Federal Aviation Administration 2022 – Federal Register Recent Federal Regulation Documents
Results 701 - 750 of 1,089
Airworthiness Directives; The Boeing Company Airplanes
The FAA proposes to supersede Airworthiness Directive (AD) 2015-12-03, which applies to certain The Boeing Company Model 777-200, -200LR, -300, and -300ER series airplanes. AD 2015-12-03 requires repetitive freeplay inspections and lubrication of the right and left elevators, rudder, and rudder tab, and related investigative and corrective actions if necessary. Since the FAA issued AD 2015-12-03, engineering testing revealed that the force being applied to the elevator to detect excessive freeplay was insufficient. This proposed AD would continue to require certain actions in AD 2015-12-03 for certain airplanes, and would require revising the existing maintenance or inspection program, as applicable, for certain other airplanes, to incorporate a revised or new elevator freeplay maintenance procedure, as applicable. This proposed AD would also add airplanes to the applicability. The FAA is proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; International Aero Engines, LLC Turbofan Engines
The FAA proposes to adopt a new airworthiness directive (AD) for certain International Aero Engines, LLC (IAE LLC) PW1122G-JM, PW1124G1-JM, PW1124G-JM, PW1127G1-JM, PW1127GA-JM, PW1127G-JM, PW1129G- JM, PW1130G-JM, PW1133GA-JM, and PW1133G-JM model turbofan engines. This proposed AD was prompted by an analysis of an event involving an International Aero Engines AG (IAE AG) V2533-A5 model turbofan engine, which experienced an uncontained failure of a high-pressure turbine (HPT) 1st-stage disk that resulted in high-energy debris penetrating the engine cowling. This proposed AD would require performance of an ultrasonic inspection (USI) of the HPT 1st-stage disk and HPT 2nd-stage disk and, depending on the results of the inspections, replacement of the HPT 1st-stage disk or HPT 2nd-stage disk. The FAA is proposing this AD to address the unsafe condition on these products.
Special Conditions: Dassault Aviation Model Falcon 6X Airplane; Electronic-System Security Protection From Unauthorized Internal Access
These special conditions are issued for the Dassault Aviation (Dassault) Model Falcon 6X airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is a digital systems architecture for the installation of a system with wireless and hardwired network and hosted application functionality that allows access, from sources internal to the airplane, to the airplane's internal electronic components. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Proposed Establishment of United States Area Navigation (RNAV) Route T-378; Fort Yukon, AK
This action proposes to establish United States Area Navigation (RNAV) route T-378 in the vicinity of Fort Yukon, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Proposed Establishment of United States Area Navigation (RNAV) Route T-377; Sitka, AK
This action proposes to establish United States Area Navigation (RNAV) route T-377 in the vicinity of Sitka, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Proposed Establishment of United States Area Navigation (RNAV) Route T-371; Kodiak, AK
This action proposes to establish United States Area Navigation (RNAV) route T-371 in the vicinity of Kodiak, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Proposed Amendment of United States Area Navigation (RNAV) Route T-230; St. Paul Island, AK
This action proposes to amend United States Area Navigation (RNAV) route T-230 in the vicinity of St. Paul Island, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Proposed Establishment of United States Area Navigation (RNAV) Route T-388; Port Heiden, AK
This action proposes to establish United States Area Navigation (RNAV) route T-388 in the vicinity of Port Heiden, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Proposed Establishment of United States Area Navigation (RNAV) Route T-386; Fairbanks, AK
This action proposes to establish United States Area Navigation (RNAV) route T-386 in the vicinity of Fairbanks, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Proposed Establishment of United States Area Navigation (RNAV) Route T-383; Sitka, AK
This action proposes to establish United States Area Navigation (RNAV) route T-383 in the vicinity of Sitka, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Proposed Establishment of United States Area Navigation (RNAV) Route T-380; Emmonak, AK
This action proposes to establish United States Area Navigation (RNAV) route T-380 in the vicinity of Emmonak, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Airworthiness Directives; Airbus Helicopters
The FAA is removing Airworthiness Directive (AD) 2021-03-16, which applied to all Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. AD 2021-03-16 required inspecting each sliding door and replacing the upper rail or front roller or removing the front roller from service if necessary. Since the FAA issued AD 2021-03-16, inspection results and further investigation have confirmed that the in-flight loss of a sliding door, which prompted AD 2021-03-16, was an isolated case resulting from incorrect operation and maintenance error. Therefore, the FAA has determined that no unsafe condition is likely to exist or develop on the sliding doors on other helicopters in the fleet. Accordingly, AD 2021-03-16 is removed.
Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. This proposed AD was prompted by reports of broken P- clamps on the pressure relief line and the motive flow line in the fuel tanks, and a subsequent determination that certain service information lacked instructions for maintaining appropriate clearance between certain fuel tubes and their support brackets, and may also have led to incorrect installation of certain TeflonTM sleeves. This proposed AD was also prompted by a determination that new or more restrictive airworthiness limitations are necessary. This proposed AD would require inspecting the motive flow line, vent line, and related parts, and adding support or additional clearance if necessary. This proposed AD would also require inspection, and replacement or relocation if necessary, of affected TeflonTM sleeves on the vent line, and installation of TeflonTM sleeves on the vent line at additional wing stations. This proposed AD would also 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.
Special Conditions: Dassault Aviation Model Falcon 6X Airplane; Flight Envelope Protection, High-Speed Limiting
These special conditions are issued for the Dassault Aviation (Dassault) Model Falcon 6X airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is an overspeed protection system in the normal mode, designed to prevent the pilot from inadvertently or intentionally exceeding certain airplane speeds. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. This special conditions document contains the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Proposed Amendment of United States Area Navigation (RNAV) Route T-282; Ruby, AK
This action proposes to amend United States Area Navigation (RNAV) route T-282 in the vicinity of Ruby, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Proposed Amendment of United States Area Navigation (RNAV) Route T-242; Utqiagvik, AK
This action proposes to amend United States Area Navigation (RNAV) route T-242 in the vicinity of Utqiagvik, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Proposed Establishment of United States Area Navigation Route T-379; Discovery, AK
This action proposes to establish United States Area Navigation (RNAV) route T-379 in the vicinity of Discovery, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Special Conditions: Dassault Aviation Model Falcon 6X Airplane; Interaction of Systems and Structures
These special conditions are issued for the Dassault Aviation (Dassault) Model Falcon 6X airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is installed systems that, directly or as a result of failure or malfunction, affect airplane structural performance. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Proposed Amendment of Class E Airspace; Rangeley, ME
This action proposes to amend Class E airspace extending upward from 700 feet above the surface at Stephen A. Bean Municipal Airport, Rangeley, ME, due to the decommissioning of the Rangeley non- directional beacon (NDB) and cancellation of associated approaches, as well as updating the airport's name and geographic coordinates. Controlled airspace is necessary for the safety and management of instrument flight rules (IFR) operations in the area.
Special Conditions: Dassault Aviation Model Falcon 6X, Limit Pilot Forces-Side-Stick Controller
These special conditions are issued for the Dassault Aviation (Dassault) Model Falcon 6X airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This airplane is equipped with an electronic flight-control system that includes pilot controls through a side stick instead of through a conventional wheel or control stick. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Airworthiness Directives; Bell Textron Inc., Helicopters
The FAA is adopting a new airworthiness directive (AD) for Bell Textron Inc., Model 412, 412EP, and 412CF helicopters. This AD was prompted by evaluation results showing flight loads that impact the collective lever fatigue life. This AD requires adding a permanent hours time-in-service (TIS) penalty for certain collective levers and prohibits installing those collective levers unless the permanent hours TIS penalty has been added. The FAA is issuing this AD to address the unsafe condition on these products.
Proposed Establishment of Class D Airspace; Chicago/Romeoville, IL
This action proposes to establish Class D airspace at Chicago/ Romeoville, IL. The FAA is proposing this action to support the establishment of an air traffic control tower at Lewis University Airport, Chicago/Romeoville, IL.
Proposed Amendment of Class E Airspace; Kansas City, MO
This action proposes to amend the Class E airspace at Kansas City, MO. The FAA is proposing this action as the result of a biennial airspace review.
Airworthiness Directives; Alexander Schleicher GmbH & Co. Segelflugzeugbau Gliders
The FAA proposes to adopt a new airworthiness directive (AD) for all Alexander Schleicher GmbH & Co. Segelflugzeugbau Model ASW-15 gliders. This proposed AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as wing root damage. This proposed AD would require repetitively inspecting the wing root ribs for cracks, looseness, and damage and replacing any root rib with a crack, a loose rib or lift pin bushing, or any damage. The FAA is proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; British Aerospace (Operations) Limited and British Aerospace Regional Aircraft Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for all British Aerospace (Operations) Limited Model Jetstream Model 3101 and British Aerospace Regional Aircraft Model Jetstream Model 3201 airplanes. This proposed AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as stress corrosion cracking of the primary flight control cable terminals. This proposed AD would require repetitively inspecting the turnbuckle type control cable terminals in the rudder and elevator primary flight control circuits for corrosion, pitting, and cracking and, depending on the inspection results, replacing an affected cable assembly. The FAA is proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier Inc. and de Havilland, Inc.) Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Viking Air Limited (type certificate previously held by Bombardier Inc. and de Havilland, Inc.) Model DHC-6-1, DHC-6-100, DHC- 6-200, DHC-6-300, and DHC-6-400 airplanes. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as binding of the rod end bearing connecting the lower fuel control unit (FCU) push rod assembly to the FCU power lever. This proposed AD would require performing tests, inspections, and lubrication of the FCU push rod assemblies, and replacing them with improved parts as necessary. The FAA is proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters
The FAA is superseding Airworthiness Directive (AD) 2020-20- 06, which applied to certain Bell Helicopter Textron Canada Limited (now Bell Textron Canada Limited) Model 429 helicopters. AD 2020-20-06 required repetitive inspections of certain cyclic and collective assembly bearings. This AD was prompted by new bellcrank assemblies, which have been upgraded with corrosion resistant steel bearings. This AD retains certain requirements of AD 2020-20-06, and depending on the inspection results, requires removing certain parts from service and installing the upgraded cyclic and collective bellcrank assemblies. This AD also requires installing the upgraded collective and cyclic bellcrank assemblies on certain helicopters if not already installed, and prohibits installing certain bellcrank assemblies. The FAA is issuing this AD to address the unsafe condition on these products.
Modification of Class D and Class E Airspace, and Establishment of Class E Airspace; Southwest Oregon Regional Airport, OR; Correction
The FAA is correcting a final rule that appeared in the Federal Register on March 3, 2022. The rule modified the Class D and Class E surface airspace, established Class E airspace designated as an extension to Class D & E surface areas, Class E airspace beginning at 700 feet above the surface, removed navigational aids (NAVAIDs) from text headers, and made administrative changes to the legal descriptions at Southwest Oregon Regional Airport, North Bend, OR. The Final Rule did not explain the purposeful removal of Class E airspace beginning at 1,200 feet above the surface, nor did it properly exclude the Sunnyhill Airport cut-out. This action adds verbiage explaining the removal of Class E airspace beginning at 1,200 feet above the surface, and corrects the legal description for the newly established Class E airspace designated as an extension to Class D & E surface areas to properly exclude Sunnyhill Airport, OR.
Airworthiness Directives; Airbus SAS Airplanes
The FAA is superseding Airworthiness Directive (AD) 2013-25- 11, which applied to all Airbus SAS Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. AD 2013-25-11 required repetitive inspections of the 80VU rack lower lateral fittings, upper fittings, and shelves for damage, repetitive inspections of the 80VU rack lower central support for cracking, and corrective action if necessary. AD 2013-25-11 also specified optional terminating action for the repetitive inspections. Since the FAA issued AD 2013-25-11, new damage occurrences have been reported, and a different compliance time has been determined for certain inspections, depending on airplane configuration. This AD expands the applicability, removes the optional terminating action, and requires new repetitive inspections; 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; Leonardo S.p.a. Helicopters
The FAA proposes to adopt a new airworthiness directive (AD) for certain Leonardo S.p.a. Model A109S and AW109SP helicopters. This proposed AD was prompted by a report of a protective sheath, installed around a fixed flight control rod, which should have been removed during assembly. This proposed AD would require borescope inspecting certain parts, and removing any foreign object if detected, 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; MARS A.S. Parachutes
The FAA is superseding Airworthiness Directive (AD) 2022-05- 09, which applied to certain MARS A.S. emergency parachutes. AD 2022- 05-09 required removing emergency parachutes with certain manufacture dates or serial numbers from service. Since the FAA issued AD 2022-05- 09, the European Union Aviation Safety Agency (EASA) superseded its mandatory continuing airworthiness information (MCAI) to correct an unsafe condition on this aviation product. The MCAI identifies the unsafe condition as the length of the ripcord between the pins being too long, which could cause a malfunction of the emergency parachute. This AD retains the actions required by AD 2022-05-09 and expands the applicability.
Airworthiness Directives; Leonardo S.p.a. Helicopters
The FAA proposes to adopt a new airworthiness directive (AD) for certain Leonardo S.p.a. Model AW169 helicopters. This proposed AD was prompted by a report of a blockage in a fuel tank vent line. This proposed AD would require inspecting the fuel tank vent lines, 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; Leonardo S.p.a. Helicopters
The FAA proposes to adopt a new airworthiness directive (AD) for certain Leonardo S.p.a. Model AB139 and AW139 helicopters. This proposed AD was prompted by a large crack detected on the tail gearbox (TGB) fitting during a scheduled inspection and the determination that certain TGB fittings are required to be inspected by the use of a borescope. This proposed AD would require a one-time borescope inspection of certain part-numbered TGB fittings, and depending on the inspection results, removing the affected part from service and replacing with an airworthy part, 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.
Amendment of V-6, V-10, V-30, V-100, and V-233 in the Vicinity of Litchfield, MI
This action amends VHF Omnidirectional Range (VOR) Federal airways V-6, V-10, V-30, V-100, and V-233 in the vicinity of Litchfield, MI. The airway modifications are necessary due to the planned decommissioning of the VOR portion of the Litchfield, MI, VOR/ Distance Measuring Equipment (VOR/DME) navigational aid (NAVAID). The Litchfield VOR/DME NAVAID provides navigational guidance for portions of the affected VOR Federal airways listed above and is being decommissioned as part of the FAA's VOR Minimum Operational Network (MON) program.
Airworthiness Directives; CFM International, S.A. Turbofan Engines
The FAA proposes to adopt a new airworthiness directive (AD) for certain CFM International, S.A. (CFM) LEAP-1A model turbofan engines. This proposed AD was prompted by reports of two in-flight shutdowns (IFSDs) and subsequent investigation by the manufacturer that revealed cracks in the high-pressure turbine (HPT) rotor stage 1 blades. This proposed AD would require initial and repetitive borescope inspections (BSIs) of the HPT rotor stage 1 blades and HPT stator stage 1 nozzle set. Depending on the results of the BSIs, this proposed AD would require either additional BSIs at reduced intervals or replacement of the HPT rotor stage 1 blades or HPT stator stage 1 nozzle set. This proposed AD would also require sending the inspection results to CFM if any unserviceable finding is found. The FAA is proposing this AD to address the unsafe condition on these products.
Establishment and Amendment of Area Navigation (RNAV) Routes; Eastern United States
This action modifies five existing high altitude area navigation (RNAV) routes (Q-routes), and establishes one new Q-route, in support of the FAA's VHF Omnidirectional Range (VOR) Minimum Operational Network (MON) Program. This action improves the efficiency of the National Airspace System (NAS) by expanding the availability of RNAV routing and reducing the dependency on ground-based navigational systems.
Proposed Amendment of United States Area Navigation (RNAV) Route T-228; Cape Newenham, AK
This action proposes to amend United States Area Navigation (RNAV) route T-228 in the vicinity of Cape Newenham, AK in support of a large and comprehensive T-route modernization project for the state of Alaska.
Revisions to Civil Penalty Amounts
This final rule provides the statutorily-prescribed 2022 adjustment to civil penalty amounts that may be imposed for violations of certain DOT regulations. In addition, this rule notes new DOT civil penalties authority provided in the Bipartisan Infrastructure Law (BIL, enacted as the Infrastructure Investment and Jobs Act).
Airworthiness Directives; The Boeing Company Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 777 airplanes. This proposed AD was prompted by reports of discrepancies between the center wing tank (CWT) fuel quantity, as indicated by the fuel quantity indicating system (FQIS), and the refueling truck uploaded fuel amount, followed by certain engine-indicating and crew-alerting system (EICAS) messages. This proposed AD would require installing new software in the fuel quantity processor unit (FQPU), or replacing the FQPU with one that includes new software, depending on airplane configuration; and doing a software version check and FQPU operational check. This proposed AD would also prohibit the installation of certain FQPUs on certain airplanes. The FAA is proposing this AD to address the unsafe condition on these products.
Petition for Exemption; Summary of Petition Received; Indro Robotics
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.
Petition for Exemption; Summary of Petition Received; Uninsured United Parachute Technologies, LLC
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.
Petition for Exemption; Summary of Petition Received; American Airlines, Inc.
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.
Petition for Exemption; Summary of Petition Received; Wittman Regional Airport.
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.
Agency Information Collection Activities: Requests for Comments; Clearance of a New Approval of Information Collection
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 collection requires responses to questions regarding an individual's identity in order to gain access to U.S. Federal Government web applications. The information to be collected will be used to verify the requestor's identity and create a user account.
Agency Information Collection Activities: Requests for Comments; Clearance of a New Information Collection(s): Airport Concession Disadvantaged Business Enterprise (ACDBE) Program Requirements
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 October 25, 2021. The deadline for submission of public comments expired on December 27, 2021. No public comments were provided. The Department of Transportation (DOT or Department) further invites public comments about our intention to request the Office of Management and Budget's (OMB) approval for an information collection for the Department's Airport Concession Disadvantaged Business Enterprise (ACDBE) program. The DOT has the important responsibility of ensuring that firms competing for concession opportunities are not disadvantaged by unlawful discrimination. The DOT's most important tool for meeting this requirement has been its ACDBE program which is regulated by 49 CFR part 23 (ACDBE regulation) and is mandated by 49 U.S.C. 47107(e), originally enacted in 1987 and amended in 1992. The information collections described in this notice are necessary to maintain successful implementation of the ACDBE program, as it helps ensure recipients that receive Federal financial assistance from the Airport Improvement Program (AIP) of the Federal Aviation Administration (FAA) do not discriminate in the provision of opportunities for disadvantaged business enterprises in airport concessions. We are required to publish this notice in the Federal Register by the Paperwork Reduction Act of 1995, Public Law 104-13 (PRA).
Airworthiness Criteria: Special Class Airworthiness Criteria for the 3DRobotics Government Services 3DR-GS H520-G Unmanned Aircraft
The FAA announces the special class airworthiness criteria for the 3DRobotics Government Services Model 3DR-GS H520-G unmanned aircraft (UA). This document sets forth the airworthiness criteria the FAA finds to be appropriate and applicable for the UA design.
Airworthiness Criteria: Special Class Airworthiness Criteria for the Flirtey Inc. Flirtey F4.5 Unmanned Aircraft
The FAA announces the special class airworthiness criteria for the Flirtey Inc. Model Flirtey F4.5 unmanned aircraft (UA). This document sets forth the airworthiness criteria the FAA finds to be appropriate and applicable for the UA design.
Airworthiness Criteria: Special Class Airworthiness Criteria for the TELEGRID Technologies, Inc. TELEGRID DE2020 Unmanned Aircraft
The FAA announces the special class airworthiness criteria for the TELEGRID Technologies, Inc. Model TELEGRID DE2020 unmanned aircraft (UA). This document sets forth the airworthiness criteria the FAA finds to be appropriate and applicable for the UA design.
Airworthiness Criteria: Special Class Airworthiness Criteria for the Wingcopter GmbH 198 US Unmanned Aircraft
The FAA announces the special class airworthiness criteria for the Wingcopter GmbH Model 198 US unmanned aircraft (UA). This document sets forth the airworthiness criteria the FAA finds to be appropriate and applicable for the UA design.
Airworthiness Directives; Goodrich Externally-Mounted Hoist Assemblies
The FAA is adopting a new airworthiness directive (AD) for various model helicopters with certain part-numbered Goodrich externally-mounted hoist assemblies (hoists) installed. This AD was prompted by hoists failing lower load limit inspections. This AD requires replacing unmodified hoists, installing placards, revising the existing Rotorcraft Flight Manual (RFM) for your helicopter, deactivating or removing a hoist if a partial peel out occurs, reviewing the helicopter's hoist slip load test records, repetitively inspecting the hoist cable and overload clutch (clutch), and reporting information to the manufacturer. This AD also requires establishing operating limitations on the hoist and prohibits installing an unmodified hoist. The FAA is issuing this AD to address the unsafe condition on these products.
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