# N9616G: 1997 Mcdonnell Douglas DC-9-83(MD-83)

- Status: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083, 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: 53563
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 9, 1997
- Certificate issued: October 18, 2023
- Expires: October 31, 2030
- Mode S code: AD630E
- Registered owner: [Jetran LLC](https://openairdocs.org/faa-owner/JETRAN%20LLC)
- Location: [Horseshoe Bay, TX](https://openairdocs.org/faa-place/TX/Horseshoe%20Bay)
- Owner type: LLC
- Owner's area on the map: 30.5258° N, 98.3759° W: Placed by OpenAirDocs at the center of ZIP code 78657, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=9616G
- Page: https://openairdocs.org/aircraft/N9616G

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): 322 in force

### Matched by airframe (Mcdonnell Douglas DC-9-83(MD-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 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 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 360: https://openairdocs.org/aircraft/N9616G/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 N9616G.

## 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 20030727016729I](https://openairdocs.org/incident/20030727016729I), Jul 27, 2003: Doug DC983 (N9616G), St Louis, MO. (-23) Right hand fuel pressure low light came on in flight. Opened fuel cross feed per emergency checklist procedure but light remained on. Closed cross feed…

## Service difficulty reports (107, 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 AALA20190416002](https://openairdocs.org/sdr/AALA20190416002), Apr 15, 2019: COMPUTER. FAULTY. AIRCRAFT WAS GROUNDED: PILOT REPORTS FLIGHT DIVERSION ON ACCOUNT OF MANY CAUTION LIGHTS; DFCG WAS BLANK, NAV BLANK, WINDSHEAR, YAW DAMPENER OFF, AUTO THROTTLE O
- [SDR AALA2019040879006](https://openairdocs.org/sdr/AALA2019040879006), Apr 6, 2019: GUST LOCK. OUT OF ADJUST. AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS THE FWD ENTRY DOOR L1 GUST LOCK IS DIFFICULT TO ENGAGE. ADJUSTED L1 DOOR GUST LOCK. OK FOR SERVICE.
- [SDR AALA20181113004](https://openairdocs.org/sdr/AALA20181113004), Nov 12, 2018: BATTERY PACK. DISCHARGED. AIRCRAFT WAS NOT GROUNDED: BOTTOM LIGHT OF THE EMERGENCY TRIPLE LIGHT STOP LIGHT FIXTURE WAS INOPERABLE. MAINTENANCE REPLACED BATTERY PACK AND PERFORMED SATISFA
- [SDR AALA20181112001](https://openairdocs.org/sdr/AALA20181112001), Nov 11, 2018: PAN. CORRODED. CORROSION FOUND ON THE FORWARD CARGO DOOR CUTOUT LOWER DOOR FRAME PAN AT THE FORWARD LOWER DOOR STOP BETWEEN BS 389 AND 395. REPAIRED THE PAN IAW EA 286867.
- [SDR AALA201809279013](https://openairdocs.org/sdr/AALA201809279013), Sep 26, 2018: BATTERY PACK. NO TEST. AFT LEFT SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER. PERFORMED A SATISFACTORY OP
- [SDR AALA201803149010](https://openairdocs.org/sdr/AALA201803149010), Mar 9, 2018: BATTERY PACK. INOPERATIVE. TAIL COMP EMERGENCY LIGHTS INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-27 AND B5-28 IAW AMM 33-53-00. TAIL CONE LIGHT CHECKED OK.
- [SDR AALA201803129039](https://openairdocs.org/sdr/AALA201803129039), Mar 9, 2018: BATTERY PACK. INOPERATIVE. TAIL COMP EMERGENCY LIGHTS ARE OUT. REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-27 AND B5-28 IAW AMM 33-53-00. TAIL CONE LIGHT CHECKED OK.
- [SDR AALA20171221003](https://openairdocs.org/sdr/AALA20171221003), Dec 20, 2017: FUEL CONTROL. FAULTY. AIRCRAFT WAS NOT GROUNDED. IRREGULAR FUEL BURN. CENTER TANK VERY SLOW TO TRANSFER. WITH ALL PUMPS A/C CONTINUED TO BURN OUT OF ALL THREE TANKS WITH CROSSFEED OP
- [SDR AALA20171126002](https://openairdocs.org/sdr/AALA20171126002), Nov 25, 2017: PUMP. FAILED. FLIGHT RETURNED TO DEPARTURE DUE TO A FUEL BOOST PUMP FAILED. REMOVED AND REPLACED FORWARD CENTER FUEL BOOST PUMP AND CONDUIT HARNESS IAW AMM 28-20-07-201. OPER
- [SDR AALA201711289001](https://openairdocs.org/sdr/AALA201711289001), Nov 24, 2017: CONDUIT. DAMAGED. AIRCRAFT WAS GROUNDED. DFW-CVG FLIGHT RETURNED TO DFW ACCOUNT FUEL BOOST PUMP FAILED. REMOVED AND REPLACED FORWARD CENTER FUEL BOOST PUMP (AALA20171126002) AND 
- [SDR AALA201709139019](https://openairdocs.org/sdr/AALA201709139019), Sep 12, 2017: CABLE. EXPOSED. L2 DOOR EMERGENCY EVACUATION SLIDE HAS A METAL CABLE PROTRUDING. REMOVED AND REPLACED SLIDE PER AMM 25-62-00. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.
- [SDR AALA20170809007](https://openairdocs.org/sdr/AALA20170809007), Aug 9, 2017: SUPPORT ANGLE. CORRODED. AIRCRAFT IN BASE MAINTENANCE. CORROSION ON ANGLE, JUST ABOVE L30, AFT SIDE OF FRAME AT STATION 788. INSTALLED NEW SUPPORT ANGLE PER SRM 51-30-05-001.
- [SDR AALA20170809006](https://openairdocs.org/sdr/AALA20170809006), Aug 9, 2017: FLOOR SUPPORT. BROKEN. AIRCRAFT IN BASE MAINTENANCE. CRACK ON MID CARGO FLOORBOARD SUPPORT EAR AT ATTACH POINT FOR RIGHT HAND TIE-DOWN TRACK. INSTALLED FLOORBOARD SUPPORT PER SRM 51-3
- [SDR AALA20170807003](https://openairdocs.org/sdr/AALA20170807003), Aug 6, 2017: CARGO TRACK. CORRODED. AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND TIE DOWN TRACK BETWEEN STATION 693 AND 788. REPLACED TIE DOWN TRACK PER SRM 51-01-00-001 AND DRAWING 59365
- [SDR AALA20170807002](https://openairdocs.org/sdr/AALA20170807002), Aug 6, 2017: CARGO TRACK. CORRODED. AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND TIE DOWN TRACK BETWEEN STATION 636 AND 788. REPLACED TIE DOWN (CARGO) TRACK PER SRM 51-01-00-001 AND DRAWIN
- [SDR AALA20170807001](https://openairdocs.org/sdr/AALA20170807001), Aug 6, 2017: LONGERON. CORRODED. AIRCRAFT IN BASE MAINTENANCE. CORROSION ON BOTTOM OF LONGERON L30 AT STATION 788. REPLACED L30 LONGERON PER SRM 51-30-05, DRAWINGS 5936360 AND 5936571.
- [SDR AALA201708039021](https://openairdocs.org/sdr/AALA201708039021), Jul 31, 2017: STUD. CORRODED. AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED INBOAR
- [SDR AALA201708039020](https://openairdocs.org/sdr/AALA201708039020), Jul 31, 2017: STUD. CORRODED. AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED INBOAR
- [SDR AALA201708039019](https://openairdocs.org/sdr/AALA201708039019), Jul 31, 2017: STUD. CORRODED. AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED INBOAR
- [SDR AALA201708039018](https://openairdocs.org/sdr/AALA201708039018), Jul 31, 2017: STUD. CORRODED. AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED OUTBOA
- [SDR AALA20170731003](https://openairdocs.org/sdr/AALA20170731003), Jul 30, 2017: DOOR SILL. CORRODED. AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MID CARGO DOOR SILL BEAM AT RIVNUT HOLES BETWEEN STATION 636 AND 693. REPAIRED SILL BEAM PER AARD 53-10-00-3.
- [SDR AALA20170731001](https://openairdocs.org/sdr/AALA20170731001), Jul 30, 2017: HINGE FITTING. CORRODED. AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTING LOWER OUTBOARD MOUNT STUDS BETWEEN STATION 984 AND 1007. REPLACED HINGE 
- [SDR AALA20170724009](https://openairdocs.org/sdr/AALA20170724009), Jul 24, 2017: CARGO TRACK. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT CARGO LEFT FORWARD TIE DOWN TRACK BETWEEN FUSELAGE STATIONS 1079 AND 1231. REMOVED AND REPLACED TRACK PER SRM
- [SDR AALA20170724008](https://openairdocs.org/sdr/AALA20170724008), Jul 24, 2017: CARGO TRACK. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT CARGO LEFT AFT TIE DOWN TRACK BETWEEN FUSELAGE STATIONS 1231 AND 1309. REMOVED AND REPLACED TRACK PER SRM 51-
- [SDR AALA201707259019](https://openairdocs.org/sdr/AALA201707259019), Jul 21, 2017: FITTING. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT ACCESSORY COMPARTMENT LOWER LEFT CANTED FRAME GUIDE PIN FITTING AT FUSELAGE STATION 1463. REMOVED AND REPLACE
- [SDR AALA20170721004](https://openairdocs.org/sdr/AALA20170721004), Jul 21, 2017: FRAME. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT ACCESSORY COMPARTMENT LOWER LEFT CANTED FRAME AT FUSELAGE STATION 1463, JUST OUTBOARD OF AIRSTAIR CUTOUT. REP
- [SDR AALA20170720004](https://openairdocs.org/sdr/AALA20170720004), Jul 20, 2017: FLOOR SUPPORT. WORN. AIRCRAFT WAS IN BASE MAINTENANCE. THREE WORN AREAS ON FLOORBOARD SUPPORT AT THE ATTACH POINTS, FUSELAGE STATION 180 BETWEEN LBL20 AND LBL40. REMOVED AND REPLACE
- [SDR AALA20170719006](https://openairdocs.org/sdr/AALA20170719006), Jul 19, 2017: WEB. CRACKED. AIRCRAFT WAS IN BASE MAINTENANCE. CRACK ON LEFT INTERNAL FUSELAGE AT STATION 208, 51 INCHES ABOVE FLOOR. REPAIRED PER 53-10-00-11.
- [SDR AALA20170719005](https://openairdocs.org/sdr/AALA20170719005), Jul 19, 2017: WEB. CRACKED. AIRCRAFT WAS IN BASE MAINTENANCE. CRACK ON LEFT INTERNAL FUSELAGE AT STATION 208, 27 INCHES ABOVE FLOOR. REPAIRED PER 53-10-00-11.
- [SDR AALA20170718005](https://openairdocs.org/sdr/AALA20170718005), Jul 18, 2017: CUSP WEB. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON RIGHT CUSP BETWEEN FUSELAGE STATIONS 642 AND 646, RBL57. REPAIRED PER AARD 53-20-00-16.
- [SDR AALA20170717004](https://openairdocs.org/sdr/AALA20170717004), Jul 17, 2017: CARGO TRACK. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT CARGO RIGHT FORWARD TIEDOWN TRACK BETWEEN FUSELAGE STATIONS 1098 AND 1155. REMOVED AND REPLACED TRACK PER AAR
- [SDR AALA20170714002](https://openairdocs.org/sdr/AALA20170714002), Jul 14, 2017: SHEAR TIE. CRACKED. AIRCRAFT WAS IN BASE MAINTENANCE. CRACK ON AFT ACCESSORY COMPARTMENT SHEAR TIE AT FUSELAGE STATION 1380 BELOW LONGERON 13R. REPAIRED PER AARD 53-10-00-20.
- [SDR AALA201706249007](https://openairdocs.org/sdr/AALA201706249007), Jun 20, 2017: PORTABLE LIGHT. INOPERATIVE. THE AIRCRAFT WAS NOT GROUNDED. PORTABLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED PORTABLE EMERGENCY FLASHLIGHT PER AMM 33-53-00 OPS CK GOOD.
- [SDR AALA20170411002](https://openairdocs.org/sdr/AALA20170411002), Apr 10, 2017: CONNECTOR. DAMAGED. CREW REPORTED LEFT HAND ENGINE OIL TEMP EXCEEDED LIMITS. CREW DECLARED EMERGENCY AND FOLLOWED QRH PROCEDURES BY SHUTTING DOWN THE LEFT ENGINE. THE FLIGHT RETURN
- [SDR AALA20170125012](https://openairdocs.org/sdr/AALA20170125012), Jan 23, 2017: OVEN. SMOKE. AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT REPORTED SMOKE ABOVE FORWARD GALLEY OUTBOARD OVEN AND IMMEDIATELY TURNED IT OFF. SMOKE AND ODOR DISSIPATED AFTER OVE
- [SDR AALA20170124007](https://openairdocs.org/sdr/AALA20170124007), Jan 21, 2017: BATTERY PACK. DISCHARGED. AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FROM ROW 20 TO ROW 32 FAILED TEST. REMOVED AND REPLACED BATTERY PACK AB5-3(AALA20170124006)
- [SDR AALA20170124006](https://openairdocs.org/sdr/AALA20170124006), Jan 21, 2017: BATTERY PACK. DISCHARGED. AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FROM ROW 20 TO ROW 32 FAILED TEST. REMOVED AND REPLACED BATTERY PACK AB5-3 AND BATTERY PACK
- [SDR AALA20170124005](https://openairdocs.org/sdr/AALA20170124005), Jan 21, 2017: BATTERY. DISCHARGED. AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGNS ABOVE OVERWING DOORS FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY B5-103 (AALA20170122003) AND BATTERY ASS
- [SDR AALA20170122003](https://openairdocs.org/sdr/AALA20170122003), Jan 21, 2017: BATTERY. DISCHARGED. AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGNS ABOVE OVERWING DOORS FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY B5-103 AND BATTERY ASSEMBLY B5-105 (AALA
- [SDR AALA20170123011](https://openairdocs.org/sdr/AALA20170123011), Jan 21, 2017: DOOR. LACK OF LUBE. AIRCRAFT WAS GROUNDED. R1 DOOR IS DIFFICULT TO UNLATCH. LUBRICATED DOOR HOLD OPEN/GUST LOCK BAYONET AND RELEASE HANDLE IAW AMM 52-11-00. OPERATIONAL CHECK GOOD.
- [SDR AALA20161220003](https://openairdocs.org/sdr/AALA20161220003), Dec 17, 2016: LENS. DETACHED. EMERGENCY EXIT SIGN AT R1 DOOR HAS A DETACHED LENS COVER. REMOVED AND REPLACED EXIT SIGN IAW AMM 33-53-01. OPERATIONAL CHECKED GOOD.
- [SDR AALA20150418003](https://openairdocs.org/sdr/AALA20150418003), Apr 17, 2015: SIGN. BROKEN. R1 DOOR EMERGENCY EXIT SIGN LIGHT HAS A BROKEN BASE. R & R R1 DOOR EMERGENCY LIGHT ASSEMBLY IAW AMM 33-53-01L. SYS CHECKED NORMAL.
- [SDR AALA20141217011](https://openairdocs.org/sdr/AALA20141217011), Dec 17, 2014: STOP FITTING. CRACKED. AFT CARGO DOOR LOWER FWD STOP IS CRACKED. R & R STOP IAW AARD 51-00-05-1.
- [SDR AALA20141217012](https://openairdocs.org/sdr/AALA20141217012), Dec 16, 2014: LONGERON. CRACKED. LONGERON 2 RT IS CRACKED AT AFT SIDE OF FS 1418. REPAIRED LONGERON IAW SRM 53-02-00-001.
- [SDR AALA20140702003](https://openairdocs.org/sdr/AALA20140702003), Jul 2, 2014: GASKET. DAMAGED. TAIL COMPARTMENT HIGH LIGHT ILLUMINATED ON CLIMB OUT. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT COLD DIVER
- [SDR AALA20140530017](https://openairdocs.org/sdr/AALA20140530017), May 30, 2014: CHECK VALVE. LEAKING. DFW CREW REPORTED TAIL COMPARTMENT HIGH LIGHT ILLUMINATED DURING CLIMBOUT. EMER DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE.
- [SDR AALA20140516021](https://openairdocs.org/sdr/AALA20140516021), May 16, 2014: OVERHEAT SENSOR. FAULTY. SJC CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH INDICATION. EMERGENCY DECLARED FLIGHT RETURNED SJC LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLA
- [SDR AALA20140414001](https://openairdocs.org/sdr/AALA20140414001), Apr 14, 2014: BATTERY. DISCHARGED. AFT SECTION OF ESCAPE PATH LIGHTING DIM. REPLACED BOTH BATTERIES, OPERATIONS CHECKED NORMAL.
- [SDR AALA20130805003](https://openairdocs.org/sdr/AALA20130805003), Aug 5, 2013: CUSP WEB. CORRODED. CORROSION ON SUB FLOOR AT STATION 217 UNDER NR 6 SEAT TRACK. INSTALLED DOUBLER IAW AARD 53-20-00-16.
- [SDR AALA20130731012](https://openairdocs.org/sdr/AALA20130731012), Jul 31, 2013: CUSP WEB. CORRODED. CORROSION ON LT CUSP FROM STATIONS 1155 - 1174. INSTALLED DOUBLER IAW AARD 53-20-00-16.

All 107: https://openairdocs.org/aircraft/N9616G/reports.md

## STCs that may be installed (OpenAirDocs) (456, 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-9-83(MD-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 456: https://openairdocs.org/aircraft/N9616G/stcs.md

## Earlier aircraft with N9616G

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N9616G before.

- [Cancelled 1973-10-09](https://openairdocs.org/deregistered/N9616G-1973-10-09): Cessna U206, S/N U206 01816. Owner: [Sutherland Paul A](https://openairdocs.org/faa-owner/SUTHERLAND%20PAUL%20A), [Dillingham, AK](https://openairdocs.org/faa-place/AK/Dillingham)

## Related

- Other Mcdonnell Douglas DC-9-83(MD-83) aircraft: https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83/aircraft.md
- The Pratt & Whitney JT8D series engine: https://openairdocs.org/engine/pratt-whitney-jt8d-series.md

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