# Douglas DC-9-32F

- Type: Aircraft model (FAA registry)
- Registry code: 3022067
- Manufacturer (registry): DOUGLAS
- Model: DC-9-32F
- 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: 1
- Page: https://openairdocs.org/model/douglas-dc-9-32f

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 2010-25-04](https://openairdocs.org/ad/2010-25-04): Compliance · Boeing DC-9-31, DC-9-32, DC-9-32 (VC-9C) and 14 more. Effective Jan 11, 2011
- [AD 2010-23-10](https://openairdocs.org/ad/2010-23-10): Wings · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective Dec 14, 2010
- [AD 2009-15-16 R1](https://openairdocs.org/ad/2009-15-16-R1): Doors · Intrusion/Penetration Resistance Flightdeck Door and Reinforced… (Aircraft Reconfig Technologies STC ST02463AT). Effective Aug 5, 2010
- [AD 2010-10-20](https://openairdocs.org/ad/2010-10-20): Fuel · Boeing DC-9-31, DC-9-32, DC-9-32 (VC-9C) and 8 more. Effective Jun 21, 2010
- [AD 2009-21-10 R1](https://openairdocs.org/ad/2009-21-10-R1): Oxygen · Airbus A300 B4-605R, A300 B4-620, A300 B4-622 and 138 more. Effective Feb 4, 2010
- [AD 2009-24-21](https://openairdocs.org/ad/2009-24-21): Landing gear · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective Jan 8, 2010
- [AD 2009-03-03](https://openairdocs.org/ad/2009-03-03): Fuel boost pump of the center tank · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective Mar 31, 2009
- [AD 2008-18-06](https://openairdocs.org/ad/2008-18-06): Tail cone slide · Protective rigid cover over the tail cone emergency evacuation… (Derlan STC ST735SO). Effective Jan 7, 2009
- [AD 2008-12-03](https://openairdocs.org/ad/2008-12-03): Auxiliary fuel tanks · Airbus BAC 1-11 400 Series, 707-100 Long Body, 707-100B Long Body and 15 more. Effective Jul 9, 2008
- [AD 2008-11-15](https://openairdocs.org/ad/2008-11-15): Fuel tank systems · Boeing 717-200, DC-9-11, DC-9-12 and 21 more. Effective Jul 3, 2008
- [AD 2008-07-09](https://openairdocs.org/ad/2008-07-09): Auxiliary fuel tanks · Boeing 727-100 Series, 727-200 Series, 727-200F Series and 7 more. Effective May 2, 2008
- [AD 2008-06-27](https://openairdocs.org/ad/2008-06-27): Evacuation system's shear-pin · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 91 more. Effective Apr 28, 2008
- [AD 2008-03-12](https://openairdocs.org/ad/2008-03-12): Rudder pedal bracket · Boeing DC-8-11, DC-8-12, DC-8-21 and 47 more. Effective Mar 11, 2008
- [AD 2007-17-18](https://openairdocs.org/ad/2007-17-18): Static port heater assemblies · Boeing DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Oct 2, 2007
- [AD 2006-21-06](https://openairdocs.org/ad/2006-21-06): Structural inspection revisions · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Nov 29, 2006
- [AD 2006-18-05](https://openairdocs.org/ad/2006-18-05): Disconnect panel · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective Oct 11, 2006
- [AD 2006-18-02](https://openairdocs.org/ad/2006-18-02): Replacing the clamp bases for the fuel vent pipe · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Oct 4, 2006
- [AD 2006-13-18](https://openairdocs.org/ad/2006-13-18): Bonding jumper from the boost pump volute to the fuel tank structure · Boeing DC-9-31, DC-9-32, DC-9-32F and 5 more. Effective Aug 9, 2006
- [AD 2006-10-14](https://openairdocs.org/ad/2006-10-14): Stop pad support fittings · Boeing 717-200, DC-9-11, DC-9-12 and 22 more. Effective Jun 21, 2006
- [AD 2006-07-08](https://openairdocs.org/ad/2006-07-08): Main fuselage frame · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective May 5, 2006
- [AD 2006-06-04](https://openairdocs.org/ad/2006-06-04): Main landing gear (MLG) · Boeing DC-9-11, DC-9-12, DC-9-13 and 17 more. Effective Apr 20, 2006
- [AD 2006-01-02](https://openairdocs.org/ad/2006-01-02): Upper lock link assembly of the nose landing gear (NLG) · Boeing DC-9-14, DC-9-15, DC-9-15F and 18 more. Effective Feb 22, 2006
- [AD 2005-13-18](https://openairdocs.org/ad/2005-13-18): Battery terminal screws · Boeing DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Aug 1, 2005
- [AD 2005-07-18](https://openairdocs.org/ad/2005-07-18): Cargo configuration · Class E cargo compartment and pallet system (Aeronautical Engineers STC SA1993SO). Effective May 11, 2005
- [AD 2005-07-03](https://openairdocs.org/ad/2005-07-03): Rear spar of the left and right wings · Boeing DC-9-11, DC-9-12, DC-9-13 and 17 more. Effective May 4, 2005
- [AD 2004-25-14](https://openairdocs.org/ad/2004-25-14): Main landing gear (MLG) · Boeing DC-9-14, DC-9-15, DC-9-15F and 17 more. Effective Jan 20, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-18-11](https://openairdocs.org/ad/2004-18-11): Outboard idler hinge fitting of the left and right wing · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective Oct 13, 2004
- [AD 2004-07-05](https://openairdocs.org/ad/2004-07-05): Engine Pylon Aft Upper Spar Straps (Caps) · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective May 5, 2004
- [AD 2004-07-04](https://openairdocs.org/ad/2004-07-04): Ballast transformers · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 more. Effective May 5, 2004
- [AD 2004-05-25](https://openairdocs.org/ad/2004-05-25): Seat Locking Pins · Boeing DC-9-14, DC-9-15, DC-9-15F and 18 more. Effective Apr 19, 2004
- [AD 2003-03-15 R1](https://openairdocs.org/ad/2003-03-15-R1): Airplane Flight Manual (AFM) - oxygen masks · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 90 more. Effective Dec 22, 2003
- [AD 2003-17-07 R1](https://openairdocs.org/ad/2003-17-07-R1): Auxiliary power unit (APU) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 57 more. Effective Sep 24, 2003
- [AD 2003-09-07](https://openairdocs.org/ad/2003-09-07): Left and right main landing gear (MLG) · Boeing DC-9-14, DC-9-15, DC-9-15F and 17 more. Effective Jun 5, 2003
- [AD 2002-26-10](https://openairdocs.org/ad/2002-26-10): Corners of the Forward Lower Cargo Doorjamb · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more. Effective Feb 10, 2003

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 258: https://openairdocs.org/model/douglas-dc-9-32f/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 (1)

- [N904CE](https://openairdocs.org/aircraft/N904CE): [Tatonduk Outfitters Limited](https://openairdocs.org/faa-owner/TATONDUK%20OUTFITTERS%20LIMITED), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1967, S/N 47040

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (2)

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 19970606017609I](https://openairdocs.org/incident/19970606017609I), Jun 6, 1997: Doug DC932F (N905AX), Middletown, PA. Narrative: aircraft landed on runway 13 at MDT. During rollout, MDT tower cleared aircraft to parking via taxiway delta (d). Crew did not recognize that…
- [Incident 19930701025009I](https://openairdocs.org/incident/19930701025009I), Jul 1, 1993: Doug DC932F (N905AX), Albany, NY, Minor damage. A ups van attempted to pass between two parked aircraft. Struck left wing tip of N905AX.

## Service difficulty reports (517, newest 50)

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

- [SDR 2022F00149](https://openairdocs.org/sdr/2022F00149), Apr 30, 2021: TURBINE BLADES. DAMAGED. DURING THE CLIMB BETWEEN 12000 AND 15000 FT, A LOUD BANG WAS HEARD, OBSERVING PARAMETERS OF THE LEFT ENGINE OUT OF RANGE IN RELATION TO THE POSITION OF THE THRO
- [SDR 2022F00144](https://openairdocs.org/sdr/2022F00144), Mar 30, 2021: WARNING MESSAGE. ILLUMINATED. INDICATION LOWER CARGO FIRE FOR ONE MINUTE.
- [SDR Y2PA201809250032](https://openairdocs.org/sdr/Y2PA201809250032), Sep 25, 2018: SKIN PANEL. CORRODED. DURING C-CHECK AT KSFB, CORROSION WAS DISCOVERED ON SKIN AT STA 1114, LONGERON 18R. MAINTENANCE AT KSFB. REMOVED AND REPLACED LOWER SKIN FROM STA 1087-1121, LON
- [SDR Y2PA2018092530030](https://openairdocs.org/sdr/Y2PA2018092530030), Sep 23, 2018: PITOT TUBE. OBSTRUCTED. CREW REPORTED 60 KNOT AIRSPEED DISCREPANCY DURING CLIMB. RAN COM 5.31.5 WITH NO SUCCESS. RETURNED TO KLRD AND DECLARED EMERGENCY. NO FURTHER INCIDENT. MAINTENAN
- [SDR Y2PA201804170013](https://openairdocs.org/sdr/Y2PA201804170013), Apr 15, 2018: CONTROL PANEL. INOPERATIVE. ENCOUNTERED AN ELECTRICAL PROBLEM DURING CLIMB. RETURNED TO DEPARTURE. NO FURTHER ISSUES OCCURRED AND LANDED SAFELY. EMERGENCY DECLARED WITH ATC. LEFT GENERATOR
- [SDR Y2PA2017112300031](https://openairdocs.org/sdr/Y2PA2017112300031), Nov 23, 2017: SENSOR. FAILED. CREW REPORTED DURING GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. PERFORMED COM PROCEDURE, DECLARED EMERGENCY, REMAINED AIRBORNE TO BURN OFF FU
- [SDR Y2PA2016092900024](https://openairdocs.org/sdr/Y2PA2016092900024), Sep 29, 2016: WARNING SYSTEM. MALFUNCTIONED. IMMEDIATELY AFTER TAKEOFF, COULD SMELL AN ELECTRICAL BURNING ODOR FOLLOWED BY A MASTER CAUTION LIGHT. SEVERAL ANNUNCIATORS CAME ON AND OFF, FOLLOWED BY THE GPWS
- [SDR Y2PA2016022800004](https://openairdocs.org/sdr/Y2PA2016022800004), Feb 25, 2016: LANDING GEAR. MALFUNCTIONED. DURING APPROACH, GEAR HANDLE PLACED IN DOWN POSITION. NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE GREEN. CYCLED GEAR, NOSE GEAR LIGHT STILL DID NOT ILLUMINATE GR
- [SDR Y2PA2016011200001](https://openairdocs.org/sdr/Y2PA2016011200001), Jan 12, 2016: SKIN. CORRODED. MAINTENANCE DISCOVERED A MISSING RIVET FROM THE BELLY SKIN AT FS 585. UPON FURTHER INSPECTION, IT WAS DETERMINED THAT THERE WAS INTERNAL AND EXTERNAL CORROSION 
- [SDR K11A2013060616001](https://openairdocs.org/sdr/K11A2013060616001), Jun 6, 2013: FUEL CAP. MISSING. FUEL REPORTED AS VENTING FROM RT WING, NOTED FUEL IMBALANCE AND RETURNED TO DEPARTURE. UPON INVESTIGATION, FOUND RT OVERWING FUEL CAP MISSING, REPLACED CAP AND 
- [SDR Y2PA20130511039](https://openairdocs.org/sdr/Y2PA20130511039), May 11, 2013: LINE. FAILED. CREW REPORTED POST V1 & JUST INTO ROTATION, MASTER CAUTION ILLUMINATED FOR LT OIL PRESSURE LOW. DECISION MADE TO LEAVE MLG DOWN. OIL PRESSURE LOW & QTY DECREASI
- [SDR Y2PA20130507036](https://openairdocs.org/sdr/Y2PA20130507036), May 6, 2013: SKIN. CRACKED. DURING C-CHECK INSPECTION AT YIP, MX DISCOVERED THE LT FLAP LOWER SKIN CRACKED. MX AT REPAIRED IAW SRM 57-01, FIGURE 3, SHEET 2 AND EA 96-51-02 R1.
- [SDR Y2PA20130507035](https://openairdocs.org/sdr/Y2PA20130507035), May 6, 2013: HINGE. CRACKED. DURING C-CHECK INSPECTION, MX DISCOVERED THE LT WING CENTER AFT FLAP HINGE CRACKED. MX R & R HINGE IAW AMM 27-51-1 AND OHM 27-50-1.
- [SDR Y2PA20130507034](https://openairdocs.org/sdr/Y2PA20130507034), May 6, 2013: BRACKET. CORRODED. DURING C-CHECK INSPECTION, MX DISCOVERED THE MAIN UPPER CARGO DOOR LOWER SILL BRACKET CORRODED. MX R & R BRACKET IAW SRM 51-30-5.
- [SDR Y2PA20130507033](https://openairdocs.org/sdr/Y2PA20130507033), May 6, 2013: PANEL. DELAMINATED. DURING C-CHECK INSPECTION, MX DISCOVERED THE INBD LT T/E WING PANEL DELAMINATED. MX R & R PANEL WITH SERVICEABLE IAW SRM 51-30-2.
- [SDR Y2PA20130507032](https://openairdocs.org/sdr/Y2PA20130507032), May 6, 2013: PANEL. DELAMINATED. DURING C-CHECK INSPECTION, MX DISCOVERED THE SECOND FROM OTBD LT T/E WING PANEL DELAMINATED. MX R & R PANEL WITH SERVICEABLE IAW SRM 51-30-2.
- [SDR Y2PA20130507031](https://openairdocs.org/sdr/Y2PA20130507031), May 6, 2013: TEE FITTING. CORRODED. DURING C-CHECK INSPECTION, MX DISCOVERED A TEE FITTING CORRODED AT BS 160 ON THE RT CUSP LINE. MX R & R TEE FITTING IAW SRM 51-30-2 AND 51-30-5.
- [SDR Y2PA20130507030](https://openairdocs.org/sdr/Y2PA20130507030), May 6, 2013: CUSP WEB. CRACKED. DURING C-CHECK INSPECTION, MX DISCOVERED A CRACKED WEB AT STATION 953, LONGERON 18L. MX REPAIRED IAW SRM 53-01, FIGURE 2, SHEET 3 AND EA 96-51-02 R1.
- [SDR Y2PA20130507029](https://openairdocs.org/sdr/Y2PA20130507029), May 6, 2013: LONGERON. CORRODED. DURING C-CHECK INSPECTION, MX DISCOVERED LONGERON END SHOVEL CORRODED IN THE LOWER AFT CARGO BAY AT BS 996 ON LONGERONS 29L. MX R & R SHOVELS IAW SRM 51-30-5.
- [SDR Y2PA20130507028](https://openairdocs.org/sdr/Y2PA20130507028), May 6, 2013: SLEEVE. CRACKED. DURING C-CHECK INSPECTION, MX DISCOVERED BOTH LT AND RT HORIZONTAL STABILIZER HINGE BOLT SLEEVES CRACKED. MX R & R SLEEVES IAW AMM 55-10-0.
- [SDR Y2PA20130507027](https://openairdocs.org/sdr/Y2PA20130507027), May 6, 2013: SKIN. CORRODED. DURING C-CHECK INSPECTION, MX DISCOVERED THE LOWER AFT CARGO BAY SKIN CORRODED AT BS 756, LONGERON 27L 29R. MX REPAIRED IAW EA 13-53-321 AND DER DWG 53-13118-1,
- [SDR Y2PA20130507026](https://openairdocs.org/sdr/Y2PA20130507026), May 6, 2013: WEB. CORRODED. DURING C-CHECK INSPECTION, MX DISCOVERED THE LOWER AFT CARGO BAY CENTERLINE WEB CORRODED AT BS 996. MX REPAIRED IAW SRM 53-01, FIG 2 SHEET 3 AND EA 96-51-02 R3.
- [SDR Y2PA20130507025](https://openairdocs.org/sdr/Y2PA20130507025), May 6, 2013: WINDOW FRAME. CRACKED. DURING INSPECTION IAW AD 2002-21-09, 2 EACH .5" CRACKS WERE DISCOVERED IN THE CENTER FRAME OF THE COCKPIT WINDOW SILL. MX R & R THE COCKPIT WINDOW SILL CENTER F
- [SDR Y2PA20130507024](https://openairdocs.org/sdr/Y2PA20130507024), May 6, 2013: SPAR. CRACKED. DURING C-CHECK X-RAY INSPECTION, MX DISCOVERED THE LT ELEVATOR FRONT SPAR CRACKED OUT OF LIMITS. MX AT YIP R & R THE LT ELEVATOR WITH A SERVICEABLE PART IAW MM 
- [SDR Y2PA20130306010](https://openairdocs.org/sdr/Y2PA20130306010), Mar 6, 2013: SKIN. CRACKED. EMERGENCY PROCEDURE, EMERGENCY DESCENT, UNSCHEDULED LANDING. FUSELAGE SKIN CRACKED AT BS 950 BETWEEN L14-15R, DISCOVERED DURING C-CHECK INSPECTION. MX REPAIRED 
- [SDR Y2PA20130306009](https://openairdocs.org/sdr/Y2PA20130306009), Mar 6, 2013: SHEAR TIE. CRACKED. UNSCHEDULED LANDING, EMERGENCY DESCENT, ETC. SHEAR TIE CRACKED AT BS 945 BETWEEN LONGERONS 14R AND 17R, DISCOVERED DURING C-CHECK INSPECTION. MX REPLACED SHEAR 
- [SDR Y2PA20130306008](https://openairdocs.org/sdr/Y2PA20130306008), Mar 6, 2013: FITTING. CRACKED. UNSCHEDULED LANDING, EMERGENCY DESCENT. RT PYLON REAR SPAR UPPER CAP FITTING AT STATION Y 1038 FOUND CRACKED DURING C-CHECK INSPECTION. MX REPLACED FITTING IAW 
- [SDR Y2PA20130306007](https://openairdocs.org/sdr/Y2PA20130306007), Mar 6, 2013: FITTING. CRACKED. UNSCHEDULED LANDING, EMERGENCY DESCENT, ETC. LT PYLON REAR SPAR UPPER CAP FITTING AT STATION 1038 FOUND CRACKED DURING C-CHECK INSPECTION. MX REPLACED FITTING I
- [SDR Y2PA20130306006](https://openairdocs.org/sdr/Y2PA20130306006), Mar 6, 2013: SKIN. CHAFED. EVIDENCE OF DAMAGE ON UPPER RT SIDE OF VERTICAL STABILIZER BETWEEN STATION ZV120 NEAR FORWARD END OF UPPER AND LOWER BODY FAIRINGS, DISCOVERED DURING C-CHECK. M
- [SDR Y2PA20130306005](https://openairdocs.org/sdr/Y2PA20130306005), Mar 6, 2013: ATTACH ANGLE. CRACKED. EMERGENCY PROCEDURE, UNSCHEDULED LANDING, EMERGENCY DESCENT. RT PYLON UPPER PYLON TO FUSELAGE ATTACH ANGLE 12, AFT OF LEADING EDGE HAS 1 CRACK AT CORNER, DISCOV
- [SDR Y2PA20120910041](https://openairdocs.org/sdr/Y2PA20120910041), Sep 10, 2012: TURBINE BLADES. DAMAGED. CREW REPORTED AFTER DEPARTURE WHEN TRANSITIONING TO QUIET EPR POWER SETTING A SUDDEN LOUD AND EXTREME VIBRATION OCCURRED. OBSERVED LOSS OF EPR, N1 & N2. LT ENGI
- [SDR Y2PA2011092000024](https://openairdocs.org/sdr/Y2PA2011092000024), Sep 16, 2011: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS INOPERATIVE DURING INSP. MX R & R BATTERY POWER SUPPLY IAW AMM 33-50-0. OPS CHECKS GOOD, NO OTHER DEFECTS NOTED.
- [SDR Y2PA2010111500028](https://openairdocs.org/sdr/Y2PA2010111500028), Nov 10, 2010: DOWNLOCK SWITCH. MALFUNCTIONED. UPON APPROACH, THE RT MLG DID NOT DISPLAY GREEN INDICATION, ONLY RED. CREW EXECUTED MISSED APPROACH AND REVIEWED COM PROCEDURES. CREW DIVERTED AND DECLARED AN E
- [SDR ABXA080151](https://openairdocs.org/sdr/ABXA080151), May 1, 2008: ATTACH ANGLE. CRACKED. LEFT VERTICAL STAB ATTACH ANGLE CRACKED, LOCATED AT BASE OF RUDDER. REPAIRED LEFT VERTICAL STAB ATTACH ANGLE IAW DC9 SRM 53-05.
- [SDR ABXA080152](https://openairdocs.org/sdr/ABXA080152), May 1, 2008: PAN. CRACKED. MAIN ENTRY DOOR PAN CRACKED FORWARD SIDE (BOTTOM HINGE) SECOND STOP FROM BOTTOM. REMOVED AND REPAIRED DOOR IAW DC9 SRM.
- [SDR ABXA080150](https://openairdocs.org/sdr/ABXA080150), Apr 30, 2008: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT STA 160, LONGERON 20 - 21 LEFT AT AIRSTAIR HINGE FORWARD SIDE. REPAIRED FUSELAGE SKIN CRACK IAW DC9 SRM.
- [SDR ABXA080120](https://openairdocs.org/sdr/ABXA080120), Apr 5, 2008: RELAY. DEFECTIVE. PRIMARY TRIM CIRCUIT BREAKER TRIPPED WHILE SETTING TAKEOFF TRIM. WHILE MECHANIC WAS TROUBLESHOOTING PRIMARY TRIM, HEAVY SMOKE PRODUCED THROUGHOUT FRONT & REAR C
- [SDR ABXR080108](https://openairdocs.org/sdr/ABXR080108), Mar 3, 2008: ATTACH ANGLE. CRACKED. ATTACH ANGLE FOR STA 41 TO STA 69 PRESSURE PANEL INTERCOSTAL CRACKED JUST RIGHT OF PLUG DOOR. REMOVED AND REPLACED ANGLES IAW DC9 SRM 51-30-5.
- [SDR ABXR080107](https://openairdocs.org/sdr/ABXR080107), Mar 3, 2008: ATTACH ANGLE. CRACKED. ATTACH ANGLE FOR STA 41 TO STA 69 PRESSURE PANEL INTERCOSTAL CRACKED. SECOND INTERCOSTAL TO THE LEFT OF THE PLUG DOOR. REMOVED AND REPLACED IAW DC9 SRM 51-30-5.
- [SDR ABXR080106](https://openairdocs.org/sdr/ABXR080106), Mar 3, 2008: FITTING. CRACKED. PYLON UPPER REAR SPAR STRAP CLIP JUST INSIDE PYLON CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW CLIP IAW DC9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXR080105](https://openairdocs.org/sdr/ABXR080105), Mar 2, 2008: ATTACH ANGLE. CRACKED. LEFT WHEEL WELL KEEL WEB UPPER ATTACH ANGLE AT STA 718 CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXR080104](https://openairdocs.org/sdr/ABXR080104), Feb 29, 2008: ATTACH ANGLE. CRACKED. INBOARD BULKHEAD STA 718 ATTACH ANGLE CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXR080103](https://openairdocs.org/sdr/ABXR080103), Feb 28, 2008: SKIN. CRACKED. AFT LOWER CARGO DOOR SKIN CRACKED AT DOOR HANDLE. REPAIRED DOOR IAW DC9 SRM 52-05, FIGURE 30, SHEET 1.
- [SDR ABXR080102](https://openairdocs.org/sdr/ABXR080102), Feb 28, 2008: SKIN. CRACKED. FORWARD LOWER CARGO DOOR SKIN CRACKED AT DOOR HANDLE. REPAIRED AND PAINTED IAW DC9 SRM 25-05 AND 51-10.
- [SDR ABXA070425](https://openairdocs.org/sdr/ABXA070425), Dec 11, 2007: BATTERY PACK. DEFECTIVE. EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW DC9 AMM CHAPTER 33.
- [SDR ABXA070424](https://openairdocs.org/sdr/ABXA070424), Dec 8, 2007: BATTERY. DISCHARGED. CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.
- [SDR Y2PA200700026](https://openairdocs.org/sdr/Y2PA200700026), Nov 2, 2007: CSD. FAILED. CREW REPORTED ENGINE VIBRATION THEN FAILURE ON NR 2 ENGINE. IRREGULARITY FILLED OUT BY CREW REPORTED AS FOLLOWS. AFTER DEPARTURE IN CLIMB, VIBRATION FOLLOWED BY
- [SDR ABXA070262](https://openairdocs.org/sdr/ABXA070262), Aug 15, 2007: FRAME. CRACKED. WHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME, REF AD 2002-21-09. REPLACED FRAME IAW DC9 SRM 51-30-02 AND 51-30-05.
- [SDR ABXA070264](https://openairdocs.org/sdr/ABXA070264), Aug 15, 2007: ANGLE. CRACKED. WHILE COMPLYING WITH EA 53300036, FOUND CRACKED ANGLE, REF AD 2002-21-09. REPLACED ANGLE IAW DC9 SRM 51-30-05.
- [SDR ABXA070263](https://openairdocs.org/sdr/ABXA070263), Aug 15, 2007: BRACKET. CRACKED. WHILE COMPLYING WITH EA 53300036, FOUND CRACKED BRACKET, REF AD 2002-21-09. REPLACED BRACKET IAW DC9 SRM 51-30-02 AND 51-30-05.

All 517: https://openairdocs.org/model/douglas-dc-9-32f/reports.md

## STCs that may be installed (OpenAirDocs) (270, 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 ST02463AT](https://openairdocs.org/stc/ST02463AT): Installation of an Intrusion/Penetration Resistance Flightdeck Door and Reinforced Flightdeck Door Surround. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST09180AC](https://openairdocs.org/stc/ST09180AC): Installation of DeVore Wing Forward Position Lights. The Boeing Company
- [STC ST09181AC](https://openairdocs.org/stc/ST09181AC): Installation of main landing gear spotlights. The Boeing Company
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA2040NM](https://openairdocs.org/stc/SA2040NM): Installation of closet and windscreen. Safran Cabin Inc
- [STC SA3469NM](https://openairdocs.org/stc/SA3469NM): Installation of Closet/Stowage Compartments/Coat Compartment/ Coatroom. Safran Cabin Inc
- [STC SA3494NM](https://openairdocs.org/stc/SA3494NM): Installation of auxiliary galley. Safran Cabin Inc. Lists DC-9 Series
- [STC ST01336LA](https://openairdocs.org/stc/ST01336LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC SA3165NM](https://openairdocs.org/stc/SA3165NM): Installation of Floor Proximity Emergency Escape Path Marking System. Bruce Aerospace Inc
- [STC ST00092LA](https://openairdocs.org/stc/ST00092LA): Instalation of interior fluorescent cabin lighting system. Bruce Aerospace Inc
- [STC ST00069AT](https://openairdocs.org/stc/ST00069AT): Installation of a Fairchild Digital or Sundstrand Universal expanded parameters digital flight data recorder. Acron Aviation Inc
- [STC ST01518NY](https://openairdocs.org/stc/ST01518NY): Installation of Flight Systems Cabin Surveillance System (CSS). Acron Aviation Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST00984CH](https://openairdocs.org/stc/ST00984CH): Installation of Rockwell Collins FPI-955 Electronic Horizontal Situation Indicators (EHSI). Amphenol Cable and Interconnect Technologies Inc
- [STC ST01017CH](https://openairdocs.org/stc/ST01017CH): Installation of an AlliedSignal CAS-81 TCAS II System with dual AlliedSignal Mode S Transponders. Amphenol Cable and Interconnect Technologies Inc
- [STC ST01019CH](https://openairdocs.org/stc/ST01019CH): Installation of a Rockwell Collins GNLS-910 GPS Flight Management System. Amphenol Cable and Interconnect Technologies Inc
- [STC ST01167CH](https://openairdocs.org/stc/ST01167CH): Installation of an AlliedSignal MK-VII Enhanced Ground Proximity Warning System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01404CH](https://openairdocs.org/stc/ST01404CH): Installation of Universal Avionics System Corporation Multi-Function Display. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01818CH](https://openairdocs.org/stc/ST01818CH): Installation of a Honeywell Enhanced Ground Proximity Warning System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01887CH](https://openairdocs.org/stc/ST01887CH): Installation of GPS antenna provisions. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST02474AK](https://openairdocs.org/stc/ST02474AK): Installation of escape tapes at the L1 and R1 entry doors and removal of evacuation slides. Tatonduk Outfitters Ltd
- [STC ST02770SE](https://openairdocs.org/stc/ST02770SE): Installation of an Improved Radio Altimeter System. AeroMech Incorporated
- [STC ST02876AT](https://openairdocs.org/stc/ST02876AT): Installation of a Free Flight Model 2101 I/O Approach Plus Global Positioning System (GPS), Universal Model MFD 640 Multi-function Display (MFD), and Provisions for an Aviation Communication & Surveillance Systems (ACSS) Terrain & Traffic Collision Avoidance System (TTCAS). Woven Electronics, LLC
- [STC ST02896AT](https://openairdocs.org/stc/ST02896AT): Installation of a Kannad Model 406-AF Emergency Locator Transmittter (ELT). Woven Electronics LLC
- [STC ST03481AT](https://openairdocs.org/stc/ST03481AT): Installation of an Artex C406-N Emergency Locator Transmitter. Woven Electronics, LLC
- [STC ST11384DS](https://openairdocs.org/stc/ST11384DS): Installation of a Universal Avionics Systems Corporation UNS‐1Lw SBAS Flight Management System with LPV Approach. Aircraft Systems and Manufacturing, Inc
- [STC SA2534SW-D](https://openairdocs.org/stc/SA2534SW-D): Replacement of Switch assembly Int'l Inflatables Co. P/N 68748, with DME Corp. P/N L-140 in emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-9 Series
- [STC SA2539SW-D](https://openairdocs.org/stc/SA2539SW-D): Replacement of light assembly, International Inflatables Co. P/N68555-1 with DME Corp. EL-104, EL-104A, and EL-104B in emergency slide lighting system. Astronics Luminescent Systems Inc. Lists DC-9 Series
- [STC SA863EA](https://openairdocs.org/stc/SA863EA): Incorporation of DME Corporation emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-9 Series
- [STC ST02580AT](https://openairdocs.org/stc/ST02580AT): Lithium cell battery pack to replace currently approved alkaline battery pack used in escape slide emergency light system. Astronics Luminescent Systems Inc
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST03838AT](https://openairdocs.org/stc/ST03838AT): Installation of an Universal Avionics Application Server Unit (ASU) System Class II Electronic Flight Bag (EFB). Technical Aero Services Inc
- [STC SA1220NW](https://openairdocs.org/stc/SA1220NW): Installation of Universal flight data recorder. Honeywell International Inc
- [STC SA3173SO](https://openairdocs.org/stc/SA3173SO): Installation of the Mark-VII ground proximity and windshear warning system. Honeywell International Inc
- [STC SA5920NM](https://openairdocs.org/stc/SA5920NM): Installation of 980-4100-HQUS Flight Data Recorder and Penny and Giles Quick Access Recorder in accordance with Document 755-3024, Rev. New-1, or later FAA approved revision. Honeywell International Inc
- [STC ST00074AT](https://openairdocs.org/stc/ST00074AT): Installation of a Bendix/King Mode S transponder. Honeywell International Inc
- [STC ST00075AT](https://openairdocs.org/stc/ST00075AT): Installation of a CAS-81 TCAS II. Honeywell International Inc
- [STC ST00136AT](https://openairdocs.org/stc/ST00136AT): Installation of a Bendix/King CAS-81 and TRA-67 Mode S trannsponder. Honeywell International Inc
- [STC ST00701AT](https://openairdocs.org/stc/ST00701AT): Installation of the RDR-4B weather radar/windshear system. Honeywell International Inc
- [STC ST01828AT](https://openairdocs.org/stc/ST01828AT): Installation of a RTA-83A VHF Communication System. Honeywell International Inc
- [STC SA3748SW](https://openairdocs.org/stc/SA3748SW): Installation of heat exchanger assembly (P/N 184060). Honeywell International Inc
- [STC SA4398SW](https://openairdocs.org/stc/SA4398SW): Modification of air to air heat exchanger (P/N 179450-2-2 or194110-1). Honeywell International Inc. Lists DC-9 Series
- [STC SA640NW](https://openairdocs.org/stc/SA640NW): Installation of contemporary deep rack interior. Safran Cabin Inc. Lists DC-9 Series
- [STC ST00939LA](https://openairdocs.org/stc/ST00939LA): Installation of passenger entertainment system. Burrana Inc. Lists DC-9 Series
- [STC ST04450AT](https://openairdocs.org/stc/ST04450AT): Installation of the dual Rockwell Collins TPR-901, ADS-B out capable trasnponder system and dual GPS-4000S position sensor. Avionics Support Group Inc
- [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

All 270: https://openairdocs.org/model/douglas-dc-9-32f/stcs.md

## The same model under other registry codes

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

- [Mcdonnell Douglas DC-9-32F](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32f): 1 registered aircraft, registry code 302206E

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