Department of Transportation June 2020 – Federal Register Recent Federal Regulation Documents

In accordance with the Paperwork Reduction Act of 1995, the FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew a previously approved information collection. On May 28, 2010, the FAA published the final rule, entitled Automatic Dependent Surveillance Broadcast (ADS-B) Equipage Mandate To Support Air Traffic Control Service. 75 FR 30160. As of January 2, 2020, when operating in the airspace designated in 14 CFR 91.225(a), (b) and (d), operators must be equipped with ADS-B Out avionics that meet the performance requirements of 14 CFR 91.227. ADS-B supports the aircraft surveillance needs of the FAA by requiring avionics equipment that meet the performance requirements of 14 CFR 91.227 and continuously transmit aircraft information to be received by the FAA, via automation, for use in providing air traffic surveillance services. ADS-B is transforming all segments of aviation (e.g., real- time precision shared situational awareness, and advanced applications for pilots and controllers alike).

The FAA is adopting a new airworthiness directive (AD) for all Gulfstream Aerospace Corporation (Gulfstream) Model G-IV airplanes. This AD was prompted by reports of un-commanded nose wheel steering turns. This AD requires replacing the nose wheel steering servo valve manifold, incorporating revised operating procedures into the airplane flight manual (AFM), doing a records inspection for any incidents of un-commanded nose wheel steering turns, and reporting the results to the FAA. The FAA is issuing this AD to address the unsafe condition on these products.

This action proposes to amend the Class E airspace extending upward from 700 feet above the surface at Clinton Regional Airport, Clinton, MO. The FAA is proposing this action as the result of an airspace review due to the decommissioning of the Golden Valley non- directional beacon (NDB) which provided navigation information to the instrument procedures at this airport. The name and geographic coordinates of the airport would also be updated to coincide with the FAA's aeronautic database.

This notice announces final environmental actions taken by the Federal Transit Administration (FTA). The purpose of this notice is to announce publicly the environmental decisions by FTA on the subject project and to activate the limitation on any claims that may challenge these final environmental actions.

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.

Mercedes-Benz AG (``MBAG'') and Mercedes-Benz USA, LLC (``MBUSA'') (collectively, ``Mercedes-Benz'') have determined that certain model year (MY) 2019 Mercedes-Benz A-Class motor vehicles do not fully comply with Federal Motor Vehicle Safety Standard (FMVSS) No. 104, Windshield Wiping and Washing Systems. Mercedes-Benz filed a noncompliance report dated February 24, 2020, and subsequently petitioned NHTSA on March 12, 2020, for a decision that the subject noncompliance is inconsequential as it relates to motor vehicle safety. This notice announces receipt of Mercedes-Benz's petition.

Daimler Trucks North America, LLC (DTNA) has determined that certain model year (MY) 2011-2021 Thomas Built Buses Saf-T-Liner HDX school buses do not fully comply with Federal Motor Vehicle Safety Standard (FMVSS) No. 222, School Bus Passenger Seating and Crash Protection. DTNA filed a noncompliance report dated December 17, 2019, and later amended the report on January 16, 2020. DTNA subsequently petitioned NHTSA on January 16, 2020, for a decision that the subject noncompliance is inconsequential as it relates to motor vehicle safety. This notice announces receipt of DTNA's petition.

Harley-Davidson Motor Company, (Harley-Davidson), has determined that certain model year (MY) 2018-2019 Harley-Davidson Softail motorcycles do not fully comply with Federal motor vehicle safety standard (FMVSS) No. 120, Tire Selection and Rims and Motor Home/Recreation Vehicle Trailer Load Carrying Capacity Information for Motor Vehicles with a GVWR of more than 4,536 kilograms (10,000 Pounds). Harley-Davidson filed a noncompliance report dated June 20, 2019. Harley-Davidson subsequently petitioned NHTSA on July 17, 2019, for a decision that the subject noncompliance is inconsequential as it relates to motor vehicle safety. This document announces receipt of Harley-Davidson's petition.

This rule amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures 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 for the safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

The FAA announces the charter renewal of the Drone Advisory Committee (DAC), a Federal Advisory Committee that works with industry, community stakeholders, and the public to improve the development of the FAA's regulations. This charter renewal will take effect on June 12, 2020, and will expire after 2 years if not renewed.

This notice announces a meeting of the Transit Advisory Committee for Safety (TRACS).

The FAA proposes to adopt a new airworthiness directive (AD) for all Pratt & Whitney Division (PW) PW4164, PW4164-1D, PW4168, PW4168-1D, PW4168A, PW4168A-1D, and PW4170 model turbofan engines with a certain outer combustion chamber assembly and 3rd stage low-pressure turbine (LPT) duct segments installed. This proposed AD was prompted by reports of damaged or failed 3rd stage LPT duct segments on PW engines with the Talon IIB outer combustion chamber assembly configuration installed. This proposed AD would require removing and replacing certain 3rd stage LPT duct segments. The FAA is proposing this AD to address the unsafe condition on these products.

The FAA proposes to remove Airworthiness Directive (AD) 2015- 17-01, which applies to certain Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. AD 2015-17- 01 requires certain inspections of each tail rotor pitch horn assembly (pitch horn) for a crack, replacement of a cracked pitch horn, and a repetitive visual inspection of certain pitch horns. AD 2015-17-01 is no longer necessary because the cause of the unsafe condition has been removed from all affected helicopter models. Accordingly, the FAA proposes to remove AD 2015-17-01.

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 March 24, 2020.

The FAA is superseding Airworthiness Directive (AD) 2011-12-08 for Bell Helicopter Textron Inc. (Bell), Model 205A, 205A-1, 205B, 212, 412, 412CF, and 412EP helicopters. AD 2011-12-08 required a one-time inspection of the tail rotor (T/R) blade for corrosion and pitting. This new AD retains the requirements of AD 2011-12-08 while excluding certain T/R blades from the applicability. This AD was prompted by new manufacturing and inspection procedures implemented by Bell that correct the unsafe condition on more recently manufactured T/R blades. The actions of this AD are intended to address an unsafe condition on these products.

The FAA proposes to supersede Airworthiness Directive (AD) 2018-26-02 for Airbus Helicopters (previously Eurocopter France) Model AS350B3, EC130B4, and EC130T2 helicopters. AD 2018-26-02 requires inspecting the pilot's and co-pilot's throttle twist for proper operation. Since the FAA issued AD 2018-26-02, the FAA received a public comment that prompted additional review. This proposed AD would retain the requirements of AD 2018-26-02 and add calendar time compliance times for the required actions. The actions of this proposed AD are intended to address an unsafe condition on these products.

In accordance with the Paperwork Reduction Act of 1995, FMCSA announces its plan to submit the Information Collection Request (ICR) described below to the Office of Management and Budget (OMB) for its renewal and invites public comment. This ICR is to collect data on the delays, by State, that applicants face when scheduling a CDL skills test. This information collection and subsequent data analysis is required by section 5506 of the Fixing America's Surface Transportation Act, 2015 (FAST Act). FMCSA reported the results of the initial ICR request in a report to congress titled ``The Commercial Driver's License Skills Test Delays Report to CongressCY 2016'' available on FMCSA's web page located here: https://www.fmcsa.dot.gov/mission/ policy/commercial-drivers-license-skills-test-delays-report-c ongress- cy-2016.

This notice contains a summary of a petition seeking relief from specified requirements of Federal Aviation 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.

PHMSA is developing a national policy regarding safety devices (UN0503 and UN3268). PHMSA has continued to see advancements in technologies for articles containing hazardous materials that have been submitted to PHMSA requesting an approval or special permit to transport as safety devices (UN0503 and UN3268). PHMSA is requesting information or data from stakeholders regarding the classification, testing, and conditions for transportation of these devices requesting an approval to be classified as safety devices.

This notice contains a summary of a petition seeking relief from specified requirements of Federal Aviation 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 superseding Airworthiness Directive (AD) 2010-23- 04, which applied to all De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. AD 2010-23-04 required repetitive detailed inspections of the nacelle attachment fittings for cracks, a conductivity inspection of the nacelle attachment fittings, and replacement if necessary. This AD continues to require these inspections and replacement if necessary, removes a certain inspection requirement for certain airplanes, and adds a new requirement to replace the rear spar fitting and nacelle attaching structure with a new nacelle attachment fitting. This AD was prompted by a determination that it is necessary to do a replacement with new nacelle attachment fittings. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA proposes to adopt a new airworthiness directive (AD) for Bell Textron Inc. (Type Certificate previously held by Bell Helicopter Textron Inc.) (Bell), Model 204B, 205A-1, and 212 helicopters. This proposed AD was prompted by reports of corrosion on main rotor hub tension-torsion strap (TT strap) assemblies. This proposed AD would require reducing the life limit of a certain part- numbered TT strap assembly and prohibit installing this TT strap assembly on any helicopter. The FAA is proposing this AD to address the unsafe condition on these products.

This action proposes to modify the Class D and Class E surface area at Bethel Airport, Bethel AK, by redefining the Hangar Lake exclusion area and eliminating the use of the VORTAC in the descriptions. This action also proposes to remove Class E airspace as an extension to the Class D and Class E surface area and modify the Class E airspace extending upward from 700 feet above the surface at the Airport. After a biennial review of the airspace, the FAA found it necessary to amend the existing airspace for the safety and management of Instrument Flight Rules (IFR) operations at this airport. This action would also update the geographical coordinates and make a minor editorial change replacing the outdated term Airport/Facility Directory with the term Chart Supplement.

The FAA is adopting a new airworthiness directive (AD) for certain Rolls-Royce Deutschland Ltd. & Co KG (RRD) Trent XWB-75, XWB- 79, XWB-79B, and XWB-84 model turbofan engines. This AD was prompted by analysis by the manufacturer of the low-pressure compressor (LPC) outlet guide vane (OGV) assembly and LPC OGV outer mount ring assembly. The analysis predicted that when the front engine mount is in the fail- safe condition, the most highly stressed LPC OGV outer mount ring assembly has a life that could be substantially less than one shop visit interval. This AD requires initial and repetitive inspections of the LPC OGV outer mount ring assembly and, depending on the results of the inspections, possible replacement of the LPC OGV outer mount ring assembly. The FAA is issuing this AD to address the unsafe condition on these products.