Data / Federal rules / 2024-29465
Special Conditions: Airbus Model A321 neo ACF and A321 neo XLR Series Airplanes; Dynamic Test Requirements for Single Occupant Oblique Seats at an Installation Angle of 49 Degrees With Airbags and 3-Point Restraint or Pretensioner Restraint Systems
The Federal Aviation Administration published this proposed rule in the Federal Register on December 23, 2024. Comments closed on January 13, 2025.
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What the agency says
This action proposes special conditions for the Airbus Model A321 neo ACF and A321 neo XLR airplanes. These airplanes 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 single-occupant oblique seat with an airbag and 3-point or pretensioner restraint system positioned at a 49-degree angle from the cabin centerline. 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.
Key facts
- Document number
- 2024-29465
- Type
- Proposed rule
- Action
- Notice of proposed special conditions
- Agency
- Transportation Department; Federal Aviation Administration
- Published
- December 23, 2024
- Comments due
- January 13, 2025
- Dates
- Send comments on or before January 13, 2025.
- Docket
- Docket No. FAA-2024-2570; Notice No. 25-24-05-SC
- Code of Federal Regulations
- 14 CFR 25
- Topics
- Aircraft; Aviation safety; Reporting and recordkeeping requirements
- Pages
- 5
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Everything from the Federal Aviation Administration · Rules on aircraft · Rules on aviation safety · Rules on reporting and recordkeeping requirements · Published in December 2024
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