Federal Aviation Administration April 4, 2024 – Federal Register Recent Federal Regulation Documents

Airworthiness Directives; Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.) Airplanes
Document Number: 2024-07033
Type: Proposed Rule
Date: 2024-04-04
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede Airworthiness Directive (AD) 2019-24-16, which applies to certain Embraer S.A. Model ERJ 190-100 STD, -100 LR, -100 IGW, and -100 ECJ airplanes; and Model ERJ 190-200 STD, -200 LR, and -200 IGW airplanes. AD 2019-24-16 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2019-24-16, 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, as specified in an Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products.
Special Conditions: Jet Aviation AG, The Boeing Company Model 737-8 Series Airplane; Dynamic Test Requirements for Single Occupant Oblique Seats With or Without Airbags and/or 3-Point Restraints
Document Number: 2024-06894
Type: Rule
Date: 2024-04-04
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for The Boeing Company (Boeing) Model 737-8 series airplane. This airplane, as modified by Jet Aviation AG (Jet Aviation), 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 oblique (side-facing) single-occupant seats equipped with airbag devices or 3-point restraints. 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.
Amendment of Class C Airspace; San Juan Luis Munoz Marin International Airport, PR
Document Number: 2024-07086
Type: Rule
Date: 2024-04-04
Agency: Federal Aviation Administration, Department of Transportation
This action modifies the San Juan Luis Munoz Marin International Airport, PR (SJU), Class C airspace by adding a cutout to the surface area near the Fernando Luis Ribas Dominicci Airport, PR (SIG). The FAA is taking this action to enhance safety and enable more efficient operations at SJU and SIG.
Amendment of United States Area Navigation (RNAV) Route Q-83; Eastern United States
Document Number: 2024-07085
Type: Proposed Rule
Date: 2024-04-04
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend United States Area Navigation (RNAV) Route Q-83 in the eastern United States. This action supports the Northeast Corridor Atlantic Coast Routes (NEC ACR) Optimization Project to improve the efficiency of the National Airspace System (NAS).
Special Conditions: Airbus Model A321neo XLR Airplane; Electronic Flight-Control System: Lateral-Directional and Longitudinal Stability, and Low-Energy Awareness
Document Number: 2024-07139
Type: Rule
Date: 2024-04-04
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Airbus Model A321neo XLR airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the applicable airworthiness standards. This design feature is an electronic flight-control system (EFCS) associated with lateral- directional and longitudinal stability, and low-energy awareness. 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.
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