Department of Transportation

This action amends the using agency and controlling agency descriptions listed for restricted areas R-5301, R-5302A, R-5302B, and R-5302C, NC. This action does not change any boundaries, altitudes, times of designation, or activities conducted within the restricted areas.

The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Model H160-B helicopters. This AD was prompted by reports of missing retaining rings on the hinge pins installed on the jettisonable window systems. This AD requires inspecting for missing retaining rings on all the hinge pins installed on the jettisonable window systems and, depending on findings, installing retaining rings found missing. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model H160-B helicopters modified by Supplemental Type Certificate (STC) SR00223IB. This AD was prompted by a report that several self-locking nuts of the window jettisoning system could be loosened by hand due to a non-conformity in the cable kit. This AD requires modifying an affected window into a serviceable window. This AD also prohibits installing an affected window or an affected door on any helicopter modified with STC SR00223IB. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is superseding Airworthiness Directive (AD) 2024-25- 10, which applied to certain Rolls-Royce Deutschland Ltd & Co KG (RRD) Model Trent XWB-97 engines. AD 2024-25-10 required a one-time set of visual and dimensional inspections of the main fuel hose assembly of the fuel manifold to confirm softness, compliance, and lack of resistance, and for shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire; and, if necessary, replacement of the main fuel hose assembly of the fuel manifold. Since the FAA issued AD 2024-25-10, the FAA has determined that additional engine models are affected by the unsafe condition and that the required inspections should be repetitive. This AD requires, for certain engines, a one-time set of on-wing visual and dimensional inspections of the main fuel hose assembly of the fuel manifold to confirm softness, compliance, and lack of resistance, and for shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire and, if necessary, replacement of the main fuel hose assembly of the fuel manifold. This AD also requires, for certain other engines, on-wing and in-shop repetitive visual and dimensional inspections of the main fuel hose assembly of the fuel manifold to confirm softness, compliance, and lack of resistance, and for shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire and, if necessary, replacement of the main fuel hose assembly of the fuel manifold. This AD also expands the applicability to include certain RRD Model Trent XWB-75, Trent XWB-79, Trent XWB-79B, and Trent XWB-84 engines. This AD also provides criteria for installation of an affected part and optional terminating action for the repetitive visual and dimensional 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 certain Gulfstream Aerospace Corporation Model GVIII-G700 and GVIII- G800 airplanes. This AD was prompted by a report indicating that a hollow pin cap on the right-side engine aft thrust strut mount interface was found broken due to a missing sleeve bushing. This AD requires a visual inspection of the upper surface of the engine mount to the forward and aft thrust strut mount at the hollow pin head interface, of the left and right engines, for evidence of movement or distress; an inspection of the forward and aft thrust strut mount hardware to ensure the sleeve bushing, nut, washers, and cotter pins are properly installed; and applicable corrective actions. The FAA previously sent an emergency AD to all known U.S. owners and operators of these airplanes. 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 The Boeing Company Model 787-8, 787-9, and 787-10 airplanes. This AD was prompted by reports of door assist handles pulled loose from their lower attach point in the doorway support bracket during pre-flight checks. This AD requires, for certain airplanes, installing a new retainer above the lower keyway of the support bracket assembly and installing a placard on certain support bracket assemblies or marking the part, and for certain airplanes, requires an inspection of the forward and aft door assist handles and applicable on-condition actions. For certain other airplanes, this AD requires installing a new retainer above the lower keyway of the support bracket assembly at certain locations and reidentifying the support bracket assembly. 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 The Boeing Company Model 747-8F series airplanes. This AD was prompted by reports of cracking in stringers and splice fittings located at stringer splices at multiple body stations. This AD requires an inspection of each free flange of the stringers at the stringer splice for radius fillers at certain fastener locations, an inspection for cracking of the stringers and stringer splice fittings at certain stringer splice locations, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.

This action establishes Class E airspace at Hub Field, Jewett, TX. The FAA is taking this action to support new instrument procedures.

The Department of Transportation (Department or DOT) is issuing this final rule to implement the Fifth Circuit's vacatur of the Department's 2024 Final Rule, Enhancing Transparency of Airline Ancillary Service Fees. Because the legal effect of the court's decision is to reinstate the rules previously in force, this action revises the Code of Federal Regulations (CFR) to restore the Department's regulations on the disclosure of fees for ancillary services as they existed before publication of the 2024 Rule, returning to the standards established in a rule issued in 2011.

The U.S. Department of Transportation (Department or DOT) is amending its regulations regarding the hearing procedures available when the Department proposes a discretionary aviation consumer protection rulemaking declaring a practice to be unfair or deceptive. This final rule revises the hearing procedures established in 2022 to align them with the more robust due process protections originally set forth in 2020, ensuring the use of neutral hearing officers and the issuance of formal findings of fact. Further, this rule rescinds the 2023 Clarification of Formal Enforcement Procedures, which specified that the Department is not limited to administrative proceedings before an Administrative Law Judge, but may also initiate civil enforcement actions in United States District Court. The Department now finds this clarification unnecessary and redundant because its authority to seek judicial enforcement is established clearly by statute.

These special conditions are issued for The Boeing Company (Boeing) Model 747-8 airplane. This airplane, as modified by AMAC Aerospace (AMAC), 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 side-facing, single-occupant and multiple-occupant seats. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.

The FAA is superseding Airworthiness Directive (AD) 2026-04- 05, which applied to all The Boeing Company Model 737-8, 737-9, and 737-8200 airplanes. AD 2026-04-05 required revising the existing airplane flight manual (AFM) to provide the flightcrew with operating procedures (non-normal checklists) if a certain circuit breaker in the standby power control unit (SPCU) trips. Since the FAA issued AD 2026- 04-05, the FAA has determined that additional revisions to the AFM are necessary to address certain environmental control system (ECS) circuit breakers downstream of the SPCU that could also trip. This AD retains the requirements of AD 2026-04-05 and requires revising the existing AFM to provide the flightcrew with operating procedures (non-normal checklists) if certain ECS circuit breakers trip. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 757 airplanes and Model 767 airplanes. This AD was prompted by the determination that radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 3.7-3.98 GHz frequency band (5G Lower C-Band) while operating in Canadian airspace, and a determination that, during approach, landings, and go-arounds, as a result of this interference, certain airplane systems may not properly function, resulting in increased flightcrew workload while on approach with the flight director, autothrottle, or autopilot engaged, which could result in reduced ability of the flightcrew to maintain safe flight and landing of the airplane. This AD requires revising the existing airplane flight manual (AFM) to incorporate limitations prohibiting certain operations requiring radio altimeter data when operating in Canadian airspace. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 787-8, 787-9, and 787-10 airplanes. This AD was prompted by the determination that radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 3.7-3.98 GHz frequency band (5G Lower C-Band) while operating in Canadian airspace, and the determination that as a result of this interference, certain airplane systems may not properly transition from AIR to GROUND mode when landing on certain runways, resulting in a longer landing distance than normal due to the effect on thrust reverser deployment, speedbrake deployment, and increased idle thrust. This AD requires revising the existing airplane flight manual (AFM) to incorporate limitations prohibiting certain operations requiring radio altimeter data when operating in Canadian airspace. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 747-8 and -8F series airplanes and Model 777- 200, -200LR, -300, -300ER, and 777F series airplanes. This AD was prompted by the determination that radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 3.7-3.98 GHz frequency band (5G Lower C-Band) while operating in Canadian airspace, and the determination that this interference may affect multiple other airplane systems using radio altimeter data, including the pitch control laws, including those that provide tail strike protection, regardless of the approach type or weather. This AD requires revising the existing airplane flight manual (AFM) to incorporate limitations prohibiting certain operations requiring radio altimeter data when operating in Canadian airspace. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 737-8, 737-9, and 737-8200 airplanes. This AD was prompted by the determination that radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 3.7-3.98 GHz frequency band (5G Lower C-Band) while operating in Canadian airspace, and the determination that, during takeoffs and landings, as a result of this interference, certain airplane systems may not properly function, resulting in longer than normal landing or rejected takeoff distances due to the effect on thrust reverser deployment, spoilers, speedbrake deployment, and increased idle thrust, regardless of the approach type or weather, which could lead to degraded deceleration performance and a runway excursion. This AD requires revising the existing airplane flight manual (AFM) to incorporate limitations prohibiting certain operations requiring radio altimeter data when operating in Canadian airspace. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 747-100, -100B, -100B SUD, -200B, -200C, - 200F, -300, -400, -400D, and -400F series airplanes. This AD was prompted by the determination that radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 3.7-3.98 GHz frequency band (5G Lower C-Band) while operating in Canadian airspace, and a determination that during takeoff, approach, landings, and go-arounds, as a result of this interference, certain airplane systems may not properly function, resulting in increased flightcrew workload while on approach with the flight director, autothrottle, or autopilot engaged, which could result in reduced ability of the flightcrew to maintain safe flight and landing of the airplane. This AD requires revising the existing airplane flight manual (AFM) to incorporate limitations prohibiting certain operations requiring radio altimeter data when operating in Canadian airspace. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 737-, -200, -200C, -300, -400, -500, -600, - 700, -700C, -800, -900, and -900ER series airplanes, except for Model 737-200 and -200C series airplanes equipped with a certain flight control system. This AD was prompted by the determination that radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 3.7-3.98 GHz frequency band (5G Lower C-Band) while operating in Canadian airspace, and the determination that, during approach, landings, and go-arounds, as a result of this interference, certain airplane systems may not properly function, resulting in increased flightcrew workload while on approach with the flight director, autothrottle, or autopilot engaged, which could result in reduced ability of the flightcrew to maintain safe flight and landing of the airplane. This AD requires revising the existing airplane flight manual (AFM) to incorporate limitations prohibiting certain operations requiring radio altimeter data when operating in Canadian airspace. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 707, 717, and 727 airplanes; Model DC-8, DC-9, and DC-10 airplanes; Model MD-10 and MD-11 airplanes; Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 airplanes; and Model MD 90-30 airplanes. This AD was prompted by the determination that radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 3.7-3.98 GHz frequency band (5G Lower C- Band) while operating in Canadian airspace, and the determination that during approach, landings, and go-arounds, as a result of this interference, certain airplane systems may not properly function, resulting in increased flightcrew workload while on approach with the flight director, autothrottle, or autopilot engaged, which could result in reduced ability of the flightcrew to maintain safe flight and landing of the airplane. This AD requires revising the existing airplane flight manual (AFM) to incorporate limitations prohibiting certain operations requiring radio altimeter data when operating in Canadian airspace. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all transport and commuter category airplanes equipped with a radio (also known as radar) altimeter. This AD was prompted by the determination that radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 3.7-3.98 GHz frequency band (5G Lower C-Band) while operating in Canadian airspace. This AD requires revising the existing airplane flight manual (AFM) to incorporate limitations prohibiting certain operations requiring radio altimeter data when operating within the Canadian airspace. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model H160-B helicopters. This AD was prompted by a discovery during a maintenance operation that several self-locking nuts of the window jettisoning system could be loosened by hand due to a non-conformity in certain cable kits. This AD requires modifying each affected window into a serviceable window. This AD also prohibits installing an affected window or an affected door on any helicopter. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is superseding Airworthiness Directive (AD) 2019-09-03 and AD 2021-05-15 for certain Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters. AD 2019-09-03 required a one-time inspection of the jettisoning mechanism of the cabin lateral sliding plug doors. AD 2021-05-15 required repetitive inspections, modifying the release system of each cabin lateral sliding plug door, or modifying the design of the jettison system of each cabin lateral sliding plug door. Since the FAA issued AD 2021-05-15, the manufacturer developed a prerequisite modification for certain helicopters, determined improved modification instructions were necessary for installation of the release system of the cabin lateral sliding plug door, and determined the compliance time could be extended. This AD requires modifying the release system of each cabin lateral sliding plug door or modifying the design of the jettison system of each cabin lateral sliding plug door as 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 certain Airbus SAS Model A321-251NX, -252NX, -253NX, -271NX, and -272NX airplanes. This AD was prompted by a review of the cold working process on the assembly line that detected a deviation to the manufacturing process. This AD requires repetitive inspections for the nominal design condition of the fastener holes in certain center fuselage frame foot joint connections and, as applicable, an inspection for cracking at the frame foot joint connections and corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, and AS350D helicopters. This AD was prompted by a report of non- conformity of a certain cargo hook. This AD requires inspecting the gap between the filler and the side plates of the affected cargo hook and, depending on the results, replacing the cargo hook. This AD also prohibits installing an affected cargo hook on any helicopter. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all Pratt & Whitney Canada Corp. (P&WC) Model PW210A, PW210A1, and PW210S engines. This AD was prompted by reports of circumferential cracks found at the turbine exhaust frame external surface caused by thermal stress from engine starts. This AD requires repetitive visual inspections of the turbine exhaust frame for cracks and, depending on the results of the inspections, replacement of the turbine exhaust frame. The FAA is issuing this AD to address the unsafe condition on these products.

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

This action establishes Class E airspace at Rancho Hielo Brazos Airport, Glen Rose, TX. This action supports new instrument procedures and instrument flight rule (IFR) operations.

This action establishes Class E airspace at Cedar Creek Ranch Airport, Barksdale, TX. This action supports new instrument procedures and instrument flight rule (IFR) operations.

This action modifies the Class E airspace area designated as a surface area (Class E2 airspace) and Class E airspace extending upward from 700 feet above the surface (Class E5 airspace) to optimize instrument flight procedure containment at the Ralph Wien Memorial Airport, Kotzebue, AK. This action supports the safety and management of instrument flight rules (IFR) operations at the airport.

This action corrects a final rule published by the FAA in the Federal Register on June 11, 2026, modifying the Class E airspace area extending upward from 700 feet above the surface at Omak Airport, Omak, WA. Specifically, this action administratively rewrites the body of the legal description as it was presented in the final rule for greater clarity, without substantive impacts.

This action extends the Order Limiting Operations at New York LaGuardia Airport (LGA) published on December 27, 2006, as most recently extended May 13, 2024. The Order remains effective until October 28, 2028.

This action extends the Order Limiting Operations at John F. Kennedy International Airport (JFK) published on January 18, 2008, and most recently extended on October 27, 2024. The Order remains effective until October 28, 2028.

This final rule implements the Tanker Security Program (TSP) and makes certain changes to the TSP interim final rule (IFR) published in the Federal Register on December 7, 2022, in response to public comments received on the IFR, feedback from stakeholders, and MARAD's own experience during initial program administration. The Secretary of Transportation is authorized to establish TSP, comprised of a fleet of active, commercially viable, militarily useful, privately owned product tank vessels of the United States. The TSP Fleet is intended to meet national defense and other security requirements and maintain a United States presence in international commercial shipping. TSP supports the United States maritime industries and workforce to promote national security and economic resilience.

This action establishes Class E airspace at Lane Airpark, Rosenberg, TX. This action supports new instrument procedures and instrument flight rule (IFR) operations.

FMCSA amends the regulations to revise the requirement that motor carriers and intermodal equipment providers sign and return a completed roadside inspection form to the issuing State agency. FMCSA is aware that not all issuing State agencies require the return of these reports, and that requiring motor carriers and intermodal equipment providers to submit these reports to a State that does not require, or even request, the return of the form creates an unnecessary burden. Through this change, completed forms will only be returned to those States that request them. This action is in response to a petition for rulemaking from the Commercial Vehicle Safety Alliance (CVSA).

FMCSA amends the regulations requiring commercial driver's license (CDL) holders to self-report motor vehicle violations to their State of domicile. With the implementation of the exclusive electronic exchange (EEE) of violations between State Drivers Licensing Agencies (SDLAs) in 2024, self-reporting is no longer necessary. This action supports the Administration's deregulatory efforts.

FMCSA amends the Federal Motor Carrier Safety Regulations (FMCSR) to rescind the requirement for a copy of the electronic logging device (ELD) operator's manual to be kept in a commercial motor vehicle (CMV). Drivers are required to understand the operation of the ELD on the vehicle to ensure the accuracy of their electronic records of duty status and to present this information during inspections by enforcement officials. There is no readily apparent benefit to continuing to require that the user's manual be in the CMV given the use of ELDs since December 2019. This final rule eliminates a regulatory burden on motor carriers without compromising safety.

PHMSA alerts the public to a petition for reconsideration and PHMSA's response.

These special conditions are issued for the Dassault Aviation Model Falcon 900EX airplane. This airplane, as modified by Honeywell Aerospace US LLC (Honeywell) 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 the installation of a digital systems architecture that will allow increased connectivity to and access from external network sources, (e.g., operator networks, wireless devices, internet connectivity, service provider satellite communications, electronic flight bags, etc.) to the airplane's previously isolated electronic assets (networks, systems, and databases). The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.

These special conditions are issued for the Dassault Aviation (Dassault) Model Falcon 900EX airplane. This airplane, as modified by Honeywell Aerospace US LLC (Honeywell), 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 the installation of a digital system that contains a wireless and hardwired network with hosted application functionality that allows access, from sources internal to the airplane, to the airplane's internal electronic components. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.

The FAA is superseding Airworthiness Directive (AD) 2022-11- 08, which applied to all Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, EC130B4, and EC130T2 helicopters. AD 2022-11-08 required incorporating into maintenance records certain requirements (airworthiness limitations). Since the FAA issued AD 2022- 11-08, it was determined that new or more restrictive airworthiness limitations are necessary. This AD requires revising the airworthiness limitations section (ALS) of the existing maintenance manual (MM) or instructions for continued airworthiness (ICAs) and the existing approved maintenance or inspection program, as applicable. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is superseding Airworthiness Directive (AD) 2022-19- 13, which applied to all Airbus Helicopters Model AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. AD 2022-19-13 required incorporating into existing maintenance records certain requirements (airworthiness limitations). Since the FAA issued AD 2022- 19-13, a determination was made that new or more restrictive airworthiness limitations are necessary. This AD requires revising the airworthiness limitations section (ALS) of the existing maintenance manual (MM) or instructions for continued airworthiness (ICAs) and the existing approved maintenance or inspection program, as applicable. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS350B2, AS350B3, EC130B4, and EC130T2 helicopters. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD requires revising the airworthiness limitations section (ALS) of the existing maintenance manual (MM) or instructions for continued airworthiness (ICAs) and the existing approved maintenance or inspection program, as applicable. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is superseding Airworthiness Directive (AD) 2023-01-04 for all Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. AD 2023-01-04 required, for helicopters with certain part- numbered tail rotor head (TRH) spider pitch change units installed, inspecting the pitch change spider nut (nut) for correct installation; marking a 2 to 5 mm wide black paint index mark and repetitively inspecting the alignment of the marking; and performing additional inspections and corrective actions if necessary. Since the FAA issued AD 2023-01-04, new or more restrictive airworthiness limitations were issued, which terminated the requirement for the repetitive inspections of the black paint index marking. This AD requires the same actions as AD 2023-01-04, except for the repetitive black paint index marking inspections and prohibits installing certain parts unless certain requirements are met. The FAA is issuing this AD to address the unsafe condition on these products.

This action corrects a final rule published by the FAA in the Federal Register on May 8, 2026, amending Jet Routes J-70 and J-94; amending Very High Frequency Omnidirectional Range (VOR) Federal Airways V-30, V-84, V-170, and V-274; and revoking Jet Routes J-547 and J-548 in the vicinity of Pullman, MI. Specifically, this action corrects an error in the preamble discussion of VOR airway V-170.

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-700-1A10, BD-700-1A11, and BD-700- 2A12 airplanes. This AD was prompted by reports that certain seat frames were assembled without applying Loctite in certain locations of concern. This AD requires modification to the non-locking fastener joints of the seat frame assembly. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A350-941 and -1041 airplanes. This AD was prompted by a determination that certain primary flight control actuators have been exposed to mechanical overloads during the acceptance test procedure. This AD requires replacing affected parts with serviceable parts and prohibits the installation of affected parts. 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 The Boeing Company Model 787-8, 787-9, and 787-10 airplanes. This AD was prompted by reports of an uncommanded change to the mode control panel (MCP) selected altitude. This AD requires replacing the existing MCP with an updated MCP and performing an installation test. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is superseding Airworthiness Directive (AD) 2020-05- 01, which applied to all Rolls-Royce Deutschland Ltd & Co KG (RRD) Model Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000-K3, Trent 1000-L3, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000- Q3, and Trent 1000-R3 engines. AD 2020-05-01 required initial and repetitive borescope inspections (BSI) of the high-pressure turbine (HPT) blades. AD 2020-05-01 also required replacement of HPT blades with parts eligible for installation when the HPT blades fail inspection or reach the new life limit. Since the FAA issued AD 2020- 05-01, RRD published updated service material introducing improved HPT blades and a combustion rear inner casing bypass case assembly, adding an acceptable method for installation of HPT blades, expanding the inspection area for BSIs of the HPT blade, adding limits for axial cracks of the HPT blades, reducing certain BSI thresholds, and removing a certain HPT blade life-limit. This AD requires performing initial and repetitive BSIs of the HPT blades for axial cracks and, depending on the results of the BSIs, this AD requires either performing additional BSIs or replacing the HPT blades. This AD also adds an optional terminating action for the repetitive BSIs of the HPT blades. The FAA is issuing this AD to address the unsafe condition on these products.

This action establishes Class E airspace at Smoky Bend Ranch Airport, Mullin, TX. This action supports new instrument procedures and instrument flight rule (IFR) operations.

This action establishes Class E airspace at Silverhorn Ranch Airport, Freer, TX. This action supports new instrument procedures and instrument flight rule (IFR) operations.

This action establishes Class E airspace at Mercy Medical Center Heliport, Canton, OH. This action supports new instrument procedures and instrument flight rule (IFR) operations.

This action modifies the Class E airspace area extending upward from 700 feet above the surface at Omak Airport, Omak, WA, to support the safety and management of instrument flight rules (IFR) operations at the airport.

By this rule, the U.S. Department of Transportation amends its regulations implementing Title VI of the Civil Rights Act of 1964 ("Title VI") to eliminate disparate-impact liability. These amendments align the Department's regulations with Title VI's original public meaning, avoid constitutional concerns, reduce compliance costs, and serve the public interest. In addition, these revisions implement changes directed in Executive Order 14281. These revisions also align with changes made by the U.S. Department of Justice (DOJ) to its Title VI Regulations at 28 CFR part 42, effective December 10, 2025.

This action finalizes proposed revisions to certain documentation requirements relating to public participation and engagement in the Uniform Procedures for State Highway Safety Grant Programs.

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.

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

The National Highway Traffic Safety Administration (NHTSA) is correcting a final rule that appeared in the Federal Register on June 3, 2026. The original document issued a final rule removing unnecessary regulatory text from Federal Motor Vehicle Safety Standard (FMVSS) No. 210, Seat belt assembly anchorages. This document corrects an amendatory instruction to ensure that only the introductory text of paragraph S6 is revised, preserving the remaining subordinate text and graphics within that section.

This action establishes Class E airspace at Franciscan Health Crown Point Hospital Heliport, Crown Point, IN. This action supports new instrument procedures and instrument flight rule (IFR) operations.

This action corrects a final rule published by the FAA in the Federal Register on June 5, 2026, amending the Class E airspace at Springfield, KY. Specifically, this action corrects a typographical error in the name of the affected airport in the airspace legal description.

This amendment adopts miscellaneous amendments to the required IFR (instrument flight rules) altitudes and changeover points for certain Federal airways, jet routes, or direct routes for which a minimum or maximum en-route authorized IFR altitude is prescribed. This regulatory action is needed because of changes occurring in the National Airspace System. These changes are designed to provide for the safe and efficient use of the navigable airspace under instrument conditions in the affected areas.

The FAA is superseding Airworthiness Directive (AD) 2025-06-04 for all Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. AD 2025-06-04 required repetitively inspecting the main gearbox (MGB) bevel wheel and the MGB magnetic plug for particles and performing corrective actions if applicable and prohibited installing an affected MGB unless certain requirements were met. Since the FAA issued AD 2025-06-04, the FAA determined that AD 2025-06-04 contains errors in the interval compliance times. This AD continues to require the actions of AD 2025-06-04 and corrects the interval compliance times. 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 Pilatus Aircraft Ltd. (Pilatus) Model PC-12/47E airplanes. This AD was prompted by a report of the stall warning protection system (SWPS) engaging when not appropriate. This AD requires updating operational software and incorporating a pilot's operating handbook (POH) temporary revision (TR). This AD also prohibits the installation of affected software. 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 Airbus SAS Model A350-941 airplanes. This AD was prompted by a manufacturing investigation that found improper application of the fastener retorque process at the center wing box (CWB) and belly fairing (BF) junctions could lead to insufficient clamping. This AD requires replacing each affected part and applying additional head nut cap protection. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is superseding Airworthiness Directive (AD) 2022-02- 11, which applied to certain Airbus SAS Model A318 series airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, 216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. AD 2022-02-11 required repetitive rototest inspections of the holes at the door stop fittings for any cracking and repair if necessary. Since the FAA issued AD 2022-02-11, it was determined that additional airplane models must be added to the applicability and the terminating action for repaired affected areas must be clarified. This AD continues to require the actions in AD 2022-02-11 and expands the applicability. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all H[eacute]licopt[egrave]res Guimbal (HG) Model Cabri G2 helicopters. The FAA previously sent this AD as an emergency AD to all known U.S. owners and operators of these helicopters. This AD was prompted by a report that was received of a crack on the main rotor (MR) mast after the crew reported an abnormal increase of vibration. This AD requires inspecting the MR mast for cracks and corrosion pitting, and depending on the results of the inspection, accomplishing corrective actions. This AD also requires modifying the MR mast, which includes applying corrosion protection to the MR mast, reporting the inspection results and prohibiting the installation of a certain main gear box (MGB), unless certain requirements are met. The FAA is issuing this AD to address the unsafe condition on these products.

This action establishes Class E airspace at Cleveland Clinic, Union Hospital Heliport, Dover, OH. This action supports new instrument procedures and instrument flight rule (IFR) operations.

FAA proposes to clarify that FAA regulations governing flightcrew member and flight attendant duty and rest periods preempt all State and local meal and rest break requirements. This proposed rule also explains the agency's view that State meal and rest break requirements are preempted by the Airline Deregulation Act of 1978 (ADA) due to their significant impact on air carrier prices, routes, and services.

The FAA proposes to supersede Airworthiness Directive (AD) 2009-04-13, which applies to certain Rolls-Royce Deutschland Ltd & Co KG (RRD) Model BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30 engines. AD 2009-04-13 requires revising the airworthiness limitations section (ALS) of the operator's existing approved engine maintenance or inspection program, as applicable, to incorporate new or more restrictive tasks and limitations and associated thresholds and intervals for life-limited parts. AD 2009-04-13 also requires removing certain low pressure compressor (LPC) (fan) disc assemblies from service and completing the Life Limited Part Tracking Sheet. Since the FAA issued AD 2009-04-13, the manufacturer has revised the engine time limits manual (TLM) to introduce new or more restrictive tasks and limitations and associated thresholds and intervals for life-limited parts. This proposed AD would require revising the ALS of the existing approved engine maintenance or inspection program, as applicable, to incorporate new or more restrictive tasks and limitations and associated thresholds and intervals for life-limited parts. The FAA is proposing this AD to address the unsafe condition on these products.

This proposal would advance the United States' leadership in next-generation aviation by replacing the longstanding prohibition on civil supersonic flight over land with a modern, performance-based regulatory framework. Consistent with national policy set forth by the Executive Order of June 6, 2025, Leading the World in Supersonic Flight, this action would enable the safe, efficient, and commercially viable operation of civil supersonic aircraft in the United States. Current regulations prohibit flight operations of civil aircraft at a true flight Mach number greater than 1 in the U.S., except under the conditions and limitations of an operation-specific authorization from the Administrator, to protect the public from sonic boom. FAA has determined the general ban on civil supersonic flight is outdated and no longer appropriate due to advancements in technology, flight techniques that prevent sonic booms from reaching the surface, and increased interest in civil supersonic flight. FAA proposes to repeal this outdated and unnecessary prohibition and establish a corresponding interim noise-based certification standard to allow supersonic flights without an operation-specific special authorization clearing the way for next-generation supersonic flight. This rule removes regulatory barriers, provides clear pathways for testing and early commercial operations, and positions the United States to serve as the leader in setting global standards for supersonic flight. These actions will ensure that the United States leads the world in the safe, lawful, and rapid development and deployment of next-generation supersonic aviation.

The FAA proposes to supersede Airworthiness Directive (AD) 2025-13-09, which applies to all Airbus Helicopters Model AS-365N2, AS 365 N3, EC 155B, EC155B1, SA-365N, and SA-365N1 helicopters. AD 2025- 13-09 requires inspecting the tightening torque, reporting the results of the inspections, and, depending on the results of the inspection, taking corrective action. Since the FAA issued AD 2025-13-09, the manufacturer determined that additional inspections of the main rotor (MR) servo-controls nut torque should be required. This proposed AD would retain some of the actions of AD 2025-13-09 and would also require additional inspections and, depending on the results of the inspection, corrective actions. This proposed AD would also require reporting certain information to the manufacturer. The FAA is proposing this AD to address the unsafe condition on these products.

The FAA proposes to adopt a new airworthiness directive (AD) for certain MD Helicopters, LLC (MDHI) Model 369D, 369E, 369F, 369FF, 369H, and 500N helicopters. This proposed AD was prompted by a report of mechanical damage to the main transmission drive shaft coupling (coupling). This proposed AD would require a one-time visual inspection of the couplings for cracks of the splines and, depending on the results, replacement of the couplings. The FAA is proposing this AD to address the unsafe condition on these products.

This notice announces a fact-finding informal airspace meeting regarding a plan to amend the Class C airspace at Ontario International Airport, CA (KONT). The purpose of the meeting is to provide relevant information about the proposal and solicit aeronautical comments on its effects on local aviation operations. All comments received during the meeting and the subsequent comment period will be considered prior to the issuance of any notice of proposed rulemaking (NPRM).

The U.S. Department of Transportation (Department or DOT) is proposing to amend its rule on air fare advertising to allow the total fare, including taxes and fees, to be displayed with the same prominence as any individual components. The current rule states that individual components of air fare, like taxes and fees, may not be displayed prominently. The Department is also proposing to eliminate a prescriptive advertising regulation stating that components of a fare may not be presented in the same or larger size as the total price. These proposed changes would ensure greater flexibility in how air fare is displayed while ensuring information is presented clearly to consumers, and in conformity with the intent of Congress as articulated in a provision of the Internal Revenue Code establishing standards for the display of taxes in advertisements for air transportation. In addition, the Department is proposing to rescind nine air fare price advertising guidance documents. They have become outdated and unnecessary because entities are bound by statute and regulatory text; furthermore, in certain cases, these documents improperly functioned as de facto regulations without adhering to the notice-and-comment procedures required by the Administrative Procedure Act.

FAA proposes to amend the regulations for certificated mechanics by replacing the inspection authorization with an inspection rating on a mechanic's certificate, similar to the existing airframe and powerplant ratings. The inspection rating would carry the same privileges and limitations as the inspection authorization but would not require renewal or have an expiration date, consistent with the other mechanic ratings. As a result, FAA proposes to require certificated mechanics with inspection ratings to complete rolling recent experience activities, maintained independently, to exercise the privileges of their rating, rather than the current requirements of presenting evidence of renewal activities each March of every odd- numbered year. These proposed changes are intended to align mechanic privileges, which would streamline and simplify the process for maintaining inspection privileges, increase FAA efficiency by reducing on-demand work tasks, and save critical hours for safety-focused missions. These proposed changes would be deregulatory since they would reduce the paperwork and resource burdens linked to complying with the existing regulations for both industry and FAA.

The FAA proposes to supersede Airworthiness Directive (AD) 2023-22-12, which applies to all Dassault Aviation Model FALCON 2000 airplanes. AD 2023-22-12 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2023-22- 12, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This proposed AD would continue to require certain actions in AD 2023-22-12 and would require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA is proposing this AD to address the unsafe condition on these products.

The FAA proposes to supersede Airworthiness Directive (AD) 2023-23-06, which applies to certain Dassault Aviation Model FALCON 2000EX airplanes. AD 2023-23-06 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2023-23-06, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This proposed AD would continue to require certain actions in AD 2023-23-06 and would require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA is proposing this AD to address the unsafe condition on these products.

The FAA proposes to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 747-400 series airplanes. This proposed AD was prompted by reports of potable water leaking into the electrical equipment bay cooling air inlet. This proposed AD would require performing repetitive inspections of potential water sources from the upper deck and the main deck, including potable water and waste water lines, for any water leaks and clogs, and applicable on- condition actions. The FAA is proposing this AD to address the unsafe condition on these products.

This action extends the comment period for the NPRM titled "Designation--Restrict the Operation of Unmanned Aircraft in Close Proximity to a Fixed Site Facility" that was published in the Federal Register on May 6, 2026, to allow commenters additional time to analyze the proposed rule and prepare a response. In the NPRM, FAA proposed a process for operators and proprietors of certain fixed site facilities to request an unmanned aircraft flight restriction (UAFR); criteria to demonstrate the UAFR is necessary for: aviation safety, protection of people and property on the ground, national security, or homeland security; and identified the types of operations allowed in the UAFR.

The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Helicopters Deutschland GmbH (AHD) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, and EC635T2+ helicopters. This proposed AD was prompted by a report of a separated tail rotor blade (TRB) assembly due to a crack caused by intergranular corrosion. This proposed AD would require repetitively inspecting a certain TRB assembly for cracks and, depending on the results, removing any cracked TRB assembly from service and replacing an affected part as terminating action for the repetitive inspections. This proposed AD would also prohibit installing a certain TRB assembly on any helicopter unless certain requirements are met. The FAA is proposing this AD to address the unsafe condition on these products.

The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus SAS Model A330-243, A330-243F, A330-341, A330-342, and A330-343 airplanes. This proposed AD was prompted by reports of cracked and broken restraint brackets of the anti-ice piccolo tube found during maintenance on certain nacelle inlet cowls. This proposed AD would require, for certain affected parts, modification of the affected part, and for certain other affected parts, repetitive special detailed inspections (SDIs) for discrepancies and, depending on findings, modification of the affected part. This proposed AD would also prohibit a certain repair on any affected part and limit the installation of affected parts under certain conditions. The FAA is proposing this AD to address the unsafe condition on these products.

The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Canada Limited Partnership Model BD-500-1A10 and BD- 500-1A11 airplanes. This AD was prompted by the discovery of a low clearance condition between a hydraulic motor pump harness and the airplane structure at the aft fuselage between certain frames, which was found during final airplane assembly. This proposed AD would require modification of the harness installation. The FAA is proposing this AD to address the unsafe condition on these products.

FAA proposes to remove obsolete references to pilot certificates and ratings issued more than 50 years ago.

NHTSA is proposing to amend Federal Motor Vehicle Safety Standard (FMVSS) No. 135, "Light vehicle brake systems." The proposed modifications would distinguish how regulations apply to vehicles with and without manually operated driving controls. The proposed modifications would clarify definitions, telltale requirements, performance requirements, and test procedures in the standard and remove sections that are no longer relevant. The stopping distance performance requirements, which address the primary safety purpose of the standard, would still apply to all subject vehicles. This rulemaking would remove unnecessary regulatory burdens and costs without detriment to vehicle safety.

This action withdraws the notice of proposed rulemaking (NPRM) published in the Federal Register on January 15, 2025, which proposed to establish the Automated Driving System-Equipped Vehicle Safety, Transparency, and Evaluation Program (AV STEP). The proposal would have created a voluntary program for vehicle manufacturers, developers of Automated Driving Systems (ADS), and fleet operators or system integrators of such vehicles. Based on its reevaluation of the proposal, consideration of the comments received, and subsequent progress on other ADS initiatives, NHTSA is withdrawing the rulemaking.

FAA proposes to amend various airworthiness regulations to modernize certain certification standards for transport category airplanes and propulsion systems. This rule would be both deregulatory and relieving by reducing the number of exemptions, special conditions, and equivalent level of safety findings required during the certification process. FAA expects that this proposal would reduce certification costs and time to certify new and changed products for both industry and FAA while maintaining or increasing the level of safety provided by the current regulations. FAA proposes to remove Special Federal Aviation Regulation (SFAR) No. 109 from part 25 and relocate certain of its requirements. Finally, this action would address industry and National Transportation Safety Board recommendations while also harmonizing FAA's regulations with international standards.

The Federal Transit Administration (FTA) is proposing amendments to its bus testing regulation. The proposed changes will improve the efficiency of the testing program for stakeholders, enhance the value of bus testing reports for consumers, and assist in removing outdated test reports.

NHTSA published a final rule on September 17, 2024 that amended the regulation on seat belt assembly anchorages. The final rule updated the test procedure for existing test devices and added an alternative test device as a compliance option. In response to the 2024 final rule, the agency received a petition for reconsideration from the Truck and Engine Manufacturers Association. After considering the petition, NHTSA is proposing to delay the compliance date from September 1, 2027 to September 1, 2030 for vehicles with a Gross Vehicle Weight Rating (GVWR) of greater than 4,536 kg.

This action proposes to establish Class E airspace extending upward from 700 feet above the surface at Tishomingo Airport, Belmont, MS. Controlled airspace is necessary for the safety and management of instrument flight rules (IFR) operations at this airport.

This action proposes to amend domestic Very High Frequency Omnidirectional Range (VOR) Federal Airways V-16, V-94, and V-159, and revoke V-535 in the eastern United States. The FAA is proposing these actions due to the planned decommissioning of the Holly Springs, MS (HLI), VOR/Tactical Air Navigation (VORTAC).

The FAA proposes to adopt a new airworthiness directive (AD) for certain Bell Textron Canada Limited Model 505 helicopters. This proposed AD was prompted by reports that the identification plate affixed to certain tail cone assemblies contains an incorrect part number (P/N), which may not accurately convey the life limit. This proposed AD would require verifying the tail cone assembly part number and, if necessary, replacing the incorrect tail cone assembly identification plate with a new tail cone assembly identification plate containing the correct P/N and updating the existing log card or equivalent record for the helicopter. The FAA is proposing this AD to address the unsafe condition on these products.

This action proposes to establish Canadian Area Navigation (RNAV) Route Q-827, amend Jet Route J-7 and revoke Jet Route J-530 in the vicinity of Great Falls, MT. The FAA is proposing these actions to provide enroute continuity with NAV Canada's ongoing route structure modernization efforts.

The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Helicopters Model AS355E, AS355F, AS355F1, AS355F2, and AS355N helicopters. This proposed AD was prompted by the determination that the tail rotor drive fan wheels (fan wheels) and the impeller second stage have been incorrectly identified during production. This proposed AD would require verifying the serial number and amendment of the log cards of the affected parts, and depending on the findings, performing a one-time borescope inspection to verify consistency between the log cards and the affected parts. Depending on the inspection results, this proposed AD would require replacing or re- identifying certain parts. This proposed AD would also prohibit the installation of certain fan wheels and impeller second stages on any helicopter. The FAA is proposing this AD to address the unsafe condition on these products.

This action proposes to amend Class E airspace over Staunton, VA. This action would expand that portion of the Staunton, VA Class E5 airspace extending to the northwest of Bridgewater Air Park from "within 1.5 miles either side of the 338[deg] bearing from the airport extending from the 8.3-mile radius to 10 miles northwest of the airport" to "within 3.2 miles each side of the 329[deg] bearing from the airport extending from the 8.3-mile radius to 15.2 miles northwest of the airport." This modification is necessary to contain Instrument Flight Rules (IFR) operations utilizing new special instrument approach procedures at Bridgewater Air Park. This action also proposes to update the geographic coordinates for Bridgewater Air Park, Bridgewater, VA in the Staunton, VA Class E5 airspace legal description.

This action proposes to amend the Class D and Class E airspace at Chicago/Rockford, IL. The FAA is proposing this action due to a biennial airspace review conducted pursuant to FAA Order JO 7400.2R, Procedures for Handling Airspace Matters. This action would bring the airspace into compliance with FAA orders and support instrument flight rule (IFR) procedures and operations.

This action proposes to amend the Class D and Class E airspace at Muncie, IN, and revoke Class E airspace at Muncie, IN, and Alexandria, IN. The FAA is proposing this action due to airspace reviews conducted due to the decommissioning of the Muncie very high frequency omnidirectional range (VOR) as part of the VOR Minimum Operational Network (MON) Program, and the cancellation of the instrument procedures at Alexandria Airport, Alexandria, IN. The geographic coordinates and name of Delaware County Regional Airport, Muncie, IN, would also be updated to coincide with the FAA's aeronautical database. This action would bring the airspace into compliance with FAA orders and support instrument flight rule (IFR) procedures and operations.

This action proposes to revoke the Class E airspace at Lake Geneva, WI. The FAA is proposing this action due to the instrument procedures being cancelled and the closure of the airport.

This action proposes to amend the Class E airspace at Bedford, IN. The FAA is proposing this action due to an airspace review conducted due to the decommissioning of the Hoosier very high frequency omnidirectional range (VOR) as part of the VOR Minimum Operational Network (MON) Program. The name of IU Health Bedford Hospital Heliport, Beford, IN, would also be updated to coincide with the FAA's aeronautical database. This action would bring the airspace into compliance with FAA orders and support instrument flight rule (IFR) procedures and operations.

The FAA proposes to supersede Airworthiness Directive (AD) 2025-15-04, which applies to all Gulfstream Aerospace LP Model G150 airplanes. AD 2025-15-04 requires revising the existing maintenance or inspection program, as applicable, to incorporate a new airworthiness limitation. Since the FAA issued AD 2025-15-04, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This proposed AD would continue to require actions in AD 2025-15-04 and would require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA is proposing this AD to address the unsafe condition on these products.

The FAA proposes to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 747-8 series airplanes. This proposed AD was prompted by a report of cracks in the fuselage skin lap splice at the upper fastener row between certain stations at certain stringers. This proposed AD would require performing repetitive external surface high frequency eddy current (HFEC) inspections of the upper fastener row of the fuselage skin lap splice for any crack and applicable on-condition actions. The FAA is proposing this AD to address the unsafe condition on these products.