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withdrawn,object_id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-2009-0660-0017,FAA,FAA-2009-0660,Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures; Reopening of Comment Period,Rule,Federal Register Publication,2010-05-05T04:00:00Z,2010,5,2010-05-05T04:00:00Z,2010-07-17T03:59:59Z,2024-11-07T22:14:43Z,2010-10578,1,0,0900006480ae7246
FAA-2009-0660-0009,FAA,FAA-2009-0660,U.S. DOT/FAA - NPRM Reference Document 11,Supporting & Related Material,Supplement,2010-01-06T05:00:00Z,2010,1,,,2024-11-07T22:13:33Z,,0,0,0900006480a76c5d
FAA-2009-0660-0012,FAA,FAA-2009-0660,U.S. DOT/FAA - NPRM Reference Document 15,Supporting & Related Material,Supplement,2010-01-06T05:00:00Z,2010,1,,,2024-11-07T22:11:32Z,,0,0,0900006480a76c76
FAA-2009-0660-0005,FAA,FAA-2009-0660,U.S. DOT/FAA - NPRM Reference Document 9,Supporting & Related Material,Supplement,2010-01-06T05:00:00Z,2010,1,,,2024-11-07T22:11:32Z,,0,0,0900006480a76c45
FAA-2009-0660-0010,FAA,FAA-2009-0660,U.S. DOT/FAA - NPRM Reference Document 12,Supporting & Related Material,Supplement,2010-01-06T05:00:00Z,2010,1,,,2012-03-24T19:28:58Z,,0,0,0900006480a76c6d
FAA-2009-0660-0011,FAA,FAA-2009-0660,U.S. DOT/FAA - NPRM Reference Document 13 and 14,Supporting & Related Material,Supplement,2010-01-06T05:00:00Z,2010,1,,,2012-03-24T19:35:59Z,,0,0,0900006480a76c72
FAA-2009-0660-0006,FAA,FAA-2009-0660,U.S. DOT/FAA - See Attachments,Supporting & Related Material,Additional Information,2010-01-06T05:00:00Z,2010,1,,,2024-11-07T22:11:32Z,,0,0,0900006480a76c78
FAA-2009-0660-0008,FAA,FAA-2009-0660,U.S. DOT/FAA - NPRM Reference Document 10B,Supporting & Related Material,Supplement,2010-01-06T05:00:00Z,2010,1,,,2024-11-07T22:13:33Z,,0,0,0900006480a76c56
FAA-2009-0660-0004,FAA,FAA-2009-0660,U.S. DOT/FAA - NPRM Reference Document 8,Supporting & Related Material,Supplement,2010-01-06T05:00:00Z,2010,1,,,2024-11-07T22:12:21Z,,0,0,0900006480a76c38
FAA-2009-0660-0007,FAA,FAA-2009-0660,U.S. DOT/FAA - NPRM Reference Document 10A,Supporting & Related Material,Supplement,2010-01-06T05:00:00Z,2010,1,,,2012-03-24T19:30:40Z,,0,0,0900006480a76c53
FAA-2009-0660-0002,FAA,FAA-2009-0660,U.S. DOT/FAA - See Attachments,Supporting & Related Material,Supplement,2010-01-06T05:00:00Z,2010,1,,,2024-11-07T22:11:31Z,,0,0,0900006480a76c23
FAA-2009-0660-0003,FAA,FAA-2009-0660,U.S. DOT/FAA - NPRM Reference Document 7,Supporting & Related Material,Supplement,2010-01-06T05:00:00Z,2010,1,,,2024-11-07T22:11:34Z,,0,0,0900006480a76c32
FAA-2009-0660-0001,FAA,FAA-2009-0660,Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures,Rule,Federal Register Publication,2010-01-06T05:00:00Z,2010,1,2010-01-06T05:00:00Z,2010-04-07T03:59:59Z,2024-11-07T22:12:41Z,E9-31381,1,0,0900006480a77926