# Airworthiness directives that may apply: N962CE

A list on [N962CE](https://openairdocs.org/aircraft/N962CE.md).

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

- [AD 2021-22-19](https://openairdocs.org/ad/2021-22-19.md): Turbine Engine Compressor Section · Effective Dec 28, 2021 · Supersedes AD 2011-07-02
- [AD 2015-14-05](https://openairdocs.org/ad/2015-14-05.md): Cracking in the low-pressure turbine (LPT) shaft · Effective Aug 25, 2015
- [AD 2011-04-04](https://openairdocs.org/ad/2011-04-04.md): Critical life-limited parts · Effective Mar 22, 2011 · Supersedes AD 2005-18-02
- [AD 2011-03-01](https://openairdocs.org/ad/2011-03-01.md): Critical life- limited parts · Effective Mar 4, 2011 · Supersedes AD 2005-25-05
- [AD 2010-21-17](https://openairdocs.org/ad/2010-21-17.md): Fan blade · Effective Nov 12, 2010
- [AD 97-17-04 R1](https://openairdocs.org/ad/97-17-04-R1.md): Front compressor front hub · Effective Apr 22, 2010 · Supersedes AD 97-17-04
- [AD 2009-24-01](https://openairdocs.org/ad/2009-24-01.md): Fan blade · Effective Jan 4, 2010 · Supersedes AD 87-14-01 R1
- [AD 2006-17-07 R1](https://openairdocs.org/ad/2006-17-07-R1.md): High pressure compressor (HPC) front hubs and HPC disk · Effective Nov 2, 2006 · Supersedes AD 2006-17-07
- [AD 2005-21-01](https://openairdocs.org/ad/2005-21-01.md): High pressure turbine (HPT) shaft · Effective Nov 21, 2005 · Supersedes AD 97-19-13
- [AD 2005-17-16](https://openairdocs.org/ad/2005-17-16.md): Critical life-limited rotating parts · Effective Sep 30, 2005
- [AD 2004-26-04](https://openairdocs.org/ad/2004-26-04.md): HPT containment hardware · Effective Feb 9, 2005 · Supersedes AD 99-22-14
- [AD 2003-16-05](https://openairdocs.org/ad/2003-16-05.md): High pressure compressor (HPC) disks · Effective Sep 12, 2003
- [AD 2003-12-07](https://openairdocs.org/ad/2003-12-07.md): 12th Stage high pressure compressor · Effective Jul 18, 2003 · Supersedes AD 98-12-07
- [AD 2003-05-07](https://openairdocs.org/ad/2003-05-07.md): Low pressure compressor (LPC) · Effective Apr 17, 2003
- [AD 2002-21-17](https://openairdocs.org/ad/2002-21-17.md): Fan duct and fan exit guide vane · Effective Nov 29, 2002
- [AD 2002-16-08](https://openairdocs.org/ad/2002-16-08.md): Combustion Chamber Outer Case (CCOC) · Effective Sep 20, 2002 · Supersedes AD 99-26-06
- [AD 2001-15-18](https://openairdocs.org/ad/2001-15-18.md): Stage Compressor Disks · Effective Sep 4, 2001
- [AD 2000-22-06](https://openairdocs.org/ad/2000-22-06.md): Main Fuel Pump · Effective Dec 4, 2000
- [AD 99-10-11](https://openairdocs.org/ad/99-10-11.md): Fan Blades and Shrouds · Effective Jun 14, 1999
- [AD 99-01-08](https://openairdocs.org/ad/99-01-08.md): Stage 7 through Stage 15 High-Pressure Compressor (HPC) Disks · Effective Jan 5, 1999
- [AD 98-21-24](https://openairdocs.org/ad/98-21-24.md): Compressor Disks · Effective Nov 16, 1998
- [AD 98-04-39](https://openairdocs.org/ad/98-04-39.md): Combustion Chamber Outer Case · Effective Feb 25, 1998
- [AD 97-19-12](https://openairdocs.org/ad/97-19-12.md): Hub Inspection · Effective Nov 18, 1997
- [AD 97-19-14](https://openairdocs.org/ad/97-19-14.md): Low Pressure Turbine (LPT) Blade Sets · Effective Oct 24, 1997
- [AD 96-23-14](https://openairdocs.org/ad/96-23-14.md): Combustion Chamber Outer Cases · Effective Jan 2, 1997
- [AD 96-15-06](https://openairdocs.org/ad/96-15-06.md): First Stage Fan Hubs · Effective Sep 3, 1996
- [AD 95-26-03](https://openairdocs.org/ad/95-26-03.md): High Pressure Compressor Disks · Effective Jan 11, 1996
- [AD 86-09-02 R2](https://openairdocs.org/ad/86-09-02-R2.md): Combustion Chamber Liners · Effective Nov 17, 1995
- [AD 95-16-07](https://openairdocs.org/ad/95-16-07.md): High Pressure Compressor (HPC) Disks · Effective Sep 11, 1995
- [AD 95-10-10](https://openairdocs.org/ad/95-10-10.md): Compressor Fan Hub · Effective Jul 21, 1995
- [AD 94-25-07](https://openairdocs.org/ad/94-25-07.md): Combustion Chamber Outer Case · Effective Mar 30, 1995
- [AD 95-02-16](https://openairdocs.org/ad/95-02-16.md): Fuel Nozzle and Support Assembly · Effective Feb 21, 1995
- [AD 94-20-09](https://openairdocs.org/ad/94-20-09.md): Low Pressure Turbine Blade Sets · Effective Nov 14, 1994
- [AD 91-24-14](https://openairdocs.org/ad/91-24-14.md): Bearing Seal Spacer · Effective Jan 21, 1992
- [AD 89-25-11](https://openairdocs.org/ad/89-25-11.md): Fan Blade Retaining Plates · Effective Jan 15, 1990
- [AD 89-24-02](https://openairdocs.org/ad/89-24-02.md): Fan Disk · Effective Nov 13, 1989
- [AD 88-04-02](https://openairdocs.org/ad/88-04-02.md): Anti-rotation Pin Failures · Effective Mar 4, 1988
- [AD 87-03-13](https://openairdocs.org/ad/87-03-13.md): Compressor Blade · Effective Feb 16, 1987
- [AD 86-08-04 R1](https://openairdocs.org/ad/86-08-04-R1.md): HPC Removable Sleeve Spacers · Effective Nov 4, 1986
- [AD 86-02-52 R1](https://openairdocs.org/ad/86-02-52-R1.md): Combustion Chamber · Effective Apr 14, 1986
- [AD 85-19-51 R1](https://openairdocs.org/ad/85-19-51-R1.md): Second Stage Turbine Disk · Effective Dec 26, 1985
- [AD 78-17-02 R3](https://openairdocs.org/ad/78-17-02-R3.md): Compressor Front Hubs · Effective Mar 30, 1984
- [AD 80-15-51](https://openairdocs.org/ad/80-15-51.md): Engine Rear Compressor Front Hubs · Effective Aug 21, 1980
- [AD 78-23-12](https://openairdocs.org/ad/78-23-12.md): Third Stage Turbine Blade Rivet · Effective Dec 20, 1978
- [AD 77-16-12](https://openairdocs.org/ad/77-16-12.md): Low Turbine Shaft · Effective Aug 31, 1977
- [AD 76-24-01](https://openairdocs.org/ad/76-24-01.md): Eighth Stage Compressor Disk · Effective Jun 22, 1977
- [AD 77-07-11](https://openairdocs.org/ad/77-07-11.md): Fourth Stage Turbine Stator And Rotor · Effective Apr 15, 1977
- [AD 77-03-06](https://openairdocs.org/ad/77-03-06.md): Compressor Front Hubs · Effective Feb 25, 1977
- [AD 75-05-06](https://openairdocs.org/ad/75-05-06.md): Fuel Manifold Leakage · Effective Feb 24, 1977
- [AD 76-20-02](https://openairdocs.org/ad/76-20-02.md): Second Stage Fan Blades · Effective Oct 10, 1976
- [AD 75-01-01](https://openairdocs.org/ad/75-01-01.md): Low Turbine Shaft Spline · Effective Sep 17, 1975
- [AD 71-25-07](https://openairdocs.org/ad/71-25-07.md): Fuel Nozzle Support Assemblies · Effective Dec 14, 1971
- [AD 71-07-01](https://openairdocs.org/ad/71-07-01.md): Front Compressor Front Hub · Effective Sep 7, 1971
- [AD 70-26-05](https://openairdocs.org/ad/70-26-05.md): First Stage Compressor Rotor Blades · Effective Dec 29, 1970
- [AD 70-25-08](https://openairdocs.org/ad/70-25-08.md): Seventh Stage Compressor Rotor Disc · Effective Dec 15, 1970
- [AD 70-11-03](https://openairdocs.org/ad/70-11-03.md): Sixth Stage Compressor Discs · Effective Jun 12, 1970
- [AD 70-02-02](https://openairdocs.org/ad/70-02-02.md): Sixth Stage Compressor Rotor Disc · Effective Apr 15, 1970
- [AD 76-12-06](https://openairdocs.org/ad/76-12-06.md): Second Stage Fan Blades
- [AD 2011-07-02](https://openairdocs.org/ad/2011-07-02.md): Turbine Blade · Historical · Effective Apr 28, 2011 · Replaced by AD 2021-22-19
- [AD 2006-17-07](https://openairdocs.org/ad/2006-17-07.md): Fretting and fluorescent magnetic particle inspections (FMPI) for cracking in the area of the tierod holes on the HPC front hubs · Historical · Effective Oct 4, 2006 · Replaced by AD 2006-17-07 R1
- [AD 2005-18-02](https://openairdocs.org/ad/2005-18-02.md): Engine manufacturer's time limits section (TLS) · Historical · Effective Feb 28, 2006 · Replaced by AD 2011-04-04
- [AD 2005-02-03](https://openairdocs.org/ad/2005-02-03.md): Turbine (LPT) Blades 3rd and 4th Stage · Historical · Effective Mar 3, 2005 · Replaced by AD 2011-07-02
- [AD 2002-23-14](https://openairdocs.org/ad/2002-23-14.md): High Pressure Compressor (HPC) Front Hubs · Historical · Effective Dec 31, 2002 · Replaced by AD 2006-17-07
- [AD 2002-13-09](https://openairdocs.org/ad/2002-13-09.md): Rotating engine parts · Historical · Effective Dec 30, 2002 · Replaced by AD 2005-18-02
- [AD 2000-21-07](https://openairdocs.org/ad/2000-21-07.md): Critical Life-Limited Parts · Historical · Effective Apr 23, 2001 · Replaced by AD 2002-13-09
- [AD 99-26-06](https://openairdocs.org/ad/99-26-06.md): Combustion Chamber Outer Case · Historical · Effective Feb 22, 2000 · Replaced by AD 2002-16-08
- [AD 99-27-01](https://openairdocs.org/ad/99-27-01.md): Low Pressure Turbine Blades · Historical · Effective Feb 2, 2000 · Replaced by AD 2005-02-03
- [AD 99-22-14](https://openairdocs.org/ad/99-22-14.md): High Pressure Turbine Shaft · Historical · Effective Dec 28, 1999 · Replaced by AD 2004-26-04
- [AD 99-12-04](https://openairdocs.org/ad/99-12-04.md): Critical Life Limited Part Inspection · Historical · Effective Jul 8, 1999 · Replaced by AD 2000-21-07
- [AD 97-19-13](https://openairdocs.org/ad/97-19-13.md): High Pressure Turbine (HPT) Shaft · Historical · Effective Oct 24, 1997 · Replaced by AD 2005-21-01
- [AD 97-17-04](https://openairdocs.org/ad/97-17-04.md): Fan Hubs · Historical · Effective Sep 30, 1997 · Replaced by AD 97-17-04 R1

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = '3023681'
    UNION ALL SELECT ad_id, 2, 'engine' FROM 'https://openairdocs.org/data/latest/faa_engine_model_directive.parquet' WHERE engine_model_code = '52053')
  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
```

This list as a web page: https://openairdocs.org/aircraft/N962CE/ads

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