Department of Transportation September 19, 2024 – Federal Register Recent Federal Regulation Documents
Results 1 - 10 of 10
U.S. Commercial Space Launch Competitiveness Act Incorporation
This final rule incorporates various changes required by the United States Commercial Space Launch Competitiveness Act of 2015. This final rule provides regulatory clarity to applicants seeking licenses for space flight operations involving government astronauts by adding two new subparts to the human space flight regulations containing requirements for operators with government astronauts with and without safety-critical roles on board vehicles.
Federal Motor Vehicle Safety Standards; Pedestrian Head Protection, Global Technical Regulation No. 9; Incorporation by Reference
NHTSA proposes a new Federal Motor Vehicle Safety Standard (FMVSS) that would ensure passenger vehicles with a gross vehicle weight rating (GVWR) of 4,536 kilograms (kg) (10,000 pounds (lb)) or less are designed to mitigate the risk of serious to fatal injury in child and adult pedestrian crashes. The proposed standard would establish test procedures simulating a head-to-hood impact and performance requirements to minimize the risk of head injury. This NPRM is based on a Global Technical Regulation (GTR) on pedestrian protection, with focused enhancements to address safety problems and a regulatory framework unique to the United States.
Amendment of Jet Route J-133 and Establishment of Area Navigation Route Q-801 in the Vicinity of Anchorage, AK
This action corrects a final rule published in the Federal Register of August 30, 2024, that amends Jet Route J-133 and establishes Area Navigation Route (RNAV) Q-801 in the vicinity of Anchorage, AK. This action corrects a typographical error in the preamble and in the regulatory text for J-133.
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) Model PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28S-160, PA-28S-180, PA-28-236, PA-28-201T, PA-32-300, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32-301FT, PA-32- 301XTC, PA-32R-301 (HP), PA-32R-301 (SP), PA-32R-301T, PA-32-301, and PA-32-301T airplanes. This proposed AD was prompted by a report of a wing separation caused by fatigue cracking in a visually inaccessible area of the lower main wing spar cap and additional reports of fatigue cracking in the wing spars of airplanes that share common type design features. This proposed AD would require reviewing airplane maintenance records to determine if an eddy current inspection of the lower main wing spar bolt holes was done and, depending on the result, doing a one-time eddy current inspection of the lower wing spar bolt holes for crack(s), and replacing any cracked main wing spar. The FAA is proposing this AD to address the unsafe condition on these products.
This site is protected by reCAPTCHA and the Google
Privacy Policy and
Terms of Service apply.
