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withdrawn,object_id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-2007-27009-0017,FAA,FAA-2007-27009,Airworthiness Directives: Turbomeca S.A. Turboshaft Engines,Rule,Final Rule,2014-04-10T04:00:00Z,2014,4,2014-04-10T04:00:00Z,,2014-04-10T13:38:06Z,2014-08008,0,0,09000064816ad7fa
FAA-2007-27009-0009,FAA,FAA-2007-27009,Airworthiness Directives: Turbomeca Arriel 2B1 Turboshaft Engines,Rule,Federal Register Publication,2010-06-02T04:00:00Z,2010,6,2010-06-02T04:00:00Z,,2024-11-12T04:46:41Z,2010-13133,1,0,0900006480afa182
FAA-2007-27009-0008,FAA,FAA-2007-27009,Airworthiness Directives: Turbomeca Arriel 2B1 Turboshaft Engines,Rule,Federal Register Publication,2010-03-22T04:00:00Z,2010,3,2010-03-22T04:00:00Z,2010-04-22T03:59:59Z,2024-11-07T22:14:24Z,2010-06179,1,0,0900006480ac4856
FAA-2007-27009-0006,FAA,FAA-2007-27009,U.S. DOT/FAA - Final Rule; Request for Comments,Rule,Federal Register Publication,2007-09-18T04:00:00Z,2007,9,2007-09-18T04:00:00Z,2007-09-19T03:59:59Z,2024-11-12T04:08:23Z,,1,0,09000064803849e8
FAA-2007-27009-0005,FAA,FAA-2007-27009,U.S. DOT/FAA - Foreign Airworthiness Directive,Rule,Foreign Airworthiness Directive,2007-03-19T04:00:00Z,2007,3,2007-03-19T04:00:00Z,2007-03-20T03:59:59Z,2024-11-07T02:26:01Z,,1,0,09000064802ad196
FAA-2007-27009-0002,FAA,FAA-2007-27009,U.S. DOT/FAA - Final Rule; Request for Comments (Original),Rule,Final Rule,2007-03-19T04:00:00Z,2007,3,2007-03-19T04:00:00Z,2007-03-20T03:59:59Z,2024-11-07T02:26:01Z,,1,0,09000064802ad193
FAA-2007-27009-0001,FAA,FAA-2007-27009,U.S. DOT/FAA -  Final Rule; Request for Comments,Rule,Federal Register Publication,2007-02-02T05:00:00Z,2007,2,2007-02-02T05:00:00Z,2007-02-03T04:59:59Z,2024-11-07T02:25:32Z,,1,0,09000064802ad18f