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withdrawn,object_id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-2015-3805-0004,FAA,FAA-2015-3805,U.S. DOT/FAA - Supplemental AD Documents,Supporting & Related Material,Supplement,2016-06-21T04:00:00Z,2016,6,,,2016-06-21T15:18:12Z,,0,0,0900006481eb585f
FAA-2015-3805-0003,FAA,FAA-2015-3805,U.S. DOT/FAA - Various Supplemental AD Documents,Supporting & Related Material,Supplement,2016-03-10T05:00:00Z,2016,3,,,2016-03-10T16:09:49Z,,0,0,0900006481db7544
FAA-2015-3805-0002,FAA,FAA-2015-3805,Airworthiness Directives: Turbomeca S.A. Turboshaft Engines,Rule,Final Rule,2016-02-09T05:00:00Z,2016,2,2016-02-09T05:00:00Z,,2016-02-09T19:35:51Z,2016-02477,0,0,0900006481e5ce53
FAA-2015-3805-0001,FAA,FAA-2015-3805,Airworthiness Directives: Turbomeca S.A. Turboshaft Engines,Proposed Rule,Notice of Proposed Rulemaking (NPRM),2015-11-05T05:00:00Z,2015,11,2015-11-05T05:00:00Z,2016-01-05T04:59:59Z,2024-11-07T23:30:57Z,2015-28011,1,0,0900006481d14562