Federal Aviation Administration February 9, 2023 – Federal Register Recent Federal Regulation Documents

Amendment of Class E Airspace; Altoona, PA
Document Number: 2023-02738
Type: Proposed Rule
Date: 2023-02-09
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend the Class E airspace at Altoona, PA. The FAA is proposing this action as the result of an airspace review caused by the decommissioning of the Revloc very high frequency omnidirectional range (VOR) navigation aids as part of the VOR Minimum Operating Network (MON) Program. The name of the airport would also be updated to coincide with the FAA's aeronautical database.
Amendment and Establishment of Area Navigation (RNAV) Routes; Eastern United States
Document Number: 2023-02766
Type: Rule
Date: 2023-02-09
Agency: Federal Aviation Administration, Department of Transportation
This action amends a final rule published by the FAA in the Federal Register on December 7, 2022, that, among other actions, amended area navigation (RNAV) route T-224 by removing the AXEJA, AL, computer navigation fix (CNF) from the route description. This action re-inserts AXEJA into the T-224 description as an RNAV waypoint (WP) instead of a CNF. This action is necessary to match the FAA National Airspace System Resource (NASR) database information.
Airworthiness Directives; Schempp-Hirth Flugzeugbau GmbH Gliders
Document Number: 2023-02773
Type: Rule
Date: 2023-02-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Schempp-Hirth Flugzeugbau GmbH Model Duo Discus and Duo Discus T gliders. This AD was prompted by 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 identifies the unsafe condition as cracks in the connecting tube of the elevator U-bracket of the horizontal tail, which could compromise the stiffness of the elevator control system and of the attachment of the horizontal tail. This AD requires repetitively inspecting the elevator U-bracket for cracks and broken weld seams, the rear connection between the horizontal tail and the rear attachment on the fuselage for play and softness, and the foam support for compression between the vertical and horizontal tail, and replacing or repairing damaged parts as applicable. The FAA is issuing this AD to address the unsafe condition on these products.
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