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withdrawn,object_id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-2006-23809-0023,FAA,FAA-2006-23809,U.S. DOT/FAA - Various Supporting AD Documents,Supporting & Related Material,Supplement,2014-08-05T04:00:00Z,2014,8,,,2014-08-05T18:18:55Z,,0,0,09000064817ff681
FAA-2006-23809-0022,FAA,FAA-2006-23809,Airworthiness Directives: Turbomeca S.A. Turboshaft Engines,Rule,Final Rule,2014-06-30T04:00:00Z,2014,6,2014-06-30T04:00:00Z,,2014-06-30T14:43:27Z,2014-14951,0,0,0900006481774edb
FAA-2006-23809-0021,FAA,FAA-2006-23809,U.S. DOT/FAA - Various Supplemental AD Documents,Supporting & Related Material,Supplement,2014-05-22T04:00:00Z,2014,5,,,2014-05-22T14:07:08Z,,0,0,0900006481709d1d
FAA-2006-23809-0020,FAA,FAA-2006-23809,Airworthiness Directives: Turbomeca S.A. Turboshaft Engines,Proposed Rule,Notice of Proposed Rulemaking (NPRM),2014-02-21T05:00:00Z,2014,2,2014-02-21T05:00:00Z,2014-04-23T03:59:59Z,2024-11-11T20:49:24Z,2014-03673,1,0,0900006481599390