2026-13924Proposed RuleWallet

FAA Writes New Rules for Gulfstream's Sideways Seats

Published Date: 7/10/2026

Proposed Rule

Summary

Gulfstream’s Model G300 airplane is getting a cool upgrade with side-facing seats that may have airbags. Since current safety rules don’t cover these seats well, the FAA is proposing new safety tests to make sure everyone stays safe. If you’re involved with this plane, get ready to follow these new rules and share your thoughts by August 24, 2026.

Analyzed Economic Effects

3 provisions identified: 2 benefits, 1 costs, 0 mixed.

Quantified Injury Thresholds to Meet

The special conditions set clear pass/fail injury limits that side‑facing seats must meet, for example: thoracic rib deflection no more than 1.73 inches (44 mm); abdominal force no more than 562 lbs (2,500 N); pubic symphysis force no more than 1,350 lbs (6,000 N); upper‑leg rotation limited to 35 degrees; and specific upper‑neck force and torque limits (e.g., upper‑neck tension <405 lb / 1,800 N). Manufacturers must demonstrate compliance with these numeric thresholds during certification testing.

Required Dynamic Test Methods

If you are the applicant or manufacturer certifying side‑facing seats for the Gulfstream G300, you must run specific dynamic tests using specified test dummies (for example ES‑2re or Hybrid‑II) and follow detailed positioning and setup steps. Tests require actions such as applying about 20 pounds (89 N) to the feet to compress the seat cushion, clothing ATDs with about 2.5 lb of clothing and size 11E shoes, and recording rebound which can require video longer than 500 ms.

Airbag and Leg‑Flail Protection Rules

If side‑facing seats include shoulder‑belt airbags or leg‑flail protection, those systems must protect occupants ranging from a 2‑year‑old child to a 95th percentile male, avoid inadvertent deployment, not impede rapid egress (must allow egress within 10 seconds after deployment), be protected from lightning and HIRF (per Sec. 25.1316 and 25.1317), function after loss of normal electrical power and transverse fuselage separation, and have inflatable material burn rate no greater than 2.5 inches per minute.

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Key Dates

Published Date
Comments Due
7/10/2026
8/24/2026

Department and Agencies

Department
Independent Agency
Agency
Transportation Department
Federal Aviation Administration
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