# N574AA: 1991 Mcdonnell Douglas DC-9-82(MD-82)

- Status: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082, 172 seats)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 53151
- Year built: 1991
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 4, 1991
- Certificate issued: January 28, 2019
- Expires: January 31, 2029
- Mode S code: A75D46
- Registered owner: [Pac Blue Aerospace](https://openairdocs.org/faa-owner/PAC%20BLUE%20AEROSPACE)
- Location: [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks)
- Owner type: Corporation
- Owner's area on the map: 64.0097° N, 144.6830° W: Placed by OpenAirDocs at the center of ZIP code 99706, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=574AA
- Page: https://openairdocs.org/aircraft/N574AA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Pratt & Whitney JT8D model are included.

## ADs that may apply (OpenAirDocs): 326 in force

### Matched by airframe (Mcdonnell Douglas DC-9-82(MD-82))

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-09-11](https://openairdocs.org/ad/2025-09-11): Flight controls · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 20 more. Effective Jun 12, 2025
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-02-09](https://openairdocs.org/ad/2023-02-09): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Mar 20, 2023
- [AD 2023-01-13](https://openairdocs.org/ad/2023-01-13): Wings · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Mar 13, 2023
- [AD 2020-10-10](https://openairdocs.org/ad/2020-10-10): Wings · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Jun 26, 2020
- [AD 2018-07-04](https://openairdocs.org/ad/2018-07-04): Ice and rain protection · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 3 more. Effective Sep 10, 2018
- [AD 2018-03-04](https://openairdocs.org/ad/2018-03-04): Airspeed/Mach Indicator · Boeing 717-200, DC-9-11, DC-9-12 and 23 more. Effective Mar 16, 2018
- [AD 2017-19-05](https://openairdocs.org/ad/2017-19-05): Smoke Detection · Airbus A330-201, A330-202, A330-203 and 30 more. Effective Oct 31, 2017
- [AD 2017-17-19](https://openairdocs.org/ad/2017-17-19): Fuselage · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Oct 4, 2017
- [AD 2016-25-06](https://openairdocs.org/ad/2016-25-06): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Jan 25, 2017
- [AD 2016-03-06](https://openairdocs.org/ad/2016-03-06): Fuel · Boeing DC-9-11, DC-9-12, DC-9-13 and 21 more. Effective Mar 23, 2016
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-21-04](https://openairdocs.org/ad/2014-21-04): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Dec 2, 2014
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2014-05-27](https://openairdocs.org/ad/2014-05-27): Navigation · Airbus A319-111, A319-112, A319-113 and 99 more. Effective May 2, 2014
- [AD 2013-05-02](https://openairdocs.org/ad/2013-05-02): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Apr 15, 2013
- [AD 2012-21-13](https://openairdocs.org/ad/2012-21-13): Wings · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Dec 4, 2012
- [AD 2011-21-08](https://openairdocs.org/ad/2011-21-08): Equipment/Furnishings · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 202 more. Effective Nov 23, 2011
- [AD 2011-17-11](https://openairdocs.org/ad/2011-17-11): Wings · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Sep 26, 2011
- [AD 2011-15-01](https://openairdocs.org/ad/2011-15-01): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Aug 19, 2011
- [AD 2011-14-03](https://openairdocs.org/ad/2011-14-03): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Aug 10, 2011
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-01-16](https://openairdocs.org/ad/2011-01-16): Fuel · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Feb 16, 2011
- [AD 2010-25-04](https://openairdocs.org/ad/2010-25-04): Compliance · Boeing DC-9-31, DC-9-32, DC-9-32 (VC-9C) and 14 more. Effective Jan 11, 2011
- [AD 2009-15-16 R1](https://openairdocs.org/ad/2009-15-16-R1): Doors · Intrusion/Penetration Resistance Flightdeck Door and Reinforced… (Aircraft Reconfig Technologies STC ST02463AT). Effective Aug 5, 2010
- [AD 2009-21-10 R1](https://openairdocs.org/ad/2009-21-10-R1): Oxygen · Airbus A300 B4-605R, A300 B4-620, A300 B4-622 and 138 more. Effective Feb 4, 2010
- [AD 2008-22-01](https://openairdocs.org/ad/2008-22-01): Auxiliary fuel tanks · Boeing 727-100 Series, 727-200 Series, 727 Series and 17 more. Effective Nov 26, 2008
- [AD 2008-13-29](https://openairdocs.org/ad/2008-13-29): Overwing frames · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Aug 12, 2008
- [AD 2008-11-15](https://openairdocs.org/ad/2008-11-15): Fuel tank systems · Boeing 717-200, DC-9-11, DC-9-12 and 21 more. Effective Jul 3, 2008
- [AD 2008-06-27](https://openairdocs.org/ad/2008-06-27): Evacuation system's shear-pin · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 91 more. Effective Apr 28, 2008
- [AD 2008-03-12](https://openairdocs.org/ad/2008-03-12): Rudder pedal bracket · Boeing DC-8-11, DC-8-12, DC-8-21 and 47 more. Effective Mar 11, 2008
- [AD 2007-25-16](https://openairdocs.org/ad/2007-25-16): Forward passenger doorjamb · Boeing DC-9-81 (MD-81) and DC-9-82 (MD-82). Effective Jan 14, 2008
- [AD 2007-17-18](https://openairdocs.org/ad/2007-17-18): Static port heater assemblies · Boeing DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Oct 2, 2007
- [AD 2006-16-02](https://openairdocs.org/ad/2006-16-02): Refueling Manifold · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Sep 7, 2006
- [AD 2006-15-15](https://openairdocs.org/ad/2006-15-15): Wire bundle for the auxiliary hydraulic pump · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Sep 5, 2006
- [AD 2006-10-14](https://openairdocs.org/ad/2006-10-14): Stop pad support fittings · Boeing 717-200, DC-9-11, DC-9-12 and 22 more. Effective Jun 21, 2006
- [AD 2006-07-11](https://openairdocs.org/ad/2006-07-11): Aft attach fitting assembly of the spoiler link · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 3 more. Effective May 5, 2006
- [AD 2006-06-04](https://openairdocs.org/ad/2006-06-04): Main landing gear (MLG) · Boeing DC-9-11, DC-9-12, DC-9-13 and 17 more. Effective Apr 20, 2006
- [AD 2006-01-02](https://openairdocs.org/ad/2006-01-02): Upper lock link assembly of the nose landing gear (NLG) · Boeing DC-9-14, DC-9-15, DC-9-15F and 18 more. Effective Feb 22, 2006
- [AD 2005-13-18](https://openairdocs.org/ad/2005-13-18): Battery terminal screws · Boeing DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Aug 1, 2005
- [AD 2005-09-04](https://openairdocs.org/ad/2005-09-04): Main landing gear (MLG) shock strut pistons · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Jun 2, 2005
- [AD 2005-07-03](https://openairdocs.org/ad/2005-07-03): Rear spar of the left and right wings · Boeing DC-9-11, DC-9-12, DC-9-13 and 17 more. Effective May 4, 2005
- [AD 2004-25-14](https://openairdocs.org/ad/2004-25-14): Main landing gear (MLG) · Boeing DC-9-14, DC-9-15, DC-9-15F and 17 more. Effective Jan 20, 2005
- [AD 2004-23-21](https://openairdocs.org/ad/2004-23-21): Power feeder cables of the auxiliary power unit (APU) · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Jan 3, 2005
- [AD 2004-23-05](https://openairdocs.org/ad/2004-23-05): Ground stud installation of the main battery · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Dec 20, 2004
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-15-13](https://openairdocs.org/ad/2004-15-13): Freeze Protection Ribbon Heaters · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Sep 2, 2004

### Matched by engine (Pratt & Whitney JT8D series)

- [AD 2021-22-19](https://openairdocs.org/ad/2021-22-19): Turbine Engine Compressor Section · Pratt & Whitney JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 28, 2021
- [AD 2015-14-05](https://openairdocs.org/ad/2015-14-05): Cracking in the low-pressure turbine (LPT) shaft · Pratt & Whitney Division JT8D-217C and JT8D-219. Effective Aug 25, 2015
- [AD 2011-04-04](https://openairdocs.org/ad/2011-04-04): Critical life-limited parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 22, 2011
- [AD 2011-03-01](https://openairdocs.org/ad/2011-03-01): Critical life- limited parts · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 9 more. Effective Mar 4, 2011
- [AD 2010-21-17](https://openairdocs.org/ad/2010-21-17): Fan blade · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-17 and 3 more. Effective Nov 12, 2010
- [AD 97-17-04 R1](https://openairdocs.org/ad/97-17-04-R1): Front compressor front hub · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217C and 1 more. Effective Apr 22, 2010
- [AD 2009-24-01](https://openairdocs.org/ad/2009-24-01): Fan blade · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-17 and 5 more. Effective Jan 4, 2010
- [AD 2006-17-07 R1](https://openairdocs.org/ad/2006-17-07-R1): High pressure compressor (HPC) front hubs and HPC disk · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Nov 2, 2006
- [AD 2005-21-01](https://openairdocs.org/ad/2005-21-01): High pressure turbine (HPT) shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Nov 21, 2005
- [AD 2005-17-16](https://openairdocs.org/ad/2005-17-16): Critical life-limited rotating parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Sep 30, 2005
- [AD 2004-26-04](https://openairdocs.org/ad/2004-26-04): HPT containment hardware · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 9, 2005
- [AD 2003-16-05](https://openairdocs.org/ad/2003-16-05): High pressure compressor (HPC) disks · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 12, 2003
- [AD 2003-12-07](https://openairdocs.org/ad/2003-12-07): 12th Stage high pressure compressor · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jul 18, 2003
- [AD 2003-05-07](https://openairdocs.org/ad/2003-05-07): Low pressure compressor (LPC) · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Apr 17, 2003
- [AD 2002-21-17](https://openairdocs.org/ad/2002-21-17): Fan duct and fan exit guide vane · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Nov 29, 2002
- [AD 2002-16-08](https://openairdocs.org/ad/2002-16-08): Combustion Chamber Outer Case (CCOC) · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 20, 2002
- [AD 2001-15-18](https://openairdocs.org/ad/2001-15-18): Stage Compressor Disks · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Sep 4, 2001
- [AD 2000-22-06](https://openairdocs.org/ad/2000-22-06): Main Fuel Pump · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 8 more. Effective Dec 4, 2000
- [AD 99-10-11](https://openairdocs.org/ad/99-10-11): Fan Blades and Shrouds · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Jun 14, 1999
- [AD 99-01-08](https://openairdocs.org/ad/99-01-08): Stage 7 through Stage 15 High-Pressure Compressor (HPC) Disks · Pratt & Whitney Division JT3D-1, JT3D-1-MC6, JT3D-1-MC7 and 30 more. Effective Jan 5, 1999
- [AD 98-21-24](https://openairdocs.org/ad/98-21-24): Compressor Disks · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Nov 16, 1998
- [AD 98-04-39](https://openairdocs.org/ad/98-04-39): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Feb 25, 1998
- [AD 97-19-12](https://openairdocs.org/ad/97-19-12): Hub Inspection · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 9 more. Effective Nov 18, 1997
- [AD 97-19-14](https://openairdocs.org/ad/97-19-14): Low Pressure Turbine (LPT) Blade Sets · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 9 more. Effective Oct 24, 1997
- [AD 96-23-14](https://openairdocs.org/ad/96-23-14): Combustion Chamber Outer Cases · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jan 2, 1997
- [AD 96-15-06](https://openairdocs.org/ad/96-15-06): First Stage Fan Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 3, 1996
- [AD 95-26-03](https://openairdocs.org/ad/95-26-03): High Pressure Compressor Disks · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jan 11, 1996
- [AD 86-09-02 R2](https://openairdocs.org/ad/86-09-02-R2): Combustion Chamber Liners · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Nov 17, 1995
- [AD 95-16-07](https://openairdocs.org/ad/95-16-07): High Pressure Compressor (HPC) Disks · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 11 more. Effective Sep 11, 1995
- [AD 95-10-10](https://openairdocs.org/ad/95-10-10): Compressor Fan Hub · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Jul 21, 1995
- [AD 94-25-07](https://openairdocs.org/ad/94-25-07): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Mar 30, 1995
- [AD 95-02-16](https://openairdocs.org/ad/95-02-16): Fuel Nozzle and Support Assembly · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Feb 21, 1995
- [AD 94-20-09](https://openairdocs.org/ad/94-20-09): Low Pressure Turbine Blade Sets · Pratt & Whitney Division JT8D-15A, JT8D-17A and JT8D-17AR. Effective Nov 14, 1994
- [AD 91-24-14](https://openairdocs.org/ad/91-24-14): Bearing Seal Spacer · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Jan 21, 1992
- [AD 89-25-11](https://openairdocs.org/ad/89-25-11): Fan Blade Retaining Plates · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Jan 15, 1990
- [AD 89-24-02](https://openairdocs.org/ad/89-24-02): Fan Disk · Pratt & Whitney Division JT8D-7, JT8D-7A and JT8D-7B. Effective Nov 13, 1989
- [AD 88-04-02](https://openairdocs.org/ad/88-04-02): Anti-rotation Pin Failures · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 4, 1988
- [AD 87-03-13](https://openairdocs.org/ad/87-03-13): Compressor Blade · Pratt & Whitney Division JT8D-209, JT8D-217 and JT8D-217A. Effective Feb 16, 1987
- [AD 86-08-04 R1](https://openairdocs.org/ad/86-08-04-R1): HPC Removable Sleeve Spacers · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Nov 4, 1986
- [AD 86-02-52 R1](https://openairdocs.org/ad/86-02-52-R1): Combustion Chamber · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Apr 14, 1986
- [AD 85-19-51 R1](https://openairdocs.org/ad/85-19-51-R1): Second Stage Turbine Disk · Pratt & Whitney Division JT8D-15, JT8D-17 and JT8D-17R. Effective Dec 26, 1985
- [AD 78-17-02 R3](https://openairdocs.org/ad/78-17-02-R3): Compressor Front Hubs · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Mar 30, 1984
- [AD 80-15-51](https://openairdocs.org/ad/80-15-51): Engine Rear Compressor Front Hubs · Pratt & Whitney Division JT8D-209, JT8D-1, JT8D-11 and 11 more. Effective Aug 21, 1980
- [AD 78-23-12](https://openairdocs.org/ad/78-23-12): Third Stage Turbine Blade Rivet · Pratt & Whitney Division JT8D-1, JT8D-1A, JT8D-1B and 5 more. Effective Dec 20, 1978
- [AD 77-16-12](https://openairdocs.org/ad/77-16-12): Low Turbine Shaft · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 8 more. Effective Aug 31, 1977
- [AD 76-24-01](https://openairdocs.org/ad/76-24-01): Eighth Stage Compressor Disk · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-1A and 6 more. Effective Jun 22, 1977
- [AD 77-07-11](https://openairdocs.org/ad/77-07-11): Fourth Stage Turbine Stator And Rotor · Pratt & Whitney Division JT8D-9 and JT8D-9A. Effective Apr 15, 1977
- [AD 77-03-06](https://openairdocs.org/ad/77-03-06): Compressor Front Hubs · Pratt & Whitney Division JT8D-1, JT8D-1A, JT8D-1B and 3 more. Effective Feb 25, 1977
- [AD 75-05-06](https://openairdocs.org/ad/75-05-06): Fuel Manifold Leakage · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Feb 24, 1977
- [AD 76-20-02](https://openairdocs.org/ad/76-20-02): Second Stage Fan Blades · Pratt & Whitney Division JT8D-1, JT8D-1A, JT8D-1B and 3 more. Effective Oct 10, 1976

### Historical (superseded or no longer in force)

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2016-07-28](https://openairdocs.org/ad/2016-07-28) (historical): Wings · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Apr 26, 2016
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2012-18-05](https://openairdocs.org/ad/2012-18-05) (historical): Fuel · Boeing DC-9-11, DC-9-12, DC-9-13 and 21 more. Effective Oct 11, 2012
- [AD 2009-15-16](https://openairdocs.org/ad/2009-15-16) (historical): Doors · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 18 more. Effective Jul 6, 2010
- [AD 2009-21-10](https://openairdocs.org/ad/2009-21-10) (historical): Oxygen · Airbus A300, Model B4-605R, A300, Model B4-620, A300, Model B4-622 and 138 more. Effective Dec 17, 2009
- [AD 2007-10-04](https://openairdocs.org/ad/2007-10-04) (historical): Horizontal stabilizer · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective May 23, 2007
- [AD 2006-07-25](https://openairdocs.org/ad/2006-07-25) (historical): Rudder pedal bracket · McDonnell Douglas DC-8-11, DC-8-12, DC-8-21 and 44 more. Effective May 16, 2006
- [AD 2003-17-07](https://openairdocs.org/ad/2003-17-07) (historical): Fire Extinguishers for the Engine and Auxiliary Power Unit (APU) · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 60 more. Effective Sep 24, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2001-06-16](https://openairdocs.org/ad/2001-06-16) (historical): AFM - Ice On Wing Upper Surfaces · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective May 7, 2001
- [AD 2001-07-10](https://openairdocs.org/ad/2001-07-10) (historical): Airplane Flight Manual - Landing Field Length · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 3 more. Effective Apr 27, 2001
- [AD 2000-15-17](https://openairdocs.org/ad/2000-15-17) (historical): Hydraulic Pipe Assembly in the Aft Fuselage · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 3 more. Effective Sep 12, 2000
- [AD 99-24-04](https://openairdocs.org/ad/99-24-04) (historical): Hi-Lok Pin Fasteners · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Dec 27, 1999
- [AD 99-13-07](https://openairdocs.org/ad/99-13-07) (historical): Main Landing Gear Shock Strut Pistons · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 3 more. Effective Jul 28, 1999
- [AD 96-19-09](https://openairdocs.org/ad/96-19-09) (historical): Main Landing Gear Pistons · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Oct 21, 1996
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 96-02-05](https://openairdocs.org/ad/96-02-05) (historical): Rudder Pedals Adjuster Hub Assembly · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Mar 25, 1996
- [AD 96-01-09](https://openairdocs.org/ad/96-01-09) (historical): Main Landing Gear Hydraulic Brake System · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Feb 26, 1996
- [AD 95-22-06](https://openairdocs.org/ad/95-22-06) (historical): Main Landing Gear Shock Strut Cylinder · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Nov 8, 1995
- [AD 95-12-25](https://openairdocs.org/ad/95-12-25) (historical): FIREX Pipe Assembly · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Jul 24, 1995
- [AD 93-13-07](https://openairdocs.org/ad/93-13-07) (historical): Install Water Drain System · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 17 more. Effective Aug 18, 1993
- [AD 92-27-07](https://openairdocs.org/ad/92-27-07) (historical): Rudder Pedals Adjuster Hub Assembly · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Jan 22, 1993
- [AD 92-03-02](https://openairdocs.org/ad/92-03-02) (historical): AFM Limitations Revision · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Jan 17, 1992
- [AD 91-21-11](https://openairdocs.org/ad/91-21-11) (historical): Slat Drive Mechanism Brackets · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Oct 30, 1991
- [AD 88-20-05](https://openairdocs.org/ad/88-20-05) (historical): Generator Power Feeder Cable · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Oct 31, 1988
- [AD 2011-07-02](https://openairdocs.org/ad/2011-07-02) (historical): Turbine Blade · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Apr 28, 2011
- [AD 2006-17-07](https://openairdocs.org/ad/2006-17-07) (historical): Fretting and fluorescent magnetic particle inspections (FMPI) for cracking in the area of the tierod holes on the HPC front hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 18 more. Effective Oct 4, 2006
- [AD 2005-18-02](https://openairdocs.org/ad/2005-18-02) (historical): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 28, 2006
- [AD 2005-02-03](https://openairdocs.org/ad/2005-02-03) (historical): Turbine (LPT) Blades 3rd and 4th Stage · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 3, 2005
- [AD 2002-23-14](https://openairdocs.org/ad/2002-23-14) (historical): High Pressure Compressor (HPC) Front Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 31, 2002
- [AD 2002-13-09](https://openairdocs.org/ad/2002-13-09) (historical): Rotating engine parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 30, 2002
- [AD 2000-21-07](https://openairdocs.org/ad/2000-21-07) (historical): Critical Life-Limited Parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Apr 23, 2001
- [AD 99-26-06](https://openairdocs.org/ad/99-26-06) (historical): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 22, 2000
- [AD 99-27-01](https://openairdocs.org/ad/99-27-01) (historical): Low Pressure Turbine Blades · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 2, 2000
- [AD 99-22-14](https://openairdocs.org/ad/99-22-14) (historical): High Pressure Turbine Shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 28, 1999
- [AD 99-12-04](https://openairdocs.org/ad/99-12-04) (historical): Critical Life Limited Part Inspection · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Jul 8, 1999
- [AD 97-19-13](https://openairdocs.org/ad/97-19-13) (historical): High Pressure Turbine (HPT) Shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Oct 24, 1997
- [AD 97-17-04](https://openairdocs.org/ad/97-17-04) (historical): Fan Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217C and 1 more. Effective Sep 30, 1997

All 365: https://openairdocs.org/aircraft/N574AA/ads.md

## Information bulletins (advisory) (12 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-08-43](https://openairdocs.org/saib/NM-08-43): Cabin Equipment/Furnishings - Seats. Issued Sep 3, 2008
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006
- [SAIB NE-16-22](https://openairdocs.org/saib/NE-16-22): Turbine Engine Combustion Section  JT8D Series Turbofan Engines. Issued Sep 2, 2016
- [SAIB NE-10-32](https://openairdocs.org/saib/NE-10-32): Turbine Engine Accessory Drive. Issued May 7, 2010
- [SAIB NE-05-75R1](https://openairdocs.org/saib/NE-05-75R1): . Issued Aug 4, 2005
- [SAIB NE-05-30](https://openairdocs.org/saib/NE-05-30): . Issued Feb 3, 2005
- [SAIB NE-02-22](https://openairdocs.org/saib/NE-02-22): . Issued Mar 26, 2002
- [SAIB NE-02-08R1](https://openairdocs.org/saib/NE-02-08R1): . Issued Feb 8, 2002
- [SAIB NE-01-42](https://openairdocs.org/saib/NE-01-42): . Issued Sep 25, 2001
- [SAIB ANE-97-03](https://openairdocs.org/saib/ANE-97-03): . Issued Apr 25, 1997
- [SAIB NE-05-75](https://openairdocs.org/saib/NE-05-75) (historical): . Issued Jul 22, 2005

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DEN06IA051](https://openairdocs.org/ntsb/DEN06IA051), Mar 21, 2006: McDonnell Douglas DC-9-82 (N574AA), Denver, CO, incident, minor damage. Probable cause: the captain's failure to follow existing company procedures for stabilized approach. **This report was modified on May 23, 2007.**

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20060321007369I](https://openairdocs.org/incident/20060321007369I), Mar 21, 2006: Doug DC982 (N574AA), Denver, CO, Minor damage. (-23) American airlines flight 2065 struck runway with the tail of the aircraft while landing on 35L. The point of impact on the runway was 575 ft beyond the…

## Service difficulty reports (60, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR AALA20150616018](https://openairdocs.org/sdr/AALA20150616018), Jun 16, 2015: FILTER. CLOGGED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH THE LT OIL STRAINER CLOGGING LIGHT ILLUMINATED. R & R NR 1 ENG FILTER & SERVICED OIL IA
- [SDR AALA20150503007](https://openairdocs.org/sdr/AALA20150503007), May 3, 2015: ELEMENT. DIRTY. LEFT OIL STRAINER, STRAINER CLOG LIGHT CAME ON DURING CRUISE & REMAINED ON. CHECKED LT ENGINE OIL STRAINER IAW AMM 72-00-02. REPLACED STRAINER TWICE & RAN ENG. 
- [SDR AALA20140804008](https://openairdocs.org/sdr/AALA20140804008), Aug 4, 2014: FILTER. CLOGGED. LEFT OIL STRAINER CLOGGING, LIGHT ILLUMINATED DURING CLIMB OUT. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND CARBON IN FILTER,
- [SDR AALA20140409010](https://openairdocs.org/sdr/AALA20140409010), Apr 7, 2014: RIB. CRACKED. RIGHT LE RIB CRACKED AT XIS 134. ACCOMPLISHED REPAIR TO CRACKED RIB IAW EA MD80-57-034316.
- [SDR AALA20140409009](https://openairdocs.org/sdr/AALA20140409009), Apr 7, 2014: RIB. CRACKED. LEFT NR 4 RIB CRACKED AT XIS 134. ACCOMPLISHED REPAIR IAW EA MD80-57-034316.
- [SDR AALA20130909001](https://openairdocs.org/sdr/AALA20130909001), Sep 9, 2013: BATTERY PACK. DISCHARGED. LT & RT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. R&R BATTERY PACK B5-105. OPERATIONS CHECKED NORMAL.
- [SDR AALA20120402001](https://openairdocs.org/sdr/AALA20120402001), Apr 1, 2012: BATTERY PACK. DISCHARGED. FLIGHT DECK AND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK BY FORWARD LAVATORY. OPS CHECK NORMAL.
- [SDR AALA20111026SAT01](https://openairdocs.org/sdr/AALA20111026SAT01), Oct 25, 2011: CHECK VALVE. CRACKED. SAT - CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED SAT LANDED WITHOUT INCIDENT. AIRCRAF
- [SDR AALA20110608TUL02](https://openairdocs.org/sdr/AALA20110608TUL02), Jun 8, 2011: CUSP WEB. DAMAGED. SEVERAL DAMAGED HOLES IN RIGHT HAND CUSP TEE BETWEEN STATIONS 636 TO 655. INSTALLED STRAP PER EA MD80-53-017180.
- [SDR AALA20110603TUL06](https://openairdocs.org/sdr/AALA20110603TUL06), Jun 3, 2011: CUSP WEB. CORRODED. CORROSION ON RIGHT CUSP SHEET STATIONS 218 TO 237. INSTALLED NEW CUSP SHEET FROM STATIONS 218 TO 237 RIGHT PER AARD 51-10-00-5.
- [SDR AALA20110603TUL04](https://openairdocs.org/sdr/AALA20110603TUL04), Jun 3, 2011: SEAT TRACK. CORRODED. FORWARD END OF SEAT TRACK NUMBER 6 STATIONS 214 TO 217 IS CORRODED. INSTALLED NUMBER 6 SEAT TRACK SPLICE STATIONS 214 TO 305 PER SRM 53-05-00 FIGURE 4F AND ATTA
- [SDR AALA20110602TUL08](https://openairdocs.org/sdr/AALA20110602TUL08), Jun 2, 2011: PAN. CRACKED. FORWARD SIDE OF RIGHT FRAME STATION 946, UPPER AFT WINDOW PAN TAB IS CRACKED. INSTALLED WINDOW PAN TAB AND STRAP PER EA MD80-53-017187 AND AARD 53-10-00-25.
- [SDR AALA20110602TUL07](https://openairdocs.org/sdr/AALA20110602TUL07), Jun 2, 2011: DOOR FRAME. CORRODED. AFT CARGO DOOR FRAME HAS CORROSION, STATIONS 1212 TO 1205, STRINGERS 28 TO 29 RIGHT. REMOVED AND REPLACED WEB PER AARD 51-10-00-5.
- [SDR AALA20110602TUL06](https://openairdocs.org/sdr/AALA20110602TUL06), Jun 2, 2011: DOOR FRAME. CORRODED. AFT CARGO DOOR FRAME HORIZONTAL DOUBLER SEAM HAS CORROSION AT STATION 1180. INSTALLED LOWER AFT DOOR STOP PAD FILLER AND DOOR BEAM DOUBLER PER AARD 53-10-00-3 A
- [SDR AALA20110602TUL03](https://openairdocs.org/sdr/AALA20110602TUL03), Jun 2, 2011: DOOR FRAME. CORRODED. AFT CARGO DOOR FRAME WEBBING HAS CORROSION STATIONS 1212 TO 1205 STRINGERS 28 TO 29 RIGHT. INSTALLED NEW WEB PER AARD 51-10-00-5.
- [SDR AALA20110602TUL02](https://openairdocs.org/sdr/AALA20110602TUL02), Jun 2, 2011: DOUBLER. CRACKED. AFT ACCS DOUBLER CRACKED 1485 CANT FRAME AT STAIR RETRACT ACTUATOR. INSTALLED NEW DOUBLER IN PLACE OF OLD CRACKED DOUBLER USING EXISTING HOLES IN FRAME PER AARD
- [SDR AALA20110601TUL15](https://openairdocs.org/sdr/AALA20110601TUL15), Jun 1, 2011: CUSP WEB. DAMAGED. DUE TO NUMEROUS REPAIRS AND DAMAGE, CUSP SHEET AT STATIONS 598 TO 712 NEEDS TO BE REMOVED. INSTALLED NEW CUSP SHEET, RIGHT HAND SIDE STATIONS 598 TO 712 PER AAR
- [SDR AALA20110601TUL12](https://openairdocs.org/sdr/AALA20110601TUL12), Jun 1, 2011: FRAME. CRACKED. AFT ACCESSORY 1510 CANT FRAME CRACKED ABOVE MAINTENANCE LIGHT SWITCH. INSTALLED DOUBLER PER EA MD80-53-017199.
- [SDR AALA20110531TUL01](https://openairdocs.org/sdr/AALA20110531TUL01), May 31, 2011: INTERCOSTAL. CRACKED. FORWARD RIGHT SIDE OF CENTER FUEL TANK AT TOP SIDE HAS CRACK IN INTERCOSTAL ANGLE AT ABOUT STATION 826 AND BELOW NUMBER 5 SEAT TRACK. INSTALLED REPAIR DOUBLERS 
- [SDR AALA20110529TUL09](https://openairdocs.org/sdr/AALA20110529TUL09), May 29, 2011: CUSP WEB. CRACKED. CRACKS TWO PLACES ON LEFT CUSP STATION 222. INSTALLED CUSP SHEET AND DOUBLER AT STATIONS 218 TO 317 LEFT SIDE PER AARD 51-10-00-5.
- [SDR AALA20110527TUL13](https://openairdocs.org/sdr/AALA20110527TUL13), May 27, 2011: CUSP WEB. CRACKED. TWO CRACKS ON CUSP STATION 222. INSTALLED CUSP SHEET AND DOUBLER PER AARD 51-10-00-05.
- [SDR AALA20110527TUL12](https://openairdocs.org/sdr/AALA20110527TUL12), May 27, 2011: SEAT TRACK. CORRODED. NUMBER 1 SEAT TRACK STATION 1174 CORROSION OUT OF LIMITS. REPLACED NUMBER 1 SEAT TRACK STATIONS 1174 TO 1309 PER AMM 53-40-01-2.
- [SDR AALA20110527TUL01](https://openairdocs.org/sdr/AALA20110527TUL01), May 27, 2011: MOUNT. CORRODED. FORWARD OUTBOARD G4 GALLEY MOUNT CORROSION OUT OF LIMITS. INSTALLED NEW G4 FORWARD OUTBOARD MOUNT IN NUMBER 1 SEAT TRACK PER SRM 51-30-5.
- [SDR AALA20110525TUL05](https://openairdocs.org/sdr/AALA20110525TUL05), May 25, 2011: SEAT TRACK. CORRODED. NUMBER 6 SEAT TRACK AT STATION 728 CORROSION OUT OF LIMITS. INSTALLED SEAT TRACK PLUG AT STATION 728 PER AARD 53-20-00-10.
- [SDR AALA20110525TUL04](https://openairdocs.org/sdr/AALA20110525TUL04), May 25, 2011: SEAT TRACK. CORRODED. NUMBER 6 SEAT TRACK AT STATION 665 CORROSION OUT OF LIMITS. INSTALLED SEAT TRACK REPAIR PLUG ON SEAT TRACK NUMBER 6 STATION 665 PER AARD 53-20-00-10.
- [SDR AALA20110525TUL03](https://openairdocs.org/sdr/AALA20110525TUL03), May 25, 2011: SEAT TRACK. CORRODED. NUMBER 6 SEAT TRACK AT STATION 625 CORROSION OUT OF LIMITS. INSTALLED SEAT TRACK REPAIR PLUG ON SEAT TRACK NUMBER 6 AT STATION 625 PER AARD 53-20-00-10.
- [SDR AALA20110524TUL05](https://openairdocs.org/sdr/AALA20110524TUL05), May 24, 2011: STRINGER. CRACKED. TOP OF RIGHT WING ANGLE/STRINGER CRACKED JUST OUTBOARD OF SECOND, FROM OUTBOARD TANK VENT PLATE. REPLACED ANGLE/STRINGER PER AARD 51-10-00-05.
- [SDR AALA20110505LGA01](https://openairdocs.org/sdr/AALA20110505LGA01), May 4, 2011: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT AT OVERHEAD PANEL BY FIRST CLASS LAVATORY INOPERATIVE. REPLACED B5-23 BATTERY PACK LIGHTS. OPS CHECK NORMAL.
- [SDR AALA20100726PHX01](https://openairdocs.org/sdr/AALA20100726PHX01), Jul 26, 2010: GENERATOR. FAILED. PHX - INFLIGHT LAS-DFW. CREW REPORTED RIGHT ENGINE GENERATOR HIGH TEMPERATURE INDICATION FAILURE. AUXILIARY POWER UNIT ALREADY ON PLACARD. EMERGENCY DECLARED DI
- [SDR AALA20100412ATL01](https://openairdocs.org/sdr/AALA20100412ATL01), Apr 11, 2010: BOTTLE. LOW PRESSURE. AFT GALLEY DOOR EVACUATION SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED AFT GALLEY DOOR EVACUATION SLIDE ASSEMBLY. OPS CHECKED NORMAL
- [SDR AALA2009062000006](https://openairdocs.org/sdr/AALA2009062000006), Jun 20, 2009: BATTERY PACK. DISCHARGED. LGA - EMERGENCY LIGHTS FOR ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROW 20.
- [SDR AALA2009062000005](https://openairdocs.org/sdr/AALA2009062000005), Jun 20, 2009: BATTERY PACK. DISCHARGED. LGA - AFT SECTION EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT SECTION EMERGENCY LIGHTS.
- [SDR AALA200802434A](https://openairdocs.org/sdr/AALA200802434A), Oct 30, 2008: LIGHT. INOPERATIVE. LGA - EMERGENCY LIGHT EXIT SIGN AT LEFT AFT STAIRWAY INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA200802665](https://openairdocs.org/sdr/AALA200802665), Oct 2, 2008: BATTERY PACK. DISCHARGED. TUL - EMERGENCY LIGHT BATTERY PACK AT AFT CABIN INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA200802664](https://openairdocs.org/sdr/AALA200802664), Oct 2, 2008: BATTERY PACK. DISCHARGED. TUL - EMERGENCY LIGHT BATTERY PACK AT FORWARD CABIN INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA200802663](https://openairdocs.org/sdr/AALA200802663), Oct 2, 2008: FITTING. CRACKED. TUL - CRACK FOUND ON LEFT GROUND SPOILER FITTING AT INBOARD FORWARD CORNER. CRACK LENGTH IS .5 INCH. REPLACED FITTING IN ACCORDANCE WITH AARD 57 20 00 15.
- [SDR AALA200802662](https://openairdocs.org/sdr/AALA200802662), Oct 2, 2008: HANDLE. FRAYED. TUL - TAIL CONE SLIDE LIFT HANDLE IS FRAYED AND NOT READABLE AT AFT ACCESSORY STATION 1500. REPLACED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA200802666](https://openairdocs.org/sdr/AALA200802666), Oct 1, 2008: BATTERY PACK. DISCHARGED. TUL - OVERHEAD EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA200801897](https://openairdocs.org/sdr/AALA200801897), Jul 17, 2008: TURBINE BLADES. FAILED. PVR - INFLIGHT T326/17 JUL. CREW REPORTED LOUD BANG FOLLOWED BY A YAW AND WIND SHEAR ALERT AS GEAR WAS RETRACTED. CAPTAIN REPORTED NR 1 ENG ROLLED BACK WHILE SH
- [SDR AALA20050499](https://openairdocs.org/sdr/AALA20050499), Jul 28, 2005: LIGHT. INOPERATIVE. TUL - EMERGENCY PATH LIGHTING AT SEATS 14DEF INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY PATH LIGHTING AT SEATS 14DEF. SYSTEM GROUND CHECKED NORMAL OPERA
- [SDR AALA20050115](https://openairdocs.org/sdr/AALA20050115), Feb 11, 2005: SMOKE. DETECTED. DFW INFLIGHT T2324/11 - STRONG ODOR OF OILY SMELL IN COCKPIT AT LIFT OFF. F/A REPORTED SMOKE IN CABIN. ALSO, VERY LIGHT HAZE IN COCKPIT. TURNED OFF RECIRCULATIO
- [SDR AALA20041250](https://openairdocs.org/sdr/AALA20041250), Dec 26, 2004: STRUT. LOW. YUL - EN ROUTE ORD GEAR WOULD NOT RETRACT. RETURNED YUL AND LANDED UNEVENTFULLY. ACCOMPLISHED SERVICING OF NOSE STRUT WITH NITROGEN ONLY PER MAINTENANCE MANUAL/
- [SDR AALA20041221](https://openairdocs.org/sdr/AALA20041221), Dec 13, 2004: SENSOR. FAULTY. ORD - AFTER TAKEOFF RED NOSE GEAR LIGHT ILLUMINATED AND REMAINED ON. FOLLOWED CHECKLIST AND RECYCLED GEAR. RED NOSE GEAR LIGHT AGAIN ILLUMINATED. NO VIBRATION W
- [SDR AALA20041144](https://openairdocs.org/sdr/AALA20041144), Nov 18, 2004: SENSOR. OUT OF ADJUST. BWI - INFLIGHT T1576/18 NOSE LANDING GEAR RED LIGHT ILLUMINATED AFTER TAKEOFF. CREW DID NOT EXPERIENCE EXCESS DRAG. CONTINUED TO BWI. ON APPROACH RECEIVED GEAR 
- [SDR AALA20041140](https://openairdocs.org/sdr/AALA20041140), Nov 17, 2004: LIGHT. INOPERATIVE. DFW - EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT ROW 17 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATIO
- [SDR AALA20040845](https://openairdocs.org/sdr/AALA20040845), Aug 15, 2004: COMPRESSOR. FAILED. DFW - INFLIGHT T1446/15 COMPRESSOR STALL AT 17500 ON CLIMBOUT AND ENGINE NUMBER 1 AT 10LR FOR REMAINDER OF FLIGHT. OIL LEAK REPORTED WITHIN CLEAR OF RUNWAY. REP
- [SDR AALA20040582](https://openairdocs.org/sdr/AALA20040582), May 20, 2004: CONNECTOR. LOOSE. DFW - EMERGENCY PATH LIGHT AT SEAT 14D INOPERATIVE. FOUND LOOSE CONNECTION UNDER SEAT 14D. REPAIRED LOOSE CONNECTION FOR EMERGENCY PATH LIGHT AT SEAT 14D. SYSTE
- [SDR AALA20030275](https://openairdocs.org/sdr/AALA20030275), Mar 4, 2003: SCHRADER VALVE. LEAKING. SEA - FLT 1760 - EN ROUTE SEA-DFW, AFTER TAKEOFF, LANDING NOSE GEAR DID NOT RETRACT. ALSO, HAD A STALL WARNING LIGHT ILLUMINATE. RETURNED AND LANDED SEA WITHOUT
- [SDR AALA20030213](https://openairdocs.org/sdr/AALA20030213), Feb 5, 2003: WEB. CORRODED. FOUND CORROSION ON CUSP WEB ABOVE MID-CARGO DOOR AT STATION 661. CUTOUT CORRODED SECTION OF CUSP AND INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4. (M)
- [SDR AALA20030215](https://openairdocs.org/sdr/AALA20030215), Feb 5, 2003: WEB. CORRODED. TUL - FOUND CORROSION ON CUSP WEB ABOVE MID CARGO DOOR CUTOUT STA 636-641. CUT OUT CORRODED CUSP AND INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4. (M)

All 60: https://openairdocs.org/aircraft/N574AA/reports.md

## STCs that may be installed (OpenAirDocs) (494, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Mcdonnell Douglas DC-9-82(MD-82))

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST01649AT-D](https://openairdocs.org/stc/ST01649AT-D): Installation of Collins DLM-900 Acars system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST01650AT-D](https://openairdocs.org/stc/ST01650AT-D): Installation of Collins VHF-900 Communication system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST01765AT-D](https://openairdocs.org/stc/ST01765AT-D): Installation of Collins VHF-900 Communications System in a provisioned aircraft. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST01766AT-D](https://openairdocs.org/stc/ST01766AT-D): Installation of Collins DLM-900 ACARS system with a Miltope printer, in a provisioned aircraft. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02463AT](https://openairdocs.org/stc/ST02463AT): Installation of an Intrusion/Penetration Resistance Flightdeck Door and Reinforced Flightdeck Door Surround. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02945AT-D](https://openairdocs.org/stc/ST02945AT-D): Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST04752NY](https://openairdocs.org/stc/ST04752NY): Replacement of Dual Analog Radio Altimeter Transceivers with Dual 5G Tolerant Collins Aerospace or Honeywell Digital Radio Altimeters Transceivers and Dual Shadin Digital-to-Analog Converters. S. LB Aircraft Engineering
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST09180AC](https://openairdocs.org/stc/ST09180AC): Installation of DeVore Wing Forward Position Lights. The Boeing Company
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA2040NM](https://openairdocs.org/stc/SA2040NM): Installation of closet and windscreen. Safran Cabin Inc
- [STC SA3469NM](https://openairdocs.org/stc/SA3469NM): Installation of Closet/Stowage Compartments/Coat Compartment/ Coatroom. Safran Cabin Inc
- [STC SA3494NM](https://openairdocs.org/stc/SA3494NM): Installation of auxiliary galley. Safran Cabin Inc. Lists DC-9 Series
- [STC SA3497NM](https://openairdocs.org/stc/SA3497NM): Installation of closet/stowage units. Safran Cabin Inc
- [STC SA4744NM](https://openairdocs.org/stc/SA4744NM): Installation of Extended Spacial Concept Interior III Retrofit Kit. Safran Cabin Inc
- [STC SA4770NM](https://openairdocs.org/stc/SA4770NM): Installation of a Modular Lavatory(Retrofit Installation). Safran Cabin Inc
- [STC SA4822NM](https://openairdocs.org/stc/SA4822NM): Installation of galleys, coatrooms, and a partition. Safran Cabin Inc
- [STC SA5786NM](https://openairdocs.org/stc/SA5786NM): Installation of an overhead life raft stowage compartment kit. Safran Cabin Inc
- [STC ST00127NY-D](https://openairdocs.org/stc/ST00127NY-D): Installation - Overhead Stowage. Safran Cabin Inc
- [STC ST00128LA](https://openairdocs.org/stc/ST00128LA): Installation of moveable class divider. Safran Cabin Inc
- [STC ST00227LA](https://openairdocs.org/stc/ST00227LA): Installation of Class Divider. Safran Cabin Inc
- [STC ST00347SE](https://openairdocs.org/stc/ST00347SE): Installation of interior kits. Safran Cabin Inc
- [STC ST00481SE](https://openairdocs.org/stc/ST00481SE): Installation of interior kits. Safran Cabin Inc
- [STC ST00649LA](https://openairdocs.org/stc/ST00649LA): Installation of Sidewall Panel Installation. Safran Cabin Inc
- [STC ST00686LA](https://openairdocs.org/stc/ST00686LA): Installation of galleys, closets, lavatories and partitions. Safran Cabin Inc
- [STC ST00687LA](https://openairdocs.org/stc/ST00687LA): Installation of Interior Kit. Safran Cabin Inc
- [STC ST00867SE](https://openairdocs.org/stc/ST00867SE): Modification to overhead stowage bins located in the passenger cabin in order to extend the bins inboard. Safran Cabin Inc
- [STC ST00868SE](https://openairdocs.org/stc/ST00868SE): Modification to overhead stowage bins located in the passenger cabin in order to extend the bins inboard. Safran Cabin Inc
- [STC ST01056LA](https://openairdocs.org/stc/ST01056LA): Installation of galleys, closet, stowage SIA, forward lavatory, bin, class divider (movable), sidewall and ceiling panels. Safran Cabin Inc
- [STC ST01147LA](https://openairdocs.org/stc/ST01147LA): Installation of a coat closet p/n 501086-1. Safran Cabin Inc
- [STC ST01336LA](https://openairdocs.org/stc/ST01336LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST01683LA](https://openairdocs.org/stc/ST01683LA): Installation of ceiling panel installation. Safran Cabin Inc
- [STC SA3165NM](https://openairdocs.org/stc/SA3165NM): Installation of Floor Proximity Emergency Escape Path Marking System. Bruce Aerospace Inc
- [STC ST00092LA](https://openairdocs.org/stc/ST00092LA): Instalation of interior fluorescent cabin lighting system. Bruce Aerospace Inc
- [STC ST00689LA](https://openairdocs.org/stc/ST00689LA): Installation of Bruce Industries Overhead Emergency Exit Marking and Locator System. Bruce Aerospace Inc
- [STC ST00069AT](https://openairdocs.org/stc/ST00069AT): Installation of a Fairchild Digital or Sundstrand Universal expanded parameters digital flight data recorder. Acron Aviation Inc
- [STC ST01518NY](https://openairdocs.org/stc/ST01518NY): Installation of Flight Systems Cabin Surveillance System (CSS). Acron Aviation Inc
- [STC ST03560AT](https://openairdocs.org/stc/ST03560AT): Installation of L3 Communications Aviation Recorders Micro Quick Access Recorder (uQAR) o. Acron Aviation Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST00694CH](https://openairdocs.org/stc/ST00694CH): Installation of single or dual Honeywell HT-9100 GNSS GPS Navigation Systems. Amphenol Cable and Interconnect Technologies Inc
- [STC ST00984CH](https://openairdocs.org/stc/ST00984CH): Installation of Rockwell Collins FPI-955 Electronic Horizontal Situation Indicators (EHSI). Amphenol Cable and Interconnect Technologies Inc
- [STC ST01017CH](https://openairdocs.org/stc/ST01017CH): Installation of an AlliedSignal CAS-81 TCAS II System with dual AlliedSignal Mode S Transponders. Amphenol Cable and Interconnect Technologies Inc
- [STC ST01019CH](https://openairdocs.org/stc/ST01019CH): Installation of a Rockwell Collins GNLS-910 GPS Flight Management System. Amphenol Cable and Interconnect Technologies Inc
- [STC ST01167CH](https://openairdocs.org/stc/ST01167CH): Installation of an AlliedSignal MK-VII Enhanced Ground Proximity Warning System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01404CH](https://openairdocs.org/stc/ST01404CH): Installation of Universal Avionics System Corporation Multi-Function Display. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01818CH](https://openairdocs.org/stc/ST01818CH): Installation of a Honeywell Enhanced Ground Proximity Warning System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01887CH](https://openairdocs.org/stc/ST01887CH): Installation of GPS antenna provisions. Amphenol Cable and Interconnect Technologies, Inc

All 494: https://openairdocs.org/aircraft/N574AA/stcs.md

## Related

- Other Mcdonnell Douglas DC-9-82(MD-82) aircraft: https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82/aircraft.md
- The Pratt & Whitney JT8D series engine: https://openairdocs.org/engine/pratt-whitney-jt8d-series.md

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