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withdrawn,object_id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-2006-23706-0027,FAA,FAA-2006-23706,Airworthiness Directives: Honeywell International Inc. Turboprop Engines,Rule,Final Rule,2016-10-24T04:00:00Z,2016,10,2016-10-24T04:00:00Z,,2024-11-11T21:32:49Z,2016-25268,1,0,090000648234339d
FAA-2006-23706-0026,FAA,FAA-2006-23706,U.S. DOT/FAA - Supplemental AD Documents,Supporting & Related Material,Supplement,2016-10-18T04:00:00Z,2016,10,,,2016-10-18T14:51:39Z,,0,0,09000064822fa17e
FAA-2006-23706-0025,FAA,FAA-2006-23706,U.S. DOT/FAA - Supplemental AD Documents,Supporting & Related Material,Supplement,2016-08-24T04:00:00Z,2016,8,,,2016-08-24T13:13:27Z,,0,0,09000064821954a8
FAA-2006-23706-0024,FAA,FAA-2006-23706,Airworthiness Directives: Honeywell International Inc. Turboprop Engines,Proposed Rule,Notice of Proposed Rulemaking (NPRM),2016-03-29T04:00:00Z,2016,3,2016-03-29T04:00:00Z,2016-06-01T03:59:59Z,2024-11-12T05:58:14Z,2016-06936,1,0,0900006481ee6fd2
FAA-2006-23706-0023,FAA,FAA-2006-23706,U.S. DOT/FAA - Various Supplemental AD Documents,Supporting & Related Material,Supplement,2016-03-10T05:00:00Z,2016,3,,,2016-03-10T16:53:03Z,,0,0,0900006481e0d056