# Douglas DC-9-14

- Type: Aircraft model (FAA registry)
- Registry code: 3022034
- Manufacturer (registry): DOUGLAS
- Model: DC-9-14
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-jet
- Seats: 85
- Weight class: 20,000 lb and over
- Cruise speed: 315 mph
- Certification: Type certificated
- Data sheet: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Holder: The Boeing Company
- Registered aircraft: 0
- Page: https://openairdocs.org/model/douglas-dc-9-14

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [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 2010-23-10](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 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 2008-11-15](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 2006-10-14](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
- [AD 2002-26-08](https://openairdocs.org/ad/2002-26-08): Emergency Power Switch Knob on the Overhead Switch Panel in the Flight Compartment · Boeing DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Feb 10, 2003
- [AD 2002-26-13](https://openairdocs.org/ad/2002-26-13): Left and right generator power relays · Boeing DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Feb 6, 2003
- [AD 2002-25-04](https://openairdocs.org/ad/2002-25-04): Circuit breakers · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Jan 17, 2003
- [AD 2002-21-09](https://openairdocs.org/ad/2002-21-09): Cockpit enclosure window sill · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Nov 29, 2002

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 245: https://openairdocs.org/model/douglas-dc-9-14/ads.md

## Information bulletins (advisory) (2)

- [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

## Registered aircraft

None registered with this model now.

## NTSB investigations (12)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA91MA010](https://openairdocs.org/ntsb/DCA91MA010), Dec 3, 1990: Mcdonnell Douglas DC-9-14 (N3313L), Romulus, MI, destroyed, 8 fatal. Probable cause: LACK OF PROPER CREW COORDN, INCLUDING VIRTUAL REVERSAL OF ROLES BY THE DC-9 PLTS, WHICH LED TO THEIR FAILURE TO STOP TAXIING & ALERT GND CTLR OF THEIR POSITIONAL UNCERTAINTY IN A TIMELY MANNER BFR &…
- [NTSB DCA88MA004](https://openairdocs.org/ntsb/DCA88MA004), Nov 15, 1987: Mcdonnell Douglas DC-9-14 (N626TX), Denver, CO, destroyed, 28 fatal
- [NTSB FTW80FA055](https://openairdocs.org/ntsb/FTW80FA055), Mar 17, 1980: Douglas DC-9 (N9103), Baton Rouge, LA, substantial damage
- [NTSB MIA79AA049](https://openairdocs.org/ntsb/MIA79AA049), Feb 9, 1979: Douglas DC-9 (N8910E), Miami, FL, destroyed
- [NTSB DCA77AA003](https://openairdocs.org/ntsb/DCA77AA003), Nov 16, 1976: Douglas DC-9 (N9104), Denver, CO, substantial damage
- [NTSB MKC75IK032](https://openairdocs.org/ntsb/MKC75IK032), Dec 19, 1974: Douglas DC-9 (N8910E), Minneapolis, MN, incident, minor damage
- [NTSB MKC74IK063](https://openairdocs.org/ntsb/MKC74IK063), Apr 20, 1974: Douglas DC-9 (N3302L), St.Louis, MO, incident, minor damage
- [NTSB IAD74II007](https://openairdocs.org/ntsb/IAD74II007), Jul 31, 1973: Douglas DC-9 (N3310L), Chattanooga, TN, incident, minor damage
- [NTSB CHI73AC100](https://openairdocs.org/ntsb/CHI73AC100), Jun 14, 1972: Douglas DC-9 (N8906E), Chicago, IL, substantial damage
- [NTSB DCA72AZ011](https://openairdocs.org/ntsb/DCA72AZ011), May 30, 1972: Douglas DC-9 (N3305L), Ft.Worth, TX, destroyed, 4 fatal
- [NTSB CHI72AC034](https://openairdocs.org/ntsb/CHI72AC034), Oct 9, 1971: Douglas DC-9 (N3308L), Chicago, IL, minor damage
- [NTSB MIA69I0080](https://openairdocs.org/ntsb/MIA69I0080), May 11, 1969: Douglas DC-9 (N8904E), St.Louis, MO, incident, minor damage

## FAA accident and incident reports (120, newest 50)

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 20020822020969I](https://openairdocs.org/incident/20020822020969I), Aug 22, 2002: Doug DC914 (N8908E), Minneapolis, MN, Minor damage. (-23) On take-off the flight crew noted an unusual buzz noise along with reports from the tower and several other aircraft of a number two engine fire. The…
- [Incident 20001006031189I](https://openairdocs.org/incident/20001006031189I), Oct 6, 2000: Doug DC914 (N500ME), Omaha, NE. (-23)Midwest express flight 527 enroute milwaukee, WI, to denver, CO, diverted to Omaha, NE, due to number one engine vibration. Company mechanics changed the…
- [Incident 19991219042079I](https://openairdocs.org/incident/19991219042079I), Dec 19, 1999: Doug DC914 (N8909E), Detroit, MI, Minor damage. (-23) At 2123 local on 12/19/99, nwa flight 1408, a DC-9 N8909E, located in the alley way between concourse c and d on spot "4" was struck from behind by an…
- [Incident 19990605025859I](https://openairdocs.org/incident/19990605025859I), Jun 5, 1999: Doug DC914 (N8912E), Cleveland, OH. There was no loss of separation.
- [Incident 19971024042129I](https://openairdocs.org/incident/19971024042129I), Oct 24, 1997: Doug DC932 (N8913E), Cleveland, OH. Narrative: on October 24, 1997, at approximately 0721, nwa 1553 crossed the 23L hold line without cle-atct clearance. PIC and SIC, both, received letters of…
- [Incident 19970126002959I](https://openairdocs.org/incident/19970126002959I), Jan 26, 1997: Doug DC914 (N800ME), Omaha, NE, Minor damage. Narrative: on Sunday, jan. 26, 1997, N800ME, a Douglas DC-9-14, operated by midwest express airlines, inc., as flight 572, experienced the loss of the retread…
- [Incident 19960329010389I](https://openairdocs.org/incident/19960329010389I), Mar 29, 1996: Doug DC914 (N8908E), Omaha, NE. Narrative: N8908E, a DC-9-1, was being operated as northwest airlines, inc., as positioning flight 9896 en-route san antonio, TX to minneapolis, MN. The crew…
- [Incident 19960116001749I](https://openairdocs.org/incident/19960116001749I), Jan 16, 1996: Doug DC914 (N400ME), Kansas City, MO. Narrative: when flt 581 departed mci the nose landing gear strut did not allow the ground shift mechanism to operate. The aircraft did not pressurize and the…
- [Incident 19951009046949I](https://openairdocs.org/incident/19951009046949I), Oct 9, 1995: Doug DC914 (N8907E), Toledo, OH. Narrative: northwest flt 1741. On 10/09/95 was climbing out of detroit (dtw) going to nashville (bna). As the auto pilot was approaching the clearance altitude…
- [Incident 19920902044769I](https://openairdocs.org/incident/19920902044769I), Sep 2, 1992: Doug DC914 (N8908E), Detroit, MI, Minor damage. Smoke and fume electrical fire in aft electrical power center generator bus bays. Removed right ac generator relay.
- [Incident 19910904043269I](https://openairdocs.org/incident/19910904043269I), Sep 4, 1991: Doug DC914 (N8908E), Covington - Cin, OH. Left generator light on when engines throttles advanced for takeoff. Returned to gate. Found bad indicating system.
- [Incident 19910514026869I](https://openairdocs.org/incident/19910514026869I), May 14, 1991: Doug DC914 (N8909E), Covington - Cin, OH. Aborted takeoff due to fuel imbalance. Continued after fuel balance obtained.
- [Incident 19910313008379I](https://openairdocs.org/incident/19910313008379I), Mar 13, 1991: Doug DC914 (N948L), Covington - Cin, OH. Pilot reported possible fuel leak. Landed safely. Later changed pacer supply and cannon plug.
- [Accident 19901203052361A](https://openairdocs.org/incident/19901203052361A), Dec 3, 1990: Doug DC914 (N3313L), Detroit, MI, Destroyed, 8 fatal. Taxiing to takeoff,became lost due fog. Stopped on active runway. Struck by departing N278US.ats coordination factor
- [Incident 19901024055889I](https://openairdocs.org/incident/19901024055889I), Oct 24, 1990: Doug DC914 (N8911E), Detroit, MI. Lost pressurization en route. Made emergency descent. Replaced outflow valve and controller.
- [Incident 19900626049829I](https://openairdocs.org/incident/19900626049829I), Jun 26, 1990: Doug DC914 (N932EA), Houston, TX. NR2 first officers window seal failed causing a decompression. Remained in pattern and landed.
- [Incident 19900626049819I](https://openairdocs.org/incident/19900626049819I), Jun 26, 1990: Doug DC914 (N932EA), Houston, TX. Flap problem in left flap inboard area. Reduced speed and returned. Made a no flap landing.
- [Incident 19900611029789I](https://openairdocs.org/incident/19900611029789I), Jun 11, 1990: Doug DC914 (N1056T), Minneapolis, MN. Section of wheel separated from aircraft while taxiing. Replaced wheel and tire.
- [Incident 19900117004089I](https://openairdocs.org/incident/19900117004089I), Jan 17, 1990: Doug DC914 (N651TX), Wichita, KS. Unsafe right gear light. Used emergency procedures. Landed safely. Position switch had loose wire.
- [Accident 19891213050369A](https://openairdocs.org/incident/19891213050369A), Dec 13, 1989: Doug DC914 (N931EA), Atlantic City, NJ, Substantial damage. Aircraft pushed back for deicing was struck on starboard elevator by boom on deicing at airport.
- [Incident 19891203063729I](https://openairdocs.org/incident/19891203063729I), Dec 3, 1989: Doug DC914 (N3308L), Detroit, MI, Minor damage. Left wing scraped runway on landing flare. Made a go around and landed. Encoutered a strong wind gust.
- [Incident 19891112062969I](https://openairdocs.org/incident/19891112062969I), Nov 12, 1989: Doug DC914 (N932EA), Atlantic City, NJ. Pilot aborted takeoff apparently due to autopressurization failure.
- [Incident 19891107061549I](https://openairdocs.org/incident/19891107061549I), Nov 7, 1989: Doug DC914 (N8908E), Worcester, MA, Minor damage. Tail cone separated from aircraft on landing. No defects noted.
- [Incident 19890406020469I](https://openairdocs.org/incident/19890406020469I), Apr 6, 1989: Doug DC914 (N700ME), Denver, CO, Minor damage. Gear door open light came on after gear extended. Landed. Had ground damage to door. Actuator had failed.
- [Incident 19881208066869I](https://openairdocs.org/incident/19881208066869I), Dec 8, 1988: Doug DC914 (N930EA), Rochester, NY. Unsafe gear light. Determined gear safe. Landed without incident. Found a loose ground wire.
- [Incident 19881204063469I](https://openairdocs.org/incident/19881204063469I), Dec 4, 1988: Doug DC914 (N930EA), Buffalo, NY. No main gear down light. Visually checked ok. Light came on just prior to touch down. Normal landing.
- [Incident 19880425021559I](https://openairdocs.org/incident/19880425021559I), Apr 25, 1988: Doug DC914 (N932EA), Rochester, NY, Minor damage. Collided with a backhoe while taxiing around construction. Airport people advised to paint temporary taxi line.
- [Incident 19880212009039I](https://openairdocs.org/incident/19880212009039I), Feb 12, 1988: Doug DC914 (N8912E), St Louis, MO. Left nose gear door failed to close on takeoff. Returned to airport. Cleaned and lubed door link and lock assembly.
- [Incident 19880105003239I](https://openairdocs.org/incident/19880105003239I), Jan 5, 1988: Doug DC914 (N655TX), Omaha, NE. On climbout the ground shift mechanism remained in ground mode position. Diverted to Omaha. Unable to correct.
- [Incident 19871104073539I](https://openairdocs.org/incident/19871104073539I), Nov 4, 1987: Doug DC914 (N8914E), Memphis, TN. Oil quanity dropped. Returned. Oil tank cap was off. Mechanic received a 3 day suspension.
- [Incident 19871028072029I](https://openairdocs.org/incident/19871028072029I), Oct 28, 1987: Doug DC914 (N8904E), Memphis, TN. Airliner evacuated after landing when tower reported smoke from right main gear. New brakes had been installed.
- [Incident 19871027073579I](https://openairdocs.org/incident/19871027073579I), Oct 27, 1987: Doug DC914 (N3309L), Memphis, TN. Oil strainer light came on after takeoff. Replaced right oil pressure differential switch.
- [Incident 19871025065739I](https://openairdocs.org/incident/19871025065739I), Oct 25, 1987: Doug DC914 (N8902E), Des Moines, IA. The nose gear initially failed to indicate down and locked. Aircraft landed safely. Downlock cannon plug cleaned.
- [Incident 19871006078919I](https://openairdocs.org/incident/19871006078919I), Oct 6, 1987: Doug DC914 (N8907E), Cedar Rapids, IA. Captain became ill during cruise. Became incapacitated. First officer took control. Ambulance met aircraft.
- [Incident 19870410028079I](https://openairdocs.org/incident/19870410028079I), Apr 10, 1987: Doug DC914 (N3308L), Memphis, TN. The engine was found to have lost 4 quarts of oil. A worn starter adapter seal was replaced.
- [Incident 19870326017329I](https://openairdocs.org/incident/19870326017329I), Mar 26, 1987: Doug DC914 (N3312L), Memphis, TN. Right engine began overheating on climb. Aircraft returned to airport. Filter to bleed valve controller blocked.
- [Incident 19870324014999I](https://openairdocs.org/incident/19870324014999I), Mar 24, 1987: Doug DC914 (N948L), Memphis, TN. Loud pop heard with gear retraction.. Returned and found nose gear door hanging. Lubricated the latch.
- [Incident 19870317025689I](https://openairdocs.org/incident/19870317025689I), Mar 17, 1987: Doug DC914 (N655TX), Houston, TX. Aircraft returned due to weather radar being inoperative and bad weather ahead.
- [Incident 19870114003449I](https://openairdocs.org/incident/19870114003449I), Jan 14, 1987: Doug DC914 (N8912E), Memphis, TN. The right main gear failed to indicate up after retraction. Aircraft returned and landed. Uplock switch failure.
- [Incident 19860910056469I](https://openairdocs.org/incident/19860910056469I), Sep 10, 1986: Doug DC914 (N626TX), Omaha, NE. Engine oil temperature light came on en route. Diverted. Found a heat valve sticking in the open position.
- [Incident 19860907053539I](https://openairdocs.org/incident/19860907053539I), Sep 7, 1986: Doug DC914 (N653TX), Denver, CO. Aircraft on approach came in close proximity to another aircraft descending. No collision avoidance maneuver.
- [Incident 19860723051109I](https://openairdocs.org/incident/19860723051109I), Jul 23, 1986: Doug DC914 (N1302T), Las Vegas, NV. Landing gear door open light remained on after takeoff. Returned. Uplock rollers on clear door loose.
- [Incident 19860708041589I](https://openairdocs.org/incident/19860708041589I), Jul 8, 1986: Doug DC914 (N652TX), Chicago, IL. Diverted due to engine vibration which varied with throttle setting. Found bird strike and ingestion in engine.
- [Incident 19860615035649I](https://openairdocs.org/incident/19860615035649I), Jun 15, 1986: Doug DC914 (N8902E), Omaha, NE. Returned after oil loss on number 2 engine. Found oil cap improperly secured.
- [Incident 19860604043999I](https://openairdocs.org/incident/19860604043999I), Jun 4, 1986: Doug DC914 (N653TX), San Antonio, TX. Pilot became ill with gastroenteritis en route. Landing made by first officer.
- [Incident 19860521022629I](https://openairdocs.org/incident/19860521022629I), May 21, 1986: Doug DC914 (N8902E), Omaha, NE. Landed safely after unsafe gear indication. Towed to parking. Found a broken wire in down and lock cannon plug.
- [Incident 19860330018909I](https://openairdocs.org/incident/19860330018909I), Mar 30, 1986: Doug DC914 (N8908E), Memphis, TN. Aborted takeoff after left engine overspeed on takeoff roll. Removed and replaced engine.
- [Incident 19860303008679I](https://openairdocs.org/incident/19860303008679I), Mar 3, 1986: Doug DC914 (N3309L), Memphis, TN. Throttle advanced itself two inches on takeoff. Other throttle was stiff. Crack in heat duct heated fuel linkage.
- [Incident 19860221012539I](https://openairdocs.org/incident/19860221012539I), Feb 21, 1986: Doug DC914 (N8903E), Detroit, MI, Minor damage. Aircraft directed forward without wing walker and wing struck a baggage cart.
- [Incident 19860127004029I](https://openairdocs.org/incident/19860127004029I), Jan 27, 1986: Doug DC914 (N8914E), Memphis, TN. Right main gear had unsafe indication. Visually checked gear down. Landed and gear pinned. Replaced micro switch.

All 120: https://openairdocs.org/model/douglas-dc-9-14/incidents.md

## Service difficulty reports (1,736, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 0401939153](https://openairdocs.org/sdr/0401939153), Oct 26, 2004: PULLEY. WORN. ON FINAL APPROACH FOR LANDING AFTER SELECTING FLAPS TO 30 DEGREES DOWN, THE CREW FELT A SLIGHT ROLL AND NOTICED THAT THE LT FLAP INDICATOR WAS AT 20 DEGREES AND
- [SDR COOSDR040041](https://openairdocs.org/sdr/COOSDR040041), Sep 24, 2004: FITTING. CRACKED. FUSELAGE NOSE LANDING GEAR WHEEL WELL RT SIDE AT Y STA 69.55-X 24 INCH -Z16 INCH FITTING (PN 49568801) WITH CRACK. (K)
- [SDR ABXA040302](https://openairdocs.org/sdr/ABXA040302), Aug 30, 2004: PAN. CORRODED. WHILE PERFORMING AN X-RAY OF THE FORWARD LOWER CARGO COMPARTMENT DOOR JAMB, FOUND THE LOWER DOOR JAMB PAN PRIOR SERVICE REWORK REPAIR CORRODED BEYOND LIMITS. RE
- [SDR 0400339155](https://openairdocs.org/sdr/0400339155), Feb 28, 2004: LINE. BROKEN. AT FL330, THE CABIN BEGAN TO CLIMB AT 500 FPM AND COULD NOT BE CORRECTED. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FT AND THEN WAS ABLE TO CLIMB BACK TO A 
- [SDR 0400099152](https://openairdocs.org/sdr/0400099152), Jan 11, 2004: LINE. LEAKING. THE RT HYDRAULIC SYSTEM FLUID QUANTITY WAS LOST DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED SAFELY AT 100 KTS AT IND. MAINTENANCE FOUND THE PRESSURE LINE O
- [SDR COOSDR030065](https://openairdocs.org/sdr/COOSDR030065), Jan 1, 2004: FLOOR SUPPORT. CRACKED. AFT AND FORWARD CARGO COMPARTMENT, FLOOR SUPPORT LATERAL ANGLES AT B/S Y:STA 351, 427, 465, AND 737 BETWEEN LONG 28L AND 28R, WITH CRACKS.
- [SDR 0302149150](https://openairdocs.org/sdr/0302149150), Dec 5, 2003: CONTROLLER. MALFUNCTIONED. DURING CLIMBOUT ON DEPARTURE, THE OUTFLOW VALVE STARTED FLUCTUATING FULL OPEN TO FULL CLOSE. AT FL240, THE AIRCRAFT LOST PRESSURIZATION ACCOMPANIED WITH MASK DE
- [SDR MWEA030442](https://openairdocs.org/sdr/MWEA030442), Nov 4, 2003: SWITCH. INTERMITTENT. INTERIOR TAIL CONE RELEASE HANDLE SWITCH IS INTERMITTENT. REMOVED AND REPLACED SWITCH.
- [SDR ABXA030443](https://openairdocs.org/sdr/ABXA030443), Oct 31, 2003: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT STRAP, ATTACH ANGLE CRACKED, FS 768 AT LONGERON 27 RIGHT. REPLACED ANGLE IAW DC-9 SRM 51-30-5.
- [SDR ABXA030442](https://openairdocs.org/sdr/ABXA030442), Oct 31, 2003: FLOOR SUPPORT. CORRODED. STA 218 FLOOR SUPPORT WAS CORRODED ABOVE LONGERON 30. REPAIRED FRAME AT FS 218, LONGERON 30 IAW DC-9 SRM 53-03.
- [SDR ABXA030441](https://openairdocs.org/sdr/ABXA030441), Oct 30, 2003: SKIN. CORRODED. RIGHT WING UPPER SKIN CORRODED AND PULLED RIVETS JUST INBOARD OF SPOILER ACTUATOR. REPLACED SECTION OF STRINGER AND SPLICE IAW DC-9 SRM 51-70-5 AND 51-30-5.
- [SDR ABXA030440](https://openairdocs.org/sdr/ABXA030440), Oct 30, 2003: FITTING. CRACKED. AFT LOWER CARGO DOOR, TRAILING EDGE NR 5 BEAM END FITTING CRACKED. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2.
- [SDR 0302039153](https://openairdocs.org/sdr/0302039153), Sep 27, 2003: RIB. CRACKED. DURING L-CHECK FOUND CRACK IN PYLON CLOSING RIB AT STATION YN 165 LT. REPAIRED PER EA 91-196348.
- [SDR MWEA030318](https://openairdocs.org/sdr/MWEA030318), Aug 18, 2003: FUEL CONTROL. MALFUNCTIONED. CREW OBSERVED THE N2 SLOWLY DROP TO 40 PERCENT. REMOVED AND REPLACED ROD END AND PERFORMED ENGINE TRIM ALL PARAMETERS NORMAL. ALSO REPLACED FUEL CONTROL.
- [SDR 0301439153](https://openairdocs.org/sdr/0301439153), Jul 31, 2003: RESERVOIR. DEFECTIVE. WHILE AT CRUISE, THE RIGHT HYDRAULIC PRESSURE LOW ANNUNCIATOR LIGHT ILLUMINATED. THE RIGHT HYDRAULIC PRESSURE AND HYDRAULIC QUANTITY INDICATORS WENT TO ZERO. CO
- [SDR 0301329156](https://openairdocs.org/sdr/0301329156), Jul 25, 2003: SKIN. CRACKED. DURING "L" CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 RBL 19. REPAIRED IAW EA 91-195858.
- [SDR 0301369156](https://openairdocs.org/sdr/0301369156), Jul 21, 2003: SKIN. CRACKED. DURING L-CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 LBL 18 TO LBL 19. REPAIRED PER EA 91-195861.
- [SDR MWEA030286](https://openairdocs.org/sdr/MWEA030286), Jul 8, 2003: STARTER. FAILED. LEFT ENGINE WOULD NOT START. REMOVED AND REPLACED LEFT STARTER.
- [SDR 0301029151](https://openairdocs.org/sdr/0301029151), May 20, 2003: SEAL. LEAKING. CLIMBING THROUGH FL 270 THE "CABIN PRESSURE" WARNING ILLUMINATED. CABIN WAS AT 10,000 AND 4.2 PSI DIFFERENTIAL WITH OUTFLOW VALVE FULLY CLOSED. BOTH PACKS WERE 
- [SDR MWEA030199](https://openairdocs.org/sdr/MWEA030199), May 1, 2003: WINDSHIELD. CRACKED. FIRST OFFICER'S WINDOW SUDDENLY CRACKED. REMOVED AND REPLACED WINDSHIELD.
- [SDR MWEA030191](https://openairdocs.org/sdr/MWEA030191), Apr 29, 2003: WIRE. ARCED. A BURNING ODOR WAS NOTICED IN THE COCKPIT AND SMOKE WAS OBSERVED COMING OUT OF THE FIRST OFFICERS MAP LIGHT AREA. FOUND GROUND WIRE TO RHEOSTAT BROKEN CAUSING W
- [SDR MWEA030143](https://openairdocs.org/sdr/MWEA030143), Mar 21, 2003: PACKING. LEAKING. EPR DROPPED DOWN TO DOWN SLIGHTLY ADVANCED THROTTLE, POWER CAME ON BACK AFTER A FEW MORE MINUTES, POWER STARTER FALLING AGAIN. REMOVED AND REPLACED RIGHT PRESSU
- [SDR MWEA030134](https://openairdocs.org/sdr/MWEA030134), Mar 9, 2003: CONTROL VALVE. INOPERATIVE. LEFT BRAKE DOES NOT WORK WITH RIGHT HYDRAULIC SYSTEM SELECTED. REMOVED AND REPLACED RIGHT WHEEL WELL BRAKE CONTROL VALVE.
- [SDR ABXA030081](https://openairdocs.org/sdr/ABXA030081), Feb 19, 2003: WIRE. BURNED. PRIMARY TRIM NR 1 CIRCUIT BREAKER TRIPPED. FOUND WIRES C104C10, C1203C10, C1202C10, C1202B10, C1203B10, C1204B10, C1213A10, C1213B10, C1211B10 BURNED. FOUND WIR
- [SDR 0204199153](https://openairdocs.org/sdr/0204199153), Dec 29, 2002: ENGINE. DAMAGED. ENGINE NR 1 FAILED AND SHUTDOWN AFTER A THRUST REDUCTION AT 17,000 FEET. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING.
- [SDR 0203899150](https://openairdocs.org/sdr/0203899150), Nov 20, 2002: SEPARATOR. CONTAMINATED. DURING CLIMB, SMOKE AND FUMES ENTERED THE CABIN WITH ASSOCIATED LAVATORY SMOKE DETECTORS ACTIVATING. AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE FOUND WATER SEPAR
- [SDR MWEA020690](https://openairdocs.org/sdr/MWEA020690), Nov 12, 2002: LONGERON. POSSIBLE CRACK AT STATION 525 LONGERON 7 RIGHT REQUIRES INTERNAL OPEN UP FOR VISUAL INSPECTION. -- FABRICATED AND INSTALL LONGERON SECTION AND REPAIR SPLICES.
- [SDR MWEA020689](https://openairdocs.org/sdr/MWEA020689), Nov 12, 2002: SHEAR TIE. CRACKED. SHEAR TIE AND DOUBLER AT STATION 840 LONGERON LEFT 14 CRACKED. -- FABRICATED AND INSTALLED FORMER.
- [SDR MWEA020687](https://openairdocs.org/sdr/MWEA020687), Nov 8, 2002: GEAR. DEFECTIVE. CREW REPORTED GEAR DOOR OPEN LIGHT STAYED ON WITH GEAR HANDLE UP. -- REMOVED AND REPLACED STIFFENER.
- [SDR MWEA020670](https://openairdocs.org/sdr/MWEA020670), Nov 8, 2002: DOUBLER. CRACKED. AFT CARGO DOOR DOUBLER AT HANDLE IS CRACKED. -- FABRICATED NEW REPAIR DOUBLER, INSTALLED NEW DOUBLER.
- [SDR MWEA020668](https://openairdocs.org/sdr/MWEA020668), Oct 31, 2002: RING. BROKEN. LANDING GEAR HANDLE WOULD NOT RETRACT. -- FOUND NOSE LANDING GEAR PISTON INNER RING BROKEN AND DAMAGED SEVERAL PARTS. REPLACED #74 RING, #75 SPACER, #77 VALVE, 
- [SDR MWEA020630](https://openairdocs.org/sdr/MWEA020630), Oct 24, 2002: LANDING GEAR. MALFUNCTIONED. CREW WAS UNABLE TO RAISE LANDING GEAR. -- FOUND TENSION ON CABLE RUN 116 A & B LOW. PERFORMED STEPS 1-5 OF ADJUSTMENT TEST, SERVICED NOSE STRUT AND REMOVED AND 
- [SDR MWEA020596](https://openairdocs.org/sdr/MWEA020596), Sep 25, 2002: FLOORBEAM. CORRODED. RIGHT LAV FLOOR BEAM AT FRAME STATION 817 HAS CORROSION AROUND 3 NUTPLATES APPROXIMATELY 24" RIGHT OF CENTER LINE. -- REMOVED DAMAGED AREA, FABRICATED, LOCATED 
- [SDR MWEA020595](https://openairdocs.org/sdr/MWEA020595), Sep 25, 2002: FRAME. CRACKED. CRACK ON FRAME AROUND FASTENER HOLE AT FRAME STATION 25 RIGHT SIDE OF NOSE WHEEL WELL AREA ABOUT 1" DOWN FROM CEILING. -- REMOVED FASTENERS, FABRICATED AND LOCA
- [SDR 0203189154](https://openairdocs.org/sdr/0203189154), Sep 22, 2002: BULKHEAD. CRACKED. During Hck in ATL, a typical crack was found in the pressure panel at sta 105 and X=35. Also, corrosion was found between x=-25 and x=-35. Repaired per EA 91-19
- [SDR MWEA020577](https://openairdocs.org/sdr/MWEA020577), Sep 20, 2002: ATTACH ANGLE. CRACKED. RIGHT SIDE OF VERTICAL TO FUSELAGE ATTACH ANGLE HAS A CRACK AT STATION 951. -- STOP DRILLED CRACK, DRILLED HOLES IN REPAIR ANGLE, INSTALLED REPAIR ANGLE, REMOVE
- [SDR MWEA020578](https://openairdocs.org/sdr/MWEA020578), Sep 20, 2002: SLIDE. DEFECTIVE. TAILCONE EMERGENCY SLIDE WILL NOT DEPLOY WHEN TAILCONE IS DROPPED USING TAILCONE SLIDE. -- REMOVED TAILCONE PANEL, ADJUSTED FORWARD HOLD DOWN STRAP ON SLIDE COV
- [SDR 0203179154](https://openairdocs.org/sdr/0203179154), Sep 13, 2002: SKIN. CRACKED. During Hck in ATL, cracks have been found on the fuselage skin at sta 503 between L17 and L18 LHS. Repaired per EA 91-190691.
- [SDR 0203169154](https://openairdocs.org/sdr/0203169154), Sep 13, 2002: SKIN. CORRODED. During an HCK in ATL, two areas of corrosion were found in the fuslage skin. Repaired per EA 91-190676.
- [SDR MWEA020541](https://openairdocs.org/sdr/MWEA020541), Sep 11, 2002: WINDOW FRAME. TOOL DAMAGE. WINDOW FRAME RETAINER FOR THE MOST FORWARD RIGHT PLUG WINDOW LOWER FORWARD CORNER HAS TOOL MARKS STATION 218 RIGHT -- BLENDED TOOL MARKS FABRICATED AND INSTALLE
- [SDR MWEA020540](https://openairdocs.org/sdr/MWEA020540), Sep 6, 2002: FLOORBOARD. CORRODED. FLOOR BOARD ATTACH FASTENER HOLES AND FORWARD EDGE LIGHTLY CORRODED ON SEAT TRACK #3 BETWEEN STATIONS 200 AND 218. -- REMOVED CORROSION, LOCATED AND DRILLED NEW
- [SDR MWEA020538](https://openairdocs.org/sdr/MWEA020538), Sep 5, 2002: FLOORBOARD. CORRODED. FLOORBOARD ATTACH FASTENERS HOLES ARE LIGHTLY CORRODED ON J-CHANNEL BETWEEN STATIONS 160 AND 200 FORWARD OF SEAT TRACK 4. REMOVED CORROSION AND INSTALLED FLOOR 
- [SDR MWEA020537](https://openairdocs.org/sdr/MWEA020537), Sep 5, 2002: ELEVATOR. CRACKED. LEFT ELEVATOR LOWER FORWARD SPAR FLANGE IS CRACKED APPROXIMATELY 2" AT STATION XE200. -- FABRICATED AND INSTALLED REPAIRED PART.
- [SDR 0203159154](https://openairdocs.org/sdr/0203159154), Sep 4, 2002: LONGERON. CRACKED. During Hck in ATL, a crack was found in the forward end of longeron 29L at staion 361 under a production splice. Repaired per EA 91-190684.
- [SDR 0202869151](https://openairdocs.org/sdr/0202869151), Sep 4, 2002: CONTROLLER. MALFUNCTIONED. LOST PRESSURIZATION AT FL290, CABIN ALTITUDE WENT TO 12,000 FEET. CREW INITIATED A RAPID DESCENT TO 10,000 FEET. MASKS DID NOT DEPLOY. AUTO PRESSURE CONTROLLER 
- [SDR ABXA020123](https://openairdocs.org/sdr/ABXA020123), Aug 23, 2002: LINK. CRACKED. NR 2 LOWER AFT LEFT THRUST REVERSER DRIVER LINK WAS CRACKED. REPLACED THE NR 2 LOWER LEFT DRIVE LINK IAW DC-9 MM 78-31-05-2-0001, NEA 7830001, TASK NEA 13435, A
- [SDR 0202789150](https://openairdocs.org/sdr/0202789150), Aug 22, 2002: ENGINE. FAILED. DURING TAKEOFF ROLL, THE RIGHT ENGINE EXPERIENCED AN UNCONTAINED FAILURE AND RELATED ENGINE FIRE. CREW ABORTED TAKEOFF AND DISCHARGED THE RIGHT ENGINE FIRE BOTT
- [SDR MWEA020513](https://openairdocs.org/sdr/MWEA020513), Aug 14, 2002: STIFFENER. CRACKED. RADIAL STIFFENER AT 5 O'CLOCK POSITION IS CRACKED AT ATTACH FASTNER LEFT ENGINE. -- REMOVED AND REPLACED STIFFENER.
- [SDR MWEA020511](https://openairdocs.org/sdr/MWEA020511), Aug 14, 2002: STIFFENER. CRACKED. RECEPTACLE UNDER RADIAL STIFFENER AT 10 O'CLOCK POSITION #6 LEFT FOUND TO BE CRACKED IN 2 PLACES. -- DRILLED UP AND INSTALLED RECEPTACLE.
- [SDR MWEA020501](https://openairdocs.org/sdr/MWEA020501), Aug 14, 2002: STIFFENER. CRACKED. AFT PRESSURE BULKHEAD RADIAL STIFFENER ON AFT SIDE AT 10 O'CLOCK POSSITION HAS A SMALL CRACK AT THE RIGHT SIDE. -- FABRICATED AND INSTALLED STIFFENER.

All 1,736: https://openairdocs.org/model/douglas-dc-9-14/reports.md

## STCs that may be installed (OpenAirDocs) (234, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [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 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 SA2130NM](https://openairdocs.org/stc/SA2130NM): Installation of the Extended spacial concept interior(ESCI) retrofit 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 ST00323SE](https://openairdocs.org/stc/ST00323SE): Installation of QB9 Interior Rebuilt. Safran Cabin Inc
- [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 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 ST03735AT](https://openairdocs.org/stc/ST03735AT): Installation of a LED Indirect Cabin Lighting System. Woven Electronics LLC
- [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 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 SA3201SO](https://openairdocs.org/stc/SA3201SO): 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 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
- [STC ST00939LA](https://openairdocs.org/stc/ST00939LA): Installation of passenger entertainment system. Burrana Inc. Lists DC-9 Series
- [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 SA2410NM](https://openairdocs.org/stc/SA2410NM): Installation of a Hughes-Avicom Audio Tape Reproducer. Burrana Inc. Lists DC-9 Series
- [STC SA4817NM](https://openairdocs.org/stc/SA4817NM): Installation of standard windshear systems. Honeywell International Inc
- [STC SA8047NM](https://openairdocs.org/stc/SA8047NM): Installation of Honeywell Digital air data computer (DADC). Honeywell International 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

All 234: https://openairdocs.org/model/douglas-dc-9-14/stcs.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Mcdonnell Douglas DC-9-14](https://openairdocs.org/model/mcdonnell-douglas-dc-9-14): 0 registered aircraft, registry code 302203F

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