# Mcdonnell Douglas DC-9-14

- Type: Aircraft model (FAA registry)
- Registry code: 302203F
- Manufacturer (registry): MCDONNELL DOUGLAS
- Model: DC-9-14
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-jet
- Seats: 116
- 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/mcdonnell-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/mcdonnell-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 (2)

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 CHI99IA115](https://openairdocs.org/ntsb/CHI99IA115), Mar 22, 1999: McDonnell Douglas DC-9-14 (N600ME), Grand Rapids, MI, incident, no damage. Probable cause: the frozen elevator control. Factors were the rain and the low temperatures.
- [NTSB CHI66A0074](https://openairdocs.org/ntsb/CHI66A0074), Mar 4, 1966: Douglas DC-9 (N3307L), Chicago, IL, no damage

## 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 19870105027729I](https://openairdocs.org/incident/19870105027729I), Jan 5, 1987: Doug DC914 (N600ME), Milwaukee, WI, Minor damage. During taxi into gate the left wing struck a baggage cart.

## 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/mcdonnell-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/mcdonnell-douglas-dc-9-14/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [9143FR-0325](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172200643320260909221022.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156729354220260909220955.0001): Sealing. 3M Aerospace · PMA PQ04414CE · Jul 7, 2026
- [9143FR-0315](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148776985720260909221013.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133606371820260909221004.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116339893920260909220945.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [AF300P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191275281320260717175324.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [AF302](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178154048320260717175326.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [AF300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172513122320260717175322.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [BACC45FN10-5S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155883645320260309212952.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN10-5S · Mar 7, 2026
- [M840105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154219509420260325172403.0001): Cylinder Assembly. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 840105 · Feb 17, 2026
- [M840105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140279722720260325180521.0001): Cylinder Assembly. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 840105 · Feb 17, 2026
- [A-S00098-17-17](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194600114720250916230001.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-17 · Sep 4, 2025
- [A-S00098-17-28](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183387928020250916225959.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-28 · Sep 4, 2025
- [A-S00098-17-82](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178150711620250916225956.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-82 · Sep 4, 2025
- [A-S00098-17-56](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169059195520250916225957.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-56 · Sep 4, 2025
- [A-S00098-16-40](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163281662820250916230005.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-16-40 · Sep 4, 2025
- [A-S00098-17-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155939207320250916230002.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-15 · Sep 4, 2025
- [A-S00098-17-40](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151212392420250916225958.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-40 · Sep 4, 2025
- [A-S00098-17-32](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148670543720250916225958.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-32 · Sep 4, 2025
- [A-S00098-17-52](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146919696220250916225957.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-52 · Sep 4, 2025
- [A-S00098-17-14](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146626669720250916230003.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-14 · Sep 4, 2025
- [A-S00098-17-55](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144525750920250916225957.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-55 · Sep 4, 2025
- [A-S00098-16-88](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127745934020250916230005.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-16-88 · Sep 4, 2025
- [A-S00098-16-94](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126984954620250916230004.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-16-94 · Sep 4, 2025
- [A-S00098-17-20](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123664054720250916230000.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-20 · Sep 4, 2025
- [A-S00098-17-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120361780420250916230004.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-7 · Sep 4, 2025
- [A-S00098-17-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120191287520250916230003.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-11 · Sep 4, 2025
- [A-S00098-17-94](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114736246220250916225956.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-94 · Sep 4, 2025
- [A-S00098-17-49](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110938953520250916225958.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-49 · Sep 4, 2025
- [A-S00098-17-96](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106281629520250916225955.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-96 · Sep 4, 2025
- [A-S00098-17-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104560208820250916230004.0001): Spacer-Insulation. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces S00098-17-10 · Sep 4, 2025
- [A-AA10061-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119151046320250825130754.0001): Scratch Pane Assembly. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces AA10061-7 · Aug 21, 2025
- [A-5614398-503C2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191270002120250820141251.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-509 · Aug 18, 2025
- [A-5614398-1C2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190276152120250820141248.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-1 · Aug 18, 2025
- [A-5614398-1G2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188020277020250820141249.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-1 · Aug 18, 2025
- [A-5614398-503G2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186460274120250820141252.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-509 · Aug 18, 2025
- [A-5614398-503G1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184978315920250820141251.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-503 · Aug 18, 2025
- [A-5614398-1C2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174731589420250820141248.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-501 · Aug 18, 2025
- [A-5614398-1G1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172191582220250820141247.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-1 · Aug 18, 2025
- [A-5614398-503B1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168261527020250820141250.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-509 · Aug 18, 2025
- [A-5614398-1B1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165969579420250820141247.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-505 · Aug 18, 2025
- [A-5614398-503B1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163616718420250820141250.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-503 · Aug 18, 2025
- [A-5614398-503C2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163466275920250820141251.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-503 · Aug 18, 2025
- [A-5614398-1G1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160713830320250820141248.0001): Pane Acoustic- Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-507 · Aug 18, 2025
- [A-5614398-1B1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154304630520250820141247.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-507 · Aug 18, 2025
- [A-5614398-503G1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150079855620250820141251.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-509 · Aug 18, 2025
- [A-5614398-1C2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149819050620250820141249.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-507 · Aug 18, 2025
- [A-5614398-1B1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149263990120250820141246.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-505 · Aug 18, 2025
- [A-5614398-1G2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138075947520250820141249.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-501 · Aug 18, 2025
- [A-5614398-1B1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137397403820250820141246.0001): Pane Acoustic-Cabin Window. AAR Component Services - Hot Springs, LLC · PMA PQ1070SW · Replaces 5914398-501 · Aug 18, 2025

All of them: https://openairdocs.org/model/mcdonnell-douglas-dc-9-14/pma.md

## The same model under other registry codes

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

- [Douglas DC-9-14](https://openairdocs.org/model/douglas-dc-9-14): 0 registered aircraft, registry code 3022034

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