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withdrawn,object_id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-2006-23809-0022,FAA,FAA-2006-23809,Airworthiness Directives: Turbomeca S.A. Turboshaft Engines,Rule,Final Rule,2014-06-30T04:00:00Z,2014,6,2014-06-30T04:00:00Z,,2014-06-30T14:43:27Z,2014-14951,0,0,0900006481774edb
FAA-2006-23809-0013,FAA,FAA-2006-23809,U.S. DOT/FAA - Final Rule,Rule,Final Rule,2007-12-28T05:00:00Z,2007,12,2007-12-28T05:00:00Z,,2024-11-07T23:54:27Z,,1,0,090000648037fa7d
FAA-2006-23809-0011,FAA,FAA-2006-23809,U.S. DOT/FAA - Final Rule; Request for Comments,Rule,Federal Register Publication,2007-05-11T04:00:00Z,2007,5,2007-05-11T04:00:00Z,2007-05-12T03:59:59Z,2024-11-08T04:19:06Z,,1,0,09000064802b5e3c
FAA-2006-23809-0007,FAA,FAA-2006-23809,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,2024-11-08T04:19:27Z,,1,0,09000064802b5e42
FAA-2006-23809-0010,FAA,FAA-2006-23809,U.S. DOT/FAA - Foreign Airworthiness Directive - No. F-2005-188,Rule,Foreign Airworthiness Directive,2006-11-28T05:00:00Z,2006,11,2006-11-28T05:00:00Z,2006-11-29T04:59:59Z,2024-11-08T04:19:05Z,,1,0,09000064802b5e3b
FAA-2006-23809-0006,FAA,FAA-2006-23809,U.S. DOT/FAA - Final Rule,Rule,Federal Register Publication,2006-10-19T04:00:00Z,2006,10,2006-10-19T04:00:00Z,2006-10-20T03:59:59Z,2024-11-08T04:19:27Z,,1,0,09000064802b5e41
FAA-2006-23809-0005,FAA,FAA-2006-23809,U.S. DOT/FAA - Foreign Airworthiness Directive F-2005-188,Rule,Foreign Airworthiness Directive,2006-04-17T04:00:00Z,2006,4,2006-04-17T04:00:00Z,2006-04-18T03:59:59Z,2024-11-08T04:19:06Z,,1,0,09000064802b5e40
FAA-2006-23809-0001,FAA,FAA-2006-23809,U.S. DOT/FAA - Notice of Proposed Rulemaking (NPRM),Rule,Federal Register Publication,2006-03-09T05:00:00Z,2006,3,2006-03-09T05:00:00Z,2006-03-10T04:59:59Z,2024-11-08T04:19:05Z,,1,0,09000064802b5e3a