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withdrawn,object_id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-2006-25970-0009,FAA,FAA-2006-25970,Airworthiness Directives: Turbomeca S.A. Turboshaft Engines,Rule,Final Rule,2016-03-17T04:00:00Z,2016,3,2016-03-17T04:00:00Z,,2016-03-17T13:33:02Z,2016-06000,0,0,0900006481ecae85
FAA-2006-25970-0002,FAA,FAA-2006-25970,U.S. DOT/FAA - Final Rule (Original),Rule,Final Rule,2006-11-28T05:00:00Z,2006,11,2006-11-28T05:00:00Z,2006-11-29T04:59:59Z,2024-11-07T17:02:54Z,,1,0,09000064802bafc4
FAA-2006-25970-0001,FAA,FAA-2006-25970,U.S. DOT/FAA - Final Rule,Rule,Federal Register Publication,2006-11-16T05:00:00Z,2006,11,2006-11-16T05:00:00Z,2006-11-17T04:59:59Z,2024-11-07T17:02:54Z,,1,0,09000064802bafc3