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withdrawn,object_id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-2009-0889-0015,FAA,FAA-2009-0889,"Airworthiness Directives: Safran Helicopter Engines, S.A., Turboshaft Engines",Rule,Final Rule,2018-08-08T04:00:00Z,2018,8,2018-08-08T04:00:00Z,,2024-11-07T01:35:56Z,2018-16652,1,0,09000064835f099a
FAA-2009-0889-0007,FAA,FAA-2009-0889,Airworthiness Directives: Turbomeca S.A. Turboshaft Engines,Rule,Final Rule,2012-02-14T05:00:00Z,2012,2,2012-02-14T05:00:00Z,,2024-11-07T21:57:30Z,2012-03255,1,0,0900006480fb55ed
FAA-2009-0889-0003,FAA,FAA-2009-0889,Airworthiness Directives: Turbomeca Arriel 2B and 2B1 Turboshaft Engines,Rule,Federal Register Publication,2010-02-04T05:00:00Z,2010,2,2010-02-04T05:00:00Z,,2011-06-11T16:20:40Z,2010-01735,0,0,0900006480a8d794
FAA-2009-0889-0001,FAA,FAA-2009-0889,Airworthiness Directives; Turbomeca Arriel 2B and 2B1 Turboshaft Engines,Rule,Federal Register Publication,2009-11-05T05:00:00Z,2009,11,2009-11-05T05:00:00Z,2009-12-08T04:59:59Z,2024-11-07T22:08:14Z,E9-26730,1,0,0900006480a517a9