documents
Data license: Public Domain (U.S. Government data) · Data source: Federal Register API & Regulations.gov API
10 rows where docket_id = "FAA-2006-25970" sorted by posted_date descending
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Suggested facets: title, subtype, posted_date, posted_month, comment_start_date, comment_end_date, last_modified, open_for_comment, posted_date (date), comment_start_date (date), comment_end_date (date), last_modified (date)
document_type 4
agency_id 1
- FAA 10
| 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| posted_year | posted_month | comment_start_date | comment_end_date | last_modified | fr_doc_num | open_for_comment | withdrawn | object_id |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-2006-25970-0010 | FAA | None FAA-2006-25970 | U.S. DOT/FAA - Supplemental AD Documents | Supporting & Related Material | Supplement | 2016-08-31T04:00:00Z | 2016 | 8 | 2016-08-31T20:10:10Z | 0 | 0 | 09000064821b007b | |||
| FAA-2006-25970-0009 | FAA | None FAA-2006-25970 | Airworthiness Directives: Turbomeca S.A. Turboshaft Engines | Rule | Final Rule | 2016-03-17T04:00:00Z | 2016 | 3 | 2016-03-17T04:00:00Z | 2016-03-17T13:33:02Z | 2016-06000 | 0 | 0 | 0900006481ecae85 | |
| FAA-2006-25970-0008 | FAA | None FAA-2006-25970 | U.S. DOT/FAA - Various Supplemental AD Documents | Supporting & Related Material | Supplement | 2015-12-22T05:00:00Z | 2015 | 12 | 2015-12-22T15:29:54Z | 0 | 0 | 0900006481db7549 | |||
| FAA-2006-25970-0007 | FAA | None FAA-2006-25970 | Airworthiness Directives: Turbomeca S.A. Turboshaft Engines | Proposed Rule | Notice of Proposed Rulemaking (NPRM) | 2015-11-25T05:00:00Z | 2015 | 11 | 2015-11-25T05:00:00Z | 2016-01-26T04:59:59Z | 2024-11-07T23:34:41Z | 2015-29886 | 1 | 0 | 0900006481d72a18 |
| FAA-2006-25970-0005 | FAA | None FAA-2006-25970 | U.S. DOT/FAA - Incorporation by Reference Approval Letter | Other | Incorporation by Reference | 2007-12-28T05:00:00Z | 2007 | 12 | 2007-12-28T05:00:00Z | 2024-11-12T04:06:27Z | 1 | 0 | 090000648037f513 | ||
| FAA-2006-25970-0006 | FAA | None FAA-2006-25970 | U.S. DOT/FAA - Incorporation by Reference Approval Letter | Other | Incorporation by Reference | 2007-12-28T05:00:00Z | 2007 | 12 | 2007-12-28T05:00:00Z | 2024-11-12T04:06:28Z | 1 | 0 | 090000648037f51d | ||
| FAA-2006-25970-0002 | FAA | None FAA-2006-25970 | U.S. DOT/FAA - Final Rule (Original) | Rule | Final Rule | 2006-11-28T05:00:00Z | 2006 | 11 | 2006-11-28T05:00:00Z | 2006-11-29T04:59:59Z | 2024-11-07T17:02:54Z | 1 | 0 | 09000064802bafc4 | |
| FAA-2006-25970-0004 | FAA | None FAA-2006-25970 | U.S. DOT/FAA - Additional Information | Other | Additional Information | 2006-11-28T05:00:00Z | 2006 | 11 | 2006-11-28T05:00:00Z | 2006-11-29T04:59:59Z | 2024-11-07T17:02:54Z | 1 | 0 | 09000064802bafc6 | |
| FAA-2006-25970-0003 | FAA | None FAA-2006-25970 | U.S. DOT/FAA - Airworthiness Directive Grid | Supporting & Related Material | Airworthiness Directive Grid | 2006-11-28T05:00:00Z | 2006 | 11 | 2024-11-07T17:02:54Z | 0 | 0 | 09000064802bafc5 | |||
| FAA-2006-25970-0001 | FAA | None FAA-2006-25970 | U.S. DOT/FAA - Final Rule | Rule | Federal Register Publication | 2006-11-16T05:00:00Z | 2006 | 11 | 2006-11-16T05:00:00Z | 2006-11-17T04:59:59Z | 2024-11-07T17:02:54Z | 1 | 0 | 09000064802bafc3 |
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CREATE TABLE documents (
id TEXT PRIMARY KEY,
agency_id TEXT,
docket_id TEXT REFERENCES dockets(id),
title TEXT,
document_type TEXT,
subtype TEXT,
posted_date TEXT,
posted_year INTEGER,
posted_month INTEGER,
comment_start_date TEXT,
comment_end_date TEXT,
last_modified TEXT,
fr_doc_num TEXT,
open_for_comment INTEGER,
withdrawn INTEGER,
object_id TEXT
);
CREATE INDEX idx_docs_agency ON documents(agency_id);
CREATE INDEX idx_docs_docket ON documents(docket_id);
CREATE INDEX idx_docs_date ON documents(posted_date);
CREATE INDEX idx_docs_year ON documents(posted_year);
CREATE INDEX idx_docs_type ON documents(document_type);
CREATE INDEX idx_docs_frnum ON documents(fr_doc_num);
CREATE INDEX idx_docs_comment_end ON documents(comment_end_date) WHERE comment_end_date IS NOT NULL AND withdrawn = 0;