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Browse 1,000 rules and proposed rules from the Federal Register.
1,000
Total Regulations
Showing 841–870 of 1,000
Page 29 / 34
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 FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A350-941 and -1041 airplanes. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in a 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 superseding Airworthiness Directive (AD) 2015-02- 14, which applied to all Airbus SAS Model A318 series airplanes; A319- 111, -112, -113, -114, -115, -131, -132, and -133 airplanes; A320-211, -212, -214, -231, -232, and -233 airplanes; and A321-111, -112, -131, - 211, -212, -213, -231, and -232 airplanes. AD 2015-02-14 required repetitive inspections for cracking, damage, correct installation, and correct adjustment of the main landing gear (MLG) door hinge and actuator fittings on the keel beam, corrective actions if necessary, and revision of the existing maintenance or inspection program, as applicable. Since the FAA issued AD 2015-02-14, a new design of the MLG door keel beam hinge and actuator fitting was developed. This AD continues to require the actions specified in AD 2015-02-14, adds an optional terminating action, and revises the applicability, as specified in a 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 superseding Airworthiness Directive (AD) 2023-10- 08, which applied to all ATR--GIE Avions de Transport R[eacute]gional Model ATR42-200, -300, and -320 airplanes. AD 2023-10-08 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2023-10-08, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This AD continues to require certain actions in AD 2023-10-08 and requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in a 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 superseding Airworthiness Directive (AD) 2006-20- 08, which applied to all Embraer S.A. Model EMB-145, -145ER, -145MR, - 145LR, -145XR, -145MP, and -145EP airplanes. AD 2006-20-08 required repetitive inspections to detect cracking or failure of the rod ends and fittings of the aileron power control actuator (PCA), and corrective actions if necessary, and provided an optional terminating action. This AD was prompted by a determination that there was an error in identifying a maintenance task number. This AD continues to require the actions in AD 2006-20-08 and corrects an error in a task number, as specified in an Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
This action proposes to amend the Class D and Class E2 surface airspace at Hickory Regional Airport, Hickory, NC, by increasing the radius to 4.6-miles and establishing an extension to the surface area due to standard instrument approach procedure and runway configuration changes. Additionally, this action would amend Class E5 airspace extending upward from 700 feet above the surface for Hickory Regional Airport, Hickory, NC, by increasing the radius to 7.1 miles and adding an extension. Lastly, this action would also amend Class E airspace extending upward from 700 feet above the surface for Foothills Regional Airport, Morganton, NC, ensuring the required protection for standard instrument approach procedures, and would also update the airport's name and geographic coordinates and remove Grace Hospital from the description. Controlled airspace is necessary for the safety and management of instrument flight rules (IFR) operations in the area.
The FAA is adopting a new airworthiness directive (AD) for all General Electric Company (GE) Model CF34-10E2A1, CF34-10E5, CF34- 10E5A1, CF34-10E6, CF34-10E6A1, CF34-10E7, and CF34-10E7-B engines with certain part-numbered high-pressure turbine (HPT) shroud/low pressure turbine (LPT) nozzle assemblies installed. This AD was prompted by a report of failed retention features of the inner and outer support air ducts (commonly referred to as spoolies) discovered during engine disassembly. This AD requires a visual inspection of the combustion case for wear and gouges, repair if necessary, and rework of the affected HPT shroud/LPT nozzle assemblies to add a positive retention of the support air duct. The FAA is issuing this AD to address the unsafe condition on these products.
This action revises an earlier notice of proposed rulemaking (NPRM) that the FAA published in Federal Register on February 27, 2025, by adding the proposed amendment of United States Area Navigation (RNAV) Route T-705 in the eastern United States. Additionally, this SNPRM proposes to add the EEGOR, CT, waypoint (WP) to RNAV Route T-461. This action continues to propose the changes to RNAV routes Q-64 and T- 414, and the establishment of new RNAV route T-463, as described in the original NPRM. This action supports FAA Next Generation Air Transportation System (NextGen) efforts to provide a modern RNAV route structure to improve the safety and efficiency of the National Airspace System (NAS).
The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A321-111, -112, -131, -211, -212, -213, -231, -232, -251N, -252N, -253N, -271N, -272N, -251NX, -252NX, -253NX, -271NX, and -272NX airplanes. This AD was prompted by the identification of an erroneous value of the main landing gear (MLG) tire width in the aircraft data files used for aircraft performance computation. This AD requires revising the existing airplane flight manual (AFM) to incorporate a complementary performance data file (CPDF) update as specified in a 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.
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 proposes to supersede Airworthiness Directive (AD) 2019-19-13, which applies to certain Airbus Helicopters Model EC225LP helicopters. AD 2019-19-13 requires determining the total hours time- in-service (TIS) of the free wheel shafts of certain main rotor gearboxes (MGBs), replacing the MGB or right-hand side (RH) free wheel shaft, installing placard(s), and revising the Rotorcraft Flight Manual (RFM) for the helicopter. Since the FAA issued AD 2019-19-13, an additional part-numbered MGB has been identified to have the same unsafe condition and the FAA determined that additional changes are necessary. This proposed AD would require the actions of AD 2019-19-13 and, expand the applicability by adding the additional part-numbered MGB, change the requirement to determine the total hours TIS of a certain free wheel shaft, require repetitive replacement of the MGB or the RH free wheel shaft, change the requirements for who can replace parts, and expand the parts installation limitation conditions. The FAA is proposing this AD to address the unsafe condition on these products.
This action revokes Alaskan Very High Frequency Omnidirectional Range (VOR) Federal Airway V-414 and amends United States Area Navigation (RNAV) Routes T-248 and T-250 in Alaska. These actions are due to the decommissioning of the Nondirectional Radio Beacon (NDB) portion of the Gambell NDB/distance measuring equipment (DME) in Alaska.
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus SAS Model A350-941 and A350-1041 airplanes. This proposed AD was prompted by reports of mechanical noises originating from the nose landing gear (NLG) shock absorber during ground maneuvers. This proposed AD would require repetitive inspections (i.e., steering checks) of the NLG shock absorber and applicable on-condition actions 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 proposed AD was prompted by reports that the interface pin of the secondary load path in the upper gimbal of the horizontal stabilizer trim actuator (HSTA) was incorrectly installed. This proposed AD would require a detailed visual inspection of the interface pin of the HSTA to determine if the interface pin is incorrectly installed, and applicable on-condition actions as specified in a Transport Canada AD, which is proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products.
PHMSA is publishing this advance notice of proposed rulemaking to solicit stakeholder feedback on potential opportunities to improve the cost-effectiveness of its repair requirements for gas transmission and hazardous liquid or carbon dioxide pipelines. PHMSA also seeks stakeholder feedback on authorizing a risk-based approach for determining the inspection interval for in-service breakout tanks.
This action amends the Class E airspace at Payson, AZ. This action is the result of an airspace review conducted due to the decommissioning of the Payson non directional beacon (NDB). This action also updates the name and geographic coordinates of the airport to coincide with the FAA's aeronautical database. This action brings the airspace into compliance with FAA orders and supports instrument flight rule (IFR) procedures and operations.
This action amends domestic Very High Frequency Omnidirectional Range (VOR) Federal Airways V-1, V-29, V-38, V-139, and V-286 in the eastern United States. The FAA is taking this action due to the planned decommissioning of the Salisbury, MD (SBY), VOR/Tactical Air Navigation (VORTAC) and the Snow Hill, MD (SWL), VORTAC. This action is in support of the FAA's VOR Minimum Operational Network (MON) Program.
As directed by the Executive order of January 20, 2025, "Restoring Names that Honor American Greatness," PHMSA is amending its regulations to change the name of the body of water known previously as the "Gulf of Mexico" to the "Gulf of America."
This document announces the availability of ASTM International (ASTM) consensus standards for use as an FAA-accepted MOC to the applicable airworthiness standards for normal category airplanes. The FAA accepts ASTM F3264-24, "Standard Specification for Normal Category Aeroplanes Certification," with changes identified in this document.
The FAA is adopting a new airworthiness directive (AD) for certain General Electric Company (GE) Model CF6-80E1A2, CF6-80E1A3, CF6-80E1A4, and CF6-80E1A4/B engines. This AD was prompted by a manufacturer investigation that revealed certain high-pressure turbine (HPT) stage 1 and HPT stage 2 disks were manufactured from powder metal material suspected to contain iron inclusion. This AD requires replacement of affected HPT stage 1 and HPT stage 2 disks with parts eligible for installation. The FAA is issuing this AD to address the unsafe condition on these products.
This action amends domestic Very High Frequency Omnidirectional Range (VOR) Federal Airways V-7, V-35, V-157, V-159, and V-198 in the eastern United States. The FAA is taking this action due to the planned decommissioning of the Cross City, FL (CTY), VOR/ Tactical Air Navigation (VORTAC) and the Taylor, FL (TAY), VORTAC. This action is in support of the FAA's VOR Minimum Operational Network (MON) Program.
The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-700-1A10 airplanes. This proposed AD was prompted by a report indicating that the clearance between therapeutic flexible oxygen hoses and electrical harnesses may be non-compliant to design requirements, and that positive separation mechanisms and appropriate protective barriers may not have been installed in accordance with the applicable installation standards. This proposed AD would require a detailed inspection of the therapeutic flexible oxygen hose for damage and protection, and the electrical harnesses for damage; a detailed inspection for the clearance between the therapeutic oxygen rigid tube to oxygen hose elbow fitting (also referred to as elbow fitting), if applicable, and the nearest electrical harness, and between the therapeutic flexible oxygen hose and electrical harness; and applicable related investigative and corrective actions. The FAA is proposing this AD to address the unsafe condition on these products.
The FAA proposes to supersede Airworthiness Directive (AD) 2020-06-18, which applies to all Airbus SAS Model A318 series airplanes; A319 series airplanes; A320-211, -212, -214, -216, -231, - 232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes; and A321 series airplanes. AD 2020-06-18 requires replacement of affected trimmable horizontal stabilizer actuators (THSAs) with serviceable THSAs. Since the FAA issued AD 2020-06-18, a new Airbus airplane model (A321-253NY) has been certified, on which affected parts could be installed in service. This proposed AD would continue to require the actions in AD 2020-06-18, would revise the applicability to include Model A321-253NY airplanes, and would prohibit the installation of affected parts, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products.
This action amends Very High Frequency Omnidirectional Range (VOR) Federal Airways V-161, V-163, and V-568; and establishes United States Area Navigation (RNAV) Route T-545. The FAA is taking this action due to the planned decommissioning of the VOR portion of the Three Rivers, TX (THX), VOR/Tactical Air Navigation (VORTAC) navigational aid (NAVAID). The Three Rivers VOR is being decommissioned in support of the FAA's VOR Minimum Operational Network (MON) program.
This action revokes Colored Federal Airway Amber 16 (A-16) in the northern United States. The FAA is taking this action due to the decommissioning of the White Rock, British Columbia (BC), Canada, Nondirectional Radio Beacon (NDB).
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus SAS Model A319-112 and -132 airplanes, and Model A320-214, -232, -233, -251N, and -271N airplanes. This proposed AD was prompted by rivet holes being left unplugged after bracket relocation or removal accomplished during certain modifications, potentially resulting in fatigue damage starting from those rivet holes. This proposed AD would require a one-time special detailed inspection (SDI) of the rivet holes and applicable corrective actions; and would also allow the installation of certain modifications, provided rivets are installed after the modification; as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products.
This action revises a notice of proposed rulemaking (NPRM) published in the Federal Register on January 7, 2025. As revised, this action proposes to modify the Class E airspace area designated as surface area, modify the Class E airspace area designated as an extension to a Class D or Class E surface area, and modify the Class E airspace extending upward from 700 feet or more above the surface of the earth at Battle Mountain Airport, Battle Mountain, NV. Additionally, this action proposes administrative amendments to update the airport's existing Class E airspace legal descriptions. These actions would support the safety and management of instrument flight rules (IFR) operations at the airport.
The FAA proposes to adopt a new airworthiness directive (AD) for all Gulfstream Aerospace Corporation Model GVI airplanes. This proposed AD was prompted by a determination that new and more restrictive airworthiness limitations are necessary. This AD requires revising the existing maintenance or inspection program, as applicable, to incorporate new and 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) 2022-15-05, which applies 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 2022-15-05 requires repetitive high frequency eddy current (HFEC) inspections for cracks on the web horizontal flange and inner cap, and applicable corrective actions. Since the FAA issued AD 2022-15-05, additional cracks have been found at the door stop fitting number 1 holes at frame (FR) 68, after disassembly of the door stop fitting as part of the inspections required by AD 2022-15-05. This proposed AD would continue to require the actions in AD 2022-15-05, but with reduced compliances times for some inspections, and would require an additional inspection at door stop fitting number 1, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference. The FAA is proposing this AD to address the unsafe condition on these products.
This action amends Jet Routes J-26, J-64, and J-181, and Very High Frequency Omnidirectional Range (VOR) Federal Airways V-10 and V- 156; and revokes VOR Federal Airway V-262. The FAA is taking this action due to the planned decommissioning of the VOR portion of the Bradford, IL (BDF), VOR/Tactical Air Navigation (VORTAC) navigational aid (NAVAID). The Bradford VOR is being decommissioned in support of the FAA's VOR Minimum Operational Network (MON) program.