Department of Transportation September 2016 – Federal Register Recent Federal Regulation Documents

This action establishes Class D airspace, Class E surface area airspace, and Class E airspace extending upward from 700 feet above the surface at Brookshire, TX, to accommodate the new air traffic control tower at Houston Executive Airport. The FAA is taking this action for the safe and efficient use of the airspace to contain Instrument Flight Rule (IFR) arrival and departure operations at the airport.

We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 757 airplanes. This proposed AD was prompted by reports of single and multiple uncommanded spoiler panel extensions during flight when there was a hydraulic system failure. This proposed AD would require replacing certain spoiler power control units (PCUs) with new or changed PCUs. We are proposing this AD to prevent an uncommanded extension of spoiler panels in the event of a hydraulic system failure, which could result in loss of control of the airplane.

The Federal Aviation Administration (FAA) is announcing the availability of Advisory Circular (AC) 187-1K which transmits an updated schedule of charges for services of FAA Flight Standards Aviation Safety Inspectors outside the United States. The advisory circular has been updated in accordance with the procedures listed in 14 CFR part 187, Appendix A.

FAA is extending the comment period on the draft FAA Order 5500.1B, Passenger Facility Charge published on August 5, 2016. This draft Order clarifies and updates statutory and regulatory requirements, including those affected by changes to the PFC statute from multiple FAA reauthorizations.

The FHWA is issuing this notice to advise the public that the Record of Decision (ROD) and the Final Environmental Impact Statement (FEIS) for the proposed Interstate 495 (Long Island Expressway) Rest Area Upgrade Project between Exits 51 & 52 (eastbound) in the Town of Huntington, Suffolk County, New York (NYSDOT Project Identification Number: 0229.14) are being rescinded.

The FAA is issuing this notice to advise the public of a meeting of Twenty Seventh Meeting of SC-217 Aeronautical Databases.

This document requests comments on data about passenger motor vehicle thefts that occurred in calendar year (CY) 2014, including theft rates for existing passenger motor vehicle lines manufactured in model year (MY) 2014. The preliminary theft data indicate that the vehicle theft rate for MY/CY 2014 vehicles (1.1525 thefts per thousand vehicles) decreased by 0.32 percent from the theft rate for MY/CY 2013 vehicles (1.1562 thefts per thousand vehicles). Publication of these data fulfills NHTSA's statutory obligation to periodically obtain accurate and timely theft data, and publish the information for review and comment.

We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A319-115, A319-132, A320-214, A320-232, A321-211, A321-213, and A321-231 airplanes. This proposed AD was prompted by a report of certain tie rod assemblies installed on the hinged fairing assembly of the main landing gear (MLG) with no cadmium plating on the rod end threads. This proposed AD would require a detailed inspection of certain tie rod assemblies installed on the hinged fairing assembly of the MLG for the presence of cadmium plating, and replacement of tie rod assemblies without cadmium plating. We are proposing this AD to detect and correct the absence of cadmium plating on the rod end threads of the tie rod assemblies. The absence of cadmium plating could lead to galvanic corrosion of the tie rod end threads, resulting in rod end failure, loss of a MLG door, and consequent damage to the airplane.

The FAA is issuing this notice to advise the public of a meeting of Twenty Seventh Meeting of SC-217 Aeronautical Databases.

We are superseding Airworthiness Directive (AD) 2005-15-07 for certain Airbus Model A320-111 airplanes and Model A320-200 series airplanes. AD 2005-15-07 required installing insulator and cable ties to the electrical cables of the S routes at the gaps in the raceway in the wing trailing edge and the wing tip and wing root areas. This new AD requires additional modifications in the trailing edges of both wings. This new AD also removes airplanes from the applicability. This AD was prompted by reports of wire chafing in the left-hand wing trailing edge. We are issuing this AD to prevent wire chafing in the trailing edge of the wings, which could result in a short circuit in the vicinity of the fuel tanks, consequently resulting in a potential source of ignition in a fuel tank vapor space and consequent fuel tank explosion.

We are adopting a new airworthiness directive (AD) for Viking Air Limited Models DHC-2 Mk. I, DHC-2 Mk. II, and DHC-2 Mk. III 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 corrosion of the elevator control rod and of the elevator actuating lever on the control column. We are issuing this AD to detect and correct corrosion and/or cracking of the elevator control rod assemblies and the elevator actuating lever, which if not detected and corrected, could cause these components to fail. This failure could result in loss of control.

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 is being forwarded to the Office of Management and Budget (OMB) for review and comments. A Federal Register notice (81 FR 13874) with a 60-day comment period soliciting comments on the proposed information collection for the agency's existing collection of vehicle safety information (OMB Control Number 2127-0629) was published on March 15, 2016. No comments were received.

This notice describes a proposed order through which the Federal Aviation Administration plans to designate a certain category of information as protected from public disclosure pursuant to a Voluntary Disclosure Reporting Program. The Federal Aviation Administration is required to protect the information from disclosure to the public, including disclosure required by statute, such as the Freedom of Information Act, following issuance of an order designating the information as protected. The instant designation is intended to encourage participation in the Voluntary Disclosure Reporting Program.

This notice provides information regarding FHWA's finding that a Buy America waiver is appropriate for the use of non-domestic iron and steel components of electric vehicle DC fast charging stations with maximum power (50 kw), voltage range (200-500 VDC), and current output (165 ADC) in the State of Massachusetts.

On August 17, 2016, National Express LLC (National Express or Applicant), a non-carrier, filed an application under 49 U.S.C. 14303 to acquire control of New Dawn Transit, LLC (New Dawn). The Board is tentatively approving and authorizing 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 at 49 CFR 1182.5 & 1182.8.

We propose to adopt a new airworthiness directive (AD) for certain Mitsubishi Heavy Industries, Ltd. Models MU-2B-10, MU-2B-15, MU-2B-20, MU-2B-25, MU-2B-26, MU-2B-26A, MU-2B-30, MU-2B-35, MU-2B-36, MU-2B-36A, MU-2B-40, and MU-2B-60 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 cracks found in the wing spacer plates. We are issuing this proposed AD to require actions to detect and correct cracks in the wing spacer plates, which could result in reduced structural integrity of the wings and loss of control.

We are superseding Airworthiness Directive (AD) 2008-19-08, for all Dassault Aviation Model Falcon 10 airplanes. AD 2008-19-08 required repetitive replacement of the flexible hoses installed in the wing (slat) anti-icing system with new hoses. This new AD requires reducing the life limit of these flexible hoses, which reduces the repetitive replacement intervals. This AD was prompted by additional reports of collapse of the flexible hoses installed in the slat anti- icing systems on airplanes equipped with new, improved hoses. We are issuing this AD to prevent collapse of the flexible hoses in the slat anti-icing system, which could lead to insufficient anti-icing capability and, if icing is encountered in this situation, could result in reduced controllability of the airplane.

Under the provisions of Title 49, U.S.C. 47153(d), notice is being given that the FAA is considering a request from the Massachusetts Port Authority (MPA) in East Boston, MA, to waive the surplus property requirements for approximately 7.1 acres of airport property located at Hanscom Field in Bedford, MA. The subject parcel has been identified for commercial development and MPA will negotiate a long term lease to generate non-aviation revenue for the airport. As such, MPA is requesting a release to change the property from aeronautical use to non-aeronautical use. It has been determined through study and master planning that the subject parcel will not be needed for future aeronautical purposes. Further, the parcel of land is separated by a road and not contiguous to the airport proper. Full and permanent relief of the surplus property requirements on this parcel will allow the airport to generate long term revenue through lease of the land. All lease revenue will continue to be subject to the FAAs revenue-use policy and dedicated to the maintenance and operation of Hanscom Field.

The FAA is issuing this notice to advise the public of a meeting of the Nineteenth Meeting of the NextGen Advisory Committee (NAC).

We are adopting a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model A109A, A109A II, A109C, A109E, A109K2, A109S, and AW109SP helicopters. This AD requires visually inspecting the tail rotor drive shaft assembly (drive shaft) for a crack. This AD was prompted by the discovery of three cracks on the drive shaft of a Model A109S helicopter. The actions of this AD are intended to detect a crack on the drive shaft to prevent failure of the driveshaft, failure of the tail rotor, and subsequent loss of helicopter control.

We are superseding Airworthiness Directive (AD) 90-11-05 for certain Airbus Model A300 B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4- 203 airplanes and Model A300 B4-600 series airplanes. AD 90-11-05 required repetitive detailed inspections for cracking in the aft hinge brackets of the outer shroud box that is located in the outer wing box, and related investigative and corrective actions if necessary. This new AD changes certain compliance times and adds airplanes to the applicability. This AD was prompted by reports of cracks in the aft hinge brackets of the outer shroud box that is located in the outer wing box, which were found during routine maintenance checks, and our subsequent determination that a change in inspection compliance times is needed. We are issuing this AD to detect and correct cracking of the aft hinge brackets of the outer shroud box; such cracking could affect the structural integrity of the airplane.

The FAA proposes to rule and invite public comment for a land release of a 6.1 acre airport owned parcel, not contiguous with the airport, located at 1612 Coates Avenue, Holbrook, NY.

The FAA is correcting an error, whereby the applicability of a regulation was extended instead of its effectivity. Consequently, a section of the pertinent regulation was relocated in Title 14, Code of Federal Regulations and all remaining provisions of the regulation inadvertently expired. However, the entire regulation was intended to be extended for four years in the final rule published on July 25, 2016 (Doc. No. 2016-17427, 81 FR 48323), which became effective on August 7, 2016.