id,agency_id,docket_id,title,document_type,subtype,posted_date,posted_year,posted_month,comment_start_date,comment_end_date,last_modified,fr_doc_num,open_for_comment,withdrawn,object_id
FAA-2022-1311-0001,FAA,FAA-2022-1311,"Airworthiness Directives: Safran Helicopter Engines, S.A. (Type Certificate previously held by Turbomeca, S.A.) Turboshaft Engines",Proposed Rule,Notice of Proposed Rulemaking (NPRM),2022-10-31T04:00:00Z,2022,10,2022-10-31T04:00:00Z,2022-12-16T04:59:59Z,2024-11-12T23:46:57Z,2022-23172,1,0,0900006485471026
FAA-2022-1311-0002,FAA,FAA-2022-1311,U.S. DOT/FAA - Supplemental AD Document (EASA AD 2022-0083),Supporting & Related Material,Supplement,2022-10-31T04:00:00Z,2022,10,,,2022-10-31T13:49:36Z,,0,0,0900006485471593