Department of Transportation May 2019 – Federal Register Recent Federal Regulation Documents

We are adopting a new airworthiness directive (AD) for certain Viking Air Limited Model CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant) airplanes. This AD was prompted by a report that a supplier fabricated Teflon parts with a charge of 15 percent fiberglass content instead of the specified 5 percent fiberglass content. This AD requires repetitive detailed visual inspections of the aileron control system cables and flap interconnect system cables for damage or disconnected cables, corrective actions if necessary, and replacement of the Teflon parts in the aileron control systems, aileron/rudder interconnect, and aileron power unit beam. The replacement of these parts terminates the repetitive inspections. We are issuing this AD to address the unsafe condition on these products.

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD was prompted by reports of cracking in the frame web, frame integral inboard chord, and fail-safe chord on multiple airplanes in multiple locations between stringers S-10 and S- 17 above the passenger floor, in addition to an evaluation by the design approval holder (DAH) indicating that certain fuselage frame splices are subject to widespread fatigue damage (WFD). This AD requires repetitive inspections of certain fuselage upper frames, side frames, fail-safe chords, inboard chords, frame webs, and stringers; an inspection for open tooling holes and the presence of repairs in certain inspection zones; and applicable on-condition actions. We are issuing this AD to address the unsafe condition on these products.

In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request Office of Management and Budget (OMB) renewal approval for information collection 2120-0765. Aircraft registration is necessary to ensure personal accountability among all users of the national airspace system. Aircraft registration also allows the FAA and law enforcement agencies to address non-compliance by providing the means for identifying an aircraft's owner and operator. This collection also permits individuals to de-register or update their record in the registration database.

This action modifies the Class E airspace extending upward from 700 feet above the surface at Manitowoc County Airport, Manitowoc, WI, and Sheboygan County Memorial Airport, Sheboygan, WI. This action is due to an airspace review caused by the decommissioning of the Manitowoc VHF omnidirectional range (VOR), which provided navigation information to the instrument procedures at these airports, as part of the VOR Minimum Operational Network (MON) Program. The geographic coordinates of Sheboygan County Memorial Airport are also being updated to coincide with the FAA's aeronautic database. Airspace redesign is necessary for the safety and management of instrument flight rules (IFR) operations at these airports.

This action proposes to remove Class E airspace extending upward from 700 feet above the surface at Sioux Center Municipal Airport, Sioux Center, IA. The FAA is proposing this action due to the closure of the airport and cancellation of the instrument procedures; and the airspace is longer required.

We propose to supersede Airworthiness Directive (AD) 2002-07- 05, which applies to all Airbus Model A300 B2, A300 B4, A300 B4-600, and A300 B4-600R series airplanes, and Model A300 F4-605R airplanes. AD 2002-07-05 requires repetitive inspections for cracking of certain fittings, corrective action if necessary, and, for certain airplanes, a modification. AD 2002-07-05 also provides an optional terminating action for the repetitive inspections. Since we issued AD 2002-07-05, we determined that, for certain airplanes, the existing inspection compliance times were not sufficient to address the unsafe condition and needed to be reduced. This proposed AD would require repetitive inspections for cracking of certain fittings, corrective actions if necessary, and, for certain airplanes, a modification, as specified in an European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. We are proposing this AD to address the unsafe condition on these products.

We propose to adopt a new airworthiness directive (AD) for certain Airbus SAS Model A330-200 Freighter, -200 and -300 series airplanes; and certain Airbus SAS Model A340-200, -300, -500, and -600 series airplanes. This proposed AD was prompted by a determination that certain wing slat tracks that were inadvertently indicated as eligible for installation on all Model A330 and A340 series airplanes are unable to sustain the ultimate loads relative to the weight variant of certain airplane configurations. This proposed AD would require inspecting any affected part for cracking, and replacing with a serviceable part, as specified in an European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. We are proposing this AD to address the unsafe condition on these products.

This notice announces final environmental actions taken by the Federal Transit Administration (FTA) for projects in Spokane, Washington, and Portland and Gresham, Oregon. 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.

In accordance with the procedures governing the application for, and the processing of, special permits from the Department of Transportation's Hazardous Material Regulations, notice is hereby given that the Office of Hazardous Materials Safety has received the application described herein.

In accordance with the procedures governing the application for, and the processing of, special permits from the Department of Transportation's Hazardous Material Regulations, 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: 1 Motor vehicle, 2Rail freight, 3Cargo vessel, 4Cargo aircraft only, 5Passenger-carrying aircraft.

The Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.-build requirements of the coastwise trade laws to allow the carriage of no more than twelve passengers for hire on vessels, which are three years old or more. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below.

The Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.-build requirements of the coastwise trade laws to allow the carriage of no more than twelve passengers for hire on vessels, which are three years old or more. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below.

The Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.-build requirements of the coastwise trade laws to allow the carriage of no more than twelve passengers for hire on vessels, which are three years old or more. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below.

The Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.-build requirements of the coastwise trade laws to allow the carriage of no more than twelve passengers for hire on vessels, which are three years old or more. 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 action proposes special conditions for The Boeing Company (Boeing) Model 777-9 airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is an electronic flight-control system requiring control-surface-position awareness. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

The Federal Aviation Administration (FAA) is considering a proposal to change 8.313 acres of airport land from aeronautical to non-aeronautical use and to authorize the lease of airport property located at John Glenn Columbus International Airport, Columbus, Ohio. The aforementioned land is not needed for aeronautical use. The subject property is located along the northern property boundary of the airport; north of Bridgeway Avenue. The parcel is currently vacant. The parcel presently serves the primary purpose of compatible land use. The parcel will continue to serve in this same capacity with a proposed change to nonaeronautical, revenue-producing use from its present aeronautical use designation. The parcel will be used for construction of a 2-story office building, approximately 19,600 square feet, connected to a 80,100 square foot building, and the potential to add a 30,000 square foot building. The proposed development also includes approximately 289 parking spaces with the flexibility to add 14 spaces for future expansion.

PHMSA's Office of Hazardous Materials Safety (OHMS) will hold a public meeting to solicit input on the development of the 2020 edition of the Emergency Response Guidebook (ERG2020). The meeting will take place on June 17, 2019, in Washington, DC. PHMSA developed the United States version of the Emergency Response Guidebook (ERG) for use by emergency services personnel to provide guidance for initial response to hazardous materials transportation incidents. Since 1980, it has been PHMSA's goal that all public emergency response personnel (e.g., fire-fighting, police, and rescue squads) have free and immediate access to the ERG. To date, PHMSA has distributed more than 14.5 million copies of the ERG to emergency service agencies and developed free online resources and downloadable mobile applications to make the ERG more accessible. Since 1996, PHMSA, Transport Canada, and the Secretariat of Communication and Transport of Mexico have collaborated in development of the ERG, with interested parties from government and industry providing additional assistance, including Argentina's Chemical Information Center for Emergencies (CIQUIME). ERG2020 will be published in English, French, and Spanish and will increase public safety by providing consistent emergency response procedures for hazardous materials transportation incidents throughout North America. During the meeting, PHMSA will respond to stakeholder requests for a public discussion of the methodology used to determine the appropriate response protective distances for poisonous vapors resulting from spills involving dangerous goods considered toxic by inhalation in the ERG2016 ``Green Pages.'' To pursue our objective of continually improving the ERG, PHMSA will solicit comments related to new methodologies and considerations for future editions of the ERG. Additionally, the meeting will include discussions on the outcomes of field experiments, ongoing research efforts to better understand environmental effects on airborne toxic gas concentrations, and updates to be published in the ERG2020. Time and Location: The meeting will be held at the U.S. Department of Transportation Conference Center at 1200 New Jersey Ave. SE, Washington, DC 20590 on June 17, 2019, from 8:30 a.m. to 2:30 p.m. Eastern Standard Time. Registration: DOT requests that attendees pre-register for this meeting by completing the form at https://www.surveymonkey.com/r/ 82Z6KYM. Conference call-in and ``live meeting'' capability will be provided. Specific information about conference call-in and live meeting access will be posted, when available, at: https:// www.phmsa.dot.gov/research-and-development/hazmat/rd-meetings -and- events. DOT is committed to providing equal access for all Americans and ensuring that information is available in appropriate alternative formats to meet the requirements of persons who have a disability. If you require an alternative version of files provided or alternative accommodations, please contact PHMSA-Accessibility@dot.gov no later than June 3, 2019.

We propose to supersede Airworthiness Directive (AD) 2016-07- 22, which applies to all Airbus SAS 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), and Model A310 series airplanes. AD 2016-07-22 requires modifying the electrical routing installation at the right-hand (RH) and left-hand (LH) wings to achieve a minimum distance between wiring bundles and surrounding structures. Since we issued AD 2016-07-22, we received reports of missing installation information for certain airplanes. This proposed AD would retain the requirements of AD 2016-07-22 and, for certain airplanes, add a requirement to further modify the electrical installations in both wings, as specified in an European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. We are proposing this AD to address the unsafe condition on these products.

We propose to supersede Airworthiness Directive (AD) 2018-20- 06, which applies to certain Airbus SAS Model A300 F4-600R series airplanes. AD 2018-20-06 requires repetitive high frequency eddy current (HFEC) inspections of the aft lower deck cargo door (LDCD) frame forks; a one-time check of the LDCD clearances; and a one-time detailed visual inspection of hooks, eccentric bushes, and x-stops; and corrective actions if necessary. Since we issued AD 2018-20-06, we determined certain compliance times need to be revised, depending on frame fork configuration. This proposed AD would continue to require the actions of AD 2018-20-06 and would require new compliance times, depending on frame fork configuration. We are proposing this AD to address the unsafe condition on these products.

We propose to adopt a new airworthiness directive (AD) for certain Airbus SAS Model A320-251N and -271N airplanes; and A321-251N, -253N, -271N, and -272N airplanes. This proposed AD was prompted by a report that during a calibration check, some torqueing tools used on the final assembly line have been found out of tolerance. This proposed AD would require retorqueing each affected connection of sense and fire extinguishing lines within the pylon area to a correct torque value, as specified in a European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. We are proposing this AD to address the unsafe condition on these products.

In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval of a new information collection. The collection involves manufacturers of small unmanned aircraft providing a safety statement to owners of the UAS they produce. This is a statutory requirement. To minimize the burden on small businesses, the FAA has developed an example safety statement that can be used to satisfy the requirement. This FRN corrects the previously submitted 60- Day FRN to include updated contact information and docket number.

Before a Federal agency can collect certain information from the public, it must receive approval from the Office of Management and Budget (OMB). Under procedures established by the Paperwork Reduction Act of 1995, before seeking OMB approval, Federal agencies must solicit public comment on proposed collections of information, including extensions and reinstatement of previously approved collections. This document describes an Information Collection Request (ICR) for which NHTSA intends to seek OMB approval.

We are adopting a new airworthiness directive (AD) for certain RECARO Aircraft Seating GmbH & Co. KG (RECARO) Model 3510A and 3510D passenger seats. This AD requires modification and re-identification of all affected RECARO model passenger seats. This AD was prompted by an analysis that the affected RECARO model passenger seats contain a seat pan assembly design that can trap a person using the seat to assist during an emergency evacuation. We are issuing this AD to address the unsafe condition on these products.

In compliance with the Paperwork Reduction Act of 1995 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 with a 60-day comment period soliciting comments on the following information collection was published on September 12, 2018 (83 FR 19836).

This action proposes an amendment to special conditions for the Airbus A380 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is associated with the complex systems and the configuration of the airplane, including its full-length double deck. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding stairways between decks. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. By issuance of this amendment to the special condition, the FAA is correcting an error that appeared in the Federal Register on August 28, 2006, for Special Conditions No. 25-326-SC, Docket No. NM314. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.