October 18, 2021 – Federal Register Recent Federal Regulation Documents

The Directorate of Defense Trade Controls and the Department of State give notice that the attached Notifications of Proposed Commercial Export Licenses were submitted to the Congress on the dates indicated.

The following virtual public hearing on proposed amendments to the Federal Rules of Criminal Procedure has been canceled: Criminal Rules Hearing on November 8, 2021. The announcement for this hearing was previously published in the Federal Register on August 11, 2021.

In accordance with the Privacy Act of 1974, as amended (``Privacy Act''), this document announces the modification of a computer matching program the Federal Communications Commission (``FCC'' or ``Commission'' or ``Agency'') and the Universal Service Administrative Company (USAC) will conduct with the Georgia Department of Human Services, Division of Children and Family Services (DHS) (``Agency''). The purpose of this matching program is to verify the eligibility of applicants to and subscribers of Lifeline (existing purpose) and the new Emergency Broadband Benefit Program, both of which are administered by USAC under the direction of the FCC. More information about these programs is provided in the SUPPLEMENTARY INFORMATION section below.

NMFS proposes to implement management measures described in a framework action to the Fishery Management Plan for the Reef Fish Resources of the Gulf of Mexico (FMP) as prepared by the Gulf of Mexico Fishery Management Council (Council). For Gulf of Mexico (Gulf) lane snapper, this proposed rule would modify the annual catch limit (ACL) and revise an accountability measure (AM). The purposes of this proposed rule are to prevent overfishing of lane snapper and achieve optimum yield (OY). This proposed rule would also make minor administrative changes to replace outdated NMFS website addresses and language about required software for the Individual Fishing Quota (IFQ) programs.

The FAA is superseding emergency Airworthiness Directive (AD) 2018-23-52, which applied to all Leonardo S.p.a. Model AW169 and AW189 helicopters. AD 2018-23-52 required inspecting the nut, cotter pin, lock-wire, and hinge bracket connected to the tail rotor servo-actuator (TRA) feedback lever link, and each connection of the TRA feedback lever link, and repair if necessary. AD 2018-23-52 also required applying a paint stripe or torque seal on the nut and reporting certain information. This AD requires repetitive inspections of the TRA, repetitive inspections and checks of the tail rotor duplex bearings (TR DB), installation of an improved TRA and TR DB, repetitive installations and checks of thermal strips, replacement of the improved TR DB (life limit), and applicable corrective actions, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD was prompted by a report of an accident of a Model AW169 helicopter, which was observed to have lost yaw control prior to the accident and a determination that certain inspections and checks of the TR DB, installation of an improved TRA and TR DB, certain other actions, and applicable corrective actions are necessary to address the unsafe condition. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for certain Bell Textron Canada Limited (type certificate previously held by Bell Helicopter Textron Canada Limited) Model 429 helicopters. This AD was prompted by reports of incorrectly staked spherical bearings in the directional control bellcrank assembly. This AD requires a one-time inspection of the lower surface of the spherical bearing in the directional control bellcrank assembly to determine if it is properly staked and, depending on the findings, applicable corrective actions. For certain helicopters, this AD also requires repetitive inspections and, depending on the findings, applicable corrective actions. This AD also provides a terminating action for the repetitive inspections. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, AS-365N2, AS 365 N3, EC120B, EC130B4, EC130T2, EC 155B, EC155B1, SA-365N, and SA-365N1 helicopters; and Airbus Helicopters Deutschland GmbH (AHD) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, MBB-BK117 C-2, and MBB-BK117 D-2 helicopters. This AD was prompted by failure of an Emergency Flotation System (EFS) float compartment to inflate during maintenance of the EFS. This AD requires inspecting certain EFSs and depending on the results, marking certain parts or removing certain parts from service, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference (IBR). The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for certain Leonardo S.p.a Model AW189 helicopters. This AD was prompted by a report of an incorrect connection of the inflation hoses to the tee manifolds of the inflation line on the emergency flotation system (EFS) assembly. This AD requires visually inspecting the yellow sleeves and hoses installed on each EFS assembly and depending on the inspection results, accomplishing the corrective actions in the applicable service information as specified in a European Aviation Safety Agency (now European Union Aviation Safety Agency) (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for certain Leonardo S.p.a. Model AW169 helicopters. This AD was prompted by reports of in-flight pilot collective stick oscillation. This AD requires a one-time measurement of the friction of the pilot collective stick assembly to verify that it is within the allowable range and, depending on findings, making an adjustment to restore the acceptable level of friction, as specified in a European Aviation Safety Agency (now European Union Aviation Safety Agency) (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

In accordance with the requirements of the Paperwork Reduction Act of 1995, this notice announces the intention of BTS to request the Office of Management and Budget (OMB) to approve continuation of the following information collection: Barrier Failure Reporting in Oil and Gas Operations on the Outer Continental Shelf (OCS). BTS has entered into a memorandum of understanding (MOU) with BSEE to expand the scope of SafeOCS to include an industry-wide repository of equipment failure data, analyze and aggregate information provided under this program, and publish reports that will provide BSEE, the industry, and all OCS stakeholders with essential information about failure types and modes of critical safety barriers for offshore operations related to well control and safety and pollution prevention.

In response to a petition filed under the Emergency Planning and Community Right-to-Know Act (EPCRA), EPA is proposing to add 12 chemicals to the list of toxic chemicals subject to the reporting requirements under EPCRA and the Pollution Prevention Act (PPA). EPA believes that each of the 12 chemicals meets the EPCRA criteria. In addition, based on the available bioaccumulation and persistence data, EPA believes that one chemical should be classified as a persistent, bioaccumulative, and toxic (PBT) chemical and designated as a chemical of special concern with a 100-pound reporting threshold.

This action proposes to establish restricted area R-2511 in the vicinity of Trona, CA in support of the Naval Air Warfare Center Weapons Division (NAWCWD) at China Lake, CA. The proposed restricted area is necessary to segregate the testing and evaluation of hazardous weapons systems, and other unproven aviation platforms in the early development cycle from non-participating aircraft.