Federal Aviation Administration December 9, 2024 – Federal Register Recent Federal Regulation Documents

Amendment of VOR Federal Airways V-68, V-76, V-212, V-222, and V-558, and United States Area Navigation Route T-220 in the Vicinity of Industry, TX
Document Number: 2024-28750
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
This action amends Very High Frequency Omnidirectional Range (VOR) Federal Airways V-68, V-212, and V-222, and United States Area Navigation (RNAV) Route T-220; and revokes VOR Federal Airway V-558. The proposed V-76 airway amendment is removed from this action due to the amendment already being accomplished by a separate airspace docket action. The FAA is taking this action due to the planned decommissioning of the VOR portion of the Industry, TX (IDU), VOR/ Tactical Air Navigation (VORTAC) navigational aid (NAVAID). The Industry VOR is being decommissioned in support of the FAA's VOR Minimum Operational Network (MON) Program.
Amendment of Jet Route J-538 and VOR Federal Airways V-129; Establishment of Canadian RNAV Routes Q-828, Q-945, Q-971, and T-797; and Revocation of Jet Routes J-483 and J-562; Northcentral United States
Document Number: 2024-28727
Type: Proposed Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend Jet Route J-538 and Very High Frequency Omnidirectional Range (VOR) Federal Airway V-129; establish Canadian Area Navigation (RNAV) Routes Q-828, Q-945, Q-971, and T-797 within United States (U.S.) airspace; and revoke Jet Routes J-483 and J-562. The FAA is proposing this action due to NAV CANADA's decommissioning of the Sioux Narrows (VBI), Ontario (ON), Canada, Very High Frequency Omnidirectional Range (VOR)/Distance Measuring Equipment (VOR/DME) navigational aid (NAVAID) and the planned decommissioning of the Lumsden (VLN), Saskatchewan (SK), Canada, VOR/Tactical Air Navigation (VORTAC) and Brandon (YBR), Manitoba (MB), Canada, VORTAC NAVAIDs. This action is proposed in support of NAV CANADA's NAVAID Modernization Program within Canada.
Amendment of Jet Routes J-60 and J-82, and VOR Federal Airways V-8, V-55, and V-221; and Revocation of VOR Federal Airways V-92 and V-126 in the Vicinity of Goshen, IN
Document Number: 2024-28726
Type: Proposed Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend Jet Routes J-60 and J-82, and Very High Frequency Omnidirectional Range (VOR) Federal Airways V-8, V- 55, and V-221; and revoke VOR Federal Airways V-92 and V-126. The FAA is proposing this action due to the planned decommissioning of the VOR portion of the Goshen, IN (GSH), VOR/Tactical Air Navigation (VORTAC) navigational aid (NAVAID). The Goshen VOR is being decommissioned in support of the FAA's VOR Minimum Operational Network (MON) program.
Amendment of Jet Routes J-26, J-64 and J-181, and VOR Federal Airways V-10 and V-156; and Revocation of VOR Federal Airway V-262 in the Vicinity of Bradford, IL
Document Number: 2024-28725
Type: Proposed Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend Jet Routes J-26, J-64, and J- 181, and Very High Frequency Omnidirectional Range (VOR) Federal Airways V-10 and V-156; and to revoke VOR Federal Airway V-262. The FAA is proposing 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.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2024-28780
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model MD-11 and MD-11F airplanes. This AD was prompted by a report of a Model MD-11F airplane experiencing an uncommanded deployment of a thrust reverser in flight at low altitude. This AD requires initial and repetitive detailed inspections and repetitive wire integrity tests of the engine pylon thrust reverser control system wire harnesses, junction box assembly and junction box cover, left-side and right-side thrust reverser electrical harnesses, core (engine compartment) miscellaneous wire harness assembly, and 30- degree bulkhead wire harness assembly; and applicable on-condition actions. This AD also requires reporting inspection results. The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus SAS Airplanes
Document Number: 2024-28779
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A321-251NX, -252NX, -253NX, -271NX, and -272NX airplanes. This AD was prompted by the discovery during a quality review performed during manufacturing, that a torque strip indicator (material "Dykem") had been applied on the orifice fitting on certain slides' inflation reservoirs' venting holes. This AD requires an inspection for discrepancies of affected parts (certain reservoirs having certain orifices) and replacement of discrepant affected parts, and prohibits installing affected parts, 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.
Airworthiness Directives; Airbus SAS Airplanes
Document Number: 2024-28759
Type: Proposed Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus SAS Model 330-200, A330-200 Freighter, and A330-300 series airplanes. This proposed AD was prompted by a report of contamination of the advanced pneumatic detector pressure switch of engine pylon fire detectors. This proposed AD would require replacement of the affected parts and would prohibit 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.
Airworthiness Directives; Airbus SAS Airplanes
Document Number: 2024-28758
Type: Proposed Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for 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. This proposed AD was prompted by cracks being found during full-scale fatigue testing of the keel beam bottom panel between the edge profile and stringer run- out at a certain frame and stringer. This proposed AD would require repetitive special detailed inspections (SDI) of the affected area, and corrective actions if necessary, 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.
Airworthiness Directives; Airbus SAS Airplanes
Document Number: 2024-28790
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding Airworthiness Directive (AD) 2023-05- 02, which applied to certain Airbus SAS Model A318, A319, A320, and A321 series airplanes. AD 2023-05-02 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. 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 additional 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.
Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
Document Number: 2024-28789
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain ATRGIE Avions de Transport R[eacute]gional Model ATR42 and ATR72 airplanes. This AD was prompted by a report that for airplanes converted from passenger to cargo configuration using certain supplemental type certificates, no height limitation for the cargo, when loaded in the cargo compartment, is defined, and that as a consequence, cargo might be loaded up to the ceiling of the cargo compartment. This AD requires modification of the cargo compartment and implementation of updated cargo loading procedures. The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
Document Number: 2024-28788
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding Airworthiness Directive (AD) 2023-03- 09, which applied to certain ATR-GIE Avions de Transport R[eacute]gional Model ATR72-101, -102, -201, -202, -211, -212, and - 212A airplanes. AD 2023-03-09 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. This AD was prompted a determination that new or more restrictive airworthiness limitations are necessary. This AD continues to require the actions in AD 2023-03- 09 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.
Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes
Document Number: 2024-28787
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding Airworthiness Directive (AD) 2018-18- 09, which applied to all Airbus Defense and Space S.A. Model CN-235, CN-235-100, CN-235-200, and CN-235-300 airplanes; and certain Model C- 295 airplanes. AD 2018-18-09 required a detailed inspection of the upper and lower lugs of each horizontal stabilizer-to-fuselage rear attachment fitting, repair if necessary, and a report of findings. This AD was prompted by reports of new occurrences of cracking. This AD requires repetitive inspections, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD also revises the applicability. The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Document Number: 2024-28786
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain MHI RJ Aviation ULC Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This AD was prompted by a determination that the overhead bin attachment could fail under certain conditions. This AD requires replacing existing overhead bin hook assemblies and support tubes with a different type, as specified in a Transport Canada AD, which is incorporated by reference (IBR). The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Airplanes
Document Number: 2024-28785
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting 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 multiple occurrences of pilot and co-pilot seats locking in a fore-aft position due to the seat fore- aft adjustment mechanism disconnecting, caused by a broken cotter pin in the seat base egress linkage. This AD requires modifying the pilot and co-pilot seats by replacing the hardware of the seat base egress linkage, as specified in a Transport Canada AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2024-28782
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 757-200, -200CB, and -200PF series airplanes. This AD was prompted by a crack growth analysis, which indicated that current inspections are not adequate to detect cracks in certain sections of the upper frame at the frame splice between certain stringers before a single frame fails. This AD requires an inspection or records review for existing repairs, repetitive inspections for cracks of the upper frame at the frame splices between certain stringers in certain sections, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2024-28781
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 767-300F series airplanes. This AD was prompted by a determination that certain cargo compartment insulation blankets do not adequately fit some locations and allow smoke to migrate past the cargo compartment sidewall liners and upward into the main cabin. This AD requires replacing cargo compartment insulation blankets. The FAA is issuing this AD to address the unsafe condition on these products.
Amendment of VOR Federal Airways V-38, V-133, and V-144, and Revocation of VOR Federal Airway V-214 in the Vicinity of Zanesville, OH
Document Number: 2024-28724
Type: Proposed Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend Very High Frequency Omnidirectional Range (VOR) Federal Airways V-38, V-133, and V-144; and to revoke VOR Federal Airway V-214. The FAA is proposing this action due to the planned decommissioning of the VOR portion of the Zanesville, OH (ZZV), VOR/Distance Measuring Equipment (VOR/DME) navigational aid (NAVAID). The Zanesville VOR is being decommissioned in support of the FAA's VOR Minimum Operational Network (MON) program.
IFR Altitudes; Miscellaneous Amendments
Document Number: 2024-28429
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
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.
Airworthiness Directives; Airbus SAS Airplanes
Document Number: 2024-28791
Type: Rule
Date: 2024-12-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding Airworthiness Directive (AD) 2022-24- 05, which applied to all Airbus SAS Model A318, A319, A320, and A321 series airplanes. AD 2022-24-05 required repetitive inspections of certain galleys for corrosion of trolley retainer aluminum blocks and delamination of the upper panel of the trolley compartment, and applicable corrective action. This AD was prompted by the list of affected galleys being revised, and a new modification that was developed to restore the design integrity of the affected galleys. This AD continues to require the actions in AD 2022-24-05, provides optional terminating action for the repetitive inspections, revises the list of affected parts, and prohibits the installation of affected parts under certain conditions; 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.
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