floating liquefaction natural gas vessels (FLNGVs), and would reuse and repurpose two existing offshore natural gas pipelines: The former U-T Operating System (UTOS) pipeline and the High Island Operating System (HIOS) pipeline (see Summary of the Application for additional project specifics). The onshore components of the proposed deepwater port would be located in Cameron Parish, Louisiana and would be reviewed by the Federal Energy Regulatory Commission (FERC) under a separate authorization process (see FERC Docket No. CP15-490-000; 80 FR 30226 (May 27, 2015)). The onshore facility would consist of reactivating approximately 1.1 miles of the existing UTOS pipeline; the addition of 74,000 horsepower of new compression and associated metering and regulation facilities; the installation of new supply header pipelines (which would consist of 0.25 miles of new 42-inch pipeline to connect the former UTOS line to the new meter station); and 0.6 miles of new twin 30-inch pipelines between Transco Station 44 and the new compressor station site. Publication of this Notice of Intent (NOI) begins a 30 day scoping process that will help identify and determine the scope of environmental issues to be addressed in the EIS. MARAD and the USCG will consider both the Delfin LNG deepwater port license application and the FERC application to be included in this review. For your convenience, we have included the Delfin LNG application to FERC under docket number USCG-2015-0472. This NOI requests public participation in the scoping process, provides information on how to participate and announces informational open houses and public meetings in Louisiana and Texas. Pursuant to the criteria provided in the Deepwater Port Act of 1974, as amended, 33 U.S.C. 1501 et seq. (the Act), both Louisiana and Texas are the Adjacent Coastal States for this application.

This action confirms the effective date of the direct final rule, request for comments, published on May 27, 2015, and dispositions the one public comment received. The rule amends commercial space transportation regulations to allow an applicant for a license, experimental permit, or safety approval the option of submitting an application electronically.

The Environmental Protection Agency (EPA) and the National Highway Transportation Safety Administration (NHTSA) are announcing public hearings to be held for the joint proposed rules ``Greenhouse Gas Emissions and Fuel Efficiency Standards for Medium- and Heavy-Duty Engines and VehiclesPhase 2,'' and also for NHTSA's Draft Environmental Impact Statement. The proposed rules were published in the Federal Register on July 13, 2015. The Draft Environmental Impact Statement was published on June 19, 2015, and is available on the NHTSA Web site mentioned below. Two hearings will be held on August 6 and August 18, 2015.

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 in the SUPPLEMENTARY INFORMATION section.

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 in the SUPPLEMENTARY INFORMATION section.

This action amends Class E Airspace at Campbellsville, KY as the Taylor County NDB has been decommissioned, requiring airspace redesign at Taylor County Airport. This action enhances the safety and management of Instrument Flight Rules (IFR) operations at the airport.

This action establishes Class E Airspace at Headland, AL, to accommodate new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAPs) serving Headland Municipal Airport. Controlled airspace is necessary for the safety and management of instrument flight rules (IFR) operations at the airport.

This action proposes to modify Class D airspace, Class E surface area airspace, Class E airspace extending upward from 700 feet above the surface, and remove Class E surface area airspace designated as an extension at Mountain Home AFB, Mountain Home, ID. After reviewing the airspace, the FAA found it necessary to increase the Class D airspace area and reduce the Class E airspace areas for the safety and management of Instrument Flight Rules (IFR) operations for arriving and departing aircraft at the airport. This action also would initiate the use of geographic coordinates as reference points instead of navigation aids to describe the controlled airspace areas, and would update the geographic coordinates of Mountain Home Municipal Airport.

We propose to adopt a new airworthiness directive (AD) for Viking Air Limited Model DHC-3 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 reports of corrugation cracking found at various wing stations and on the main spar lower cap. We are issuing this proposed AD to require actions to address the unsafe condition on these products.

We are superseding airworthiness directive (AD) 2014-19-05 for all Turbomeca S.A. Arriel 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2, 1K1, 1S, 1S1, 2B, 2B1, 2C, 2C1, 2C2, 2S1, and 2S2 turboshaft engines. AD 2014-19-05 required an initial one-time vibration check of the engine accessory gearbox (AGB) on certain Arriel 1 and Arriel 2 model engines, and repetitive vibration checks for all Arriel 1 and Arriel 2 engines. This AD was prompted by our determination that we incorrectly identified technical references in AD 2014-19-05. We are issuing this AD to prevent failure of the engine AGB, which could lead to in-flight shutdown and damage to the engine, which may result in damage to the aircraft.

We are superseding Airworthiness Directive (AD) 2013-14-05 for certain The Boeing Company Model 747-400 and 747-400F series airplanes. AD 2013-14-05 required repetitive inspections of the longeron extension fittings for cracking, and related investigative and corrective actions if necessary. This new AD would continue to require the actions specified in AD 2013-14-05, and would add new repetitive high frequency eddy current (HFEC) inspections of any modified, repaired, or replaced longeron extension fitting for cracking, and applicable related investigative and corrective actions if necessary. This AD was prompted by reports of cracking in the outboard flange of the longeron extension fittings, and our determination that more work is necessary on airplanes on which a permanent repair, longeron extension fitting replacement, or modification was accomplished. We are issuing this AD to detect and correct cracks in the longeron extension fittings, which can become large and adversely affect the structural integrity of the airplane.