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withdrawn,object_id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-2006-25513-0010,FAA,FAA-2006-25513,U.S. DOT/FAA - Supplemental AD Documents,Supporting & Related Material,Supplement,2016-08-26T04:00:00Z,2016,8,,,2016-08-26T18:46:29Z,,0,0,090000648219ff77
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-2006-25513-0008,FAA,FAA-2006-25513,U.S. DOT/FAA - Supporting Documentation,Supporting & Related Material,Supplement,2016-05-11T04:00:00Z,2016,5,,,2016-05-11T19:20:09Z,,0,0,0900006481fc539e
FAA-2006-25513-0006,FAA,FAA-2006-25513,Airworthiness Directives: Rolls-Royce Deutschland Ltd&Co KG Turbofan Engines,Proposed Rule,Notice of Proposed Rulemaking (NPRM),2016-03-11T05:00:00Z,2016,3,2016-03-11T05:00:00Z,2016-05-11T03:59:59Z,2024-11-12T06:00:19Z,2016-05463,1,0,0900006481ebbef7