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withdrawn,object_id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-2006-24261-0012,FAA,FAA-2006-24261,Airworthiness Directives; General Electric Company (GE) CT7-8A Turboshaft Engines,Rule,Federal Register Publication,2008-12-22T05:00:00Z,2008,12,2008-12-22T05:00:00Z,,2011-06-11T16:11:26Z,E8-29722,0,0,09000064807e6853
FAA-2006-24261-0008,FAA,FAA-2006-24261,Airworthiness Directives; General Electric Company Aircraft Engines (GEAE) CT7-8A Turboshaft Engines,Rule,Federal Register Publication,2008-03-19T04:00:00Z,2008,3,2008-03-19T04:00:00Z,2008-05-20T03:59:59Z,2024-11-12T04:11:11Z,E8-05492,1,0,09000064803ff0aa
FAA-2006-24261-0002,FAA,FAA-2006-24261,U.S. DOT/FAA - Final Rule; Request for Comments (Original),Rule,Final Rule,2006-05-08T04:00:00Z,2006,5,2006-05-08T04:00:00Z,2006-05-09T03:59:59Z,2024-11-11T22:02:29Z,,1,0,09000064802afea3
FAA-2006-24261-0001,FAA,FAA-2006-24261,U.S. DOT/FAA - Final Rule; Request for Comments,Rule,Federal Register Publication,2006-04-17T04:00:00Z,2006,4,2006-04-17T04:00:00Z,2006-04-18T03:59:59Z,2024-11-11T22:02:29Z,,1,0,09000064802afea2