N331UP
Airworthiness directives that may apply · 80
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
Query with SQL
duckdb -csv -c "SELECT d.ad_number, d.status, d.subject, d.effective_date, m.matched_by
FROM (
SELECT ad_id, min(rank) AS rank, arg_min(matched_by, rank) AS matched_by
FROM (SELECT ad_id, 1 AS rank, 'airframe' AS matched_by FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_directive.parquet' WHERE aircraft_model_code = '1385212'
UNION ALL SELECT ad_id, 2, 'engine' FROM 'https://openairdocs.org/data/latest/faa_engine_model_directive.parquet' WHERE engine_model_code = '30025')
GROUP BY ad_id
) m JOIN 'https://openairdocs.org/data/latest/faa_directive.parquet' d USING (ad_id)
ORDER BY d.status = 'Historical', m.rank, coalesce(d.effective_date, d.publication_date, d.issue_date) DESC, d.ad_number DESC"Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT d.ad_number, d.status, d.subject, d.effective_date, m.matched_by
FROM (
SELECT ad_id, min(rank) AS rank, arg_min(matched_by, rank) AS matched_by
FROM (SELECT ad_id, 1 AS rank, 'airframe' AS matched_by FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_directive.parquet' WHERE aircraft_model_code = '1385212'
UNION ALL SELECT ad_id, 2, 'engine' FROM 'https://openairdocs.org/data/latest/faa_engine_model_directive.parquet' WHERE engine_model_code = '30025')
GROUP BY ad_id
) m JOIN 'https://openairdocs.org/data/latest/faa_directive.parquet' d USING (ad_id)
ORDER BY d.status = 'Historical', m.rank, coalesce(d.effective_date, d.publication_date, d.issue_date) DESC, d.ad_number DESCRun it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
| 1985 | 1 |
|---|---|
| 1986 | 1 |
| 1989 | 1 |
| 1990 | 2 |
| 1991 | 6 |
| 1992 | 1 |
| 1993 | 1 |
| 1994 | 3 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 4 |
| 2000 | 6 |
| 2001 | 2 |
| 2002 | 2 |
| 2003 | 4 |
| 2004 | 3 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 5 |
| 2008 | 3 |
| 2009 | 7 |
| 2011 | 1 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2020 | 2 |
| 2021 | 2 |
| 2022 | 2 |
| 2023 | 1 |
| 2025 | 1 |
Engine · GE CF6-80 series
AD 2024-24-03Engine ExhaustAD 2023-20-08Engine (Turbine/Turboprop)AD 2021-26-22Turbine SectionAD 2022-02-18Engine Mount SectionAD 2021-14-11Turbine SectionAD 2021-03-02Fuel Control/Turbine EnginesAD 2020-22-02Engine Fuel and ControlAD 2018-07-05Turbine SectionAD 2017-11-15Turbine/ Turboprop Engine--Turbine SectionAD 2016-08-10Accessory heat shieldAD 2014-21-01Fuel manifoldAD 2013-08-20Fuel tubeAD 2012-03-12No. 3 bearing packingAD 2012-04-05Electronic control unit (ECU)AD 2011-23-04Forward engine mount assembly side linksAD 2009-21-07Thrust and thrust controlAD 2009-14-08High-pressure compressor rotor (HPCR) stages 11-14 spool/ shaftsAD 2009-08-06Stage 1 high-pressure turbine (HPT) rotor disksAD 2009-07-10High-pressure turbine rotor (HPTR)AD 2009-07-03Eddy current inspection (ECI)AD 2009-04-10Critical life-limited partsAD 2008-21-11Low-pressure turbine (LPT) casesAD 2008-02-17Thrust reverser actuation systemsAD 2007-24-07Thermal spray coating on certain stage 1 fan disksAD 2007-22-07Electronic control unit (ECU)AD 2007-21-06Electronic control unit (ECU)AD 2007-11-20Fuel shroud retaining ringsAD 2007-05-14Cast titanium weld- repaired forward engine mount platformsAD 2006-16-06Certain stage 1 high- pressure turbine (HPT) rotor disksAD 2006-06-08Latching system of the fan reverserAD 2005-17-05High pressure compressor rotor (HPCR)AD 2005-06-07Directional pilot valve (DPV) assemblyAD 2004-22-07Stage 2 nozzle guide vanes (HPT S2 NGVs)AD 2004-07-13High pressure turbine (HPT) stage 1 disksAD 2003-12-08Directional pilot valveAD 2003-02-07Low pressure turbine (LPT) shroudsAD 2002-25-08High pressure compressor rotorAD 2002-22-12Titeflex hosesAD 2001-06-09Aft Engine Mount Link AssembliesAD 2000-12-08Mount Link AssembliesAD 2000-03-04Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan EnginesAD 99-01-01Accessory Gearbox (AGB) idler adaptersAD 98-22-06Fan DisksAD 97-22-14(HPCR) 3-9 SpoolAD 96-16-07Rear Right Hand Mount LinkAD 95-17-16Compressor Rear FrameAD 95-10-11Fan ReversersAD 94-20-06Oil SystemAD 94-07-04High Pressure Turbine DiskAD 94-06-03High Pressure Turbine DiskAD 93-14-18High pressure turbine (HPT) thermal shieldsAD 92-04-08Stage 1 Disk/ShaftsAD 91-23-13Fan DisksAD 91-15-25High Pressure Compressor RotorAD 91-11-05High Pressure Compressor RotorAD 91-05-21High Pressure TurbineAD 91-01-04Fan DiskAD 90-23-05Engine Aft Mount,AD 89-16-08ManifoldAD 86-15-04Stage 1 High Pressure Turbine (HPT) DisksAD 85-15-51Fuel Manifold Supply TubeSuperseded and historical ADs · 19
AD 2020-20-13Turbine SectionHistoricalAD 2018-15-04Turbine/Turboprop Engine--Turbine SectionHistoricalAD 2009-05-02Drainless fuel manifold assembliesHistoricalAD 2007-12-07Electronic control units (ECUs)HistoricalAD 2006-12-24Five-link forward mount assemblyHistoricalAD 2004-04-07Stage 1 HPT rotor disksHistoricalAD 2003-01-05Dovetail slotsHistoricalAD 2002-07-12Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited PartsHistoricalAD 2001-10-07High Pressure Turbine Rotor DisksHistoricalAD 2000-08-12Life-limited PartsHistoricalAD 2000-16-12High Pressure Compressor Rotor Stage 3-9 SpoolsHistoricalAD 2000-04-14Fuel tube flange seatingHistoricalAD 99-24-15High Pressure Compressor Rotor (HPCR) Stage 3-9 SpoolsHistoricalAD 99-18-20Inadvertent In-flight Thrust ReverserHistoricalAD 99-18-19Inadvertent Thrust ReverserHistoricalAD 99-08-13Airworthiness Directives; General Electric Company CF6-80A, CF6-80C2, and CF6-80E1 Series Turbofan EnginesHistoricalAD 98-15-17Link AssemblyHistoricalAD 91-20-02Fuel ManifoldsHistoricalAD 90-26-01Fuel Manifold SystemsHistorical