TCDS E34NE

Airworthiness directives · 37

ADs whose products are models on this data sheet, matched by model and maker. Those in force first, newest first.

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_directive_product.parquet' WHERE tcds_number = 'E34NE')
  ORDER BY d.status = 'Historical', coalesce(d.effective_date, d.publication_date) 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.

AD 2026-19-03Engine (Turbine/Turboprop)Effective Nov 2, 2026 · Supersedes AD 2023-15-03AD 2026-08-12Engine Fuel PumpEffective Jun 2, 2026AD 2025-13-07Engine Fuel and ControlEffective Aug 6, 2025AD 2024-24-02Engine Fuel PumpEffective Dec 10, 2024AD 2023-24-09Engine Indicating SystemEffective Jan 17, 2024AD 2023-15-03Engine (Turbine/Turboprop)Effective Sep 7, 2023AD 2021-26-26Engine ControlsEffective Feb 23, 2022 · Supersedes AD 2005-12-08AD 2021-17-05Fuel Controlling SystemEffective Oct 12, 2021 · Supersedes AD 2014-04-06AD 2018-12-03Fuel Controlling SystemEffective Aug 9, 2018 · Supersedes AD 2013-11-09AD 2018-07-17Turbine SectionEffective Apr 27, 2018AD 2018-05-03Engine Oil System (Airframe Furnished)Effective Mar 21, 2018AD 2015-17-18Oil pumpEffective Oct 2, 2015AD 2015-10-07Ejector assembly nozzleEffective Jun 12, 2015 · Supersedes AD 2014-01-01AD 2012-07-09P3 air pipe (first section) and the RH rear half-wallEffective May 24, 2012 · Supersedes AD 2009-14-11AD 2009-21-11Cycle life limit value for ARRIUS 1A balancing piston.Effective Nov 20, 2009AD 2009-14-01Check valve pistonEffective Aug 3, 2009 · Supersedes AD 2005-17-17 R1AD 2008-19-11Electronic control (EEC) unitEffective Oct 8, 2008AD 2008-13-27PropellerEffective Aug 6, 2008AD 2007-11-06Constant delta pressure (delta P) diaphragmEffective Jun 26, 2007 · Supersedes AD 2005-19-10AD 2006-26-07A simultaneous interruption of the lubrication on both engines may lead to a double non-commanded in-flight shutdown.Effective Jan 18, 2007AD 2005-17-15Fuel filter-holder assemblyEffective Sep 12, 2005AD 2005-11-01Free Turbine Overspeed Protection SystemEffective Jun 13, 2005AD 2005-09-51Emergency ADModule 2Effective Jun 3, 2005AD 2003-19-06Gas generator high pressure (HP) turbine diskEffective Oct 22, 2003AD 2003-11-10Fuel Flow Mechanical Stop PositionEffective Jul 3, 2003AD 2002-01-02Main Fuel InjectorsEffective Jan 22, 2002AD 2000-06-09Fuel Injection SystemEffective Jun 12, 2000AD 2014-04-06HistoricalHydro-mechanical metering unit (HMU)Effective Mar 31, 2014 · Replaced by AD 2021-17-05AD 2014-01-01HistoricalEjector assembly nozzleEffective Feb 6, 2014 · Replaced by AD 2015-10-07AD 2013-11-09HistoricalFuel injection manifolds and the privilege injectorEffective Jul 5, 2013 · Replaced by AD 2018-12-03AD 2009-14-11HistoricalP3 air pipeEffective Aug 19, 2009 · Replaced by AD 2012-07-09AD 2005-17-17 R1HistoricalO-rings on the check valve pistonEffective Mar 21, 2007 · Replaced by AD 2009-14-01AD 2001-08-14 R1HistoricalRight injector half manifold and left injector half manifoldEffective Feb 23, 2006 · Replaced by AD 2013-11-09AD 2005-19-10HistoricalFuel control units (FCUs)Effective Oct 3, 2005 · Replaced by AD 2007-11-06AD 2005-17-17HistoricalCheck valve piston in the lubrication unitEffective Sep 12, 2005 · Replaced by AD 2005-17-17 R1AD 2005-12-08HistoricalEngine Electronic Control Unit (EECU)Effective Jun 29, 2005 · Replaced by AD 2021-26-26AD 2001-08-14HistoricalFuel Injector ManifoldEffective May 31, 2001 · Replaced by AD 2001-08-14 R1
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