# N560AA: 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: 53090
- Year built: 1991
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 23, 1991
- Certificate issued: January 28, 2019
- Expires: January 31, 2029
- Mode S code: A726EB
- 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=560AA
- Page: https://openairdocs.org/aircraft/N560AA

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/N560AA/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 N560AA.

## 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 20031115031639I](https://openairdocs.org/incident/20031115031639I), Nov 15, 2003: Doug DC982 (N560AA), Newark, NJ, Minor damage. (-23) On November 15, 2003, aala flight 1328 at 3,000 feet over kteb and on approach to kewr runway 22R, the aircraft encountered large birds in its flight…

## Service difficulty reports (78, 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 AALA20141106007](https://openairdocs.org/sdr/AALA20141106007), Nov 6, 2014: GENERATOR. FAILED. LEFT GEN FAILED & APU UNABLE TO START. ACFT DIVERTED. SERVICED APU, STARTED OK. LT GEN WAS PLACARDED. REPLACED LT ENG GEN IAW AMM 24-20-01-401 & CONSTANT SPEED 
- [SDR AALA20131204004](https://openairdocs.org/sdr/AALA20131204004), Nov 27, 2013: RIB. CRACKED. LT HAND WING SLAT TRACK RIB IS CRACKED AT TOP AFT LUG. INSTALLED REPAIR DOUBLER & HAT BUSHING IAW EA MD80-57-032638.
- [SDR AALA20131204003](https://openairdocs.org/sdr/AALA20131204003), Nov 27, 2013: RIB. CRACKED. RT HAND WING SLAT TRACK RIB CRACKED AT TOP OF LUG. INSTALLED REPAIR DOUBLER & HAT BUSHING IAW EA MD80-57-032638.
- [SDR AALA20131126005](https://openairdocs.org/sdr/AALA20131126005), Nov 26, 2013: STOP FITTING. CRACKED. MID CARGO DOOR, FWD SIDE THIRD STOP PAD FITTING FROM THE TOP CRACKED. R & R STOP PAD FITTING IAW AARD 51-00-05-1.
- [SDR AALA20131126004](https://openairdocs.org/sdr/AALA20131126004), Nov 26, 2013: STOP FITTING. CRACKED. FWD CARGO DOOR, FWD SIDE UPPER STOP PAD FITTING CRACKED. R & R STOP PAD FITTING IAW AARD 51-00-05-1.
- [SDR AALA20131101004](https://openairdocs.org/sdr/AALA20131101004), Oct 31, 2013: BATTERY. DISCHARGED. AB5-3 EGRESS POWER SUPPLY FAILS DUAL FEEDBACK CHECK. REPLACED BATTERY. OPERATIONS CHECKED NORMAL.
- [SDR AALA20131101003](https://openairdocs.org/sdr/AALA20131101003), Oct 31, 2013: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS FROM ROWS 27 TO 31 FAILED. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.
- [SDR AALA20130419006](https://openairdocs.org/sdr/AALA20130419006), Apr 18, 2013: SKIN. CRACKED. CRACK IN FUSELAGE TAIL SECTION LEFT SIDE AT STATION 1477. INSTALLED DOUBLER PER AARD 53-30-00-4 AND SRM 53-01-00.
- [SDR AALA20130107023](https://openairdocs.org/sdr/AALA20130107023), Jan 7, 2013: ACTUATOR. INOPERATIVE. DFW - CREW REPORTED THE RIGHT MAIN GEAR DOOR INDICATED UNSAFE AND THE AMBER *GEAR DOOR OPEN* LIGHT REMAINED ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW 
- [SDR AALA20121005001](https://openairdocs.org/sdr/AALA20121005001), Oct 5, 2012: TAB. CRACKED. CRACKS AND DENTS IN OUTBOARD END OF TAB. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-0-10.
- [SDR AALA20120907034](https://openairdocs.org/sdr/AALA20120907034), Sep 7, 2012: GENERATOR. FAILED. DFW - CREW REPORTED LEFT GENERATOR FAILED IN-FLIGHT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE GENERATOR.
- [SDR AALA20120625013](https://openairdocs.org/sdr/AALA20120625013), Jun 25, 2012: BATTERY PACK. DISCHARGED. AFT GALLEY DOOR EXIT LIGHT INOPERATIVE. REPLACED MODULE NUMBER 1 BATTERY PACK AT AFT SERVICE DOOR. OPS CHECK NORMAL.
- [SDR AALA20120601014](https://openairdocs.org/sdr/AALA20120601014), Jun 1, 2012: FRAME. CRACKED. STATION 1510 CANT FRAME CRACKED ABOVE MAINTENANCE LIGHT SWITCH. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER EA MD80-53-024052.
- [SDR AALA20111114LGA01](https://openairdocs.org/sdr/AALA20111114LGA01), Nov 13, 2011: BATTERY PACK. MALFUNCTIONED. RIGHT NUMBER 1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RESET BATTERY PACK AT FORWARD OVERHEAD CEILING PANEL. OPS CHECK NORMAL.
- [SDR AALA20110603DFW07](https://openairdocs.org/sdr/AALA20110603DFW07), Jun 3, 2011: WINDSHIELD. CRACKED. DFW - CREW REPORTED CENTER WINDSHIELD CRACKED DURING CRUISE. PULLED K-25 CIRCUIT BREAKER. DESCENDED TO 10,000 FT AND REDUCED PRESSURIZATION DIFFERENTIAL. EMERGE
- [SDR AALA20110428TUL05](https://openairdocs.org/sdr/AALA20110428TUL05), Apr 28, 2011: TARGET. BROKEN. DEN - CREW REPORTED MAIN LANDING GEAR DOOR WARNING INDICATION. GEAR WAS MANUALLY RELEASED. EMERGENCY DECLARED FLIGHT RETURNED DEN LANDED WITHOUT INCIDENT. AIRCR
- [SDR AALA20101119TUL04](https://openairdocs.org/sdr/AALA20101119TUL04), Nov 19, 2010: BEAM. DAMAGED. DAMAGE TO I BEAM STATION 1160. REPLACED I BEAM.
- [SDR AALA20101118TUL17](https://openairdocs.org/sdr/AALA20101118TUL17), Nov 18, 2010: SHEAR TIE. DAMAGED. SHEAR TIE STATION 180 DAMAGED. INSTALLED SHEAR TIE.
- [SDR AALA20101118TUL03](https://openairdocs.org/sdr/AALA20101118TUL03), Nov 18, 2010: INTERCOSTAL. CRACKED. INTERCOSTAL IN CARGO CEILING STATIONS 1271 TO 1287 BUTTLINE-0 IS CRACKED AT FASTENER HOLES. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL PER AARD 5
- [SDR AALA20101117TUL14](https://openairdocs.org/sdr/AALA20101117TUL14), Nov 17, 2010: CARGO TRACK. CORRODED. AFT CARGO - CORROSION ON THE LEFT TIE DOWN TRACK UPPER AND LOWER SIDES BETWEEN BETWEEN STATIONS 1212 AND 1231. REMOVED AND REPLACED DAMAGED SPLICE PLATES PER SR
- [SDR AALA20101117TUL15](https://openairdocs.org/sdr/AALA20101117TUL15), Nov 17, 2010: SKIN. DENTED. DENT IN FUSELAGE AT STATION 329 BELOW LONGERON 27 RIGHT. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 12B.
- [SDR AALA20101117TUL13](https://openairdocs.org/sdr/AALA20101117TUL13), Nov 17, 2010: CARGO TRACK. CORRODED. LEFT AFT TIE DOWN TRACK HAS CORROSION SEVERAL PLACES ALONG THE LENGTH APPROXIMATE STATIONS 1220 TP 1322. REMOVED AND REPLACED DAMAGED TRACK PER SRM 51-30-05 AND
- [SDR AALA20101117TUL12](https://openairdocs.org/sdr/AALA20101117TUL12), Nov 17, 2010: SKIN. DENTED. FUSELAGE SKIN DENTED WITH A CREASE AT FRAME STATIONS 313 TO 332, BETWEEN LONGERON 27 TO 28 RIGHT. REMOVED DAMAGED SECTION OF SKIN, INSTALLED DOUBLER REPAIR PER 
- [SDR AALA20101117TUL02](https://openairdocs.org/sdr/AALA20101117TUL02), Nov 17, 2010: CUSP WEB. CRACKED. RIGHT CUSP CRACKED STATION 1300, LIGHTNING HOLE TO LIGHTNING HOLE. INSTALLED RIGHT CUSP AT STATIONS 1250 TO 1309 PER AARD 51-10-00-5 REPAIR 1.
- [SDR AALA20101117TUL05](https://openairdocs.org/sdr/AALA20101117TUL05), Nov 17, 2010: CUSP WEB. DAMAGED. TOOL DAMAGE ON CUSP UNDER NUMBER 1 SEAT TRACK STATION 824. INSTALLED NEW CUSP SHEET PER AARD 51-10-00-5 REPAIR 1.
- [SDR AALA20101116TUL13](https://openairdocs.org/sdr/AALA20101116TUL13), Nov 16, 2010: CUSP WEB. CORRODED. RIGHT CUSP SHEET STATIONS 598 TO 712 CORRODED. REMOVED AND REPLACED CUSP PER AARD 53-20-00-16.
- [SDR AALA20101116TUL12](https://openairdocs.org/sdr/AALA20101116TUL12), Nov 16, 2010: BEAM. CORRODED. AFT CARGO DOOR CUT OUT LOWER BEAM, CORROSION REMOVAL BEYOND LIMITS. INSTALLED DOUBLER PER AARD 53-10-00-3.
- [SDR AALA20101116TUL11](https://openairdocs.org/sdr/AALA20101116TUL11), Nov 16, 2010: FRAME. CRACKED. FRAME 1418 CRACKED ON AFT SIDE AT LONGERON 2 LEFT. STOP-DRILLED CRACK INSTALLED DOUBLER REPAIR PER SRM 53-10-00-15.
- [SDR AALA20101116TUL08](https://openairdocs.org/sdr/AALA20101116TUL08), Nov 16, 2010: HINGE BRACKET. CORRODED. AFT CARGO DOOR CUTOUT-FORWARD HINGE BRACKET CORRODED. REMOVED AFT CARGO DOOR- FORWARD HINGE BRACKET ON THE AIRCRAFT. INSTALLED NEW HINGE BRACKET PER SRM 51-30-0
- [SDR AALA20101116TUL07](https://openairdocs.org/sdr/AALA20101116TUL07), Nov 16, 2010: CUSP WEB. CORRODED. CORROSION AT LEFT AFT SERVICE DOOR-UNDER AFT GIRT BAR BRACKET. REMOVED CORRODED CUSP SECTION, INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20101115TUL12](https://openairdocs.org/sdr/AALA20101115TUL12), Nov 15, 2010: CUSP WEB. CORRODED. RIGHT CUSP CORRODED STATIONS 1174 TO 1250. REPLACED CUSP SHEET PER SRM 51-30-01 AND SRM 51-30-05.
- [SDR AALA20101115TUL06](https://openairdocs.org/sdr/AALA20101115TUL06), Nov 15, 2010: CUSP WEB. CORRODED. LEFT CUSP, STATIONS 712 TO 731 CORROSION OUT OF LIMITS. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20101115TUL05](https://openairdocs.org/sdr/AALA20101115TUL05), Nov 15, 2010: CUSP WEB. CORRODED. LEFT CUSP, STATIONS 1098 TO 1103 HAS CORROSION THAT IS OUT OF LIMITS. INSTALLED DOUBLER AND SPACER PER AARD 53-20-00-16.
- [SDR AALA20101115TUL01](https://openairdocs.org/sdr/AALA20101115TUL01), Nov 15, 2010: ATTACH FITTING. CRACKED. RIGHT WING GROUND SPOILER FITTING CRACK IN OUTBOARD SIDE OF CASTING TRAILING EDGE OF WING. INSTALLED NEW SPOILER ATTACH FITTING PER AARD 51-10-00-5.
- [SDR AALA20101114TUL11](https://openairdocs.org/sdr/AALA20101114TUL11), Nov 14, 2010: BEAM. CORRODED. AFT CARGO - DOOR FRAME UPPER BOX TOP SIDE HAS CORROSION AT THE UPPER FORWARD END JUST FORWARD OF THE FORWARD HINGE MOUNT APPROXIMATELY STATION 1160. REMOVED AND
- [SDR AALA20101114TUL10](https://openairdocs.org/sdr/AALA20101114TUL10), Nov 14, 2010: CUSP WEB. CORRODED. CORROSION UNDER FORWARD GIRT BAR BRACKET AT STATION 1140. INSTALLED .040" 6AL-4V TITANIUM REPAIR DOUBLER STATION 1140 PER AARD 53-20-00-16.
- [SDR AALA20101114TUL09](https://openairdocs.org/sdr/AALA20101114TUL09), Nov 14, 2010: CUSP WEB. CORRODED. CORROSION UNDER AFT GIRT BAR BRACKET AT STATION 1166. INSTALLED .040" 6AL-4V TITANIUM REPAIR DOUBLER STATION 1166 PER AARD 53-20-00-16.
- [SDR AALA20101114TUL01](https://openairdocs.org/sdr/AALA20101114TUL01), Nov 14, 2010: CUSP WEB. CORRODED. LEFT CUSP STATIONS 1098 TO 1103 HAS CORROSION THAT IS OUT OF LIMITS. INSTALLED DOUBLER AND SPACER PER AARD 53-20-00-16.
- [SDR AALA20101113TUL01](https://openairdocs.org/sdr/AALA20101113TUL01), Nov 13, 2010: CUSP WEB. CORRODED. LEFT CUSP STATIONS 636 TO 655 HAS CORROSION THAT IS OUT OF LIMITS. CUT OUT DAMAGE PER AARD 53-20-00-16 AND INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20101112TUL10](https://openairdocs.org/sdr/AALA20101112TUL10), Nov 12, 2010: FITTING. CORRODED. NUMBER 1 GALLEY TIE DOWN FITTING CORRODED. REPLACED TIE DOWN FITTING PER 51-30-05.
- [SDR AALA20101111TUL17](https://openairdocs.org/sdr/AALA20101111TUL17), Nov 11, 2010: STOP FITTING. CRACKED. AFT VAULT DOOR JAMB, DOOR STOP CRACKED, LEFT SIDE MIDDLE STOP. REMOVED CRACKED FITTING, DRILLED UP NEW FITTING AND INSTALLED PER AARD 51-10-00-3.
- [SDR AALA20101111TUL13](https://openairdocs.org/sdr/AALA20101111TUL13), Nov 11, 2010: MEMBRANE. PUNCTURED. SUBFLOOR HAS PUNCTURE AT STATION 198 FORWARD OF NUMBER 3 SEAT TRACK. REMOVED DAMAGE INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.
- [SDR AALA20101110TUL11](https://openairdocs.org/sdr/AALA20101110TUL11), Nov 10, 2010: PAN. DAMAGED. STATION 946 LOWER FORWARD WINDOW PAN CRACKED LEFT. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20101110TUL15](https://openairdocs.org/sdr/AALA20101110TUL15), Nov 10, 2010: TIE DOWN. CORRODED. CORROSION ON NUMBER 2 GALLEY TIE DOWN FITTING AT STATION 218 INBOARD OF NUMBER 4 SEAT TRACK. (MKD) INSTALLED NEW SERVICEABLE G-2 GALLEY TIE DOWN SUPPORT FITTING
- [SDR AALA20101110TUL14](https://openairdocs.org/sdr/AALA20101110TUL14), Nov 10, 2010: TIE DOWN. CORRODED. CORROSION ON NUMBER 2 GALLEY TIE DOWN FITTING AT STATION 208 INBOARD OF NUMBER 4 SEAT TRACK. (MKD) INSTALLED NEW SERVICEABLE G-2 GALLEY TIE DOWN SUPPORT FITTING
- [SDR AALA20101110TUL10](https://openairdocs.org/sdr/AALA20101110TUL10), Nov 10, 2010: PAN. DAMAGED. STATION 946 UPPER FORWARD WINDOW PAN CRACKED LEFT. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20101110TUL09](https://openairdocs.org/sdr/AALA20101110TUL09), Nov 10, 2010: PAN. DAMAGED. STATION 1060 LOWER FORWARD WINDOW PAN CRACKED LEFT. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20101110TUL08](https://openairdocs.org/sdr/AALA20101110TUL08), Nov 10, 2010: PAN. DAMAGED. STATION 1098 UPPER AFT WINDOW PAN CRACKED LEFT. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20090624TUL18](https://openairdocs.org/sdr/AALA20090624TUL18), Jun 15, 2009: CUSP WEB. CORRODED. RIGHT CUSP HAS CORROSION STATIONS 200-205. DAMAGED MATERIAL REMOVED, REPAIR DOUBLER INSTALLED PER EA MD-80-53-006501 AND AARD 53-20-00-14.
- [SDR AALA20090624TUL08](https://openairdocs.org/sdr/AALA20090624TUL08), Jun 13, 2009: FRAME. CRACKED. THE 1418 FRAME CRACKED LONGERON 2 LEFT AND 2 RIGHT. INSTALLED DOUBLER PER EA MD80-53-006493.

All 78: https://openairdocs.org/aircraft/N560AA/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/N560AA/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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