# N930CE: 1969 Mcdonnell Douglas DC-9-33F

- Status: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-33F](https://openairdocs.org/model/mcdonnell-douglas-dc-9-33f) (registry code 302207C, 116 seats)
- Engine: [Pratt & Whitney JT8D-9A](https://openairdocs.org/engine/pratt-whitney-jt8d-9a) (registry code 51729)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 47363
- Year built: 1969
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 20, 2012
- Certificate issued: December 14, 2009
- Expires: January 31, 2029
- Mode S code: ACE5E0
- Registered owner: [Tatonduk Outfitters Ltd](https://openairdocs.org/faa-owner/TATONDUK%20OUTFITTERS%20LTD)
- Location: [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks)
- Owner type: Corporation
- Owner's area on the map: 64.0097° N, 144.6830° W: Placed by OpenAirDocs at the center of ZIP code 99706, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=930CE
- Page: https://openairdocs.org/aircraft/N930CE

From the FAA registry file of October 22, 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): 268 in force

### Matched by airframe (Mcdonnell Douglas DC-9-33F)

- [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 2024-20-02](https://openairdocs.org/ad/2024-20-02): Fuselage · Boeing 717-200, DC-9-11, DC-9-12 and 16 more. Effective Oct 21, 2024
- [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 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 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 2014-22-05](https://openairdocs.org/ad/2014-22-05): Fuselage · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Dec 11, 2014
- [AD 2014-22-04](https://openairdocs.org/ad/2014-22-04): Fuselage · Boeing DC-9-11, DC-9-12, DC-9-13 and 13 more. Effective Dec 11, 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 2013-25-12](https://openairdocs.org/ad/2013-25-12): Fuselage Main Bulkhead · Boeing DC-9-11, DC-9-12, DC-9-13 and 13 more. Effective Jan 31, 2014
- [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 2011-12-01](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 2011-07-04](https://openairdocs.org/ad/2011-07-04): Fuel · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective May 6, 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 2010-23-10](https://openairdocs.org/ad/2010-23-10): Wings · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective Dec 14, 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 2010-10-20](https://openairdocs.org/ad/2010-10-20): Fuel · Boeing DC-9-31, DC-9-32, DC-9-32 (VC-9C) and 8 more. Effective Jun 21, 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 2009-24-21](https://openairdocs.org/ad/2009-24-21): Landing gear · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective Jan 8, 2010
- [AD 2009-03-03](https://openairdocs.org/ad/2009-03-03): Fuel boost pump of the center tank · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective Mar 31, 2009
- [AD 2008-18-06](https://openairdocs.org/ad/2008-18-06): Tail cone slide · Protective rigid cover over the tail cone emergency evacuation… (Derlan STC ST735SO). Effective Jan 7, 2009
- [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 2008-11-15](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 2008-07-09](https://openairdocs.org/ad/2008-07-09): Auxiliary fuel tanks · Boeing 727-100 Series, 727-200 Series, 727-200F Series and 7 more. Effective May 2, 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 2006-21-06](https://openairdocs.org/ad/2006-21-06): Structural inspection revisions · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Nov 29, 2006
- [AD 2006-18-05](https://openairdocs.org/ad/2006-18-05): Disconnect panel · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective Oct 11, 2006
- [AD 2006-18-02](https://openairdocs.org/ad/2006-18-02): Replacing the clamp bases for the fuel vent pipe · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Oct 4, 2006
- [AD 2006-13-18](https://openairdocs.org/ad/2006-13-18): Bonding jumper from the boost pump volute to the fuel tank structure · Boeing DC-9-31, DC-9-32, DC-9-32F and 5 more. Effective Aug 9, 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 2006-07-08](https://openairdocs.org/ad/2006-07-08): Main fuselage frame · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective May 5, 2006
- [AD 2006-06-04](https://openairdocs.org/ad/2006-06-04): Main landing gear (MLG) · Boeing DC-9-11, DC-9-12, DC-9-13 and 17 more. Effective Apr 20, 2006
- [AD 2006-01-02](https://openairdocs.org/ad/2006-01-02): Upper lock link assembly of the nose landing gear (NLG) · Boeing DC-9-14, DC-9-15, DC-9-15F and 18 more. Effective Feb 22, 2006
- [AD 2005-13-18](https://openairdocs.org/ad/2005-13-18): Battery terminal screws · Boeing DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Aug 1, 2005
- [AD 2005-07-18](https://openairdocs.org/ad/2005-07-18): Cargo configuration · Class E cargo compartment and pallet system (Aeronautical Engineers STC SA1993SO). Effective May 11, 2005
- [AD 2005-07-03](https://openairdocs.org/ad/2005-07-03): Rear spar of the left and right wings · Boeing DC-9-11, DC-9-12, DC-9-13 and 17 more. Effective May 4, 2005
- [AD 2004-25-14](https://openairdocs.org/ad/2004-25-14): Main landing gear (MLG) · Boeing DC-9-14, DC-9-15, DC-9-15F and 17 more. Effective Jan 20, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-18-11](https://openairdocs.org/ad/2004-18-11): Outboard idler hinge fitting of the left and right wing · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective Oct 13, 2004
- [AD 2004-07-05](https://openairdocs.org/ad/2004-07-05): Engine Pylon Aft Upper Spar Straps (Caps) · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective May 5, 2004
- [AD 2004-07-04](https://openairdocs.org/ad/2004-07-04): Ballast transformers · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective May 5, 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 2003-03-15 R1](https://openairdocs.org/ad/2003-03-15-R1): Airplane Flight Manual (AFM) - oxygen masks · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 90 more. Effective Dec 22, 2003
- [AD 2003-17-07 R1](https://openairdocs.org/ad/2003-17-07-R1): Auxiliary power unit (APU) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 57 more. Effective Sep 24, 2003
- [AD 2003-09-07](https://openairdocs.org/ad/2003-09-07): Left and right main landing gear (MLG) · Boeing DC-9-14, DC-9-15, DC-9-15F and 17 more. Effective Jun 5, 2003
- [AD 2002-26-10](https://openairdocs.org/ad/2002-26-10): Corners of the Forward Lower Cargo Doorjamb · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Feb 10, 2003

### Matched by engine (Pratt & Whitney JT8D-9A)

- [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 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 2005-17-16](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 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 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 99-01-08](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 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 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 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 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 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 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 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 2005-19-08](https://openairdocs.org/ad/2005-19-08) (historical): Main landing gear (MLG) shock strut cylinder · McDonnell Douglas DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective Oct 21, 2005
- [AD 2004-23-11](https://openairdocs.org/ad/2004-23-11) (historical): Center wing rear spar · Boeing DC-9-14, DC-9-15, DC-9-21 and 11 more. Effective Dec 20, 2004
- [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 2003-03-08](https://openairdocs.org/ad/2003-03-08) (historical): Eletrical connectors · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Mar 7, 2003
- [AD 2001-26-24](https://openairdocs.org/ad/2001-26-24) (historical): Transformer Ballast Assembly · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 14 more. Effective Feb 8, 2002
- [AD 2001-24-15](https://openairdocs.org/ad/2001-24-15) (historical): Chafing of the Wiring of the Attendants' Work Light of the Aft Cabin · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 13 more. Effective Jan 16, 2002
- [AD 98-26-09](https://openairdocs.org/ad/98-26-09) (historical): Fatigue Cracking In Doorstops And Doorjamb · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Jan 22, 1999
- [AD 98-08-24](https://openairdocs.org/ad/98-08-24) (historical): Fuselage Skin Or Doubler · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective May 22, 1998
- [AD 96-21-01](https://openairdocs.org/ad/96-21-01) (historical): Main Landing Gear Hydraulic Damper Assembly · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Nov 14, 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 96-13-03](https://openairdocs.org/ad/96-13-03) (historical): Structural Integrity · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Jul 24, 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 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 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 94-03-01](https://openairdocs.org/ad/94-03-01) (historical): Maintenance Inspection Program · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Mar 14, 1994
- [AD 93-13-07](https://openairdocs.org/ad/93-13-07) (historical): Install Water Drain System · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 17 more. Effective Aug 18, 1993
- [AD 92-27-07](https://openairdocs.org/ad/92-27-07) (historical): Rudder Pedals Adjuster Hub Assembly · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Jan 22, 1993
- [AD 87-14-07 R1](https://openairdocs.org/ad/87-14-07-R1) (historical): Maintenance Inspection Program · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Dec 23, 1988
- [AD 77-14-19](https://openairdocs.org/ad/77-14-19) (historical): Engine Pylon · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Aug 23, 1977

All 293: https://openairdocs.org/aircraft/N930CE/ads.md

## Information bulletins (advisory) (2 in force)

- [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

## NTSB investigations

None matched to N930CE.

## FAA accident and incident reports

None matched to N930CE.

## Service difficulty reports (45)

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 FXGA2018062700001](https://openairdocs.org/sdr/FXGA2018062700001), Jun 25, 2018: DOWNLOCK SWITCH. WORN. GEAR DOWN FOR LANDING AT PANC, NO GEAR SAFE INDICATION FOR RIGHT MAIN GEAR.
- [SDR FXGA201711211720](https://openairdocs.org/sdr/FXGA201711211720), Nov 21, 2017: FITTING. CRACKED. FITTING AT BS 351 LONGERON 32L CRACKED. REPLACED THE DAMAGED FITTING IAW EA 25-2017-138
- [SDR FXGA20170215001](https://openairdocs.org/sdr/FXGA20170215001), Feb 11, 2017: POSITION SWITCH. STICKING. DURING GEAR RETRACTION, GEAR DOOR OPEN LIGHT AND GEAR RED UNSAFE LIGHTS FOR LEFT AND RIGHT MAIN GEAR ILLUMINATED WITH GEAR HANDLE IN UP POSITION.
- [SDR FXGA201610261638](https://openairdocs.org/sdr/FXGA201610261638), Oct 26, 2016: SKIN. CRACKED. REPAIR OF CRACKS IN FUSELAGE SKIN FS 102.5 BELOW STRINGER R18. REPAIR CRACKS EXTENDING FROM RIVETS IN SKIN AT FS 102.5 STRUCTURAL REPAIR MANUAL 53-01 FIGURE 4 (
- [SDR FXGA201610261637](https://openairdocs.org/sdr/FXGA201610261637), Oct 25, 2016: STRUCTURE. CRACKED. REPAIR OF 4" CRACK IN FUSELAGE TAIL STA 1205 RT 3 O-CLOCK POSITION. MAJOR REPAIR OF CRACK PER SRM REFERENCE SRM 53-01 FIGURE 4.
- [SDR FXGA201610240001](https://openairdocs.org/sdr/FXGA201610240001), Oct 24, 2016: SUPPORT BRACKET. CRACKED. RIGHT FLAP I/B ACTUATOR SUPPORT BRACKET CRACKED.
- [SDR FXGA20160128001](https://openairdocs.org/sdr/FXGA20160128001), Jan 27, 2016: STRUT. LOW PRESSURE. AFTER TAKEOFF COULD NOT RETRACT GEAR, HANDLE WOULD NOT MOVE TO UP POSITION. THE CAUSE WAS THE NLG STRUT WAS LOW ON PRESS.
- [SDR FXGA201505061516](https://openairdocs.org/sdr/FXGA201505061516), May 6, 2015: FRAME. CRACKED. FRAME REPAIR, STATION 389, LONGERON 12R - 14R. MAJOR REPAIR. FUSELAGE FRAME INBD FLANGE CRACKED AT STATION 389 BETWEEN LONGERON 12R & 14R.
- [SDR FXGA201505061515](https://openairdocs.org/sdr/FXGA201505061515), May 6, 2015: FRAME. CORRODED. FRAME REPAIR STA 180, L-28L TO L-28R. MAJOR REPAIR. FUSELAGE FRAME LOWER FLANGE CORRODED AT STATION 180 BTWN LONGERON 28 LEFT AND LONGERON 28 RIGHT.
- [SDR FXGA201505061517](https://openairdocs.org/sdr/FXGA201505061517), May 6, 2015: SKIN. DAMAGED. LIGHTNING STRIKE REPAIR FUSELAGE SKIN BETWEEN STATION 101 - 110, LONGERON 17L & 18L. MAJOR REPAIR. TWO EACH LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN.
- [SDR FXGA201505061518](https://openairdocs.org/sdr/FXGA201505061518), May 6, 2015: SKIN. DAMAGED. LIGHTNING STRIKE REPAIR FUSELAGE SKIN BETWEEN STATION 83.550 - 89.050, LONGERON 16R & 17R. MAJOR REPAIR, 3 EACH LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN.
- [SDR 7AHR2015043000420](https://openairdocs.org/sdr/7AHR2015043000420), Apr 30, 2015: FRAME. CRACKED. FRAME AT BS 389 BETWEEN LONGERONS 12 - 14R IS CRACKED. REPAIRED SECTION OF FRAME IAW SRM 53-03, FIG 4.
- [SDR 7AHR2015043000371](https://openairdocs.org/sdr/7AHR2015043000371), Apr 30, 2015: FRAME. CORRODED. E & E BAY BILGE AREA FLOOR FRAME HAS CORRISON FROM LONGERON 28L-28R STA 180. R & R SECTION OF FRAME, STA 180, LONGERON 28L-28R IAW SRM 53-03, FIG 5.
- [SDR 7AHR2015043000346](https://openairdocs.org/sdr/7AHR2015043000346), Apr 30, 2015: SEAT TRACK. CORRODED. LIGHT SURFACE CORROSION ON SEAT TRACK, FLOOR ATTACHMENT AREAS IN VARIOUS LOCATIONS IN PASSENGER CABIN, STA 160-996, RBL5435 TO LBL 54.5. REMOVED LIGHT CORROSION
- [SDR 7AHR2015043000203](https://openairdocs.org/sdr/7AHR2015043000203), Apr 30, 2015: MOUNT. CRACKED. RT INBD SPOILER CONTROL MOUNT BRACKET CRACKED ON REAR SPAR. INSTALLED A REPAIR TO MOUNT BRACKET IAW SRM 51-10-3A, 51-30-2,51-10-2, 51-10-4 AND 51-30-5.
- [SDR 7AHR2015043000138](https://openairdocs.org/sdr/7AHR2015043000138), Apr 30, 2015: FITTING. CRACKED. WING TO FUSELAGE FITTING CRACKED LT SIDE BS 600, LONGERON 22L. R & R THE FITTING IAW SRM 51-30-1, 51-10-02, 51-10-4, 5110-2 AND 57-31-4.
- [SDR 7AHR2015043000137](https://openairdocs.org/sdr/7AHR2015043000137), Apr 30, 2015: FITTING. CRACKED. RIGHT WING TO FUSELAGE FITTING IS CRACKED AT BS 600-LONGERON 22R. R & R THE FITTING IAW SRM 51-30-5, PGS 12-14, 51-30-01,51-10-4.51-10-2 AND 57-31-4.
- [SDR 7AHR2015043000122](https://openairdocs.org/sdr/7AHR2015043000122), Apr 30, 2015: CARGO TRACK. CORRODED. FORWARD LOWER CARGO COMPARTMENT CARGO TRACK SUPPORT HAS CORROSION FROM BS 427-513, RBL 14. REMOVED CORROSION FROM AREA. TRACK SUPPORT CHANNEL AND UPPER SUPPORT 
- [SDR 7AHR2015043000110](https://openairdocs.org/sdr/7AHR2015043000110), Apr 29, 2015: ATTACH ANGLE. CRACKED. RIGHT PLYON LOWER ATTACH ANGLE CRACKED AT 996. INSTALLED NEW SECTION OF RT PYLON LOWER ATTACH ANGLE IAW SRM 54-04, FIG 10.
- [SDR FXGA20131023001](https://openairdocs.org/sdr/FXGA20131023001), Oct 19, 2013: SKIN. DAMAGED. AIRCRAFT WAS STRUCK BY LIGHTNING DURING CLIMB. NO ABNORMAL INDICATIONS AFTER STRIKE. COMPLIED WITH LIGHTNING STRIKE INSPECTION PROCEDURES, IAW EAC POLICIES AND 
- [SDR EE4Y201303270045](https://openairdocs.org/sdr/EE4Y201303270045), Mar 27, 2013: FRAME. DAMAGED. AFT CARGO COMPARTMENT BS 889 BETWEEN L27 AND 28L FRAME WITH AN ELONGATE HOLE. REPAIRED IAW SRM 53-03 PARA 1C, FIG 2A.
- [SDR EE4Y201303270042](https://openairdocs.org/sdr/EE4Y201303270042), Mar 27, 2013: SHEAR TIE. CRACKED. UPPER FUSELAGE, CARGO CABIN, AT BS 945 BETWEEN L15 TO 16R FRAME SHEAR TIE CRACKED. REPLACED SHEAR TIE IAW SRM 51-01, PARA 2D.
- [SDR EE4Y201303270041](https://openairdocs.org/sdr/EE4Y201303270041), Mar 27, 2013: BULKHEAD. CORRODED. LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 996 L23L AFT PRESSURE BULKHEAD WEB CORRODED. REPAIRED PRESSURE BULKHEAD WEB SECTION IAW SRM 53-03 PARA 17, FIG 23.
- [SDR EE4Y201303270038](https://openairdocs.org/sdr/EE4Y201303270038), Mar 27, 2013: SKIN. DENTED. LOWER FUSELAGE BS 248.5 BETWEEN L19 AND 20L SKIN DENTED. REPAIRED SKIN IAW SRM 53-01, FIG 1.
- [SDR EE4Y2013032700037](https://openairdocs.org/sdr/EE4Y2013032700037), Mar 27, 2013: TEE FITTING. CRACKED. UPPER FUSELAGE AFT PRESSURE BULKHEAD TEE BETWEEN L15 AND 17L, AT Z=14 AND Z=24 TEE CRACKED. REPLACED PRESSURE BULKHEAD TEE SECTION IAW S/B A53-232 ACCOMPLISHMEN
- [SDR EE4Y2013032700036](https://openairdocs.org/sdr/EE4Y2013032700036), Mar 27, 2013: FRAME. CRACKED. CARGO CABIN AT BS 813, L17R, FRAME WEB WITH CRACK. REPAIRED CARGO CABIN FRAME SECTION BS 813 BETWEEN L16 AND 18R DUE TO CRACK IAW SRM 53-03, FIG 32, PARA 26.
- [SDR EE4Y2013032700035](https://openairdocs.org/sdr/EE4Y2013032700035), Mar 27, 2013: FITTING. CRACKED. LOWER FUSELAGE, AFT CARGO COMPARTMENT DOOR AT BEAM NR 5, AFT BEAM END CRACKED. REPLACED NR 5 DOOR BEAM END FITTING IAW S/B DC-9-52-189 ACOMPLISMENT INSTRUCTIONS
- [SDR EE4Y2013032700034](https://openairdocs.org/sdr/EE4Y2013032700034), Mar 27, 2013: FITTING. CRACKED. LOWER FUSELAGE, AFT CARGO COMPARTMENT DOOR AT BEAM NR 3, FWD BEAM END CRACKED. REPLACED NR 3 DOOR BEAM END FITTING IAW S/B DC-9-52-189 ACOMPLISMENT INSTRUCTIONS
- [SDR EE4Y2013032700033](https://openairdocs.org/sdr/EE4Y2013032700033), Mar 27, 2013: FITTING. CRACKED. LOWER FUSELAGE, AFT CARGO COMPARTMENT DOOR AT BEAM NR 1, FWD BEAM END CRACKED. REPLACED DOOR BEAM FITTING IAW S/B DC-9-52-189 ACOMPLISMENT INSTRUCTIONS, WORK IN
- [SDR EE4Y2013032700032](https://openairdocs.org/sdr/EE4Y2013032700032), Mar 27, 2013: FITTING. CRACKED. LOWER FUSELAGE, AFT CARGO COMPARTMENT DOOR AT BEAM NR 2, AFT BEAM END CRACKED. REPLACED NR 2 DOOR BEAM IAW S/B DC-952-189 ACOMPLISMENT INSTRUCTIONS, WORK INSTRU
- [SDR EE4Y201303270040](https://openairdocs.org/sdr/EE4Y201303270040), Mar 26, 2013: FITTING. CRACKED. LOWER FUSELAGE FWD CARGO COMPARTMENT, BS 237, ON L24R, FRAME AREA AFT FITTING CRACKED. REPLACED, FRAME FITTING IAW SRM 51-01 PARA 2D.
- [SDR EE4Y2013032000031](https://openairdocs.org/sdr/EE4Y2013032000031), Mar 26, 2013: ACOUSTIC LINER. DELAMINATED. ENGINE NR 1 NOSE COWL ACOUSTIC INNER BARREL INNER SKIN WITH DELAMINATION. THE MENTION DAMAGE WAS REPAIRED UNDER NRI A1B089 4-3 AND EO# COO-CMP9-54-035-13.
- [SDR EE4Y2013032000025](https://openairdocs.org/sdr/EE4Y2013032000025), Mar 22, 2013: FITTING. BROKEN. DURING THE STRUCTURAL INSPECTION WAS FOUND ON FWD CARGO COMPARMENT STA 237, LONG 24 LEFT FITTING CRACKED. THE MENTIONED FITTING WAS REPLACED PER SRM GUIDELINES.
- [SDR EE4Y2013032000024](https://openairdocs.org/sdr/EE4Y2013032000024), Mar 22, 2013: FITTING. BROKEN. DURING THE STRUCTURAL INSPECTION WAS FOUND ON FWD CARGO COMPARTMENT STA 256, LONG 24 LEFT FITTING CRACKED. THE MENTIONED FITTING WAS REPLACED PER SRM GUIDELINES
- [SDR EE4Y2013032000023](https://openairdocs.org/sdr/EE4Y2013032000023), Mar 20, 2013: FITTING. CRACKED. DURING THE STRUCTURAL INSPECTION WAS FOUND ON FWD CARGO COMPARTMENT STA 256, LONG 24 RIGHT FITTING CRACKED. THE MENTIONED FITTING WAS REPLACED PER SRM GUIDELINE
- [SDR EE4Y2013032000022](https://openairdocs.org/sdr/EE4Y2013032000022), Mar 20, 2013: FITTING. CRACKED. DURING THE STRUCTURAL INSPECTION WAS FOUND ON FWD CARGO COMPARTMENT STA 237, LONG 24 RIGHT FITTING CRACKED. THE MENTIONED FITTING WAS REPLACED PER SRM GUIDELINE
- [SDR EE4Y201303270043](https://openairdocs.org/sdr/EE4Y201303270043), Mar 18, 2013: SKIN. CRACKED. UPPER AFT FUSELAGE BS 1038 LONGERON 14 LT SIDE SKIN CRACKED. REPAIRED IAW SRM 53-04 FIG 18.
- [SDR EE4Y2013031500020](https://openairdocs.org/sdr/EE4Y2013031500020), Mar 15, 2013: FITTING. CRACKED. DURING THE STRUCTURAL INSPECTION, "C1" SERVICE ON RT WING FRON SPAR SECTION AT XRS 204, FITTING CRACKED. THE FITTING WAS REPLACED IAW SRM GUIDELINES UNDER W/O A
- [SDR EE4Y201303270044](https://openairdocs.org/sdr/EE4Y201303270044), Mar 13, 2013: SKIN. CRACKED. UPPER AFT FUSELAGE BS 1038 L14R SKIN CRACKED. REPAIRED SKIN SECTION IAW SRM 53-04, FIG 18.
- [SDR EE4Y2013032600029](https://openairdocs.org/sdr/EE4Y2013032600029), Mar 10, 2013: ANGLE. CRACKED. LOWER FUSELAGE AFT CARGO COMPARTMENT, BS 869 BETWEEN LONGERON 28-30L FRAME AREA, TITANIUM ANGLE WITH CRACK. DAMAGED ANGLE WAS REPAIRED IAW EO COO-9-53-039-13.
- [SDR EE4Y2013032200028](https://openairdocs.org/sdr/EE4Y2013032200028), Mar 10, 2013: ANGLE. CRACKED. LOWER FUSELAGE AFT CARGO COMPARTMENT BS 889, BETWEEN LONGERON 28-29L, FRAME AREA TITANIUM ANGLE WITH CRACK. DAMAGED ANGLE WAS REPAIRED IAW THE EO COO-9-53-039-1
- [SDR EE4Y2013032600030](https://openairdocs.org/sdr/EE4Y2013032600030), Mar 9, 2013: ANGLE. CRACKED. LOWER FUSELAGE FWD CARGO COMPARTMENT, STA Y:427, BETWEEN LONGERON 24-26L FRAME AREA, TITANIUM ANGLE WITH CRACK. DAMAGED ANGLE WAS REPAIRED IAW E/O COO-9-53-039-
- [SDR EE4Y2013032600027](https://openairdocs.org/sdr/EE4Y2013032600027), Mar 9, 2013: ANGLE. CRACKED. LOWER FUSELAGE FWD CARGO COMPARTMENT, BS 332 BETWEEN LONGERON 28R AND 28L FRAME AREA, STEEL ANGLE WITH CRACK. DAMAGED ANGLE WAS REPAIRED IAW THE EO COO-9-53-039
- [SDR EE4Y2013032600026](https://openairdocs.org/sdr/EE4Y2013032600026), Mar 9, 2013: FRAME. CRACKED. LOWER FUSELAGE FWD CARGO COMPARTMENT, BS 332, BETWEEN LONGERON 28R AND 28L, FRAME AREA, TITANIUM ANGLE WITH CRACK. DAMAGED ANGLE WAS REPAIRED IAW EO COO-9-53-03
- [SDR FXGA201204251229](https://openairdocs.org/sdr/FXGA201204251229), Apr 25, 2012: FRAME. GOUGED. FWD CARGO DOOR FRAME WEB REPAIR AT FS 435, GOUGE APPROXIMATELY 2 INCHES ABOVE LONGERON L15 AT FS 435. REMOVE DAMAGE & FABRICATE FILLER FROM MATERIAL SAME AS PAR

## STCs that may be installed (OpenAirDocs) (270, 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-9-33F)

- [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 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 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 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 SA2040NM](https://openairdocs.org/stc/SA2040NM): Installation of closet and windscreen. Safran Cabin Inc
- [STC SA2134NM](https://openairdocs.org/stc/SA2134NM): Installation of a Contemporary Deep Rack Interior (CDRI) Modification Kit. 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 ST01336LA](https://openairdocs.org/stc/ST01336LA): Installation of a reinforced cockpit door. 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 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 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 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 ST02876AT](https://openairdocs.org/stc/ST02876AT): Installation of a Free Flight Model 2101 I/O Approach Plus Global Positioning System (GPS), Universal Model MFD 640 Multi-function Display (MFD), and Provisions for an Aviation Communication & Surveillance Systems (ACSS) Terrain & Traffic Collision Avoidance System (TTCAS). Woven Electronics, LLC
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST02896AT](https://openairdocs.org/stc/ST02896AT): Installation of a Kannad Model 406-AF Emergency Locator Transmittter (ELT). Woven Electronics LLC
- [STC ST11384DS](https://openairdocs.org/stc/ST11384DS): Installation of a Universal Avionics Systems Corporation UNS‐1Lw SBAS Flight Management System with LPV Approach. Aircraft Systems and Manufacturing, Inc
- [STC SA2534SW-D](https://openairdocs.org/stc/SA2534SW-D): Replacement of Switch assembly Int'l Inflatables Co. P/N 68748, with DME Corp. P/N L-140 in emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-9 Series
- [STC SA2539SW-D](https://openairdocs.org/stc/SA2539SW-D): Replacement of light assembly, International Inflatables Co. P/N68555-1 with DME Corp. EL-104, EL-104A, and EL-104B in emergency slide lighting system. Astronics Luminescent Systems Inc. Lists DC-9 Series
- [STC SA863EA](https://openairdocs.org/stc/SA863EA): Incorporation of DME Corporation emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-9 Series
- [STC ST02580AT](https://openairdocs.org/stc/ST02580AT): Lithium cell battery pack to replace currently approved alkaline battery pack used in escape slide emergency light system. Astronics Luminescent Systems Inc
- [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 SA1220NW](https://openairdocs.org/stc/SA1220NW): Installation of Universal flight data recorder. Honeywell International Inc
- [STC SA3173SO](https://openairdocs.org/stc/SA3173SO): Installation of the Mark-VII ground proximity and windshear warning system. Honeywell International Inc
- [STC SA5920NM](https://openairdocs.org/stc/SA5920NM): Installation of 980-4100-HQUS Flight Data Recorder and Penny and Giles Quick Access Recorder in accordance with Document 755-3024, Rev. New-1, or later FAA approved revision. Honeywell International Inc
- [STC ST00074AT](https://openairdocs.org/stc/ST00074AT): Installation of a Bendix/King Mode S transponder. Honeywell International Inc
- [STC ST00075AT](https://openairdocs.org/stc/ST00075AT): Installation of a CAS-81 TCAS II. Honeywell International Inc
- [STC ST00136AT](https://openairdocs.org/stc/ST00136AT): Installation of a Bendix/King CAS-81 and TRA-67 Mode S trannsponder. Honeywell International Inc
- [STC ST00701AT](https://openairdocs.org/stc/ST00701AT): Installation of the RDR-4B weather radar/windshear system. Honeywell International Inc
- [STC ST02555AK](https://openairdocs.org/stc/ST02555AK): Installation of three 1800 gallon Boeing bulk liquid tanks. Everts Air Cargo
- [STC ST01828AT](https://openairdocs.org/stc/ST01828AT): Installation of a RTA-83A VHF Communication System. Honeywell International Inc
- [STC SA3748SW](https://openairdocs.org/stc/SA3748SW): Installation of heat exchanger assembly (P/N 184060). Honeywell International Inc
- [STC SA4398SW](https://openairdocs.org/stc/SA4398SW): Modification of air to air heat exchanger (P/N 179450-2-2 or194110-1). Honeywell International Inc. Lists DC-9 Series
- [STC SA640NW](https://openairdocs.org/stc/SA640NW): Installation of contemporary deep rack interior. Safran Cabin Inc. Lists DC-9 Series
- [STC ST00939LA](https://openairdocs.org/stc/ST00939LA): Installation of passenger entertainment system. Burrana Inc. Lists DC-9 Series
- [STC ST04450AT](https://openairdocs.org/stc/ST04450AT): Installation of the dual Rockwell Collins TPR-901, ADS-B out capable trasnponder system and dual GPS-4000S position sensor. Avionics Support Group Inc

All 270: https://openairdocs.org/aircraft/N930CE/stcs.md

## Related

- Other Mcdonnell Douglas DC-9-33F aircraft: https://openairdocs.org/model/mcdonnell-douglas-dc-9-33f/aircraft.md
- The Pratt & Whitney JT8D-9A engine: https://openairdocs.org/engine/pratt-whitney-jt8d-9a.md

---
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