# N883GA: 1988 Douglas DC-9-83

- Status: Valid registration
- Airframe: [Douglas DC-9-83](https://openairdocs.org/model/douglas-dc-9-83) (registry code 3020305, 85 seats)
- Engine: [Pratt & Whitney JT8D-219](https://openairdocs.org/engine/pratt-whitney-jt8d-219) (registry code 51694)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company), [TCDS E9NE](https://openairdocs.org/tcds/E9NE) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 49710
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 22, 2006
- Certificate issued: September 8, 2025
- Expires: September 30, 2032
- Mode S code: AC2991
- Registered owner: [Falcon Commercial Aviation LLC](https://openairdocs.org/faa-owner/FALCON%20COMMERCIAL%20AVIATION%20LLC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: LLC
- Owner's area on the map: 25.6544° N, 80.4122° W: Placed by OpenAirDocs at the center of ZIP code 33186, 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=883GA
- Page: https://openairdocs.org/aircraft/N883GA

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.

## ADs that may apply (OpenAirDocs): 287 in force

### Matched by airframe (Douglas DC-9-83)

- [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 2016-07-08](https://openairdocs.org/ad/2016-07-08): Fuel · Boeing DC-9-83 (MD-83). Effective Apr 20, 2016
- [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 2007-17-18](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 2006-01-02](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 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
- [AD 2004-13-23](https://openairdocs.org/ad/2004-13-23): Seat track locking pins · Boeing DC-9-82 (MD-82), DC-9-83 (MD-83) and MD-88. Effective Aug 13, 2004
- [AD 2004-11-07](https://openairdocs.org/ad/2004-11-07): Structural Integrity · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Jul 9, 2004

### Matched by engine (Pratt & Whitney JT8D-219)

- [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 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 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 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 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 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 95-02-16](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 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 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 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 70-26-05](https://openairdocs.org/ad/70-26-05): First Stage Compressor Rotor Blades · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Dec 29, 1970
- [AD 70-25-08](https://openairdocs.org/ad/70-25-08): Seventh Stage Compressor Rotor Disc · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Dec 15, 1970
- [AD 70-11-03](https://openairdocs.org/ad/70-11-03): Sixth Stage Compressor Discs · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Jun 12, 1970
- [AD 70-02-02](https://openairdocs.org/ad/70-02-02): Sixth Stage Compressor Rotor Disc · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Apr 15, 1970

### 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 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 325: https://openairdocs.org/aircraft/N883GA/ads.md

## Information bulletins (advisory) (6 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

## NTSB investigations

None matched to N883GA.

## FAA accident and incident reports (2)

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 20170330005159I](https://openairdocs.org/incident/20170330005159I), Mar 30, 2017: Douglas DC-9-83 (N883GA), Mesa, AZ, No damage. During climb the LH engine was not Producing full power. Between low Teens up to 10000 our climb rate was About 500FPM. Initial engine numbers On climb LH 1.98…
- [Incident 20071210827779I](https://openairdocs.org/incident/20071210827779I), Dec 10, 2007: Doug DC983 (N883GA), Idaho Falls, ID, No damage. (-23) On Monday December 10, 2007, at 1937Z (1237 mountain time) an allegiant airlines (designator WX0A) Douglas DC-9-83, N883GA, s/n 49710 reported that while…

## Service difficulty reports (69, 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 WX0A201710063291](https://openairdocs.org/sdr/WX0A201710063291), Oct 5, 2017: UNKNOWN. ODOR. ACRID FUMES IN CABIN DURING CLIMB.
- [SDR WX0A2017082300286](https://openairdocs.org/sdr/WX0A2017082300286), Aug 19, 2017: BALLAST. SMOKE. OVERHEAD LIGHT FLICKERED & SMOKE CAME FROM IT. R & R THE BALLAST AND ASSOCIATED HARNESS FOR UPPER SIDEWALL LIGHTS.
- [SDR JR2R20170630142](https://openairdocs.org/sdr/JR2R20170630142), Jun 30, 2017: RIB. CRACKED. RIGHT WING LEADING EDGE RIB HAS A CRACK INBOARD OF SLAT TRACK NR 9 BETWEEN XFS 151.125 - 145. REMOVED AND REPLACED THE RIB IAW SRM 57-06B, FIG 18.
- [SDR JR2R20170606333](https://openairdocs.org/sdr/JR2R20170606333), Jun 6, 2017: SKIN. CORRODED. LOWER FUSELAGE SKIN AND INTERNAL DOUBLER CORRODED. REPLACED THE SKIN AND INTERNAL DOUBLER IAW SRM 53-04, FIG 12C.
- [SDR JR2R20170604196](https://openairdocs.org/sdr/JR2R20170604196), Jun 4, 2017: GUSSET. CRACKED. RIGHT ENGINE INLET INTERNAL LOWER INBOARD GUSSET IS CRACKED. REMOVED AND REPLACED RIGHT ENGINE INLET INTERNAL LOWER INBOARD GUSSET IAW SRM 51-30-5, 51-30-2, AND
- [SDR JR2R201706033671](https://openairdocs.org/sdr/JR2R201706033671), Jun 3, 2017: FAIRING. CRACKED. LEFT OUTBOARD ELEVATOR TAB FAIRING HAS A CRACK AT FASTNER HOLE. WELDED PERMANENT REPAIR TO THE LT OTBD ELEVATOR TAB FAIRING IAW SPEC 9908.
- [SDR JR2R20170530198](https://openairdocs.org/sdr/JR2R20170530198), May 30, 2017: GUSSET. CRACKED. RIGHT NOSE COWL INTERNAL UPPER GUSSET CRACKED. REMOVED AND REPLACED THE GUSSETT IAW CMM 71-10-1H.
- [SDR JR2R20170530173](https://openairdocs.org/sdr/JR2R20170530173), May 30, 2017: INTERCOSTAL. CORRODED. INTERCOSTAL CORRODED ON INBD SIDE, AROUND FASTNER. REPAIRED THE INTERCOSTAL IAW SRM 53-01, FIG 2.
- [SDR JR2R20170530371](https://openairdocs.org/sdr/JR2R20170530371), May 30, 2017: BRACKET. CRACKED. CENTER FUEL TANK FUEL LINE BRACKET CRACKED. FABRICATED REPLACEMENT CENTER FUEL TANK FUEL LINE BRACKET IAW SRM 51-10-4.
- [SDR JR2R20170528056](https://openairdocs.org/sdr/JR2R20170528056), May 28, 2017: DOUBLER. CRACKED. LEFT WING FIXED LEADING EDGE RIB CONTROL CABLE FAIRLEAD DOUBLER IS CRACKED AT XOS 206. REPAIRED LT WING FIXED LE RIB CONTROL CABLE FAIRLEAD DOUBLER IAW SRM 57-0
- [SDR JR2R20170528251](https://openairdocs.org/sdr/JR2R20170528251), May 28, 2017: LONGERON. CRACKED. LONGERON 2L IS CRACKED AT BS 547. REPAIRED THE LONGERON IAW SRM 53-02, FIG 18, SHT 1.
- [SDR JR2R20170526361](https://openairdocs.org/sdr/JR2R20170526361), May 26, 2017: SKIN. CRACKED. VERTICAL STAB PANEL AT VSS ZFS-6.562, LT SIDE HAS A CRACK FROM EDGE OF PANEL EXTENDING 5/8 INCH PAST FASTNER. FIRST HOLE BELOW UPPER AFT CORNER OF INLET PANEL. 
- [SDR JR2R20170526055](https://openairdocs.org/sdr/JR2R20170526055), May 26, 2017: RIB. CRACKED. LEFT WING FIXED LEADING EDGE RIB UPPER END CAP/CABLE FAIRLEAD IS CRACKED AT W.S. XOS 219. REPAIRED LT WING FIXED LEADING EDGE RIB UPPER END CLIP /CABLE FAIRLEAD
- [SDR JR2R20170525263](https://openairdocs.org/sdr/JR2R20170525263), May 25, 2017: LONGERON. CORRODED. AFT CARGO BAY, LONGERON 22L IS CORRODED AT BS 1287. THE CORROSSION WAS FOUND TO BE 100% MATERIAL LOSS. REPAIRED THE LONGERON IAW SRM 53-02.
- [SDR JR2R20160524054](https://openairdocs.org/sdr/JR2R20160524054), May 24, 2017: DOUBLER. CRACKED. LEFT WING FIXED LEADING EDGE RIB UPPER END CLIP FAIRLEAD DOUBLER IS CRACKED. REPAIRED IAW SRM 57-06B
- [SDR JR2R20160524](https://openairdocs.org/sdr/JR2R20160524), May 24, 2017: DOUBLER. CRACKED. LT WING FIXED LEADING EDGE RIB UPPER END CLIP/FAIRLEAD DOUBLER IS CRACKED. REPAIRED IAW SRM 57-06B.
- [SDR WX0A2017031073238](https://openairdocs.org/sdr/WX0A2017031073238), Mar 30, 2017: BULLET. DAMAGED. DURING CLIMB, THE LT ENGINE WAS NOT PRODUCING FULL POWER, CLIMB RATE WAS ABOUT 500 FPM. EMERGENCY DECLARED. R & R ENGINE NOSE BULLET AND PT2 FLEX LINE IN PYLON.
- [SDR WX0A073188](https://openairdocs.org/sdr/WX0A073188), Sep 30, 2016: WARNING LIGHT. ILLUMINATED. (EMERGENCY DECLARED) MID TAKE ROLL. NOSE GEAR SEEMED TO BE BOTTOMING OUT AFTER ROTATION & GEAR WAS NOT RETRACTED. THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATE
- [SDR WX0A2015102072957](https://openairdocs.org/sdr/WX0A2015102072957), Oct 19, 2015: SKIN. CORRODED. EVIDENCE OF CORROSION AT LONGERON 29R, STATION 726. ALSO CRACK EMANATING FROM RIVET IN SAME AREA. ACCOMPLISHED ERO 5334-007, REPAIR OF CORROSION DAMAGE AT LOWER
- [SDR WX0A2015101672946](https://openairdocs.org/sdr/WX0A2015101672946), Oct 13, 2015: SKIN. CRACKED. HAS A RIVET WITH A CRACK EMANATING FROM IT & ASSOCIATED CORROSION IN THAT AREA. DIMENSION OF CRACK IS ½ OF AN INCH. AREA OF CORROSION AS EVIDENCED BY BULGING SK
- [SDR WX0A2015100872927](https://openairdocs.org/sdr/WX0A2015100872927), Oct 6, 2015: BATTERY. DISCHARGED. EMERGENCY LIGHTS IN TAIL COMPARTMENT ARE INOPERATIVE. R & R BATTERIES TO BOTH EMER POWER SUPPLY B5-27 & B5-28. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.
- [SDR WX0A072825](https://openairdocs.org/sdr/WX0A072825), Aug 20, 2015: BATTERY. DISCHARGED. EMERGENCY BATTERIES NEED CHARGED. EMER LIGHTS OPERATIONAL, CHECKED OK.
- [SDR WX0A2015081672801](https://openairdocs.org/sdr/WX0A2015081672801), Aug 11, 2015: TRIM SYSTEM. MALFUNCTIONED. ALL PRIMARY PITCH TRIM FAILED ON DEPARTURE. AFTER COMPLETION OF QRH PRIMARY PITCH, TRIM OPERATES NORMAL. THIS LOG TRANSFERRED TO LOG 578598. SEE LOG PAGE 578598
- [SDR WX0A2015070272707](https://openairdocs.org/sdr/WX0A2015070272707), Jun 26, 2015: VANE. OUT OF TOLERANCE. ON FINAL, BELOW 1200 AGL RECEIVED BOTH STALL INDICATION & AUTO SLAT FAIL CAUTION MSGS ON OAP. PERFORMED AR 511257 AUTO SLAT FAIL TROUBLE SHOT. FOUND RT AOA VANE
- [SDR WX0A2015062272676](https://openairdocs.org/sdr/WX0A2015062272676), Jun 18, 2015: LIGHT. INOPERATIVE. OVERHEAD EMER LIGHT IN FWD GALLEY INOPERATIVE. RELAMPED FWD GALLEY EMER LIGHT IAW AMM 33-50-00.
- [SDR WX0A2015060372637](https://openairdocs.org/sdr/WX0A2015060372637), Jun 1, 2015: BATTERY. DISCHARGED. EMERGENCY LIGHTS INOPERATIVE ROWS 24 & 25. EMER EXIT LT & RT EMER LIGHT INOPERATIVE ROW 25 ISLE LT. REPLACED EMER EXIT ROWS LIGHT EMER BATTERY'S. OPERATIONS CHE
- [SDR WX0A2015060372636](https://openairdocs.org/sdr/WX0A2015060372636), Jun 1, 2015: LIGHT. INOPERATIVE. REFERENCE LOG PAGE 564424 ITEM 1. EMER EXIT LIGHTS OVERWING INOPERATIVE, RT & LT. RELAMPED RT & LT OVERWING EXIT EMER LIGHTS. OPERATIONS CHECKED GOOD IAW MM 26-
- [SDR WX0A2015060372635](https://openairdocs.org/sdr/WX0A2015060372635), Jun 1, 2015: POWER SUPPLY. INOPERATIVE. OVERHEAD EMER LIGHTS INOPERATIVE AT SEAT ROW 33 & 34. R & R BATTERY POWER SUPPLY AT SEAT ROW 33 & 34. OPERATIONS CHECKED GOOD IAW MM 25-60-00.
- [SDR WX0A2015040272502](https://openairdocs.org/sdr/WX0A2015040272502), Mar 29, 2015: APU. LEAKING. AFTER PARKING AT THE GATE, THE CABIN & COCKPIT FILLED WITH SMOKE & AN ODOR. APU WAS RUNNING & PACKS WERE ON. NOTICED ON WALK AROUND AFT BELLY OF ACFT HAD DRIPPI
- [SDR WX0A2014110772262](https://openairdocs.org/sdr/WX0A2014110772262), Nov 6, 2014: BATTERY. DISCHARGED. FOUND ON WAKE-UP. EMER LIGHTS AT ROW 34 INOPERATIVE. REPLACED BATTERIES FOR EMER LIGHTS AT ROW 34 IAW AMM 33-53-01.
- [SDR WX0A2014110372242](https://openairdocs.org/sdr/WX0A2014110372242), Oct 30, 2014: BATTERY. DISCHARGED. FOUND ON WAKE UP, EMER LIGHTS INOPERATIVE AT ROWS 32 & 24. REPLACED BATTERIES. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.
- [SDR WX0A072092](https://openairdocs.org/sdr/WX0A072092), Aug 10, 2014: INDICATION SYS. ACTIVATED. RT ENG EGT 645 FOR 30 TO 40 SECONDS. NO LOG PAGE OR MI YET, 8/14 MI OPEN. ADDITIONAL INFO TO BE ADDED WHEN AVAILABLE.
- [SDR WX0A2014080572071](https://openairdocs.org/sdr/WX0A2014080572071), Jul 17, 2014: ACM. FAULTY. CABIN TEMP EXCEEDS 38C THRU 15,000 FT DURING CLIMB OUT & WILL NOT DECREASE REF LOG PAGE 508152. REPLACED LT ACM IAW MM 21-51-01. PERFORMED OPERATIONS & LEAK CHE
- [SDR WX0A071989](https://openairdocs.org/sdr/WX0A071989), Jun 10, 2014: BATTERY PACK. INOPERATIVE. AFT EXIT OVERWING LIGHTS OUT. REPLACED BATTERY PACK FOR AFT OVERWING EMER LIGHTS IAW AMM 33-50-00.
- [SDR WX0A071983](https://openairdocs.org/sdr/WX0A071983), Jun 3, 2014: BATTERY. DISCHARGED. OVERWING EMER EXIT LIGHTS INOPERATIVE. R & R BATTERIES FOR OVERWING EMER EXIT LIGHTS IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.
- [SDR WX0A071945](https://openairdocs.org/sdr/WX0A071945), May 8, 2014: WIRE. OUT OF POSITION. AFT CABIN OVER DOOR EMERGENCY LIGHT INOPERATIVE, FOUND ON WAKE-UP. REPLACED POWER SUPPLY, NO HELP. FOUND T2 & T7 WIRES WERE SWAPPED. RESTORED WIRES TO CORRECT T
- [SDR WX0A071942](https://openairdocs.org/sdr/WX0A071942), May 2, 2014: TAB. DELAMINATED. LEFT ELEVATOR INBD TAB, (CONTROL TAB, OTBD AFT CORNER REPAIR DELAMINATED. REMOVED DAMAGE DOUBLER, FABRICATED REPAIR PARTS & INSTALLED IAW SRM 51-70-2.
- [SDR WX0A071841](https://openairdocs.org/sdr/WX0A071841), Feb 7, 2014: BATTERY. DISCHARGED. AFT CABIN FLASHLIGHT NOT FLASHING. REPLACED AFT CABIN EMERGENCY FLASHLIGHT BATTERY & OPERATIONS CHECKED GOOD.
- [SDR WX0A071834](https://openairdocs.org/sdr/WX0A071834), Feb 1, 2014: POWER SUPPLY. DEFECTIVE. EMERGENCY LIGHTS FLASHED ON & OFF DURING CRUISE. R & R POWER SUPPLY AT STATION 223 IAW AMM CH 33-53-00, OPERATIONS CHECKED GOOD.
- [SDR WX0A071770](https://openairdocs.org/sdr/WX0A071770), Dec 6, 2013: FAN. MALFUNCTIONED. FLIGHT ATTENDANT CALLED UP COMPLAINING OF BURNING SMELL BETWEEN ROWS 18 - 21. AFTER 7 MINUTES SMELL WENT AWAY. COMPLIED WITH TASK CARD F0592102 CABIN ODOR, SMOK
- [SDR WX0A071605](https://openairdocs.org/sdr/WX0A071605), May 27, 2013: BATTERY. DISCHARGED. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX PERSONNEL R & R THE APPROPRIATE 
- [SDR WX0A2013032171543](https://openairdocs.org/sdr/WX0A2013032171543), Mar 15, 2013: BATTERY. DISCHARGED. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TE
- [SDR WX0A071464](https://openairdocs.org/sdr/WX0A071464), Dec 27, 2012: BATTERY. DISCHARGED. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TE
- [SDR WX0A071402](https://openairdocs.org/sdr/WX0A071402), Nov 18, 2012: CUSP WEB. CORRODED. AFT CARGO COMPARTMENT CUSP WEB CORRODED BETWEEN FLOORBEAMS AT STATION 1174 TO 1193 RBL 52. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER REPAIR.
- [SDR WX0A071390](https://openairdocs.org/sdr/WX0A071390), Nov 18, 2012: CUSP WEB. CORRODED. AFT CARGO COMPARTMENT TO CABIN CSP WEB CORRODED BETWEEN STATION 1193 TO 1211 AT RBL 52. REMOVED DAMAGE AREA AND INSTALLED FILLER AND DOUBLER.
- [SDR WX0A071389](https://openairdocs.org/sdr/WX0A071389), Nov 17, 2012: DOOR FRAME. CRACKED. AFT ENTRY DOOR FRAME CRACKED AT LEFT UPPER CORNER.
- [SDR WX0A071420](https://openairdocs.org/sdr/WX0A071420), Nov 15, 2012: BATTERY. DISCHARGED. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TE
- [SDR WX0A071388](https://openairdocs.org/sdr/WX0A071388), Nov 15, 2012: WEB. CRACKED. LEFT ENGINE INLET COWL AFT WEB CRACKED AT ACCESS PANEL FASTENER AT 4:30 O'CLOCK POSITION.
- [SDR WX0A071387](https://openairdocs.org/sdr/WX0A071387), Nov 15, 2012: PAN. CHAFED. FWD ACCESSORY DOOR JAMB PAN CHAFED AT FWD END IN LOWER RADIUS.
- [SDR WX0A071386](https://openairdocs.org/sdr/WX0A071386), Nov 13, 2012: SEAT TRACK. DAMAGED. PASSENGER CABIN RIGHT SEAT TRACK RBL 22 STA 927 TO 1003 HAD DOUBLE DRILLED HOLES. REMOVED AND REPLACED TRACK WITH SPLICE IAW MD80-SRM 5305.

All 69: https://openairdocs.org/aircraft/N883GA/reports.md

## STCs that may be installed (OpenAirDocs) (439, 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 (Douglas DC-9-83)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [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 ST02463AT](https://openairdocs.org/stc/ST02463AT): Installation of an Intrusion/Penetration Resistance Flightdeck Door and Reinforced Flightdeck Door Surround. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST03203AT](https://openairdocs.org/stc/ST03203AT): Installation of a Flight Data Acquisition Module (FDAM) and Flight Data Recorder (FDR), sensors Sensor Kit with Level E software. 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 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 SA5542NM](https://openairdocs.org/stc/SA5542NM): Installation of galley, stowage unit, coatroom, PSU kit, drop ceiling. Safran Cabin Inc
- [STC SA5786NM](https://openairdocs.org/stc/SA5786NM): Installation of an overhead life raft stowage compartment kit. Safran Cabin Inc
- [STC SA7079NM](https://openairdocs.org/stc/SA7079NM): Installation C&D Interiors passenger service units, overhead storage units, sidewall panels, and ceiling panels. Safran Cabin Inc
- [STC ST00128LA](https://openairdocs.org/stc/ST00128LA): Installation of moveable class divider. Safran Cabin Inc
- [STC ST00649LA](https://openairdocs.org/stc/ST00649LA): Installation of Sidewall Panel Installation. 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 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 SA8716SW](https://openairdocs.org/stc/SA8716SW): Replacement of Douglas P/N 22514-1 connector assy with Southern Aeroparts P/N S22514-1 for the lavatory actuator cable. Southern Aeropartners 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
- [STC ST01992CH](https://openairdocs.org/stc/ST01992CH): Installation of a Smiths SDS2000 Electronic Display System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST02316CH](https://openairdocs.org/stc/ST02316CH): Upgrade of existing Mode S transponder installation to add enhanced surveillance Mode S. Amphenol Cable and Interconnect Technologies Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST02474AK](https://openairdocs.org/stc/ST02474AK): Installation of escape tapes at the L1 and R1 entry doors and removal of evacuation slides. Tatonduk Outfitters Ltd
- [STC ST02770SE](https://openairdocs.org/stc/ST02770SE): Installation of an Improved Radio Altimeter System. AeroMech Incorporated
- [STC ST01987AT](https://openairdocs.org/stc/ST01987AT): Installation of STG Aerospace Inc. photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc

All 439: https://openairdocs.org/aircraft/N883GA/stcs.md

## Related

- Other Douglas DC-9-83 aircraft: https://openairdocs.org/model/douglas-dc-9-83/aircraft.md
- The Pratt & Whitney JT8D-219 engine: https://openairdocs.org/engine/pratt-whitney-jt8d-219.md

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