# N586AA: 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: 53249
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 27, 1991
- Certificate issued: November 18, 2021
- Expires: November 30, 2028
- Mode S code: A78C33
- Registered owner: [Aerothrust Holdings Leasing LLC](https://openairdocs.org/faa-owner/AEROTHRUST%20HOLDINGS%20LEASING%20LLC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: LLC
- Owner's area on the map: 25.8166° N, 80.3105° W: Placed by OpenAirDocs at the center of ZIP code 33166, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=586AA
- Page: https://openairdocs.org/aircraft/N586AA

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/N586AA/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

None matched to N586AA.

## FAA accident and incident reports

None matched to N586AA.

## Reports on N586AA not matched to an aircraft (1)

They name N586AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19800413049489I](https://openairdocs.org/incident/19800413049489I), Apr 13, 1980: Boeing 707/ (N586AA). #4 Engine would not accelerate above 64 percent. Flight aborted.

## Service difficulty reports (87, 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 AALA20150607008](https://openairdocs.org/sdr/AALA20150607008), Jun 7, 2015: TARGET. FAULTY. EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB OUT, GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLING GEAR 
- [SDR AALA20150320017](https://openairdocs.org/sdr/AALA20150320017), Mar 20, 2015: LINE. CRACKED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. RT ENG OIL QTY LOW INDICATION. FOUND CRACKED OIL LINE ON OIL PRESS TRANSMITTER, REPL
- [SDR AALA20150223011](https://openairdocs.org/sdr/AALA20150223011), Feb 19, 2015: GCU. FAULTY. AIR INTERRUPT, NO EMER DECLARED & LANDING UNEVENTFUL. ACFT WAS NOT OVERWEIGHT. RT ENG RATIO WENT TO ZERO ON ROTATION. THEN AT 300 - 400 FEET ALTITUDE, BOTH DIGI
- [SDR AALA20150219013](https://openairdocs.org/sdr/AALA20150219013), Feb 19, 2015: GENERATOR. FAULTY. AIR INTERRUPT, NO EMER DECLARED & LANDING UNEVENTFUL. ACFT WAS NOT OVERWEIGHT. RT ENG PRESS RATIO WENT TO ZERO ON ROTATION. THEN AT 300 - 400 FEET ALTITUDE, BOT
- [SDR AALA20140619008](https://openairdocs.org/sdr/AALA20140619008), Jun 19, 2014: STRUCTURE. CRACKED. LEFT HAND STRUT DOOR AFT HINGE CUT OUT CRACKED. INSTALLED DOUBLER IAW SRM 53-05-00 FIGURE 62.
- [SDR AALA20140619007](https://openairdocs.org/sdr/AALA20140619007), Jun 19, 2014: BRACKET. CRACKED. RIGHT WW GREEN SHELF BRACKET AT THE UPPER END OF THE GEAR DOOR ACTUATOR IS CRACKED AT THE AFT INBD SIDE. INSTALLED DOUBLER IAW AARD 53-10-00-38.
- [SDR AALA20140619006](https://openairdocs.org/sdr/AALA20140619006), Jun 19, 2014: STRUCTURE. CRACKED. RIGHT HAND STRUT DOOR AFT HINGE CUT OUT CRACKED. INSTALLED DOUBLER IAW SRM 53-05-00 FIGURE 62.
- [SDR AALA20140617003](https://openairdocs.org/sdr/AALA20140617003), Jun 17, 2014: STOP FITTING. CRACKED. MID CARGO DOOR FWD SIDE STOP FITTING CRACKED. REPLACED STOP FITTING IAW AARD 51-00-05-1.
- [SDR AALA20140607003](https://openairdocs.org/sdr/AALA20140607003), Jun 7, 2014: CONNECTOR. LEAKING. CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND RT PACK LE
- [SDR AALA20140527013](https://openairdocs.org/sdr/AALA20140527013), May 27, 2014: RIB. CRACKED. RIGHT NR 4 LE SLAT RIB INBD CASTING CRACKED. REPLACED CASTING IAW AARD 51-00-05-1.
- [SDR AALA20140527035](https://openairdocs.org/sdr/AALA20140527035), May 24, 2014: FORMER. CRACKED. LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-03 & EA MD80-57-034944.
- [SDR AALA20140111007](https://openairdocs.org/sdr/AALA20140111007), Jan 11, 2014: CONTROLLER. INOPERATIVE. IAD INFLIGHT DFW-DCA. CREW REPORTED ANTI SKID FAULT INDICATION DURING APPROACH. FLIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPL
- [SDR AALA20121205004](https://openairdocs.org/sdr/AALA20121205004), Dec 5, 2012: BATTERY PACK. DISCHARGED. TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED RIGHT AFT LAVATORY BATTERY PACK. OPS CHECK NORMAL.
- [SDR AALA20110812TUL02](https://openairdocs.org/sdr/AALA20110812TUL02), Aug 12, 2011: SKIN. DENTED. DENT ON LEFT SIDE OF FUSELAGE AT THE TOP OF AA OF 586AA. INSTALLED FILLER AND DOUBLER AT STATION 1431 LONGERON 8 LEFT PER SRM 53-04-00 FIGURE 18 SHEET 1 AND 2.
- [SDR AALA20110808TUL01](https://openairdocs.org/sdr/AALA20110808TUL01), Aug 8, 2011: SKIN. DENTED. TWO DENTS APPROXIMATELY 2 INCHES APART IN FUSELAGE 40 AND 58 INCHES FORWARD OF CENTER CARGO DOOR CUTOUT AND 10 INCHES BELOW RIGHT TURNOFF LIGHT STATION 579 AT L
- [SDR AALA20110805TUL02](https://openairdocs.org/sdr/AALA20110805TUL02), Aug 5, 2011: CUSP WEB. DAMAGED. ELONGATED HOLES IN CUSP, UNDER NUMBER 6 SEAT TRACK STATIONS 221 TO 235. INSTALLED CUSP SHEET ON RIGHT SIDE AT STATIONS 218 TO 237 PER AARD 51-10-00-5.
- [SDR AALA20110805TUL01](https://openairdocs.org/sdr/AALA20110805TUL01), Aug 5, 2011: SEAT TRACK. CORRODED. NUMBER 6 SEAT TRACK CORRODED BEYOND LIMITS AT STATIONS 215 TO 218. INSTALLED NEW SEAT TRACK NUMBER 6 STATIONS 215 TO 265 AND SPLICE AT STATION 265 PER SRM 53-05
- [SDR AALA20110804TUL07](https://openairdocs.org/sdr/AALA20110804TUL07), Aug 4, 2011: STRUCTURE. CORRODED. CORROSION AROUND AFT LAV SERVICE PANEL CUTOUT IN CARGO, STATIONS 1316 TO 1322, LONGERONS 21 TO 22. INSTALLED REPAIR DOUBLER PER EA MD80 53-018439.
- [SDR AALA20110804TUL05](https://openairdocs.org/sdr/AALA20110804TUL05), Aug 4, 2011: MEMBRANE. CORRODED. CORROSION ON SUBFLOOR UNDER G1 GALLEY DRAIN PAN. INSTALLED G1 GALLEY SUB-FLOOR DOUBLER AARD 53-20-00-16.
- [SDR AALA20110804TUL04](https://openairdocs.org/sdr/AALA20110804TUL04), Aug 4, 2011: MEMBRANE. CRACKED. CABIN FORWARD SUBFLOOR CRACKED AT FASTENER STATIONS 179, 26 INCHES RIGHT OF CENTER LINE. INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20110804TUL03](https://openairdocs.org/sdr/AALA20110804TUL03), Aug 4, 2011: TIE DOWN. CORRODED. CORROSION ON TOP OF RIGHT TIE-DOWN TRACK, STATIONS 1007 TO 1155. INSTALLED NEW TIE-DOWN TRACK PER AARD 51-10-00-5 AND SRM 51-30-01.
- [SDR AALA20110804TUL01](https://openairdocs.org/sdr/AALA20110804TUL01), Aug 4, 2011: ANGLE. CORRODED. AFT CARGO CORROSION ON LOWER FORWARD ANGLE IN DOOR CUTOUT FORWARD OF STATION 1155 FRAME. INSTALLED NEW LOWER ANGLE AT STATION 1155 PER SRM 51-30-05.
- [SDR AALA20110808TUL03](https://openairdocs.org/sdr/AALA20110808TUL03), Aug 2, 2011: SKIN. GOUGED. GOUGE IN SKIN AT STATION 1406 ABOVE STRINGER 5 RIGHT. INSTALLED DOUBLER AND FILLER PER SRM 53-01-00 FIGURE 2 SHEET 3.
- [SDR AALA20110802TUL01](https://openairdocs.org/sdr/AALA20110802TUL01), Aug 2, 2011: CUSP WEB. DAMAGED. ELONGATED HOLES IN CUSP UNDER NUMBER 6 SEAT TRACK, STATIONS 221 TO 235. REMOVED DAMAGED CUSP, STATIONS 218 TO 237, AND INSTALLED SERVICEABLE CUSP PER AARD 51-10
- [SDR AALA20110801TUL06](https://openairdocs.org/sdr/AALA20110801TUL06), Aug 1, 2011: MEMBRANE. CORRODED. CORROSION ON SUBFLOOR UNDER FIBERGLASS HAT CHANNEL INBOARD OF FORWARD SERVICE DOOR. INSTALLED DIAPHRAM REPAIR DOUBLER AT STATIONS 160 TO 200 RIGHT BUTTLINES 36 
- [SDR AALA20110731TUL08](https://openairdocs.org/sdr/AALA20110731TUL08), Jul 31, 2011: MOUNT. CORRODED. CORROSION ON G1 GALLEY FORWARD MOUNT, 12 INCHES INBOARD OF FORWARD SERVICE DOOR AT STATION 160. INSTALLED NEW GALLEY MOUNT PER AARD 51-10-00-5.
- [SDR AALA20110731TUL07](https://openairdocs.org/sdr/AALA20110731TUL07), Jul 31, 2011: MOUNT. CORRODED. CORROSION ON G1 GALLEY FORWARD MOUNT, 6 INCHES INBOARD OF FORWARD SERVICE DOOR AT STATION 160. INSTALLED NEW G1 GALLEY MOUNT PER AARD 51-10-00-5.
- [SDR AALA20110731TUL02](https://openairdocs.org/sdr/AALA20110731TUL02), Jul 31, 2011: MOUNT. CORRODED. CORROSION ON G2 AFT INBOARD MOUNT. INSTALLED NEW G2 AFT INBOARD MOUNT PER AARD 51-10-00-5.
- [SDR AALA20110731TUL01](https://openairdocs.org/sdr/AALA20110731TUL01), Jul 31, 2011: DIAPHRAGM. CORRODED. CORROSION UNDER AFT G-2 MOUNT INBOARD. INSTALLED NEW DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20110730TUL07](https://openairdocs.org/sdr/AALA20110730TUL07), Jul 30, 2011: CUSP WEB. CORRODED. CORROSION ON BOTTOM OF SUBFLOOR BELOW NUMBER 1 SEAT TRACK STATION 1175. INSTALLED NEW CUSP MEMBRANE PER DRAWING SG09530019.
- [SDR AALA20110730TUL06](https://openairdocs.org/sdr/AALA20110730TUL06), Jul 30, 2011: SKIN. DAMAGED. GOUGED DENT IN SKIN STATION 1380 BETWEEN STRINGERS 8 AND 9 RIGHT. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-01-00 FIGURE 2 SHEET 3.
- [SDR AALA20110730TUL05](https://openairdocs.org/sdr/AALA20110730TUL05), Jul 30, 2011: SKIN. GOUGED. AFT FUSELAGE IS GOUGED STATION 1320 JUST BELOW LONGERON 24 RIGHT. INSTALLED REPAIR DOUBLERS AND FILLER PER SRM 53-04-02 AND BOEING DOCUMENT SG09530001 ZONE 104 
- [SDR AALA20110730TUL01](https://openairdocs.org/sdr/AALA20110730TUL01), Jul 30, 2011: CUSP WEB. CORRODED. CORROSION ON SUBFLOOR WEB STATION 1142 INBOARD OF AFT SERVICE DOOR. INSTALLED .040" 6A1-4V TITANIUM REPAIR DOUBLER LEFT SUBFLOOR WEB STATION 1142 PER AARD 53-20
- [SDR AALA20110731TUL05](https://openairdocs.org/sdr/AALA20110731TUL05), Jul 29, 2011: MEMBRANE. CRACKED. SUBFLOOR CRACKED AT FASTENER STATION 179, 26 INCHES RIGHT OF CENTER LINE. INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20110729TUL08](https://openairdocs.org/sdr/AALA20110729TUL08), Jul 29, 2011: CUSP WEB. CRACKED. CORROSION ON SUBFLOOR WEB STATION 1165 INBOARD OF AFT SERVICE DOOR. INSTALLED LEFT CUSP DOUBLER REPAIR AT STATION 1165 PER AARD 53-20-00-16.
- [SDR AALA20110729TUL06](https://openairdocs.org/sdr/AALA20110729TUL06), Jul 29, 2011: CUSP WEB. CORRODED. HOLE ON LEFT CUSP AT STATION 551. INSTALLED DOUBLER ON LEFT CUSP AT STATION 551 PER AARD 53-20-00-16.
- [SDR AALA20110729TUL02](https://openairdocs.org/sdr/AALA20110729TUL02), Jul 29, 2011: DOOR. DENTED. FORWARD CARGO DOOR HAS DENT JUST BELOW NUMBER 3 BEAM AT FORWARD END OF DOOR. INSTALLED DOUBLER ON CARGO DOOR PER SRM 52-02-00 PG 6 FIGURE 1 SHEET 1.
- [SDR AALA20110731TUL04](https://openairdocs.org/sdr/AALA20110731TUL04), Jul 27, 2011: CUSP WEB. CRACKED. CRACK ON LEFT CUSP AT STATION 1244. INSTALLED REPAIR DOUBLER ON LEFT CUSP AT STATION 1244 PER AARD 53-20-00-16.
- [SDR AALA20110727TUL07](https://openairdocs.org/sdr/AALA20110727TUL07), Jul 27, 2011: CUSP WEB. DAMAGED. RIGHT CUSP DAMAGED AT STATIONS 550 TO 551. INSTALLED DOUBLER PER AARD 53-10-00-25.
- [SDR AALA20110727TUL05](https://openairdocs.org/sdr/AALA20110727TUL05), Jul 27, 2011: PAN. CRACKED. WINDOW PAN CRACKED STATION 1174 RIGHT FORWARD LOWER. INSTALLED REPAIR ANGLE AS PER AARD 53-10-00-25.
- [SDR AALA20110727TUL04](https://openairdocs.org/sdr/AALA20110727TUL04), Jul 27, 2011: PAN. CRACKED. WINDOW PAN CRACKED STATION 1041 RIGHT AFT UPPER. INSTALLED DOUBLER PER AARD 53-10-00-25.
- [SDR AALA20110727TUL03](https://openairdocs.org/sdr/AALA20110727TUL03), Jul 27, 2011: PAN. CRACKED. WINDOW PAN CRACKED STATION 1060 RIGHT AFT UPPER. INSTALLED DOUBLER PER AARD 53-10-00-25.
- [SDR AALA20110726TUL05](https://openairdocs.org/sdr/AALA20110726TUL05), Jul 26, 2011: PAN. CRACKED. WINDOW PAN CRACKED STATION 1174 RIGHT AFT UPPER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20110726TUL04](https://openairdocs.org/sdr/AALA20110726TUL04), Jul 26, 2011: PAN. CRACKED. WINDOW PAN CRACKED STATION 1174 RIGHT FORWARD UPPER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20110726TUL03](https://openairdocs.org/sdr/AALA20110726TUL03), Jul 26, 2011: PAN. CRACKED. WINDOW PAN CRACKED BETWEEN STATIONS 769 AND 788 LEFT SIDE, TOP FORWARD CORNER. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.
- [SDR AALA20110726TUL02](https://openairdocs.org/sdr/AALA20110726TUL02), Jul 26, 2011: PAN. CRACKED. WINDOW PAN CRACKED BETWEEN STATIONS 769 AND 788 LEFT SIDE, TOP FORWARD CORNER. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.
- [SDR AALA20110725TUL08](https://openairdocs.org/sdr/AALA20110725TUL08), Jul 25, 2011: PAN. CRACKED. WINDOW PAN CRACKED BETWEEN STATIONS 1041 AND 1060 LEFT SIDE, TOP AFT CORNER, AROUND FASTENER. INSTALLED DOUBLER PER AARD 53-10-00-25.
- [SDR AALA20110725TUL07](https://openairdocs.org/sdr/AALA20110725TUL07), Jul 25, 2011: PAN. CRACKED. WINDOW PAN CRACKED BETWEEN STATIONS 1022 AND 1041 LEFT SIDE, LOWER FORWARD CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20110725TUL06](https://openairdocs.org/sdr/AALA20110725TUL06), Jul 25, 2011: PAN. CRACKED. WINDOW PAN CRACKED BETWEEN STATIONS 946 AND 965 LEFT SIDE, LOWER FORWARD CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.
- [SDR AALA20110725TUL05](https://openairdocs.org/sdr/AALA20110725TUL05), Jul 25, 2011: PAN. CRACKED. WINDOW PAN CRACKED BETWEEN STATIONS 1003 AND 1022 LEFT SIDE, TOP AFT CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

All 87: https://openairdocs.org/aircraft/N586AA/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/N586AA/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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