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withdrawn,object_id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-2007-27009-0018,FAA,FAA-2007-27009,U.S. DOT/FAA - Various Supplemental AD Documents,Supporting & Related Material,Supplement,2014-07-17T04:00:00Z,2014,7,,,2014-07-17T19:20:48Z,,0,0,09000064817b0661
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-2007-27009-0016,FAA,FAA-2007-27009,U.S. DOT/FAA - Foreign Airworthiness Directive,Supporting & Related Material,Supplement,2014-03-31T04:00:00Z,2014,3,,,2014-03-31T15:29:35Z,,0,0,090000648168ab56
FAA-2007-27009-0015,FAA,FAA-2007-27009,U.S. DOT/FAA - See Attachments,Supporting & Related Material,Supplement,2014-01-16T05:00:00Z,2014,1,,,2014-01-16T14:59:14Z,,0,0,090000648150a58a
FAA-2007-27009-0014,FAA,FAA-2007-27009,Airworthiness Directives: Turbomeca S.A. Turboshaft Engines,Proposed Rule,Notice of Proposed Rulemaking (NPRM),2013-12-24T05:00:00Z,2013,12,2013-12-24T05:00:00Z,2014-02-25T04:59:59Z,2024-11-07T22:59:58Z,2013-30488,1,0,09000064814d547f
FAA-2007-27009-0013,FAA,FAA-2007-27009,U.S. DOT/FAA -  See Attachment,Supporting & Related Material,Supplement,2010-12-13T05:00:00Z,2010,12,,,2012-03-24T19:37:16Z,,0,0,0900006480bb3b89
FAA-2007-27009-0012,FAA,FAA-2007-27009,U.S. DOT/FAA -  See Attachment,Supporting & Related Material,Supplement,2010-12-13T05:00:00Z,2010,12,,,2012-03-24T19:30:05Z,,0,0,0900006480bb3a43
FAA-2007-27009-0011,FAA,FAA-2007-27009,U.S. DOT/FAA -  See Attachment,Supporting & Related Material,Supplement,2010-12-13T05:00:00Z,2010,12,,,2012-03-24T19:31:15Z,,0,0,0900006480bb3201
FAA-2007-27009-0010,FAA,FAA-2007-27009,U.S. DOT/FAA - See Attachments,Supporting & Related Material,Supplement,2010-09-07T04:00:00Z,2010,9,,,2012-03-24T19:32:14Z,,0,0,0900006480b44e1b
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-2007-27009-0007,FAA,FAA-2007-27009,U.S. DOT/FAA - See Attachments,Other,Additional Information,2008-08-11T04:00:00Z,2008,8,2008-08-11T04:00:00Z,,2013-08-11T02:55:18Z,,0,0,09000064806bc12e
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-2007-27009-0004,FAA,FAA-2007-27009,U.S. DOT/FAA - Economic & Regulatory Evaluation,Supporting & Related Material,Economic Assessment,2007-03-19T04:00:00Z,2007,3,,,2024-11-07T02:26:01Z,,0,0,09000064802ad195
FAA-2007-27009-0003,FAA,FAA-2007-27009,U.S. DOT/FAA - Airworthiness Directive Grid,Supporting & Related Material,Airworthiness Directive Grid,2007-03-19T04:00:00Z,2007,3,,,2024-11-07T02:26:01Z,,0,0,09000064802ad194
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