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withdrawn,object_id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-2005-21624-0010,FAA,FAA-2005-21624,Airworthiness Directives: Turbomeca S.A. ARRIEL 2B Turboshaft Engines,Rule,Federal Register Publication,2010-09-27T04:00:00Z,2010,9,2010-09-27T04:00:00Z,2010-10-28T03:59:59Z,2011-06-11T16:11:17Z,2010-23581,0,0,0900006480b60a46
FAA-2005-21624-0007,FAA,FAA-2005-21624,U.S. DOT/FAA - Final Rule; Request for Comments,Rule,Federal Register Publication,2007-04-17T04:00:00Z,2007,4,2007-04-17T04:00:00Z,2007-04-18T03:59:59Z,2024-11-11T21:59:13Z,,1,0,09000064802af983
FAA-2005-21624-0004,FAA,FAA-2005-21624,Final Rule; Request for Comments (Original),Rule,Final Rule,2005-07-27T04:00:00Z,2005,7,2005-07-27T04:00:00Z,2005-07-28T03:59:59Z,2024-11-11T21:59:13Z,,1,0,09000064802af97d
FAA-2005-21624-0002,FAA,FAA-2005-21624,U.S. DOT/FAA - Final Rule; Request for Comments - 2005-NE-17-AD,Rule,Final Rule,2005-07-27T04:00:00Z,2005,7,2005-07-27T04:00:00Z,2005-07-28T03:59:59Z,2024-11-11T21:59:13Z,,1,0,09000064802af97b
FAA-2005-21624-0001,FAA,FAA-2005-21624,U.S. DOT/FAA - Final Rule; Request for Comments,Rule,Federal Register Publication,2005-06-24T04:00:00Z,2005,6,2005-06-24T04:00:00Z,2005-06-25T03:59:59Z,2024-11-11T21:59:13Z,,1,0,09000064802af979