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withdrawn,object_id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-2006-25513-0009,FAA,FAA-2006-25513,Airworthiness Directives: Rolls-Royce Deutschland Ltd and Co KG Turbofan Engines,Rule,Final Rule,2016-08-23T04:00:00Z,2016,8,2016-08-23T04:00:00Z,,2024-11-11T21:30:19Z,2016-20081,1,0,0900006482193b70
FAA-2006-25513-0002,FAA,FAA-2006-25513,U.S. DOT/FAA - Final Rule (Original),Rule,Final Rule,2006-10-16T04:00:00Z,2006,10,2006-10-16T04:00:00Z,2006-10-17T03:59:59Z,2024-11-07T16:56:18Z,,1,0,09000064802badc7
FAA-2006-25513-0001,FAA,FAA-2006-25513,U.S. DOT/FAA - Final Rule,Rule,Federal Register Publication,2006-09-08T04:00:00Z,2006,9,2006-09-08T04:00:00Z,2006-09-09T03:59:59Z,2024-11-07T16:56:17Z,,1,0,09000064802badc6