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withdrawn,object_id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-2009-0889-0011,FAA,FAA-2009-0889,"Airworthiness Directives: Safran Helicopter Engines, S.A., Turboshaft Engines",Proposed Rule,Notice of Proposed Rulemaking (NPRM),2017-10-06T04:00:00Z,2017,10,2017-10-06T04:00:00Z,2017-11-21T04:59:59Z,2024-11-07T01:19:00Z,2017-21344,1,0,0900006482ba4f80
FAA-2009-0889-0006,FAA,FAA-2009-0889,Airworthiness Directives: Turbomeca S.A. Arriel 2B and 2B1 Turboshaft Engines,Proposed Rule,Notice of Proposed Rulemaking (NPRM),2011-11-07T05:00:00Z,2011,11,2011-11-07T05:00:00Z,2012-01-07T04:59:59Z,2011-11-07T13:59:40Z,2011-28677,0,0,0900006480f67011