GE CF6-80A3
Airworthiness directives that may apply · 38
Matched by model name and maker. Each AD’s applicability may narrow it by serial number, part number or configuration.
Query with SQL
duckdb -csv -c "SELECT d.ad_number, d.status, d.subject, d.effective_date
FROM 'https://openairdocs.org/data/latest/faa_directive.parquet' d
WHERE d.ad_id IN (SELECT ad_id FROM 'https://openairdocs.org/data/latest/faa_engine_model_directive.parquet' WHERE engine_model_code IN ('30096'))
ORDER BY 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
FROM 'https://openairdocs.org/data/latest/faa_directive.parquet' d
WHERE d.ad_id IN (SELECT ad_id FROM 'https://openairdocs.org/data/latest/faa_engine_model_directive.parquet' WHERE engine_model_code IN ('30096'))
ORDER BY 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.
| 1986 | 1 |
|---|---|
| 1989 | 1 |
| 1990 | 1 |
| 1991 | 4 |
| 1992 | 1 |
| 1993 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1998 | 2 |
| 1999 | 3 |
| 2000 | 3 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 3 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 2 |
| 2008 | 1 |
| 2009 | 3 |
| 2011 | 1 |
| 2018 | 2 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 1 |
Engine · GE CF6-80A3
AD 2021-26-22Turbine SectionAD 2021-14-11Turbine SectionAD 2018-07-05Turbine SectionAD 2011-23-04Forward engine mount assembly side linksAD 2009-08-06Stage 1 high-pressure turbine (HPT) rotor disksAD 2009-07-10High-pressure turbine rotor (HPTR)AD 2009-04-10Critical life-limited partsAD 2008-02-17Thrust reverser actuation systemsAD 2006-16-06Certain stage 1 high- pressure turbine (HPT) rotor disksAD 2005-06-07Directional pilot valve (DPV) assemblyAD 2003-12-08Directional pilot valveAD 2002-25-08High pressure compressor rotorAD 2001-06-09Aft Engine Mount Link AssembliesAD 98-22-06Fan DisksAD 95-17-16Compressor Rear FrameAD 94-07-04High 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 91-01-04Fan DiskAD 90-23-05Engine Aft Mount,AD 89-16-08ManifoldAD 86-15-04Stage 1 High Pressure Turbine (HPT) DisksSuperseded and historical ADs · 13
AD 2020-20-13Turbine SectionHistoricalAD 2018-15-04Turbine/Turboprop Engine--Turbine SectionHistoricalAD 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 2000-08-12Life-limited PartsHistoricalAD 2000-16-12High Pressure Compressor Rotor Stage 3-9 SpoolsHistoricalAD 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 AssemblyHistorical