Pratt & Whitney JT8D-209
Airworthiness directives that may apply · 37
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 ('51690'))
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 ('51690'))
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.
| 1970 | 4 |
|---|---|
| 1977 | 1 |
| 1980 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 1 |
| 1999 | 4 |
| 2000 | 2 |
| 2001 | 1 |
| 2002 | 4 |
| 2003 | 1 |
| 2005 | 4 |
| 2006 | 3 |
| 2010 | 1 |
| 2011 | 2 |
| 2021 | 1 |
Engine · Pratt & Whitney JT8D-209
AD 2021-22-19Turbine Engine Compressor SectionAD 2011-04-04Critical life-limited partsAD 97-17-04 R1Front compressor front hubAD 2006-17-07 R1High pressure compressor (HPC) front hubs and HPC diskAD 2005-21-01High pressure turbine (HPT) shaftAD 2005-17-16Critical life-limited rotating partsAD 2004-26-04HPT containment hardwareAD 2003-16-05High pressure compressor (HPC) disksAD 2002-21-17Fan duct and fan exit guide vaneAD 2002-16-08Combustion Chamber Outer Case (CCOC)AD 99-10-11Fan Blades and ShroudsAD 99-01-08Stage 7 through Stage 15 High-Pressure Compressor (HPC) DisksAD 98-21-24Compressor DisksAD 96-15-06First Stage Fan HubsAD 95-02-16Fuel Nozzle and Support AssemblyAD 91-24-14Bearing Seal SpacerAD 88-04-02Anti-rotation Pin FailuresAD 87-03-13Compressor BladeAD 80-15-51Engine Rear Compressor Front HubsAD 75-05-06Fuel Manifold LeakageAD 70-26-05First Stage Compressor Rotor BladesAD 70-25-08Seventh Stage Compressor Rotor DiscAD 70-11-03Sixth Stage Compressor DiscsAD 70-02-02Sixth Stage Compressor Rotor DiscSuperseded and historical ADs · 13
AD 2011-07-02Turbine BladeHistoricalAD 2006-17-07Fretting and fluorescent magnetic particle inspections (FMPI) for cracking in the area of the tierod holes on the HPC front hubsHistoricalAD 2005-18-02Engine manufacturer's time limits section (TLS)HistoricalAD 2005-02-03Turbine (LPT) Blades 3rd and 4th StageHistoricalAD 2002-23-14High Pressure Compressor (HPC) Front HubsHistoricalAD 2002-13-09Rotating engine partsHistoricalAD 2000-21-07Critical Life-Limited PartsHistoricalAD 99-26-06Combustion Chamber Outer CaseHistoricalAD 99-27-01Low Pressure Turbine BladesHistoricalAD 99-22-14High Pressure Turbine ShaftHistoricalAD 99-12-04Critical Life Limited Part InspectionHistoricalAD 97-19-13High Pressure Turbine (HPT) ShaftHistoricalAD 97-17-04Fan HubsHistorical