Official abstract: This action establishes Class E airspace at Graham Hospital Heliport, Canton, IL. This action supports new instrument procedures and instrument flight rule (IFR) operations.
Read the original on FederalRegister.gov →Official abstract: The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to certain The Boeing Company Model 787-8, 787-9, and 787-10 airplanes. As published, a paragraph reference specified in the regulatory text is incorrect. This document corrects that error. In all other respects, the original document remains the same.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain MD Helicopters, LLC (MDHI) Model 369D, 369E, 369F, 369FF, 369H, and 500N helicopters. This AD was prompted by a report of mechanical damage to the main transmission drive shaft coupling (coupling). This AD requires 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 issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain General Electric Company (GE) Model CF34-8C1, CF34-8C5, CF34- 8C5A1, CF34-8C5A2, CF34-8C5B1, CF34-8E2, CF34-8E2A1, CF34-8E5, CF34- 8E5A1, CF34-8E5A2, CF34-8E5A2HA, CF34-8E6, and CF34-8E6A1 engines. This AD was prompted by reports of in-flight "Engine Degraded" messages from the engine indicating and crew alerting system (EICAS) due to corrosion of the variable geometry (VG) system actuator. This AD requires removing certain electronic engine control (EEC) full authority digital electronic control (FADEC) software versions from service and installing an updated EEC FADEC software that is eligible for installation. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: This action establishes Class E airspace at Mason District Hospital Heliport, Havana, IL. This action supports new instrument procedures and instrument flight rule (IFR) operations.
Read the original on FederalRegister.gov →Official abstract: This action revokes Class E airspace at Diamond "O" Ranch Airport, Santa Elena, TX. This action supports the instrument procedures being cancelled and the decommissioning of the Santa Elena radio beacon (RBN).
Read the original on FederalRegister.gov →Official abstract: This action establishes Class E airspace at Northwestern Memorial Healthcare Heliport, DeKalb, IL. This action supports new instrument procedures and instrument flight rule (IFR) operations.
Read the original on FederalRegister.gov →Official abstract: This action administratively corrects identified final rules published by FAA in the Federal Register between May and September 2026 so that certain published airspace designation amendments are transferred to the most-current revision of FAA Order JO 7400.11, which is incorporated by reference.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Helicopters Model AS350B3, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. This proposed AD was prompted by a report of the loss of the tightening torque between the upper ball bearing end and a main rotor (MR) servo-control. This proposed AD would require an inspection of the nut tightening torque of the upper ball bearing end of all the MR servo-controls and, depending on the results, corrective actions. The proposed AD would also require reporting the inspection results. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to supersede Airworthiness Directive (AD) 2025-09-07, which applies to certain Airbus SAS Model A330-243, -243F, -841, and -941 airplanes. AD 2025-09-07 requires revising the existing airplane flight manual (AFM) by providing instructions to address dual loss of radio management panel (RMP) data synchronization, and the existing minimum equipment list (MEL) by removing relief for an inoperative RMP 3. Since the FAA issued AD 2025-09-07, a modification that addresses the unsafe condition has been developed. This proposed AD would continue to require the actions specified in AD 2025-09-07 and would require modifying the airplane. This proposed AD also reduces the applicability. This proposed AD would also prohibit the installation of affected parts under certain conditions. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD was prompted by reports from multiple operators of pitch oscillation events due to excessive horizontal stabilizer freeplay. This AD requires measuring the freeplay of the horizontal stabilizer pivot hinges and the jackscrew and applicable on- condition actions. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD was prompted by a report that some passenger service unit (PSU)-mounted video monitors became detached from the PSU rails during a hard landing. This AD requires replacing PSU-mounted video monitors that do not have secondary retention lanyards. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is superseding Airworthiness Directive (AD) 2025-04- 05, which applied to all Airbus SAS Model A330-841 and -941 airplanes. AD 2025-04-05 required a revision of the existing airplane flight manual (AFM) and removal of the previously required limitations; a revision of the existing minimum equipment list (MEL); one-time or repetitive seal integrity tests of each engine bleed air system (EBAS) high pressure valve (HPV); additional maintenance instructions and corrective actions; and repetitive replacement of affected HPV clips; as applicable. AD 2025-04-05 also limited the installation of affected HPV clips. Since the FAA issued AD 2025-04-05, an improved EBAS HPV with unaffected HPV clips was certified, and it was determined that the bleed monitoring computer (BMC) software (SW) must be updated. This AD continues to require the actions in AD 2025-04-05, except for repetitive replacement of affected HPV clips. This AD also requires updating the BMC SW, additional work, and an additional revision of the existing MEL for the engine bleed overpressure valve; as applicable. This AD also prohibits the installation of certain BMC software. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: 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 a report indicating that the protection system on the left fan cowl of the right engine does not sufficiently cover the components and systems from possible cross engine debris. This AD requires performing a maintenance records check or inspection of the right engine to determine the part number of the left fan cowl and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A330-243, A330-243F, A330-341, A330-342, A330-343, A330-841, and A330-941 airplanes; and Model A340-211, A340-212, A340- 213, A340-311, A340-312, A340-313, A340-541, and A340-642 airplanes. This AD was prompted by reports of leaks on closed fuel low pressure shut-off valves (LPSOVs). This AD requires repetitive leak checks of certain fuel LPSOVs and replacement of an affected part if any discrepancy is detected. This AD also allows the installation of an affected part under certain conditions. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to supersede Airworthiness Directive (AD) 2026-09-02, which applies to certain Pratt & Whitney RTX Corporation (PW) Model PW4074, PW4074D, PW4077, PW4077D, PW4084D, PW4090, and PW4090-3 engines. AD 2026-09-02 requires repetitive angle ultrasonic scan inspections (AUSIs) of the high-pressure compressor (HPC) 15th- stage disks, front turbine hubs, high-pressure turbine (HPT) 1st-stage air seals, and HPT 2nd-stage hubs for crack indications, and removal from service and replacement if necessary, and for certain serial numbers, removal from service and replacement of the HPT 1st-stage air seal. Since the FAA issued AD 2026-09-02, the FAA was notified that a certain part number was omitted from AD 2026-09-02 and the applicability of the optional terminating action was matched to an unrelated requirement. This proposed AD would require repetitive AUSIs of the HPC 15th-stage disks, front turbine hubs, HPT 1st-stage air seals, and HPT 2nd-stage hubs for crack indications, and removal from service and replacement if necessary, and for certain serial numbers, removal from service and replacement of the HPT 1st-stage air seal. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for all Pratt & Whitney Division (PW) Model PW4052, PW4056, PW4060, PW4060A, PW4060C, PW4062, PW4062A, PW4152, PW4156, PW4156A, PW4158, PW4460, and PW4462 engines. This AD was prompted by multiple reports of tailpipe fire, loss of thrust control, and engine in-flight shutdown due to undetected deterioration of pressure burner (Pb) sensors. This AD requires replacing Pb sensors. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is superseding Airworthiness Directive (AD) 2009-04-13 for certain Rolls-Royce Deutschland Ltd & Co KG (RRD) Model BR700- 715A1-30, BR700-715B1-30, and BR700-715C1-30 engines. AD 2009-04-13 required 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 required 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 AD requires 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 issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: This action revokes Very High Frequency (VHF) Omnidirectional Range (VOR) Federal Airway V-320 in Alaska due to navigational signal limits causing portions of this route to be unusable. There are two routes with the identifier V-320, one located in the state of Alaska, and one located in the state of Michigan. This action only revokes the V-320 located in Alaska. FAA is also establishing United States Area Navigation (RNAV) Route T-550 near Anchorage, AK.
Read the original on FederalRegister.gov →Official abstract: This action establishes restricted areas R-5306G and R-5306H at Marine Corps Air Station (MCAS), Cherry Point, NC. This action also amends R-5306C and R-5306D by modifying two latitude/longitude coordinates and amends the controlling agency for R-5306A, R-5306C, R- 5306D, and R-5306E to reflect MCAS Cherry Point Combined Center Radar Approach Control (CERAP).
Read the original on FederalRegister.gov →Official abstract: This action establishes Class E airspace at Ranch at Double Gates Airport, Coleman, TX. This action supports new instrument procedures and instrument flight rule (IFR) operations.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Helicopters Deutschland GmbH (AHD) Model MBB-BK 117 D-2 helicopters. This proposed AD was prompted by certification test results of a certain common cargo hook beam (CCHB) on the affected helicopters, which revealed that the installed CCHB could result in fuel leakage following a survivable accident. This proposed AD would require modification of the CCHB and fuel system and installation of structural reinforcement. This proposed AD would also prohibit installing a certain CCHB on any helicopter. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: 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.
Read the original on FederalRegister.gov →Official abstract: 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.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus SAS Model A318 series airplanes; Model A319 series airplanes; Model A320 series airplanes; and Model A321 series airplanes. This proposed AD was prompted by reports of door evacuation slide systems failing to inflate during emergency evacuations, due to the fracture and separation of the connector on the inflation hose assembly. This proposed AD would require the replacement of each affected slide with a serviceable slide. This proposed AD would also prohibit the installation of affected parts. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to supersede Airworthiness Directive (AD) 2024-05-06, which applies to all Leonardo S.p.a Model AW169 helicopters. AD 2024-05-06 requires revising the airworthiness limitations section (ALS) of the existing helicopter maintenance manual (MM) or instructions for continued airworthiness (ICA) and the existing approved maintenance or inspection program for the helicopter. Since the FAA issued AD 2024-05-06, it was determined that incorrect material was referenced to revise the ALS. This proposed AD would require revising the ALS of the existing MM or ICA and the existing approved maintenance or inspection program. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-700-2A12 airplanes. This AD was prompted by reports of low clearance in the right wing between the fuel line flexible coupling and the harness support bracket clip-nut, between the fuel line flexible coupling and hydraulic system, and between the hydraulic system and fuel vent tube. This AD requires rectifying the low clearance condition between the fuel line flexible coupling and the harness support bracket clip-nut, rectifying the low clearance condition between the fuel line flexible coupling and the hydraulic system, and doing an inspection for adequate clearance between the hydraulic system and the fuel vent tube and applicable on-conditions actions. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is withdrawing a notice of proposed rulemaking (NPRM) that proposed to adopt a new airworthiness directive (AD) that would have applied to certain The Boeing Company Model 787-8, 787-9, and 787-10 airplanes. The NPRM was prompted by reports that very high frequency (VHF) radio frequencies transfer between the active and standby windows of the tuning control panel (TCP) without flightcrew input. The uncommanded frequency changes could result in missed communications between the flightcrew and Air Traffic Control. The NPRM would have required updating the TCP operational software (OPS) and performing a software configuration check. Since issuance of the NPRM, the FAA has determined that the TCP OPS version specified in the NPRM does not correct the unsafe condition. Accordingly, the NPRM is withdrawn.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for certain Baykar Piaggio Aerospace S.p.A. (Piaggio) Model P-180 airplanes. This proposed AD was prompted by a report of corrosion and cracks found around the head of attaching fasteners on main wing lower skin external reinforcement doublers. This proposed AD would require repetitive high frequency eddy current (HFEC) inspections of the lower skin reinforcement and, depending on findings, corrective action. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: This action amends domestic Very High Frequency Omnidirectional Range (VOR) Federal Airways V-16, V-35, V-37, V-53, V- 133, V-136, V-143, V-259, V-310, V-364, V-409, V-415, V-454, and V-605. The FAA is taking this action due to the decommissioning of the Charlotte, NC (CLT), VOR/Distance Measuring Equipment (VOR/DME); Foothills, SC (ODF), VOR/DME; Holston Mountain, TN (HMV), VOR/Tactical Air Navigation (VORTAC); and the relocation of the Spartanburg, SC (SPA), VORTAC.
Read the original on FederalRegister.gov →Official abstract: This action amends geographic coordinates for boundary points listed in the airspace descriptions for restricted areas R-5301, R- 5302B, and R-5302C to correct minor discrepancies that resulted in gaps and overlaps between the areas. This action does not expand any external boundaries or change any altitudes, times of designation, or activities conducted within the restricted areas.
Read the original on FederalRegister.gov →Official abstract: In accordance with the National Environmental Policy Act of 1969, as amended (NEPA) and FAA Order 1050.1G, FAA National Environmental Policy Act Implementing Procedures, FAA is announcing its intent to prepare a PEIS analyzing Space Exploration Technologies Corp.'s (SpaceX) proposal to increase Starship-Super Heavy operations at the Boca Chica Launch Site at Starbase, TX and expand Starship landing and expenditure locations. Subsequent license modifications or renewals under 14 CFR part 400 are within the scope of the PEIS, and the issuance of temporary airspace closures associated with the Proposed Action are included in FAA's Federal Action. FAA is requesting comments concerning the scope and content of the PEIS. A Draft PEIS will be released for public review and comment at a later date.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to supersede Airworthiness Directive (AD) 2024-18-01, which applies to Leonardo S.p.A. Model A119 and AW119 MKII helicopters. AD 2024-18-01 requires repetitive inspections of certain collective stick torque tube assemblies for deficiencies and corrective action, as applicable. Since the FAA issued AD 2024-18-01, an improved collective stick torque tube assembly was designed, and replacement instructions were issued. This proposed AD would require repetitive inspections of certain collective stick torque tube assemblies and, depending on the results of the inspection, replacement of affected parts. This proposed AD would also require modification of the helicopter through replacement of an affected part with a serviceable part, which would constitute terminating action for the repetitive inspections. This proposed AD would also prohibit installation of an affected part on any helicopter. The FAA is proposing this airworthiness directive (AD) to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Helicopters Model H160-B helicopters. This proposed AD was prompted by a report of the inability to operate the jettisoning function of a window due to a blocked jettisoning mechanism. This proposed AD would require removing the jettisonable windows, cleaning the ropes of the jettisonable windows, and performing an operational test of the windows jettison systems. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for all Rolls-Royce Deutschland Ltd & Co KG (RRD) Model RB211 Trent 768-60, 772-60, and 772B-60 engines. This AD was prompted by a report that a batch of low-pressure compressor (LPC) blades were exposed to a non- conforming repair and are more prone to cracking due to a deviation from the approved blade configuration design. This AD requires removal from service of the affected LPC blades and replacement with a serviceable part. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The Federal Aviation Administration (FAA) considered a proposal to permanently close the Indianapolis Downtown Heliport and change 5.36 acres of land from aeronautical use to non-aeronautical use and to authorize the sale of the heliport property located at the Indianapolis Downtown Heliport (8A4/Heliport), Indianapolis, Indiana. This notice is published pursuant to 49 U.S.C. 46319, Permanent Closure of an Airport without Providing Sufficient Notice, and 49 U.S.C. 47107(h)(2), Public Notice Before Waiver of Aeronautical Land-Use Assurance. The Indianapolis Airport Authority (IAA/Authority/Sponsor) submitted a request to release the Authority from its Federal Airport Improvement Program (AIP) obligations associated with Indianapolis Downtown Heliport. Upon reconsideration of its initial decision, the FAA has determined the AIP obligations associated with 8A4 will not be released.
Read the original on FederalRegister.gov →Official abstract: This action amends United States Area Navigation (RNAV) Route T-437 in the eastern United States. 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).
Read the original on FederalRegister.gov →Official abstract: This action amends Jet Routes J-83 and J-85 in the eastern United States. This action supports the Spartanburg, SC (SPA), Very High Frequency Omnidirectional Range/Tactical Air Navigation (VORTAC) relocation project.
Read the original on FederalRegister.gov →Official abstract: The FAA, in cooperation with the United States Air Force, is announcing the public review/comment period and public workshops for the ATAAPS DEA for the proposed Anchorage terminal airspace redesign. ATAAPS involves changes to the airspace, aircraft flight paths, and aircraft altitudes in the Anchorage basin and surrounding areas. The DEA evaluates the potential environmental impacts of the proposed airspace redesign (Proposed Action) and the No Action alternative. The FAA has not made a final decision on any airspace/procedure amendments related to the Proposed Action. A copy of the DEA, appendices, and the Workshop announcements will be posted to the FAA ATAAPS web page at: https://www.faa.gov/about/office_org/headquarters_offices/ara/ alaskan_region/ataaps. Early notification of the FAA's intent to prepare a DEA was published in the Federal Register on July 16, 2026 (91 FR 43723, FR Doc. 2026-14367). In accordance with the National Environmental Policy Act of 1969, 42 U.S.C. 4321 et seq., and in accordance with FAA Order 1050.1G, FAA National Environmental Policy Act Implementing Procedures, the FAA issues this notice that it has prepared a DEA for the ATAAPS project and has made it available for public review and comments. The ATAAPS Project would improve safety and efficiency of the National Airspace System (NAS) and homeland defense capabilities, by optimizing aircraft arrival and departure procedures that serve multiple airports--specifically in the Anchorage basin and surrounding areas--including: Ted Stevens Anchorage International Airport (ANC), Elmendorf Air Force Base Airport (EDF), Bryant Army Airfield Airport (FRN), Lake Hood Airport (LHD), and Merrill Field Airport (MRI). As a critical strategic gateway for homeland defense, Joint Base Elmendorf-Richardson (JBER) is currently restricted from operating at its intended capacity and fleet mix until the surrounding airspace is officially modified. The Instrument Landing System (ILS) for Runway 17 is integral to improving JBER operations, but cannot become operational under the current airspace design. (JBER runway designations are currently 16/34 and 06/24; Runway 16/34 will be updated due to Magnetic Variation changes to Runway 17/35 before completion of the Final Rule).
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for all Elixir Aircraft Model Elixir airplanes. This AD was prompted by a fatal accident on a Model Elixir airplane during a production flight. The cause of the accident is still under investigation. This AD prohibits operation until approved inspection or modification procedures are identified, accomplished, and incorporated. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: Under this notice, FAA announces the submission deadline of October 16, 2026, for Summer 2027 flight schedules at Chicago O'Hare International Airport (ORD), John F. Kennedy International Airport (JFK), Los Angeles International Airport (LAX), Newark Liberty International Airport (EWR), and San Francisco International Airport (SFO).
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Deutschland GmbH (AHD) Model MBB-BK 117 C-1 helicopters. This AD was prompted by a report of a louver box assembly detaching in flight due to incorrect installation. This AD requires repetitively accomplishing a play check of the affected louver box assembly and, depending on the results of the check, accomplishing corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus SAS Model A350-941 and -1041 airplanes. This proposed AD was prompted by a girt bar fitting safety hook on an airplane in the production line was found stuck in the upward position due to excessive sealant applied between the girt bar fitting and door mat. This proposed AD would require a detailed inspection of each affected part and applicable corrective actions, and provide additional requirements for maintenance. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus SAS Model A318, A319, A320, and A321 series airplanes. This proposed AD was prompted by a finding that severe corrosion could occur on affected slotted nuts located at the wing thrust spigots. This proposed AD would require repetitive inspections of the affected slotted nuts and applicable corrective actions. This proposed AD would also prohibit the installation of affected parts. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is superseding Airworthiness Directive (AD) 2019-20- 07, which applied to The Boeing Company Model 787-8, 787-9, and 787-10 airplanes. AD 2019-20-07 required repetitive operational checks of the leading edge (LE) outboard (OB) slats and applicable on-condition actions. AD 2019-20-07 also required revising the airplane flight manual (AFM) to prohibit flap retraction under icing conditions after landing and revising the existing maintenance or inspection program, as applicable, to incorporate a new operation check. This AD was prompted by the manufacturer developing further actions to address the unsafe condition. This AD continues to require all requirements of AD 2019-20- 07. This AD would also require replacing the LE outboard geared rotary actuator (GRA) with a LE outboard lockout actuator (LEOLA) at leading edge OB slat locations and revising the existing maintenance or inspection program, as applicable, to incorporate a new certification maintenance requirement (CMR), which terminates the retained requirements of AD 2019-20-07. This AD also removes airplanes from the applicability. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for all helicopters equipped with a radio (also known as radar) altimeter. This proposed 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 to 3.98 GHz frequency band (5G Lower C-Band) while operating in Canadian airspace. This proposed AD would require revising the existing rotorcraft flight manual (RFM) for the helicopter to incorporate limitations prohibiting certain operations requiring radio altimeter data when operating within Canadian airspace. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain Engine Alliance (EA) Model GP7270, GP7272, and GP7277 engines. This AD was prompted by a report of an aborted takeoff that resulted from an uncontained failure of the high-pressure turbine (HPT) interstage seal. This AD requires removal from service and replacement of the HPT interstage seal with a part eligible for installation. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: Federal Aviation Administration (FAA) is granting JetBlue Airways Corporation's (JetBlue) and Spirit Airlines, LLC's (Spirit) (together, the carriers) joint petition for an exemption from the prohibition on transferring Operating Authorizations (slots) at LaGuardia Airport (LGA) beyond the duration of the applicable order. The relief permits the carriers to consummate a transaction in which Spirit would transfer to JetBlue 22 slots at LGA. The relief is granted on the condition that JetBlue is prohibited from leasing or trading any of those 22 slots to any carrier until after April 2028.
Read the original on FederalRegister.gov →Official abstract: The FAA is revising a notice of proposed rulemaking (NPRM) to supersede Airworthiness Directive (AD) 2014-16-22 and AD 2017-25-13, which apply to certain Airbus SAS Model A330-200, A330-200 Freighter, A330-300, A340-200, A340-300, A340-500, and A340-600 series airplanes; and AD 2024-25-11, which applies to certain Airbus SAS Model A330-200, A330-200 Freighter, A330-300, A330-800 and A330-900 series airplanes. This action revises the NPRM by referencing later service information with new or more restrictive airworthiness limitations and expanding the applicability. The FAA is proposing this airworthiness directive (AD) to address the unsafe condition on these products. Since these actions would impose an additional burden over those in the NPRM, the FAA is requesting comments on this SNPRM.
Read the original on FederalRegister.gov →Official abstract: This notice contains a summary of a petition seeking relief from specified requirements of Federal Aviation Regulations. The purpose of this notice is to improve the public's awareness of, and participation in, the FAA's exemption process. Neither publication of this notice nor the inclusion nor omission of information in the summary is intended to affect the legal status of the petition or its final disposition.
Read the original on FederalRegister.gov →Official abstract: The FAA is considering a request from the Santa Maria Public Airport District to waive the requirement that 35 (+/-) acres of surplus airport property located at the Santa Maria Public Airport in Santa Maria, California, from the requirement that it be used for aeronautical purposes. The release, if approved, would allow the property to be sold at Fair Market Value (FMV) for compatible non- aeronautical use.
Read the original on FederalRegister.gov →Official abstract: In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval for a new information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on May 11, 2026. The collection involves voluntarily reporting when National Airspace System (NAS) surface weather systems (AWOS and ASOS) experience operational issues, such as erroneous data or full outages. The information to be collected will be used to verify and track these errors and outages, and publish the status onto the FAA's Surface Weather Status Dashboard for user awareness.
Read the original on FederalRegister.gov →Official abstract: This action establishes Class E airspace at OSF St Francis Medical Center Heliport, Peoria, IL. This action supports new instrument procedures and instrument flight rule (IFR) operations.
Read the original on FederalRegister.gov →Official abstract: This action proposes to modify the Class E airspace designated as a surface area, the Class E airspace area designated as an extension to a Class E surface area, and the Class E airspace area extending upward from 700 feet above the surface at Gunnison-Crested Butte Regional Airport, Gunnison, CO. These actions would support the safety and management of instrument flight rules (IFR) operations at the airport.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to supersede Airworthiness Directive (AD) 2026-12-09, which applies to all Airbus Helicopters Model AS350B, AS350BA, AS350B1, and AS350D helicopters. AD 2026-12-09 requires revising the airworthiness limitations section (ALS) of the existing maintenance manual (MM) or instructions for continued airworthiness (ICA) and the existing approved maintenance or inspection program, as applicable. Since the FAA issued AD 2026-12-09, a determination was made that new and more restrictive airworthiness limitations and maintenance tasks are necessary. This proposed AD would require incorporating these airworthiness limitations into the ALS of the existing MM or ICA and the existing approved maintenance or inspection program, as applicable. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to supersede Airworthiness Directive (AD) 2025-13-08, which applies to all DG Aviation GmbH Model DG-1000T gliders. AD 2025-13-08 requires revising the glider flight manual and installing "Motor INOP" placards to prohibit operation with the powerplant. Since issuance of AD 2025-13-08, a design improvement to the propeller adapter ring has been developed that is considered terminating action for the operational prohibition of AD 2025-13-08. This proposed AD would retain the requirement to revise the flight manual, would provide an optional terminating action for the retained actions by incorporating a specified modification, would allow removal of the "Motor INOP" placards following accomplishment of that optional terminating action, and would require removal, inspection, and reinstallation of the propeller adapter disk, including installation of safety pins. This proposed AD would also prohibit the installation of affected propeller adapter rings. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: FAA proposes to amend its commercial space launch and reentry licensing regulations to streamline the licensing process and reduce regulatory burden for license applicants. Specifically, FAA proposes to amend the regulations to state that a far-field overpressure blast effects analysis required for license applicants does not need to account for members of the public in hypothetical locations.
Read the original on FederalRegister.gov →Official abstract: FAA proposes to amend its commercial space launch and reentry licensing regulations to streamline the licensing process and reduce regulatory burden for license applicants. Specifically, FAA proposes to add an exception for compliance with lightning hazard mitigation requirements for certain licensed launch and reentry operations.
Read the original on FederalRegister.gov →Official abstract: FAA proposes to amend its commercial space launch and reentry licensing regulations to streamline the licensing process. Specifically, FAA proposes to alleviate regulatory burden for license applicants by consolidating information required for an operator's flight safety analysis.
Read the original on FederalRegister.gov →Official abstract: FAA proposes to amend its commercial space launch and reentry licensing regulations to allow for submission of license and permit applications and requests for waivers, alternative time frames, and safety element approvals through additional electronic methods.
Read the original on FederalRegister.gov →Official abstract: FAA proposes to amend its commercial space launch and reentry licensing regulations to streamline the licensing process and reduce regulatory burden on operators. Specifically, FAA proposes to relieve the burden by specifying that, when using physical containment as a hazard control strategy, operators do not need to develop flight hazard areas in accordance with FAA's existing flight hazard area analysis requirements.
Read the original on FederalRegister.gov →Official abstract: This action proposes to amend domestic Very High Frequency Omnidirectional Range (VOR) Federal Airways V-16, V-184, and revoke V- 284 and V-577 in the eastern United States. The FAA is proposing these actions due to the planned decommissioning of the Cedar Lake, NJ (VCN), VOR/Distance Measuring Equipment (DME).
Read the original on FederalRegister.gov →Official abstract: This action proposes special conditions for the Honda Aircraft Company LLC (Honda) Model HA-480 airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for normal category airplanes. This airplane will have design features associated with high altitude operations up to 47,000 feet. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed 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.
Read the original on FederalRegister.gov →Official abstract: The Federal Aviation Administration (FAA) is announcing the availability of Advisory Circular (AC) 187-1V which transmits an updated schedule of charges for services of FAA Flight Standards Aviation Safety Inspectors outside the United States. The advisory circular has been updated in accordance with the procedures listed in 14 CFR part 187, Appendix A.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to rule and invites public comment on the release and sale of two parcels of land at the Liberal Mid-America Regional Airport (LBL), Liberal, Kansas, under the provisions of 49 U.S.C. 47107(h)(2).
Read the original on FederalRegister.gov →Official abstract: This notice announces the FAA's intent to designate VanDyke Russell Supplemental Type Certificate (STC) No. SA176CE as abandoned and make the related engineering data available upon request. The FAA has been unsuccessful in contacting VanDyke Russell concerning the STC. This action is intended to enhance aviation safety.
Read the original on FederalRegister.gov →Official abstract: In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The collection involves practices that permitted certificated air carriers to operate two-engine airplanes over long range routes. The FAA uses this information collection to ensure that aircraft for long range flights are equipped to minimize diversions, to preclude and prevent diversions in remote areas, and to ensure that all personnel are trained to minimize any adverse impacts of a diversion.
Read the original on FederalRegister.gov →Official abstract: In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on April 24, 2026. The information collected is used to determine program compliance or non-compliance of regulated aviation employers and contractors (including certificated foreign repair stations that must comply with the FAA's final rule, Drug and Alcohol Testing of Certificated Repair Station Employees Located Outside of the United States), conduct oversight planning, determine employers required to provide annual Management Information System (MIS) testing information, and communicate with entities subject to the program regulations.
Read the original on FederalRegister.gov →Official abstract: This action proposes to amend Class D airspace for Maxwell Air Force Base (AFB), Montgomery, AL, by making administrative updates. It also proposes to amend Class E airspace from 700 feet by expanding it by 0.5 NM from a 7-mile to a 7.5-mile radius around Maxwell AFB to contain IFR departures, along with making administrative changes. Finally, it proposes to revoke Class E airspace from the surface around Maxwell AFB, as the airport no longer meets the qualifications for Class E surface area airspace. Controlled airspace is necessary for the safety and management of instrument flight rules (IFR) operations in the area.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 757-300 series airplanes. This AD was prompted by a crack growth analysis that indicated that existing maintenance planning data (MPD) and supplemental structural inspection program (SSIP) tasks do not provide adequate inspection opportunities to detect cracks in the upper frames around the uppermost fastener common to the fail-safe chord at the fuselage frame splices. This AD requires an inspection or maintenance record check for existing repairs, repetitive inspections of the upper frames around the uppermost fastener common to the fail-safe chord at the fuselage frame splices for any cracks, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is superseding Airworthiness Directive (AD) 2021-03- 08, which applied to certain Airbus SAS Model A350-941 and -1041 airplanes. AD 2021-03-08 required repetitive inspections for migration of the bushings of the horizontal tail plane (HTP) lateral load fittings (LLFs) on the left- and right-hand sides and terminating repair or modification of any affected bushing. Since the FAA issued AD 2021-03-08, new occurrences of bushing migration on HTP LLFs were reported, and a determination was made that certain repairs can no longer be considered terminating action to the repetitive inspections. This AD continues to require the actions in AD 2021-03-08, removes a certain terminating action, and expands the applicability. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: 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.
Read the original on FederalRegister.gov →Official abstract: 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.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC120B, and EC130B4 helicopters. This AD was prompted by a determination that the instructions on how to open the sliding door emergency exit on affected helicopters are insufficient. This AD requires installing additional safety labels or replacing existing safety labels, as applicable. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain Leonardo S.p.a. Model AB139 and AW139 helicopters. This AD was prompted by a report of a nozzle exhaust duct clamp separating from the engine nozzle duct and coming to rest on the tail rotor (TR) drive shaft. This AD requires repetitively inspecting certain clamp assemblies and, depending on the results of the inspection, replacing parts. This AD also prohibits the installation of an affected clamp assembly, unless certain requirements are met. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval for a new information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on June 16, 2025. The collection involves application for a Special Purpose Pilot Authorization (SPPA) submitted to the FAA for the purpose of performing pilot duties on a civil aircraft of the United States and leased by a non-U.S. citizen. The information to be collected will be used to determine applicant eligibility for the issuance of a SPPA under 14 CFR part 61, Section 61.77.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS355E, AS355F, AS355F1, AS355F2, and AS355N helicopters. This 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 AD requires 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 results of the inspection, this AD requires replacing or re-identifying certain parts. This AD also prohibits the installation of certain fan wheels and impeller second stages on any helicopter. The FAA is issuing this AD to address the unsafe conditions on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to supersede Airworthiness Directive (AD) 2024-05-13, which applied to all Embraer S.A. Model EMB-545 and EMB-550 airplanes. AD 2024-05-13 requires revising the Limitations and Normal Procedures sections of the existing airplane flight manual (AFM) to incorporate new operational airspeed limitations, and flight control limitations and approach procedures when angle of attack (AOA) limiter protection is engaged. AD 2024-05-13 also requires inspecting records for instances of AOA limiter engagement during a certain phase of flight and reporting findings to the FAA. Since the FAA issued AD 2024- 05-13, the manufacturer developed a modification to the flight control computer (FCC) software and related AFM revisions. This proposed AD would continue to require certain actions in AD 2024-05-13. This proposed AD would also require updating the FCC software and incorporating a new revision of the existing AFM, which would terminate the operational airspeed limitations, and flight control limitations and approach procedures when AOA limiter protection is engaged. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to supersede Airworthiness Directive (AD) 2026-10-16, which applies to all Airbus Helicopters Model AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. AD 2026-10- 16 requires revising the airworthiness limitations section (ALS) of the existing maintenance manual (MM) or instructions for continued airworthiness (ICA) and the existing approved maintenance or inspection program, as applicable. Since the FAA issued AD 2026-10-16, a determination was made that new or more restrictive airworthiness limitations and maintenance tasks are necessary. This proposed AD would require incorporating these airworthiness limitations into the ALS of the existing MM or ICA and the existing approved maintenance or inspection program, as applicable. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is hosting an Industry Engagement Event for a Spectrum Interference Detection Solution October 13-15, 2026. The FAA will use the information from vendor responses during event registration to assist in determining any future phases of market investigation and engagement. The FAA does not commit to an acquisition with this notice.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for certain Vulcanair S.p.A. Model P.68 and P.68B airplanes. This proposed AD was prompted by a report of fuel starvation that resulted in an uncommanded in-flight engine shutdown. This proposed AD would require, for certain airplanes, modification of the fuel level indicator and, for all airplanes, calibration of the fuel level indicator, installation of new quantity and warning placards, and updating the aircraft flight manual (AFM) and the aircraft maintenance manual (AMM). The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for certain 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 loss of the tail rotor controls due to a broken control rod of the yaw actuator. This proposed AD would require a one-time inspection of the ball pivot, yaw actuator assembly, and associated parts, and a repetitive inspection of the ball pivot. Depending on the inspection results, this proposed AD would require replacement of affected parts, further inspections, and application of new sealing compound. This proposed AD would also prohibit the installation of an affected part unless it is a serviceable part and certain requirements are met. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for certain Bell Textron Canada Limited (Bell) Model 505 helicopters. This proposed AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This proposed AD would require revising the airworthiness limitation schedule (ALS) of the existing maintenance manual (MM) or instructions for continued airworthiness (ICA) and the existing approved maintenance or inspection program, as applicable. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to supersede Airworthiness Directive (AD) 2025-17-06, which applies to certain Airbus SAS Model A330-200 series airplanes, A330-200 Freighter series airplanes, A330-300 series airplanes, A330-841 airplanes, and A330-941 airplanes. AD 2025-17-06 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2025-17-06, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This proposed AD 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.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787-8 and 787-9 airplanes. This AD was prompted by a report of the lack of data to substantiate engine operability when an airplane is dispatched under a certain master minimum equipment list (MMEL) item. This AD prohibits dispatching an airplane under the operational procedures of the operator's minimum equipment list item corresponding to a certain MMEL item. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: In accordance with the National Environmental Policy Act of 1969, as amended (NEPA), FAA Order 1050.1G, FAA National Environmental Policy Act Implementing Procedures, and Department of War (DoW) and Department of the Air Force (DAF) NEPA Implementing Procedures, FAA is announcing its intent to prepare a Supplemental Environmental Impact Statement (SEIS) concerning Space Exploration Technologies Corp.'s (SpaceX) proposal obtain a modification to their existing vehicle operator license from the FAA to authorize commercial Starship-Super Heavy operations at Space Launch Complex 37 (SLC-37) at Cape Canaveral Space Force Station (CCSFS). This SEIS supports FAA's adoption of the Final Environmental Impact Statement for the SpaceX Starship-Super Heavy Cape Canaveral Space Force Station (2025 DAF EIS), EIS Identification Number: EISX-007-057-USF-1730277197. The proposed operations would include up to 76 Starship-Super Heavy launches and up to 152 landings per year (up to 76 Super Heavy Booster and up to 76 Starship vehicle landings), including return-to-launch-site (RTLS) and ocean landings. FAA is requesting comments concerning the scope and content of the SEIS. A Draft SEIS will be released for public review and comment later.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for certain Leonardo S.p.a. Model AW189 helicopters. This proposed AD was prompted by reports that the safety pin of the emergency flotation system and life raft was installed on the cylinder valve of the life raft bottle assembly. This proposed AD would require inspecting the left-hand (LH) side and right-hand (RH) side of the life raft bottle assembly and, depending on the inspection results, removing the safety pin from the cylinder valve. This proposed AD would also prohibit extended overwater flights until the corrective actions are accomplished. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to all MD Helicopters, LLC Model 369, 369A, 369D, 369E, 369F, 369FF, 369H, 369HE, 369HM, 369HS, 500N, and 600N helicopters. As published, the header of the regulatory text is missing the AD number and the amendment number. This document corrects those errors. In all other respects, the original document remains the same.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to supersede Airworthiness Directive (AD) 2025-13-06, which applies to certain Airbus Helicopters Deutschland GmbH (AHD) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, and EC635T2+ helicopters. AD 2025-13-06 requires inspections of the ball pivot, control rod, and yaw actuator assembly and, depending on the results of these inspections, corrective actions. AD 2025-13-06 also prohibits installing an affected part unless it is a serviceable part and certain requirements are met. Since the FAA issued AD 2025-13-06, the manufacturer developed a repetitive inspection of the ball pivot. This proposed AD would retain some of the actions of AD 2025-13-06 and would require repetitive inspection of the ball pivot and, depending on the results of those inspections, corrective actions. This proposed AD would also prohibit installing an affected part unless it is a serviceable part and certain requirements are met. Additionally, this proposed AD would require reporting the results of the inspections. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: In accordance with the National Environmental Policy Act of 1969, as amended (NEPA), DOT Order 5610.1D, DOT's Procedures for Considering Environmental Impacts, and FAA Order 1050.1G, FAA National Environmental Policy Act Implementing Procedures, the FAA is announcing the availability of and requesting comment on the Draft Environmental Assessment Blue Origin New Glenn Cadence Increase at Space Launch Complex 36A, Cape Canaveral Space Force Station, Florida (Draft EA).
Read the original on FederalRegister.gov →Official abstract: Based on safety concerns and a review that revealed widespread non-compliance with the exemptions, the FAA is announcing its decision to cease issuing exemptions that allow certain Cessna aircraft that require two pilots to operate as a single-pilot operation, and notifying current exemption holders that their exemptions will be rescinded by separate action. This notice also serves to inform pilots who obtained single-pilot endorsements from training providers that held exemptions that they must cease single-pilot operations in aircraft that require two pilots under the regulations as they have no relief from the regulations.
Read the original on FederalRegister.gov →Official abstract: This action supplements a notice of proposed rulemaking (NPRM) published by the FAA in the Federal Register on June 17, 2025, which proposed to establish Class E domestic en route airspace (Class E6) within a designated landmass and within 12 miles from a designated shoreline associated with the state of Alaska to facilitate the vectoring of instrument flight rules (IFR) aircraft on direct routes where the current en route structure is insufficient or improper within the proposed airspace areas. As revised in this SNPRM, the FAA now proposes to establish five discrete areas of Class E domestic en route airspace over the state. Due to redundancy, the NPRM also proposed to remove two Class E6 airspace areas and modify 101 Class E airspace areas extending upward from at least 700 feet or more above the surface of the earth (Class E5) to remove any portion extending upward from 1,200 feet above the surface. This SNPRM continues to propose these actions, but also now proposes to remove two Class E airspace areas extending upward from 1,200 feet above the surface, revoke a duplicate Class E5 airspace legal description, and redefine airspace areas from a "Point of Origin" instead of using their respective airport reference points. Finally, both the NPRM and this SNPRM propose administrative amendments to the legal descriptions of 101 Class E5 airspace areas that would correct or update nomenclature as needed. This action would support IFR operations while enhancing the safety and management of aircraft operations within the National Airspace System (NAS).
Read the original on FederalRegister.gov →Official abstract: The FAA is superseding Airworthiness Directive (AD) 2023-15-03 for all Safran Helicopter Engines, S.A. (Safran) Model Arrius 2B2 engines. AD 2023-15-03 required revising the airworthiness limitations section (ALS) of the existing engine maintenance manual (EMM) or instructions for continued airworthiness (ICA) and the existing approved maintenance or inspection program, as applicable, by incorporating the actions and associated thresholds and intervals, including life limits. Since the FAA issued AD 2023-15-03, the manufacturer has revised the ALS of the existing maintenance and overhaul manuals, introducing new and more restrictive instructions and maintenance tasks. This AD requires updating the ALS of the existing EMM or ICA and the existing approved maintenance or inspection program, as applicable, by incorporating the actions and associated thresholds and intervals, including life limits. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain H[eacute]licopt[egrave]res Guimbal (HG) Model Cabri G2 helicopters. This AD was prompted by a report of a potential malfunction of the helicopter emergency locator transmitter (ELT) and subsequent findings of weak ELT signals on 121.5 MHz and 406 MHz frequencies due to improper antenna installation (location). This AD requires revising the existing rotorcraft flight manual (RFM) for the helicopter. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain Costruzioni Aeronautiche Tecnam S.p.A. (Tecnam) Model P2006T airplanes. This AD was prompted by a report of partial detachment of the left aileron due to a missing hinge pin. This AD requires a one- time detailed visual inspection of the affected aileron hinges for damage (cracks, warping of the hinges or hinge pin, scratched paint, missing or broken torque stripe, etc.) and cotter pins for improper installation and, depending on the findings, applicable corrective action. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Model EC 130 T2 helicopters. This AD was prompted by the determination that helicopter operators received main rotor blades (MRB) that are not certified to be installed on their helicopters and thus, without instructions for continued airworthiness, cannot be properly maintained. This AD requires replacing the affected parts with serviceable parts and prohibits installing the affected MRBs on Airbus Helicopters Model EC 130 T2 helicopters. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting 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 AD was prompted by a determination that in cases of loss of oil from the main gearbox (MGB), the low pressure caution or warning light might not activate. This AD requires revising the existing rotorcraft flight manual (RFM) for the helicopter by incorporating updated emergency, malfunction, and normal procedures. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: 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 a report that cargo liner joint sealing tape could be missing in particular areas on certain airplanes. The absence of this tape could allow a fire to propagate into the cabin. This AD requires a detailed inspection of these areas for the missing tape, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 777-200, -200LR, -300, -300ER, and 777F series airplanes. This AD was prompted by a report of an overheated alternating current motor pump (ACMP) that caused a fire in the main landing gear (MLG) wheel well. This AD requires a records check or inspection for any installed ACMP with a certain part number and applicable on-condition actions. This AD also prohibits the installation of affected parts. The FAA is issuing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →Official abstract: The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Helicopters Model AS 365 N2, AS 365 N3, EC 155 B, EC 155 B1, SA 365 N, and SA 365 N1 helicopters. This proposed AD was prompted by gaps between the seals and engine cowling, which were found during an investigation related to an engine compartment fire. Gaps between the seals and engine cowling could cause inadequate sealing of the engine compartment firewalls leading to fire propagation between engine compartments and reduced effectiveness of the extinguishing agent. This proposed AD would require modifying the engine compartment firewalls by installing angle-brackets along the firewalls. The FAA is proposing this AD to address the unsafe condition on these products.
Read the original on FederalRegister.gov →