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Special Conditions: Airbus Model A321neo ACF and A321neo 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

other · Rule · Final special conditions. · Published 2025-02-05 · Effective 2025-02-05 · 90 FR 9003

Document

Document number
2025-02218
Federal Register citation
90 FR 9003
Type
Rule
Action
Final special conditions.
Category
other
Publication date
2025-02-05
Effective date
2025-02-05
FAA docket
Docket No. FAA-2024-2570

Abstract

These special conditions are issued for the Airbus Model A321neo ACF and A321neo 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 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.

Source

Authoritative
Federal Register document
Machine
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