# N963DN: 1999 Boeing MD-90-30

- Status: Valid registration
- Airframe: [Boeing MD-90-30](https://openairdocs.org/model/boeing-md-90-30) (registry code 13848ME, 142 seats)
- Engine: [IAE V2528-D5](https://openairdocs.org/engine/iae-v2528-d5) (registry code 34609)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company), [TCDS E40NE](https://openairdocs.org/tcds/E40NE) (International Aero Engines AG (IAE)) (OpenAirDocs)
- Serial number: 53533
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 2, 2012
- Certificate issued: May 18, 2023
- Expires: May 31, 2030
- Mode S code: AD67A3
- Registered owner: [Boeing Company](https://openairdocs.org/faa-owner/BOEING%20COMPANY)
- Location: [Renton, WA](https://openairdocs.org/faa-place/WA/Renton)
- Owner type: Corporation
- Owner's area on the map: 47.4719° N, 122.2194° W: Placed by OpenAirDocs at the center of ZIP code 98057, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=963DN
- Page: https://openairdocs.org/aircraft/N963DN

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): 115 in force

### Matched by airframe (Boeing MD-90-30)

- [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 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 2019-24-17](https://openairdocs.org/ad/2019-24-17): Wings · Boeing MD-90-30. Effective Jan 24, 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 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2017-11-02](https://openairdocs.org/ad/2017-11-02): Stabilizers · Boeing MD-90-30. Effective Jun 27, 2017
- [AD 2016-25-26](https://openairdocs.org/ad/2016-25-26): Navigation · Boeing MD-90-30. Effective Feb 2, 2017
- [AD 2016-22-18](https://openairdocs.org/ad/2016-22-18): Fuselage · Boeing MD-90-30. Effective Nov 21, 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 2014-24-03](https://openairdocs.org/ad/2014-24-03): Stabilizers · Boeing MD-90-30. Effective Jan 27, 2015
- [AD 2014-24-04](https://openairdocs.org/ad/2014-24-04): Stabilizers · Boeing MD-90-30. Effective Jan 13, 2015
- [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 2012-22-04](https://openairdocs.org/ad/2012-22-04): Wings · Boeing MD-90-30. Effective Dec 5, 2012
- [AD 2012-21-18](https://openairdocs.org/ad/2012-21-18): Wings · Boeing MD-90-30. Effective Dec 5, 2012
- [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 2011-12-12](https://openairdocs.org/ad/2011-12-12): Stabilizers · Boeing MD-90-30. Effective Jul 22, 2011
- [AD 2011-06-12](https://openairdocs.org/ad/2011-06-12): Stabilizers · Boeing MD-90-30. Effective Apr 26, 2011
- [AD 2011-03-09](https://openairdocs.org/ad/2011-03-09): Ignition · Boeing MD-90-30. Effective Mar 14, 2011
- [AD 2011-01-11](https://openairdocs.org/ad/2011-01-11): Stabilizers · Boeing MD-90-30. Effective Feb 9, 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 2010-22-04](https://openairdocs.org/ad/2010-22-04): Nacelles/Pylons · Boeing MD-90-30. Effective Dec 3, 2010
- [AD 2010-21-16](https://openairdocs.org/ad/2010-21-16): Hydraulic Power · Boeing MD-90-30. Effective Nov 18, 2010
- [AD 2010-16-11](https://openairdocs.org/ad/2010-16-11): Wings · Boeing MD-90-30. Effective Sep 22, 2010
- [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 2010-05-04](https://openairdocs.org/ad/2010-05-04): Fuselage · Boeing MD-90-30. Effective Apr 1, 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 2009-13-08](https://openairdocs.org/ad/2009-13-08): Stabilizers · Boeing MD-90-30. Effective Aug 3, 2009
- [AD 2009-11-11](https://openairdocs.org/ad/2009-11-11): Fuel · Boeing MD-90-30. Effective Jul 7, 2009
- [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 2007-17-19](https://openairdocs.org/ad/2007-17-19): Static port heater assemblies · Boeing MD-90-30. Effective Oct 2, 2007
- [AD 2006-16-09](https://openairdocs.org/ad/2006-16-09): Refueling manifold in the right wing refueling station area · Boeing MD-90-30. Effective Sep 13, 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 2005-13-14](https://openairdocs.org/ad/2005-13-14): Dual anti-skid control manifolds (DACM) · Boeing MD-90-30. Effective Jul 29, 2005
- [AD 2005-09-08](https://openairdocs.org/ad/2005-09-08): Aft left lavatory · Boeing MD-90-30. Effective May 20, 2005
- [AD 2005-06-03](https://openairdocs.org/ad/2005-06-03): fluorescent light lamp holders · Boeing MD-90-30. Effective Apr 20, 2005
- [AD 2005-05-02](https://openairdocs.org/ad/2005-05-02): Electrical/electronics (E/E) compartment · Boeing MD-90-30. Effective Apr 6, 2005
- [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 2004-07-12](https://openairdocs.org/ad/2004-07-12): Terminal studs on the 3-phase limiter blocks · Boeing MD-90-30. Effective May 11, 2004
- [AD 2004-05-25](https://openairdocs.org/ad/2004-05-25): Seat Locking Pins · Boeing DC-9-14, DC-9-15, DC-9-15F and 18 more. Effective Apr 19, 2004
- [AD 2004-05-18](https://openairdocs.org/ad/2004-05-18): Main Landing Gear (MLG) · Boeing MD-90-30. Effective Apr 13, 2004
- [AD 2004-05-03](https://openairdocs.org/ad/2004-05-03): Shock strut cylinders · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 3 more. Effective Mar 15, 2004
- [AD 2003-26-07](https://openairdocs.org/ad/2003-26-07): Circuit Breakers · Boeing MD-90-30. Effective Feb 4, 2004
- [AD 2003-11-15 R1](https://openairdocs.org/ad/2003-11-15-R1): Pressure relief door · Boeing MD-90-30. Effective Jan 27, 2004

### Matched by engine (IAE V2528-D5)

- [AD 2026-17-03](https://openairdocs.org/ad/2026-17-03): Turbine Engine Compressor Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Sep 24, 2026
- [AD 2025-19-13](https://openairdocs.org/ad/2025-19-13): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Oct 29, 2025
- [AD 2025-17-16](https://openairdocs.org/ad/2025-17-16): Turbine Engine Compressor Sections · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Oct 10, 2025
- [AD 2024-11-03](https://openairdocs.org/ad/2024-11-03): Turbine Engine · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Jun 26, 2024
- [AD 2022-02-09](https://openairdocs.org/ad/2022-02-09): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Mar 15, 2022
- [AD 2021-14-19](https://openairdocs.org/ad/2021-14-19): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Aug 5, 2021
- [AD 2021-05-18](https://openairdocs.org/ad/2021-05-18): Turbine Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 8 more. Effective Apr 29, 2021
- [AD 2021-01-03](https://openairdocs.org/ad/2021-01-03): Turbine Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 8 more. Effective Jan 21, 2021
- [AD 2020-09-03](https://openairdocs.org/ad/2020-09-03): Turbine Engine Compressor Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 8 more. Effective May 29, 2020
- [AD 2020-07-51](https://openairdocs.org/ad/2020-07-51): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 6 more. Effective Apr 28, 2020
- [AD 2019-16-01](https://openairdocs.org/ad/2019-16-01): Turbine section · International Aero Engines V2525-D5 and V2528-D5. Effective Sep 19, 2019
- [AD 2017-14-07](https://openairdocs.org/ad/2017-14-07): Turbine Engine · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Aug 21, 2017
- [AD 2016-25-11](https://openairdocs.org/ad/2016-25-11): No. 3 bearing · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Jan 20, 2017
- [AD 2016-18-10](https://openairdocs.org/ad/2016-18-10): High- pressure turbine (HPT) stage 2 hub · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 6 more. Effective Oct 7, 2016
- [AD 2015-10-04](https://openairdocs.org/ad/2015-10-04): HPC stage 3 to 8 drum · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jul 1, 2015
- [AD 2013-07-10](https://openairdocs.org/ad/2013-07-10): Bearing internal scavenge tube and  bearing external scavenge tube · International Aero Engines V2525-D5 and V2528-D5. Effective May 20, 2013
- [AD 2011-25-08](https://openairdocs.org/ad/2011-25-08): High- pressure turbine (HPT) case burn-through events · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jan 17, 2012
- [AD 2010-06-18](https://openairdocs.org/ad/2010-06-18): Vortex reducers · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Apr 22, 2010
- [AD 2009-22-06](https://openairdocs.org/ad/2009-22-06): HPC stage 9-12 disc assembly · International Aero Engines V2500-A1, V2527E-A5, V2528-D5 and 1 more. Effective Nov 30, 2009
- [AD 2008-14-15](https://openairdocs.org/ad/2008-14-15): No. 4 bearing oil system components · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Aug 20, 2008
- [AD 2007-21-05](https://openairdocs.org/ad/2007-21-05): Monitoring of N2 vibration on all IAE V2500 series engines · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Nov 15, 2007
- [AD 2004-12-08](https://openairdocs.org/ad/2004-12-08): Airworthiness Limitations Section (ALS) · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jul 23, 2004
- [AD 2000-22-07](https://openairdocs.org/ad/2000-22-07): High Pressure Turbine (HPT) · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 6 more. Effective Dec 6, 2000
- [AD 99-04-03](https://openairdocs.org/ad/99-04-03): High Pressure Compressor (HPC) Stage 9-12 Drum · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 5 more. Effective Apr 12, 1999

### 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 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 2009-07-04](https://openairdocs.org/ad/2009-07-04) (historical): Auxiliary hydraulic power system · McDonnell Douglas MD-90-30. Effective May 5, 2009
- [AD 2008-18-10](https://openairdocs.org/ad/2008-18-10) (historical): Aft mount support fitting · McDonnell Douglas MD-90-30. Effective Sep 24, 2008
- [AD 2005-03-05](https://openairdocs.org/ad/2005-03-05) (historical): Aft left lavatory · Boeing MD-90-30. Effective Feb 22, 2005
- [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 2003-11-15](https://openairdocs.org/ad/2003-11-15) (historical): Pressure relief door for the thrust reverser · McDonnell Douglas MD-90-30. Effective Jul 9, 2003
- [AD 2003-04-10](https://openairdocs.org/ad/2003-04-10) (historical): Wire Chafing · McDonnell Douglas MD-90-30. Effective Apr 4, 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 2001-07-10](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 2000-20-04](https://openairdocs.org/ad/2000-20-04) (historical): Electrical Power Control Unit (EPCU) · McDonnell Douglas MD-90-30. Effective Nov 13, 2000
- [AD 2000-16-01](https://openairdocs.org/ad/2000-16-01) (historical): Electrical Power Control Unit (EPCU) · McDonnell Douglas MD-90-30. Effective Sep 19, 2000
- [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 2000-03-08](https://openairdocs.org/ad/2000-03-08) (historical): Main Landing Gear (MLG) Piston · McDonnell Douglas MD-90-30. Effective Mar 22, 2000
- [AD 2000-03-51](https://openairdocs.org/ad/2000-03-51) (historical): Jackscrew Assembly · McDonnell Douglas 717-200, DC-9 Series (all), MD-88 and 1 more. Effective Mar 6, 2000
- [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 97-11-07](https://openairdocs.org/ad/97-11-07) (historical): Structural Integrity · Boeing MD-90-30. Effective Jun 26, 1997
- [AD 95-04-01](https://openairdocs.org/ad/95-04-01) (historical): AFM - Limitations - Windshear · Boeing 727-100 Series, 727-200 Series, 737-100 Series and 54 more. Effective Mar 8, 1995
- [AD 2021-11-15](https://openairdocs.org/ad/2021-11-15) (historical): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Jul 13, 2021
- [AD 2019-06-06](https://openairdocs.org/ad/2019-06-06) (historical): Turbine Engine Combustion Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Apr 12, 2019
- [AD 2012-09-09](https://openairdocs.org/ad/2012-09-09) (historical): High-pressure compressor (HPC) stage 3 to 8 drums · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jun 27, 2012
- [AD 2010-20-07](https://openairdocs.org/ad/2010-20-07) (historical): Initial and repetitive on-wing ultrasonic inspections · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Nov 1, 2010
- [AD 99-08-11](https://openairdocs.org/ad/99-08-11) (historical): International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective May 13, 1999

All 141: https://openairdocs.org/aircraft/N963DN/ads.md

## Information bulletins (advisory) (5 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-18-33](https://openairdocs.org/saib/NM-18-33): Engine Fuel and Control. Issued Dec 17, 2018
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [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 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## NTSB investigations

None matched to N963DN.

## 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 20130624012709I](https://openairdocs.org/incident/20130624012709I), Jun 24, 2013: Boeing MD-90-30 (N963DN), Washington, DC, Minor damage. Delta airlines flight 1763, an MD-90, N963DN, departing Ronald Reagan Washington national airport (kdca) to minneapolis-st. paul international airport (kmsp),…

## Service difficulty reports (148, 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 DALA2020080602719](https://openairdocs.org/sdr/DALA2020080602719), Aug 5, 2020: ATTACH ANGLE. CRACKED. CRACK ON RH ATTACH ANGLE THROUGH ACCESS PANEL 370AL. NRC 00156: RH ATTACH ANGLE WAS REPLACED IAW DWG #5912188 REV BD AND MD-90 SRM 51-30-02 AND 51-30-05 VOL.II.
- [SDR DALA2020080542718](https://openairdocs.org/sdr/DALA2020080542718), Aug 4, 2020: FRAME. CRACKED. CRACK ON FRAME STA 1458 AND LONG 1 AT AFT ACCESSORY COMPARTMENT (CAT). NRC 00251: FRAME STA 1458 AND LONG 1 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER MD-90 
- [SDR DALA2019101515905](https://openairdocs.org/sdr/DALA2019101515905), Oct 11, 2019: PIN. UNSECURE. FOUND L1 ENTRY DOOR SLIDE PACK HAD BOTH PINS FELL OUT OF SLIDE EYELETS. REMOVED AND REPLACED SLIDE PACK PER WC 2561-4641. SYS CKS OK. ACFT OK FOR SERVICE.
- [SDR DALA2019073004489](https://openairdocs.org/sdr/DALA2019073004489), Jul 29, 2019: UNKNOWN. ODOR. STRONG SMELL OF FUEL IN THE CABIN AFTER LANDING.THE SMELL IS STRONGER IN THE AFT CABIN, BUT IS STILL PRESENT UP TO THE FLAT DECK. INSPECTED A/C, APU, ENGINES, F
- [SDR DALA2019073004487](https://openairdocs.org/sdr/DALA2019073004487), Jul 27, 2019: ATTACH ANGLE. CRACKED. FOUND 2" CRACK AT STRINGER 1307 JUST LEFT OF CENTER LINE. FOUND CRACK TO BE IN FLOOR PANEL TO FORMER ATTACH ANGLE SUBSTRUCTURE. FABRICATED & INSTALLED REPAIR AN
- [SDR DALA2019061873627](https://openairdocs.org/sdr/DALA2019061873627), Jun 16, 2019: CHARGER. INOPERATIVE. DURING SVC, FOUND EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT DOOR OUT. R/R BATTERY CHARGER PER MD90 AMM 33-51, OPS CHECK GOOD.
- [SDR DALA201811206695](https://openairdocs.org/sdr/DALA201811206695), Nov 17, 2018: SKIN. DEBONDED. FOUND VERTICAL STABILIZER PANEL 370TL LEADING EDGE DISBONDING. REMOVED PANEL 370TL AND ROUTED TO COMPOSITE SHOP. REMOVED DELAMINATED MESH AND DAMAGED PAINT IN P
- [SDR DALA201811206694](https://openairdocs.org/sdr/DALA201811206694), Nov 17, 2018: TAIL CONE. LACK OF LUBE. DURING OPS CHECK OF TAIL CONE DROP, AFT ENTRY DOOR DID NOT RELEASE TAIL CONE. LUBED TAIL CONE PER MD-90 AM 53-52. OPS WILL BE DONE ON AMDS 5352-7116. ALL RII CO
- [SDR DALA2018062904274](https://openairdocs.org/sdr/DALA2018062904274), Jun 27, 2018: CABLE. BINDING. AFT VENTRAL STAIRS INOPERATIVE WILL NOT OPEN. DURING CHECKS, FOUND THE CONTROL CABLE ASSY FROM THE HANDLE BINDING IN THE OPEN DIRECTION. R & R BRACKET ASSEMBLY.
- [SDR DALA2018031701777](https://openairdocs.org/sdr/DALA2018031701777), Mar 16, 2018: BRACKET. CRACKED. DURING INSPECTION, FOUND A CRACKED BRACKET ON FWD BULKHEAD AT THE RT UPPER ENGINE THRUST REVERSER. THE BRACKET WAS REPLACED.
- [SDR DALA2018031601727](https://openairdocs.org/sdr/DALA2018031601727), Mar 15, 2018: RIB. CRACKED. CRACK ON RIB OF FIXED LEADING EDGE INTERIOR SURFACE SATA XOS 530 APROX LT WING. RIB WAS REPLACED PER SRM VOL II 51-30-02 AND 51-30-05, DWG 9919331-39 REV N.
- [SDR DALA2018031401679](https://openairdocs.org/sdr/DALA2018031401679), Mar 13, 2018: BEAM. CRACKED. CRACK RT/LT WHEEL WELL DOOR JAMB INTERNAL SKIN STA Y= 47 AT NLG. BEAM WAS REPAIRED PER SRM VOL I 53-90-01 PAR 8. (LENGHT CRACK WAS 0.500"), FOR BEAM RT WAS ISSU
- [SDR DALA2018031401678](https://openairdocs.org/sdr/DALA2018031401678), Mar 13, 2018: WEB. CRACKED. CRACK ON WEB AT STA CANT Y=1542 AND 1HRS POSITION VENT BOX LOUVERS AREA AT AFT ACCESSORY COMPARTMENT. WEB WAS REMOVED PER VOL II SRM 51-30-02 DAMAGE WAS REMOVED
- [SDR DALA2018031401677](https://openairdocs.org/sdr/DALA2018031401677), Mar 13, 2018: SKIN. CRACKED. CRACK RT WHEEL WELL DOOR JAMB INTERNAL SKIN STA Y=47 AT NLG. REPAIRED PER REV ETI-90-18-013 REV 4 AND ER/A 566722-14 REV ORIGINAL.
- [SDR DALA2018031401676](https://openairdocs.org/sdr/DALA2018031401676), Mar 13, 2018: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL STA Y= 163 PROTECTION LONG 28L AT INNER FUSELAGE STRUCTURE E&E COMPARTMENT AREA. REPLACED PER SRM VOL II 51-30-02 AND 51-30-05, DWG 991
- [SDR DALA2018031301583](https://openairdocs.org/sdr/DALA2018031301583), Mar 12, 2018: SUPPORT. CRACKED. CRACK ON INBD/OUTBD WEB SUPPORTS (2EAS) STA CANT 1542 AND 1HRS POSITION VENT BOX LOUVERS AREA AT AFT ACCESSORY COMPARTMENT. ANGLES WERE REPLACE PER VOL II SRM 5
- [SDR DALA2018031301582](https://openairdocs.org/sdr/DALA2018031301582), Mar 12, 2018: FRAME. CORRODED. CORROSION ON FRAME OF STA Y 1362 BTW LONGS 29R-26L AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2 WAS REPAIRED PER SRM VOL I 53-10-02 FIG 2.
- [SDR DALA2018031301581](https://openairdocs.org/sdr/DALA2018031301581), Mar 12, 2018: ANGLE. CRACKED. CRACK ON WEB ANGLE STA CANT 1542 AT 11 HRS POSITION AFT ACCESORY COMPARTMENT VENT BOX LOUVERS AREA. ANGLE WAS REPLACE PER VOL II SRM 51-30-05, SRM 51-30-01 AND 
- [SDR DALA2018031301580](https://openairdocs.org/sdr/DALA2018031301580), Mar 12, 2018: ANGLE. CRACKED. CRACK ON AFT ACCESORY COMPARTMENT VENT BOX LOUVER UPPER ANGLE STA CANT 1520 AND 1HRS POSITION. ANGLE WAS REPLACE PER VOL II SRM 51-30-05 AND 51-30-02.
- [SDR DALA2018031201555](https://openairdocs.org/sdr/DALA2018031201555), Mar 11, 2018: SKIN. CRACKED. CRACK ON SKIN CUTOUT ON LT AFT NLG DOOR AFT HINGE AT EXTERNAL FUSELAGE. SKIN CUTOUT ON LT AFT NLG DOOR AFT HINGE AT EXTERNAL WAS REPAIRED PER SRM VOL I 53-30-01
- [SDR DALA2018031201554](https://openairdocs.org/sdr/DALA2018031201554), Mar 11, 2018: LONGERON. CRACKED. CRACKED LONG 20 LT STA Y= 1050 AT LT MLG WHEEL WELL AREA. LONG 20 LT STA Y= 1050 WAS REPAIRED (CRACK 1") PER SRM VOL I 53-10-01 FIG 9.
- [SDR DALA2018031201553](https://openairdocs.org/sdr/DALA2018031201553), Mar 11, 2018: FITTING. CORRODED. CORROSION ON SEVERAL CLIPS FROM STA Y 1212-1269 LONG 19R AT AFT CARGO COMPARTMENT DOOR JAMB. CLIPS WERE REPLACED PER SRM VOL II 51-10-05.
- [SDR DALA2018031101551](https://openairdocs.org/sdr/DALA2018031101551), Mar 10, 2018: LONGERON. CORRODED. CORROSION LEVEL 2. CORROSION ON LONG 30 STA Y=218 AT INNER STRUCTURE E/E COMPARTMENT. LONGERON 30 BTW STA Y=160-229 WAS REPLACED PER SRM VOL II 51-30-02 AND 51-
- [SDR DALA2018031001550](https://openairdocs.org/sdr/DALA2018031001550), Mar 9, 2018: FITTING. CORRODED. CORROSION ON CLIP SUPPORT OF STA Y=1212 AT AFT CARGO COMPARTMENT. CLIP WAS REPLACED PER SRM VOL II 51-30-05 DWG 5936660 REV BZ.
- [SDR DALA2018031001549](https://openairdocs.org/sdr/DALA2018031001549), Mar 9, 2018: FITTING. CORRODED. CRACKED FITTING SUPPORT STA Y=932, X=0 AT WING CENTER SECTION KEEL BEAM AREA. FITTING WAS REPLACED PER SRM VOL II 51-30-05.
- [SDR DALA2018031001548](https://openairdocs.org/sdr/DALA2018031001548), Mar 9, 2018: DOUBLER. CRACKED. CRACKED REPAIR DOUBLER ON LOWER AFT CORNER INBD SECTION AT LH MLG INBD DOOR. THE REPAIR DOUBLER WAS REPLACED IAW SRM 52-80-02, FIG 8, SRM 51-30-01, AND 51-30-02
- [SDR DALA2018030901511](https://openairdocs.org/sdr/DALA2018030901511), Mar 8, 2018: ANGLE. CRACKED. DURING INSPECTION. A CRACKED ANGLE BS 1364, LONGERON 16R. REPLACED THE ANGLE IAW SRM 51-30-05.
- [SDR DALA2018030901510](https://openairdocs.org/sdr/DALA2018030901510), Mar 8, 2018: LONGERON. CRACKED. DURING INSPECTION. A CRACKED LONGERON 16L, BS 1364. THE AREA WAS REPAIRED IAW SRM 53-10-01, FIG 7.
- [SDR DALA2018030901508](https://openairdocs.org/sdr/DALA2018030901508), Mar 8, 2018: ANGLE. CRACKED. DURING INSPECTION. FOUND A CRACKED ANGLE BS 1046, X=5 AT THE LT MLG WHEEL WELL KEEL BEAM AREA. REPAIRED IAW SRM 53-00-01, FIG 4, VOL I.
- [SDR DALA2018030801494](https://openairdocs.org/sdr/DALA2018030801494), Mar 7, 2018: STRUCTURE. DAMAGED. DURING INSPECTION, FOUND AN ELONGATED SCREW HOLE ON THE AFT UPPER CORNER OF THE L2 DOOR. REPAIRED IAW ETI-90-18-005, REV 1 AND ERA 566537-14, REV ORIGINAL.
- [SDR DALA2018030801493](https://openairdocs.org/sdr/DALA2018030801493), Mar 7, 2018: PAN. CRACKED. DURING INSPECTION, FOUND A CRACK ON THE UPPER AFT PAN BETWEEN BS 195 & 200 AT THE L1 DOOR. THE PAN WAS REPAIRED IAW ETI-90-18-007, REV. 3 AND ERA 566290-14, REV
- [SDR DALA2018030701464](https://openairdocs.org/sdr/DALA2018030701464), Mar 6, 2018: DOOR FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND BEYOND A STOP DRILL ON THE AFT MLG DOOR FRAME AT THE RT MLG WW . REPAIRED IAW SRM VOL II 51-30-02 AND 51-30-05.
- [SDR DALA2018030701463](https://openairdocs.org/sdr/DALA2018030701463), Mar 6, 2018: WEB. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE WEB AT BS 884, BETWEEN LONGERONS 28L - 28R. THE WEB WAS REPAIRED IAW ER/A 566426-14, REV ORIG, AND ETI -90-18-003,
- [SDR DALA2018030701462](https://openairdocs.org/sdr/DALA2018030701462), Mar 5, 2018: ANGLE. CRACKED. DURING INSPECTION, FOUND A CRACKED ANGLE ON THE LT MLG DOOR FWD FRAME. THE ANGLE WAS REPLACED IAW SRM 51-30-02, AND 51-30-05.
- [SDR DALA2018030701461](https://openairdocs.org/sdr/DALA2018030701461), Mar 5, 2018: DOUBLER. CORRODED. DURING INSPECTION, FOUND CORROSION ON THE INNER PRODUCTION DOUBLER, BS 1395 BETWEEN LONGERONS 29R - 29L IN THE AFT CARGO BAY. THE DOUBLER WAS REPLACED IAW SRM 5
- [SDR DALA2018030701459](https://openairdocs.org/sdr/DALA2018030701459), Mar 5, 2018: ANGLE. CRACKED. CRACKED ANGLE IN FWD OUTBD CHANNEL ON FWD RT. THE ANGLE WAS REPLACED IAW SRM 51-30-02, AND 51-30-05.
- [SDR DALA2018030701458](https://openairdocs.org/sdr/DALA2018030701458), Mar 5, 2018: ANGLE. CRACKED. CRACKED ANGLE, BS 110, IN THE NLG W/W. THE ANGLE WAS REPLACED IAW SRM 51-30-08.
- [SDR DALA2018030501363](https://openairdocs.org/sdr/DALA2018030501363), Mar 4, 2018: FLOOR PANEL. DELAMINATED. DELAMINATION ON FLOOR PANELS NBRS 222AF, 222HG, 222LG, 222AKG, 222MF, 222RF, AND 222VF AT PAX CAB. FLOOR PANELS NBRS 222AF, 222HG, 222LG, 222AKG, 222MF, 222RF, 
- [SDR DALA2018030501362](https://openairdocs.org/sdr/DALA2018030501362), Mar 4, 2018: FLOOR PANEL. DELAMINATED. DELAMINATION ON FLOOR PANELS NBRS 221LF, 221BF, AND 221JF AT PAX CAB. FLOOR PANELS NBRS 221LF, 221BF, AND 221JF WERE REPLACED, FABRICATE AND IDENTIFIED PER MD-9
- [SDR DALA2018030501361](https://openairdocs.org/sdr/DALA2018030501361), Mar 4, 2018: FLOOR PANEL. CRACKED. CRACKS ON FLOOR PANELS NBRS 221GF, 211FG, 221PF, 211AJF 221NF, 223EF, 221QF, 222CG, 222TF AND FLOOR PANEL P/N 9981474-41 AT PAX CAB (CPAX ). FLOOR PANELS NBRS 2
- [SDR DALA2018030501360](https://openairdocs.org/sdr/DALA2018030501360), Mar 4, 2018: BRACKET. CRACKED. INITIAL INSPECTION. CRACKED HYD LINE BRACKET ON LT MLG WHEEL WELL FWD DOOR JAMB. BRACKET WAS REPLACED (CRACK 2") PER VOL II SRM 51-30-02.
- [SDR DALA2018030501359](https://openairdocs.org/sdr/DALA2018030501359), Mar 4, 2018: STIFFENER. CORRODED. CORROSION ON STIFFENER OF STA Y 1395 AND LONG 30 WAS FOUND DURING REMOVAL OF INNER PRODUCTION DOUBLER OF STA Y 1395 BTW LONGS 29R-29L. STIFFENER WAS REPLACED PE
- [SDR DALA2018030501358](https://openairdocs.org/sdr/DALA2018030501358), Mar 4, 2018: FLOOR PANEL. CORRODED. CORROSION ON FLOOR PANEL 160G FROM STA Y 160-200 AND STA X -54 TO -60 AT PAX CABIN. LEVEL CORROSION 2 FLOOR PANEL 160G FROM STA Y 160-200 AND STA X -54 TO -60 W
- [SDR DALA2018030501357](https://openairdocs.org/sdr/DALA2018030501357), Mar 4, 2018: CHANNEL. CRACKED. CRACK FWD INBD JAMB OF LT MLG DOOR WHEEL WELL. CHANNEL WAS REPLACED (CRACK 1") PER SRM VOL II 51-30-02 AND 51-30-05.
- [SDR DALA2018030301354](https://openairdocs.org/sdr/DALA2018030301354), Mar 2, 2018: SPLICE. CRACKED. CRACKED SPLICE AND CLIP ANGLE ON LT WING INTERNAL FIXED LEADING EDGE STA XFS 194. SPLICE AND CLIP WERE REPLACED PER SRM VOL II 51-30-02 AND 51-30-05 AND DWG9937
- [SDR DALA2018030301353](https://openairdocs.org/sdr/DALA2018030301353), Mar 2, 2018: PANEL SUPPORT. CRACKED. CRACKED PANEL SUPPORTS (2EAS) STA Y=1473 X=-10 AND X=10 AT AFT ACCESSORY COMPARTMENT. PANEL SUPPORTS (BRACKETS 2EAS) STA Y=1473 X=-10 AND X=10 WERE REPLACED PER
- [SDR DALA2018030301352](https://openairdocs.org/sdr/DALA2018030301352), Mar 2, 2018: ANGLE. CRACKED. CRACKED ANGLES BETWEEN BS 883, LBL 43, RBL 43, Z=-6. THE ANGLES WERE REPAIRED IAW ER/A 498192-14MA, REV A.
- [SDR DALA2018030301351](https://openairdocs.org/sdr/DALA2018030301351), Mar 2, 2018: SKIN. CRACKED. CRACKED AND LOOSE FASTENERS ON AFT BIFURCATION TRACK FAIRING SKIN OUTBOARD SIDE AT RT LOWER ENGINE THRUST REVERSER C-DUCT. DAMAGE WAS REPAIRED IAW SRM 54-30-13,
- [SDR DALA2018030301350](https://openairdocs.org/sdr/DALA2018030301350), Mar 2, 2018: WEB. CORRODED. CORROSION ON WEB BETWEEN BS 131 TO 141, RBL 30 TO 52. REPAIRED IAW. SRM 51-10-01, FIG 10.
- [SDR DALA2018030301349](https://openairdocs.org/sdr/DALA2018030301349), Mar 2, 2018: ANGLE. CRACKED. CRACKED ANGLES BETWEEN BS 962, LBL 44, RBL 44, Z=-7 LT & RT SIDE AT WING BOX AREA. THE ANGLES WERE REPLACED IAW SRM 51-30-05, AND DWG 9923417-17, REV B.

All 148: https://openairdocs.org/aircraft/N963DN/reports.md

## STCs that may be installed (OpenAirDocs) (119, 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 (Boeing MD-90-30)

- [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 ST03815AT-D](https://openairdocs.org/stc/ST03815AT-D): Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST03966AT](https://openairdocs.org/stc/ST03966AT): Lavatory refurbishment and PED power installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST04231AT](https://openairdocs.org/stc/ST04231AT): PED power installation. 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 ST01541AT-D](https://openairdocs.org/stc/ST01541AT-D): Installation of Collins DLM-900 ACARS Management unit. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [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 ST09180AC](https://openairdocs.org/stc/ST09180AC): Installation of DeVore Wing Forward Position Lights. The Boeing Company
- [STC ST09181AC](https://openairdocs.org/stc/ST09181AC): Installation of main landing gear spotlights. The Boeing Company
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST00275LA](https://openairdocs.org/stc/ST00275LA): Installation of Passenger Service Cart. 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 ST01336LA](https://openairdocs.org/stc/ST01336LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST01990LA-D](https://openairdocs.org/stc/ST01990LA-D): Installation of Overhead Stowage Bin Extension Kits. Safran Cabin Inc
- [STC ST01991LA-D](https://openairdocs.org/stc/ST01991LA-D): Interior Installations. Safran Cabin Inc
- [STC ST01998LA-D](https://openairdocs.org/stc/ST01998LA-D): Installation of Overhead Stowage Bin Kits. Safran Cabin Inc
- [STC ST02255LA](https://openairdocs.org/stc/ST02255LA): Modification and installation of Window Shades. Safran Cabin 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 ST01818CH](https://openairdocs.org/stc/ST01818CH): Installation of a Honeywell Enhanced Ground Proximity Warning 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 ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST01932AT](https://openairdocs.org/stc/ST01932AT): Installation of SAF-T-GLO Aerospace Limited's photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST02928AT](https://openairdocs.org/stc/ST02928AT): Installation of a Honeywell Enhanced Ground Proximity Warning System (EGPWS). Woven Electronics LLC
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC SA9024NM-D](https://openairdocs.org/stc/SA9024NM-D): Installation of Scandinavian Bellyloading Company, sliding carpet loading system. SBC-America LLC
- [STC ST03276AT](https://openairdocs.org/stc/ST03276AT): Installation of a Honeywell MK II Aircraft Communications Addressing and Reporting System (ACARS). Woven Electronics, LLC
- [STC ST02896AT](https://openairdocs.org/stc/ST02896AT): Installation of a Kannad Model 406-AF Emergency Locator Transmittter (ELT). Woven Electronics LLC
- [STC ST01997CH](https://openairdocs.org/stc/ST01997CH): Installation of a Honeywell RESCU 406AF emergency locator transmitter (ELT) system. Honeywell International Inc
- [STC ST03988AT](https://openairdocs.org/stc/ST03988AT): Installation of the EMTEQ LED Lights in the main cabin. Woven Electronics LLC
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST03838AT](https://openairdocs.org/stc/ST03838AT): Installation of an Universal Avionics Application Server Unit (ASU) System Class II Electronic Flight Bag (EFB). Technical Aero Services Inc
- [STC ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation
- [STC ST00491SE](https://openairdocs.org/stc/ST00491SE): Installation of the AlliedSignal Enhanced Ground Proximity Warning System. Honeywell International Inc
- [STC ST01023SE](https://openairdocs.org/stc/ST01023SE): Installation of a the TPA-81A Traffic Alert and Collision Avoidance System (TCAS) Processor in accordance with Master Drawing List 756-0119-001, Revision D, dated November 21, 2003, or later FAA approved revisions. Honeywell International Inc
- [STC ST01915AT](https://openairdocs.org/stc/ST01915AT): Installation of a RDR-4B Weather Radar/Windshear System. Honeywell International Inc
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST02541CH](https://openairdocs.org/stc/ST02541CH): Installation of an Aircell Broadband Services (ABS) System. Intelsat Inflight LLC
- [STC ST02532LA](https://openairdocs.org/stc/ST02532LA): Modify the wing fuel tanks access cover installation by replacing the existing rubstrip and seal with a new encapsulated wire mesh gasket and a new seal. Aviation Devices & Electronic Components LLC
- [STC ST02502LA](https://openairdocs.org/stc/ST02502LA): Installation of TDG Aerospace, Inc. Universal Fault Interrupter (UFI). TDG Aerospace Inc
- [STC ST04167CH](https://openairdocs.org/stc/ST04167CH): Installation of CMC CMA-5024 GLSSU units and ACSS NXT-800 Mode S Transponders. Canard Aerospace Corporation
- [STC ST04283AT](https://openairdocs.org/stc/ST04283AT): Interior Modification to add a Cart Stowage unit. Delta Air Lines Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC SA8339SW](https://openairdocs.org/stc/SA8339SW): Installation of a fuselage nose radome shell. The NORDAM Group LLC
- [STC ST01395AT-D](https://openairdocs.org/stc/ST01395AT-D): Installation of Collins DLM-700 B ACARS system installed with a Miltope Printer. HAECO Cabin Solutions LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC

All 119: https://openairdocs.org/aircraft/N963DN/stcs.md

## Related

- Other Boeing MD-90-30 aircraft: https://openairdocs.org/model/boeing-md-90-30/aircraft.md
- The IAE V2528-D5 engine: https://openairdocs.org/engine/iae-v2528-d5.md

---
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