Department of Transportation April 22, 2021 – Federal Register Recent Federal Regulation Documents

Airworthiness Directives; Uninsured United Parachute Technologies, LLC Parachutes
Document Number: 2021-08460
Type: Rule
Date: 2021-04-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Uninsured United Parachute Technologies, LLC (UPT) parachutes. This AD results from reserve pin covers (RPCs) catching on the parachute container flaps and preventing the reserve parachute from deploying. This AD requires modifying the RPC before the next parachute jump and replacing the RPC at the next reserve parachute packing. The FAA is issuing this AD to address the unsafe condition on these products.
Petition for Waiver of Compliance
Document Number: 2021-08386
Type: Notice
Date: 2021-04-22
Agency: Federal Railroad Administration, Department of Transportation
Petition for Extension of Waiver of Compliance
Document Number: 2021-08385
Type: Notice
Date: 2021-04-22
Agency: Federal Railroad Administration, Department of Transportation
Petition for Waiver of Compliance
Document Number: 2021-08384
Type: Notice
Date: 2021-04-22
Agency: Federal Railroad Administration, Department of Transportation
Establishment of Class E Airspace; Calais, ME
Document Number: 2021-08349
Type: Rule
Date: 2021-04-22
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E airspace extending upward from 700 feet above the surface for Calais Regional Heliport, Calais, ME. The FAA discovered that necessary language was inadvertently omitted to the description of the airspace that excluded airspace outside of the United States.
Qualification of Drivers; Exemption Applications; Epilepsy and Seizure Disorders
Document Number: 2021-08341
Type: Notice
Date: 2021-04-22
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces its decision to renew exemptions for 11 individuals from the requirement in the Federal Motor Carrier Safety Regulations (FMCSRs) that interstate commercial motor vehicle (CMV) drivers have ``no established medical history or clinical diagnosis of epilepsy or any other condition which is likely to cause loss of consciousness or any loss of ability to control a CMV.'' The exemptions enable these individuals who have had one or more seizures and are taking anti-seizure medication to continue to operate CMVs in interstate commerce.
Combi USA, Receipt of Petition for Decision of Inconsequential Noncompliance
Document Number: 2021-08329
Type: Notice
Date: 2021-04-22
Agency: National Highway Traffic Safety Administration, Department of Transportation
Combi USA (Combi), has determined that certain Combi USA BabyRide rear-facing child restraint systems manufactured between March 1, 2016, and September 2, 2019, do not fully comply with Federal Motor Vehicle Safety Standard (FMVSS) No. 213, Child Restraint Systems. Combi filed an original noncompliance report dated March 8, 2021, and later amended it on March 10, 2021, and March 11, 2021. Subsequently, Combi petitioned NHTSA on March 30, 2021, for a decision that the subject noncompliance is inconsequential as it relates to motor vehicle safety. This notice announces receipt of Combi's petition.
Airworthiness Directives; Pratt & Whitney Turbofan Engines
Document Number: 2021-08327
Type: Rule
Date: 2021-04-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding Airworthiness Directive (AD) 2012-04-15 for all Pratt & Whitney (PW) JT9D-3A, JT9D-7, JT9D-7A, JT9D-7AH, JT9D- 7F, JT9D-7H, JT9D-7J, JT9D-7Q, JT9D-7Q3, JT9D-7R4D, JT9D-7R4D1, JT9D- 7R4E, JT9D-7R4E1, JT9D-7R4E4, JT9D-7R4G2, JT9D-7R4H1, JT9D-20, JT9D- 20J, JT9D-59A, and JT9D-70A (JT9D) model turbofan engines. AD 2012-04- 15 required revisions to the Airworthiness Limitations Section (ALS) of the manufacturer's Instructions for Continued Airworthiness (ICA) to include required enhanced inspection of selected critical life-limited parts at each piece-part opportunity. AD 2012-04-15 also required additional revisions to the ALS of the manufacturer's ICA for JT9D model turbofan engines. This AD requires revising the required inspections of selected critical life-limited parts specified in the ALS of the manufacturer's ICA and, for air carriers, to the existing continuous airworthiness air carrier maintenance program (CAMP). The FAA is issuing this AD to address the unsafe condition on these products.
Proposed Amendment, Establishment, and Revocation of Multiple Air Traffic Service (ATS) Routes in the Vicinity of Neosho, MO
Document Number: 2021-08284
Type: Proposed Rule
Date: 2021-04-22
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend Jet Route J-181 and VHF Omnidirectional Range (VOR) Federal airways V-13, V-14, V-15, and V- 307; establish Area Navigation (RNAV) routes T-411 and T-413; and remove VOR Federal airway V-506. The FAA is proposing this action due to the planned decommissioning of the VOR portion of the Neosho, MO (EOS), VOR/Distance Measuring Equipment (VOR/DME) navigation aid (NAVAID). The Neosho VOR is being decommissioned in support of the FAA's VOR Minimum Operational Network (MON) program.
Admission and Training of Midshipmen at the United States Merchant Marine Academy; Amendment Providing an Emergency Waiver for Scholastic Requirements
Document Number: 2021-08265
Type: Rule
Date: 2021-04-22
Agency: Maritime Administration, Department of Transportation
This final rule adopts, without change, an October 22, 2020, interim final rule (IFR) amending Maritime Administration (MARAD) regulations governing admission to the United States Merchant Marine Academy (USMMA). The amendments allow the MARAD Administrator to waive the requirement for USMMA applicants to have taken the College Board's Scholastic Aptitude Test (SAT) or the American College Testing Program (ACT) examination in the event of a State or national emergency. The ability to waive SAT and ACT requirements for prospective students is necessary to address testing disruptions caused by the coronavirus disease 2019 (COVID-19) pandemic and to provide for future emergencies.
Extension of Compliance Dates for Medical Examiner's Certification Integration
Document Number: 2021-08238
Type: Proposed Rule
Date: 2021-04-22
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA proposes to amend its regulations to extend the compliance date from June 22, 2021, to June 23, 2025, for several provisions of its April 23, 2015, Medical Examiner's Certification Integration final rule. FMCSA issued an interim final rule (IFR) on June 21, 2018, extending the compliance date for these provisions until June 22, 2021. FMCSA proposes to finalize the IFR by further extending the compliance date to June 23, 2025. This action is being taken to provide FMCSA time to complete certain information technology (IT) system development tasks for its National Registry of Certified Medical Examiners (National Registry) and to provide the State Driver's Licensing Agencies (SDLAs) sufficient time to make the necessary IT programming changes after the new National Registry system is available.
Airworthiness Directives; Airbus SAS Airplanes
Document Number: 2021-08202
Type: Proposed Rule
Date: 2021-04-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede Airworthiness Directive (AD) 2017-12-13, which applies to certain Airbus SAS Model A320-212, -214, - 232, and -233 airplanes. AD 2017-12-13 requires repetitive low frequency eddy current inspections or repetitive high frequency eddy current inspections of the pocket radius at certain areas of the fuselage frame, and repair if necessary. Since the FAA issued AD 2017- 12-13, it was determined that cracks can initiate and develop between certain other fuselage frames of the pocket radii and additional airplanes are subject to the unsafe condition. This proposed AD would require new repetitive inspections at the left- (LH) and right-hand (RH) sides of the fuselage skin at certain frames for any cracking, and repair if necessary, as specified in a European Union Aviation Safety Agency (EASA), which is proposed for incorporation by reference. The FAA is proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Helicopters
Document Number: 2021-08183
Type: Proposed Rule
Date: 2021-04-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede Airworthiness Directive (AD) 2014-11-02 for Airbus Helicopters Model SA-365N, SA-365N1, AS-365N2, and AS 365 N3 helicopters. AD 2014-11-02 requires repetitively inspecting frame number (No.) 9 for a crack. Since the FAA issued AD 2014-11-02, Airbus Helicopters developed a modification that would provide an optional terminating action for the repetitive inspections required by AD 2014-11-02. This proposed AD would retain the requirements of AD 2014-11-02, provide an optional terminating action for the repetitive inspections, and reduce the applicability by excluding certain post-modified helicopters. The actions of this proposed AD are intended to address an unsafe condition on these products.
Airworthiness Directives; Airbus Helicopters
Document Number: 2021-08182
Type: Proposed Rule
Date: 2021-04-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters. This proposed AD was prompted by a report of a yaw control failure that was the result of the disconnection of the tail rotor hub (TRH) pitch control rod from the tail rotor servo-control, which resulted from a seized TRH bearing. The TRH bearing had grease dissolving after contamination by leaked hydraulic fluid from the tail rotor servo-control that came through the TRH assembly boot. This proposed AD would require repetitive inspections for hydraulic leaks, corrective actions if necessary, and an optional modification which constitutes terminating action, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Helicopters
Document Number: 2021-08179
Type: Proposed Rule
Date: 2021-04-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Helicopters Model EC155B1 helicopters. This proposed AD was prompted by a report of difficulties when jettisoning the co- pilot door during non-scheduled maintenance. This proposed AD would require a functional check of the pilot and co-pilot door jettisoning system and corrective actions if necessary, as specified in a European 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; Rolls-Royce Deutschland Ltd & Co KG (Type Certificate Previously Held by Rolls-Royce plc) Turbofan Engines
Document Number: 2021-07660
Type: Proposed Rule
Date: 2021-04-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede Airworthiness Directive (AD) 2020-15-12, which applies to certain Rolls-Royce Deutschland Ltd & Co KG (RRD) Trent 1000 model turbofan engines. AD 2020-15-12 requires initial and repetitive ultrasonic or visual inspections of the intermediate-pressure compressor (IPC) stage 1 rotor blade root (front face), IPC stage 2 rotor blade root (front and rear face), and IPC shaft stage 2 dovetail post (front face), and removal of any cracked parts from service. AD 2020-15-12 also requires an inspection after asymmetric power and cabin depressurization events. Since the FAA issued AD 2020-15-12, the manufacturer introduced IPC stage 1 and stage 2 rotor blades in kitted sets, which terminate the need for initial and repetitive ultrasonic or visual inspections for certain IPC parts. This proposed AD would continue to require initial and repetitive ultrasonic or visual inspections of certain IPC parts until replacement of the IPC stage 1 and stage 2 rotor blades with redesigned IPC stage 1 and stage 2 rotor blades in kitted sets. The FAA is proposing this AD to address the unsafe condition on these products.
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