# Mcdonnell Douglas DC-8-63

- Type: Aircraft model (FAA registry)
- Registry code: 302198B
- Manufacturer (registry): MCDONNELL DOUGLAS
- Model: DC-8-63
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-jet
- Seats: 152
- Weight class: 20,000 lb and over
- Cruise speed: 444 mph
- Certification: Type certificated
- Data sheet: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Holder: The Boeing Company
- Registered aircraft: 1
- Page: https://openairdocs.org/model/mcdonnell-douglas-dc-8-63

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 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 2016-04-21](https://openairdocs.org/ad/2016-04-21): Wings · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Apr 5, 2016
- [AD 2014-22-10](https://openairdocs.org/ad/2014-22-10): Fuselage · Boeing DC-8-55, DC-8-61, DC-8-61F and 12 more. Effective Jan 2, 2015
- [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 2011-18-23](https://openairdocs.org/ad/2011-18-23): Wings · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Oct 25, 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 2010-21-03](https://openairdocs.org/ad/2010-21-03): Fuel · Boeing DC-8-31, DC-8-32, DC-8-33 and 21 more. Effective Nov 12, 2010
- [AD 2009-08-02](https://openairdocs.org/ad/2009-08-02): Fuel pumps · Boeing DC-8-51, DC-8-52, DC-8-53 and 15 more. Effective May 13, 2009
- [AD 2008-25-05](https://openairdocs.org/ad/2008-25-05): Structural inspections · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Jan 28, 2009
- [AD 2008-16-11](https://openairdocs.org/ad/2008-16-11): Forward and aft service doors · Boeing DC-8-61, DC-8-61F, DC-8-63 and 3 more. Effective Sep 17, 2008
- [AD 2008-06-23](https://openairdocs.org/ad/2008-06-23): Aft fuselage skin panel · Boeing DC-8-55, DC-8-61, DC-8-61F and 12 more. Effective Apr 22, 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 2007-21-18](https://openairdocs.org/ad/2007-21-18): Flat aft pressure bulkhead · Boeing DC-8-53, DC-8-55, DC-8-61 and 13 more. Effective Nov 28, 2007
- [AD 2007-13-02](https://openairdocs.org/ad/2007-13-02): Sump heater, scavenge valve, and scavenge pump · Boeing DC-8-62, DC-8-62F, DC-8-63 and 4 more. Effective Jul 25, 2007
- [AD 2007-12-02](https://openairdocs.org/ad/2007-12-02): Left and right wing front spar · Boeing DC-8-33, DC-8-42, DC-8-43 and 16 more. Effective Jul 10, 2007
- [AD 2007-04-06](https://openairdocs.org/ad/2007-04-06): Engine thrust brake circuit · Boeing DC-8-62, DC-8-62F, DC-8-63 and 1 more. Effective Mar 21, 2007
- [AD 2006-03-04](https://openairdocs.org/ad/2006-03-04): Main cabin cargo door · Boeing DC-8-33, DC-8-51, DC-8-53 and 11 more. Effective Mar 13, 2006
- [AD 2005-18-07](https://openairdocs.org/ad/2005-18-07): Lower cargo doorjamb corners · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Oct 7, 2005
- [AD 2005-15-14](https://openairdocs.org/ad/2005-15-14): Upper inboard spar cap of the wing · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Sep 1, 2005
- [AD 2005-08-08](https://openairdocs.org/ad/2005-08-08): Engine fire extinguisher containers · Boeing DC-8-33, DC-8-43, DC-8-51 and 17 more. Effective May 26, 2005
- [AD 2005-06-05](https://openairdocs.org/ad/2005-06-05): Left and right elevator control tabs · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Apr 22, 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 2004-14-05](https://openairdocs.org/ad/2004-14-05): Seat locking pins · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Aug 13, 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 2003-21-02](https://openairdocs.org/ad/2003-21-02): Lower inboard auxiliary spar cap · Boeing DC-8-11, DC-8-12, DC-8-21 and 21 more. Effective Nov 20, 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 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2002-14-19](https://openairdocs.org/ad/2002-14-19): Collins Air Data Computers (ADC) · Boeing DC-8-11, DC-8-12, DC-8-21 and 36 more. Effective Aug 23, 2002
- [AD 2002-16-01](https://openairdocs.org/ad/2002-16-01): Main cargo door area · Forward cargo door (Aeronautical Engineers STC SA1063SO or 2 others). Effective Aug 22, 2002
- [AD 2002-03-05](https://openairdocs.org/ad/2002-03-05): Blue Ice · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Mar 19, 2002
- [AD 2001-26-04](https://openairdocs.org/ad/2001-26-04): Main Deck Cargo Door Structure and Fuselage Structure · Cargo door, cargo restraint bulkhead, heavy duty flooring… (Plattner STC SA1802SO or SA421NW). Effective Jan 30, 2002
- [AD 2001-26-03](https://openairdocs.org/ad/2001-26-03): Main Deck Cargo Door Structure and Fuselage Structure · Cargo door and cargo interior (Plattner STC SA1832SO). Effective Jan 30, 2002
- [AD 2001-26-02](https://openairdocs.org/ad/2001-26-02): Main Deck Cargo Door Structure and Fuselage Structure · Cargo door (Agro Air Associates STC SA1862SO or ST00309AT). Effective Jan 30, 2002
- [AD 2001-26-01](https://openairdocs.org/ad/2001-26-01): Main Deck Cargo Door Structure and Fuselage Structure · Forward cargo door (Aeronautical Engineers STC SA1063SO or SA1377SO). Effective Jan 30, 2002
- [AD 2001-24-28](https://openairdocs.org/ad/2001-24-28): Rudder Pedals Adjuster Hub Assembly · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Jan 16, 2002
- [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001
- [AD 2001-08-20](https://openairdocs.org/ad/2001-08-20): Flush Pump Motor · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-08-19](https://openairdocs.org/ad/2001-08-19): Transformer Ballast Assemblies · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-08-18](https://openairdocs.org/ad/2001-08-18): Cabin Electrical Service Panel · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-08-17](https://openairdocs.org/ad/2001-08-17): Heating or Antifogging Wiring · Boeing DC-8-11, DC-8-12, DC-8-21 and 18 more. Effective May 31, 2001
- [AD 2001-08-16](https://openairdocs.org/ad/2001-08-16): Circuit Breakers and Wiring · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-06-02](https://openairdocs.org/ad/2001-06-02): Front Spar Lower Cap · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Apr 27, 2001
- [AD 2001-04-15](https://openairdocs.org/ad/2001-04-15): Pitot Tube Lines · Pneumatic flow control system (National Aircraft Service STC ST466CH). Effective Mar 21, 2001
- [AD 2000-20-08](https://openairdocs.org/ad/2000-20-08): Doorjambs Of Passenger And Service Doors · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Nov 13, 2000
- [AD 2000-15-11](https://openairdocs.org/ad/2000-15-11): Main Deck Cargo Door · Cargo door (Agro Air Associates STC SA1862SO). Effective Sep 7, 2000
- [AD 2000-13-03 R1](https://openairdocs.org/ad/2000-13-03-R1): Main Deck Cargo Door · Forward cargo door (Aeronautical Engineers STC SA1063SO). Effective Aug 1, 2000
- [AD 2000-09-01 R1](https://openairdocs.org/ad/2000-09-01-R1): Main Deck Cargo Door · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Jun 7, 2000

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 2008-26-07](https://openairdocs.org/ad/2008-26-07) (historical): Lower skin and stringers · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Jan 28, 2009
- [AD 2008-09-04](https://openairdocs.org/ad/2008-09-04) (historical): Fuel tank systems · McDonnell Douglas DC-8-31, DC-8-32, DC-8-33 and 21 more. Effective May 27, 2008
- [AD 2007-02-02](https://openairdocs.org/ad/2007-02-02) (historical): Aft fuselage skin panel · McDonnell Douglas DC-8-55, DC-8-61, DC-8-61F and 12 more. Effective Feb 28, 2007
- [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 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 2001-25-01](https://openairdocs.org/ad/2001-25-01) (historical): Engine Fire Extinguishing System Electrical Connectors · McDonnell Douglas DC-8-33, DC-8-43, DC-8-51 and 17 more. Effective Dec 20, 2001
- [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 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 93-20-02](https://openairdocs.org/ad/93-20-02) (historical): AFM Changes - Cargo Door Inspection · Cargo door, cargo restraint bulkhead, heavy duty flooring… (Plattner STC SA1802SO or SA421NW). Effective Nov 17, 1993

All 152: https://openairdocs.org/model/mcdonnell-douglas-dc-8-63/ads.md

## Information bulletins (advisory) (4)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [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)

- [N797AL](https://openairdocs.org/aircraft/N797AL): [Skybus Jet Cargo Inc](https://openairdocs.org/faa-owner/SKYBUS%20JET%20CARGO%20INC), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), built 1972, S/N 46163

## NTSB investigations (7)

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 DCA02WA057](https://openairdocs.org/ntsb/DCA02WA057), Sep 10, 2002: Douglas DC-8-63 (N441J), Gander, Newfndl, Canada, incident, minor damage
- [NTSB DCA97MA016](https://openairdocs.org/ntsb/DCA97MA016), Dec 22, 1996: Douglas DC-8-63F (N827AX), Narrows, VA, destroyed, 6 fatal. Probable cause: the inappropriate control inputs applied by the flying pilot during a stall recovery attempt, the failure of the nonflying pilot-in-command to recognize, address, and correct these inappropriate…
- [NTSB DCA95MA020](https://openairdocs.org/ntsb/DCA95MA020), Feb 17, 1995: Douglas DC-8-63 (N782AL), Kansas City, MO, destroyed, 3 fatal. Probable cause: (1) THE LOSS OF DIRECTIONAL CONTROL BY THE PILOT IN COMMAND DURING THE TAKEOFF ROLL, AND HIS DECISION TO CONTINUE THE TAKEOFF AND INITIATE A ROTATION BELOW THE COMPUTED ROTATION AIRSPEED, RESULTING…
- [NTSB BFO93IA176](https://openairdocs.org/ntsb/BFO93IA176), Sep 15, 1993: Douglas DC-8-63 (N870BX), Toledo, OH, incident, minor damage. Probable cause: THE OPERATOR MAINTENANCE PERSONNEL'S FAILURE TO PERFORM AN ADEQUATE INSPECTION OF THE AIRPLANE, WHICH LED TO A WORN AILERON CABLE WHICH SEPARATED IN FLIGHT AND CAUSED A LOSS OF CONTROL.
- [NTSB CHI89MA132](https://openairdocs.org/ntsb/CHI89MA132), Jul 13, 1989: Mcdonnell Douglas DC8-63F (N950R), Vandalia, OH, substantial damage. Probable cause: FAILURE OF THE LEFT MAIN LANDING GEAR, BOGIE TRIM CYLINDER, AND MALFUNCTION OF THE EMERGENCY AIRBRAKE CONTROL VALVE.
- [NTSB NYC87MA236](https://openairdocs.org/ntsb/NYC87MA236), Aug 20, 1987: Mcdonnell Douglas DC-8-63 (N951R), Newburgh, NY, substantial damage
- [NTSB DCA86RA010](https://openairdocs.org/ntsb/DCA86RA010), Dec 12, 1985: Douglas DC-8-63 (N950JW), Gander, Canada, 256 fatal

## FAA accident and incident reports (27)

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 19990108016279I](https://openairdocs.org/incident/19990108016279I), Jan 8, 1999: Doug DC863 (N815AX), Wilmington, OH, Minor damage. (-5)A later decision to execute a missed approach to rwy. 4L at iln resulted in the left outboard engine nacelle striking the rwy. The first officer was flying…
- [Incident 19971014046729I](https://openairdocs.org/incident/19971014046729I), Oct 14, 1997: Doug DC863 (N964R), Jacksonville, FL. (-23) Crewmember flight engineer john hickman experienced chest pains aboard emery worldwide airlines, inc., flight 228 on October 14, 1997 enroute from…
- [Incident 19970702024639I](https://openairdocs.org/incident/19970702024639I), Jul 2, 1997: Doug DC863 (N869BX), Toledo, OH, Minor damage. Cargo door came open on rotation. Circled and returned. Unable find cause. One latch bent.
- [Accident 19961222039609A](https://openairdocs.org/incident/19961222039609A), Dec 22, 1996: Doug DC8* (N827AX), Narrows, VA, Destroyed, 6 fatal. On maintenance flight crashed. (.4) on December 22, 1996, at about 1810 eastern standard time (EST), a Douglas DC-8-63F, N827AX, operated by airborne express…
- [Incident 19950811034319I](https://openairdocs.org/incident/19950811034319I), Aug 11, 1995: Doug DC863 (N781AL), Polo, MO. Given heading to elp. NORDO until ATC realized KS ATC gave handoff but failed notify DC8 crew. Crew initiated call.
- [Incident 19950615020839I](https://openairdocs.org/incident/19950615020839I), Jun 15, 1995: Doug DC873 (N868BX), Raleigh-Durham, NC. Lost hydraulic quantity. Used aux pump. Landed at destination. Broken hydraulic line at rudder aux pump.
- [Accident 19950216001889A](https://openairdocs.org/incident/19950216001889A), Feb 16, 1995: Doug DC863 (N782AL), Kansas City, MO, Destroyed, 3 fatal. Attempted three engine takeoff. Lost control. Aborted. Lacked speed for vmcg. Pilot fatigue. Training a factor.
- [Incident 19941101046959I](https://openairdocs.org/incident/19941101046959I), Nov 1, 1994: Doug DC863 (N964R), Detroit, MI, Minor damage. Ran into starty cart after starting engine without setting parking brake.
- [Incident 19940209024289I](https://openairdocs.org/incident/19940209024289I), Feb 9, 1994: Doug DC863 (N345JW), Chicago, IL, Minor damage. Narrative: non FAA facilities- this incident occurred on the united parcel service ramp at ord. F.a.r. violation-121.135 non compliance with approved company…
- [Incident 19940127024799I](https://openairdocs.org/incident/19940127024799I), Jan 27, 1994: Doug DC863 (N951R), Chicago, IL, Minor damage. Narrative: o'Hare ATC tower cleared emery flt. 36 to land on runway 9L at ord, with a braking action report as good, based on two previous BE-1900 aircraft…
- [Incident 19930915044069I](https://openairdocs.org/incident/19930915044069I), Sep 15, 1993: Doug DC863 (N870BX), Toledo, OH. Had severe aileron control problems on approach. Made missed approach, landed safely.
- [Incident 19930409015969I](https://openairdocs.org/incident/19930409015969I), Apr 9, 1993: Doug DC863 (N870BX), Milwaukee, WI, Minor damage. Lost a main wheel while taxiing for departure. Pilot not aware of problem until after landing at destination.
- [Incident 19930312007289I](https://openairdocs.org/incident/19930312007289I), Mar 12, 1993: Doug DC863 (N870BX), Toledo, OH. While turning off runway onto taxiway aircraft rolled off taxiway uncontroled. Had no braking action.
- [Incident 19920214010889I](https://openairdocs.org/incident/19920214010889I), Feb 14, 1992: Doug DC863 (N782AL), Houston, TX, Minor damage. On takeoff aircraft experienced yaw and buffeting. Continued. On landing found NR1 engine forward cowl missing.
- [Incident 19910516028419I](https://openairdocs.org/incident/19910516028419I), May 16, 1991: Doug DC863 (N816AX), Greensboro, NC, Minor damage. While on a test flight engine one and two compressor stalled when recovery power advanced. Pilot recovered.
- [Incident 19910419025489I](https://openairdocs.org/incident/19910419025489I), Apr 19, 1991: Doug DC863 (N868BX), Houston, TX. Fuel tank access panel seal was leaking. Area was hosed down by fire department.
- [Incident 19910129004219I](https://openairdocs.org/incident/19910129004219I), Jan 29, 1991: Doug DC863 (N951R), Ft Lauderdale, FL. A system hydraulic failure. Declared emergency. Landed safely. Hydraulic line to uplock side of actuator replaced.
- [Incident 19901004053489I](https://openairdocs.org/incident/19901004053489I), Oct 4, 1990: Doug DC863 (N950R), Dayton, OH, Minor damage. Left main gear contacted ground 4 feet east of runway. Struck 2 runway lights. Had a wind shear on approach.
- [Incident 19900326005759I](https://openairdocs.org/incident/19900326005759I), Mar 26, 1990: Doug DC863 (N796AL), Stockton, CA, Minor damage. NR1 engine struck the runway while making a touch and go landing. Aircraft ferried to miami for engine change.
- [Accident 19890713022169A](https://openairdocs.org/incident/19890713022169A), Jul 13, 1989: Doug DC863F (N950R), Dayton, OH, Substantial damage. Lost hydraulic pressure taxiing to gate. Auxiliary braking failed. Hit parked aircraft.
- [Incident 19890203014799I](https://openairdocs.org/incident/19890203014799I), Feb 3, 1989: Doug DC863 (N868BX), Fort Wayne, IN, Minor damage. Maneuvering for a turn on ice, left gear left runway. Power application caused right gear to leave also.
- [Incident 19881013062529I](https://openairdocs.org/incident/19881013062529I), Oct 13, 1988: Doug DC863 (N869BX), Fort Wayne, IN. Left main anti-skid locked on landing. Slid to side hitting runway light with nose gear. Recovered without incident
- [Incident 19880122014329I](https://openairdocs.org/incident/19880122014329I), Jan 22, 1988: Doug DC863 (N951R), Ft Lauderdale, FL, Minor damage. Smoke and flame from main wheel. Fire extinguished. Found hydraulic fluid from main gear strut flowing onto brake.
- [Accident 19870820079082A](https://openairdocs.org/incident/19870820079082A), Aug 20, 1987: Doug DC863 (N951R), Newburgh, NY, Substantial damage. Cleared back taxi on runway after landing. On turn off tail was hit by landing DC9 N908AX. ATC failed advise DC9.
- [Incident 19861113079889I](https://openairdocs.org/incident/19861113079889I), Nov 13, 1986: Doug DC863 (N964R), Ft Lauderdale, FL. Aircraft was taxied at the direction of a marshaller onto unstressed pavement. Damge to pavement only.
- [Accident 19851212077879A](https://openairdocs.org/incident/19851212077879A), Dec 12, 1985: Doug DC863 (N950JW), Gander, CN, Destroyed, 253 fatal. Stalled during takeoff,with ice on wing. Wrong vref, possible loss of engine thrust. Casb dissenting opinion on file
- [Incident 19841206072199I](https://openairdocs.org/incident/19841206072199I), Dec 6, 1984: Doug DC863 (N4935C), Orlando, FL, Minor damage. Diverted after warning light for gear door and latch lighted. Aeroquip line broken.

## Service difficulty reports (1,601, newest 50)

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

- [SDR ABXA060151](https://openairdocs.org/sdr/ABXA060151), Mar 23, 2006: SKIN. CORRODED. FOUND FUSELAGE EXTERIOR FASTENER SHEARED AT LONGERON 39 LEFT AND SKIN BULGED AT FS -32.00. REPAIRED FUSELAGE EXTERIOR SKIN AT FS 32.00, LONGERON 30 LEFT IAW DC8
- [SDR ABXA060149](https://openairdocs.org/sdr/ABXA060149), Mar 15, 2006: STRUT. CORRODED. RIGHT MAIN LANDING GEAR STRUT CYLINDER SHOWED PITTING ALONG THE INNER SURFACE AT LOWER FLANGE AT CHROME AREA. DAMAGED GLAND THREADS. RIGHT MAIN LANDING GEAR STR
- [SDR ABXA060150](https://openairdocs.org/sdr/ABXA060150), Mar 14, 2006: SUPPORT. CRACKED. RIGHT INBOARD AILERON MANUAL REVERSION MECHANISM CRACKED AT UPPER MOUNT HOLE. REMOVED AND REPLACED SUPPORT ASSEMBLY ON AILERON MANUAL REVERSION MECHANISM IAW DC
- [SDR ABXA060148](https://openairdocs.org/sdr/ABXA060148), Mar 13, 2006: FITTING. CRACKED. FOUND RIGHT WING FUEL, NR 6 STRINGER TIE INSIDE PANEL 505C CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA060147](https://openairdocs.org/sdr/ABXA060147), Mar 13, 2006: FITTING. CORRODED. RIGHT WHEEL WELL LONGERON 24 RIGHT, BATHTUB FITTING STA 879 CORRODED. DAMAGE OUT OF LIMITS AND CRACKED. REMOVED CORRODED BATHTUB FITTING. DRILLED UP NEW ONE AND
- [SDR ABXA060079](https://openairdocs.org/sdr/ABXA060079), Feb 2, 2006: LANDING GEAR. MALFUNCTIONED. AFTER TAKEOFF AT ILN, UNABLE TO RAISE LANDING GEAR HANDLE. DID NOT USE FLIGHT HANDLE RELEASE, AIRCRAFT WAS IN FLIGHT MODE. CREW FLEW AIRCRAFT WITH ALL THREE GEA
- [SDR ABXA060041](https://openairdocs.org/sdr/ABXA060041), Jan 15, 2006: STRINGER. CRACKED. LEFT WING (AFT SIDE) STRINGER LONGERON 58 WS 428 - 463 END FITTING CRACKED. REMOVED DAMAGED STRINGER END FITTING TWO CRACKS, ONE 4.5" AND ONE 12.0". FABRICATED 
- [SDR ABXA060045](https://openairdocs.org/sdr/ABXA060045), Jan 14, 2006: SPAR CAP. CORRODED. WING CENTER SECTION UPPER SURFACE HAD TWO AREAS OF CORROSION WITH PITTING BS 851, RIGHT BUTT LINE 12, BS 851, RIGHT BUTT LINE 17. CUT OUT DAMAGED AREA AND REPAI
- [SDR ABXA060043](https://openairdocs.org/sdr/ABXA060043), Jan 14, 2006: FITTING. CORRODED. BATHTUB FITTING HAD CORROSION AT LONGERON 34, ATTACH POINT BS 879. CORROSION FOUND OUT OF LIMITS OF DC8 SRM 53-2-0. REMOVED FITTING IAW DC8 SRM 51-1-20D. INSTAL
- [SDR ABXA060044](https://openairdocs.org/sdr/ABXA060044), Jan 13, 2006: FITTING. CORRODED. BATHTUB FITTING HAD CORROSION AT LONGERON 24, ATTACH POINT BS 940. CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-20. INSTALLED NEW FITTING IAW DC8 SRM 53-2
- [SDR ABXA060042](https://openairdocs.org/sdr/ABXA060042), Jan 12, 2006: SKIN. CORRODED. DEFOLIATED SKIN ON BELLY OF PLANE JUST AFT OF SKIN DOUBLER AT APPROXIMATELY STA 1420, LONGERON 36. REPAIRED AREA IAW ABX REA D853-51398-MR.
- [SDR ABXA060025](https://openairdocs.org/sdr/ABXA060025), Jan 12, 2006: BOLT. BROKEN. INFLIGHT WITH AIRLOAD WHEN FLAPS 12 DEGREES SELECTED, THERE WAS AN AUDIBLE NOISE AND A NOTICEABLE SHUDDER. FOUND ROUND ROLLER HANGER BOLTS BROKEN ON THE RIGHT I
- [SDR ABXA060046](https://openairdocs.org/sdr/ABXA060046), Dec 23, 2005: STRAP. CORRODED. CORROSION ON ANGLE STRAP ON TOP OF MAIN LANDING GEAR WHEEL WELL BOX FORWARD OF FLOORBEAM STA 902, LEFT BUTT LINE 65. REMOVED CORROSION IAW DC8 SRM 51-1-8. DETER
- [SDR ABXA050263](https://openairdocs.org/sdr/ABXA050263), Nov 4, 2005: CABIN PRESSURE. UNKNOWN. DURING CLIMB AT FL310, CABIN RATE OF CLIMB WENT FROM 500 FPM TO 6,000 FPM. COULD NOT STOP THE CABIN FROM CLIMBING USING AUTO OR MANUAL LEVER. CABIN WENT TO 11,0
- [SDR ABXA050189](https://openairdocs.org/sdr/ABXA050189), Aug 17, 2005: ENGINE. FAILED. LOW OIL PRESSURE LIGHT NR 2 ENGINE OIL PRESSURE DROPPED TO 30 PSI. SHUT DOWN NR 2 ENGINE DOWN AT 0350Z. ZERO OIL PRESSURE AFTER ENGINE SHUT DOWN. REMOVED AND RE
- [SDR ABXA050179](https://openairdocs.org/sdr/ABXA050179), Jul 28, 2005: TRANSMITTER. DEFECTIVE. NR 3 ENGINE OIL PRESSURE PEGGED OFF SCALE HIGH. ENGINE WAS SECURED AND FLIGHT CONTINUED ON TO IAD. OIL PRESSURE REMAINED PEGGED OUT HIGH. PERFORMED ENGINE INSPE
- [SDR ABXA050178](https://openairdocs.org/sdr/ABXA050178), Jul 26, 2005: WIRE. BROKEN. PLACING GEAR HANDLE DOWN, NOSE GEAR LIGHT WOULD NOT COME ON WITH NO RED UNSAFE LIGHT. PERFORMED GEAR RECYCLE, VERIFIED. FOUND BROKEN WIRE AT CONNECTOR P1-215, P
- [SDR ABXA050093](https://openairdocs.org/sdr/ABXA050093), Apr 18, 2005: O-RING. FAILED. OUT OF MSP ENROUTE TO ILN, THE CREW REPORTED HYDRAULIC QUANTITY LOSS DOWN TO THE STANDPIPE. FOUND O-RING ON SLOT CONTACT VALVE BLOWN. REMOVED AND REPLACED O-RIN
- [SDR ARWA20041204](https://openairdocs.org/sdr/ARWA20041204), Dec 28, 2004: DRIVE LINK. BROKEN. DURING SERVICE CHECK, FOUND LEFT WING INBOARD FLAP DRIVE LINK BROKEN. REMOVED AND REPLACED LEFT WING INBOARD FLAP DRIVE LINK IN ACCORDANCE WITH DC8-MM 27-51-4. 
- [SDR ARWA20041101](https://openairdocs.org/sdr/ARWA20041101), Nov 5, 2004: O-RING. DAMAGED. LOSS OF HYDRAULIC PRESSURE EN ROUTE HYDRAULIC QUANTITY NORMAL. FOUND O-RING DAMAGED AT NR 3 ENGINE HYDRAULIC DRIVEN PUMP PRESSURE PORT. REMOVED AND REPLACED O-R
- [SDR ABXA040351](https://openairdocs.org/sdr/ABXA040351), Oct 15, 2004: OUTFLOW VALVE. MALFUNCTIONED. DURING DESCENT, CABIN PRESS WENT TO 2000 FT/MIN. RATE OF CLIMB UP TO 9500 CABIN ALT WITH NO CONTROL EITHER MANUALLY OR AUTOMATICALLY. RECOVERED AT FL 19000. COU
- [SDR ARWA20040902](https://openairdocs.org/sdr/ARWA20040902), Sep 27, 2004: BLEED VALVE. DEFECTIVE. DURING LINE UP FOR TAKE-OFF, NR 4 ENGINE FAIL TO ACCELERATE. FOUND DEFECTIVE SURGE BLEED VALVE. REMOVED AND REPLACED NR 4 SURGE BLEED VALVE IAW MM 75-30-3 AND S
- [SDR ABXA040381](https://openairdocs.org/sdr/ABXA040381), Sep 23, 2004: SKIN. CORRODED. CORROSION FUSELAGE SKIN STA 1040, LONGERON 36. DEFERRED TIL 9-6-04 IAW REA D853-50415, IAW ABX GMM CHAPTER 1 07-04. FABRICATED DOUBLER AND FILLER IAW REA D853-5
- [SDR ABXA040313](https://openairdocs.org/sdr/ABXA040313), Aug 26, 2004: SPAR CAP. DAMAGED. FRONT SPAR CAP AT NR 3 PYLON, INSIDE NR 4 MAIN TANK, HAD 3 EACH OVERSIZE HOLES. REPAIRED IAW REA D857-50013MR.
- [SDR ABXA040312](https://openairdocs.org/sdr/ABXA040312), Aug 20, 2004: SKIN. CORRODED. LEFT WHEEL WELL AFT TORQUE BOX LOWER SKIN, STA 980, INSIDE TORQUE WELL, CORRODED. REPAIRED AREA IAW REA D853-50008MR, REV A.
- [SDR ABXA040314](https://openairdocs.org/sdr/ABXA040314), Aug 17, 2004: LONGERON. CORRODED. FORWARD CARGO STA 600, LONGERON 31 LEFT, CORRODED. REPAIRED AREA IAW REA D853-50003-MR.
- [SDR ABXA040315](https://openairdocs.org/sdr/ABXA040315), Aug 9, 2004: SKIN. CORRODED. MAIN CABIN FS 759, RIGHT BUTT LINE 8, WING CENTER SECTION, CORRODED. FABRICATED REPAIR DOUBLER AND REPAIRED AREA IAW REA D857-49995-MR.
- [SDR ABXA040264](https://openairdocs.org/sdr/ABXA040264), Jul 12, 2004: LONGERON. CRACKED. LT MAIN LANDING GEAR WHEEL WELL LONGERON 24 CRACKED ON LOWER FLANGE AT BOTTLE BOLT CAVITY. REPAIRED AREA IAW REA D853-49163MR.
- [SDR ABXA040235](https://openairdocs.org/sdr/ABXA040235), Jun 30, 2004: FUEL CONTROL. DEFECTIVE. PASSING FL 200 ON DESCENT 320 KTS, AS THROTTLE ADVANCED NR 1 ENG FLAMED OUT. IMMEDIATE ACTION ITEM COMPLETED & ENG RESTARTED NORMALLY. MX INSPECTED FUEL TANK BO
- [SDR ARWA20040604](https://openairdocs.org/sdr/ARWA20040604), Jun 25, 2004: HYDRAULIC SYSTEM. CONTAMINATED. PRIOR TO TOP OF DESCEND BOTH HYDRAULIC PUMPS OUTPUT PRESSURE ZERO. AILERON AND RUDDER REVERSION LIGHTS ON. COMPLETED EMERGENCY ABNORMAL HYDRAULIC CHECKLIST. CHE
- [SDR ARWA20040503](https://openairdocs.org/sdr/ARWA20040503), May 11, 2004: SEAL DEPRESSOR. DAMAGED. ON CLIMB PRESSURIZATION LEAK HAPPENED AT FL 280. UNABLE TO MAINTAIN CABIN PRESSURE 10,000 FT. REMOVED AND REPLACED LOWER SEAL DEPRESSOR IAW AERONAUTICAL ENGINEE
- [SDR ARWA20040504](https://openairdocs.org/sdr/ARWA20040504), May 11, 2004: ACTUATOR. INOPERATIVE. DUMP CHUTE WILL NOT RETRACT ELECTRICALLY. REMOVE AND REPLACED AC MOTOR ACTUATOR IAW DC8 MM 28-30-2. OPERATIONAL CHECK ACCOMPLISHED FOUND OK IAW DC8 MM 28-30-2.
- [SDR ABXA040173](https://openairdocs.org/sdr/ABXA040173), Apr 28, 2004: SKIN. DAMAGED. RUDDER TRAILING EDGE TIP HAS METAL MISSING. REPAIRED ARE IAW DC-9 SRM 55-2-0, 51-1-2, 51-1-21A, 51-4-8 AND REA D855-49316MR.
- [SDR ABXA040155](https://openairdocs.org/sdr/ABXA040155), Apr 27, 2004: CONTROL BOX. DEFECTIVE. AFTER TAKEOFF, GEAR WARNING LIGHT REMAINED ON. LANDING GEAR AND DOOR INDICATOR PANEL SHOWED NOSE GEAR. RECYCLED, SAME RESULT. CONSULTED ABNORMAL AND PROCEEDED T
- [SDR ABXA040137](https://openairdocs.org/sdr/ABXA040137), Apr 5, 2004: FLOORBEAM. CORRODED. MAIN CABIN STA 920 FLOORBEAM LOWER FLANGE FORWARD SIDE WAS CORRODED APPROXIMATELY 5 INCHES INBOARD OF CUSP LEFT SIDE. REPAIRED AREA IAW REA D853-49122MR.
- [SDR ABXA040058](https://openairdocs.org/sdr/ABXA040058), Jan 30, 2004: ANGLE. GOUGED. LEFT WING OUTBOARD FLAP STA 219 FOLD HINGE COVER WELL OUTBOARD LOWER SIDE GOUGED. REPAIRED AREA IAW REA D827-48510MR.
- [SDR ABXA040054](https://openairdocs.org/sdr/ABXA040054), Jan 30, 2004: LONGERON. CORRODED. FORWARD ACCESSORY AT STA 25, LONGERON 31 LEFT WAS CORRODED. REPAIRED AREA IAW REA D853-48515MR.
- [SDR ABXA040057](https://openairdocs.org/sdr/ABXA040057), Jan 30, 2004: SPAR. CRACKED. RIGHT WING REAR SPAR XRS 139 JACKPAD TO REAR SPAR FITTING CRACKED. REPAIRED AREA IAW REA D857-48845MR.
- [SDR ABXA040056](https://openairdocs.org/sdr/ABXA040056), Jan 30, 2004: FINGER DOUBLER. CORRODED. FORWARD CARGO LOWER LEFT SKIN FINGER DOUBLER CORRODED UNDERNEATH FROM STA 200 TO 220, LONGERON 35 LEFT TO 33 LEFT, BUTTLINE 7 TO BUTTLINE 20. REPAIRED AREA IAW 
- [SDR ABXA040053](https://openairdocs.org/sdr/ABXA040053), Jan 30, 2004: LONGERON. CRACKED. RIGHT WHEEL WELL LONGERON 24 FITTING WAS CRACKED JUST UNDER BOTTLE BOLT. REMOVED AND REPLACED LONGERON 24 RIGHT IAW ABX REA D853-48504MR.
- [SDR ABXA040055](https://openairdocs.org/sdr/ABXA040055), Jan 30, 2004: LONGERON. CORRODED. AFT ACCESSORY COMPARTMENT CORROSION AT FUSELAGE SKIN AND DOUBLER LONGERON 33 RIGHT, FS 1620 - 1628, ADJACENT TO OUTFLOW VALVE. REPAIRED AREA IAW REA D853-48508M
- [SDR KO0R0323](https://openairdocs.org/sdr/KO0R0323), Jan 15, 2004: FITTING. CORRODED. EXTERNAL FUSELAGE SKIN HAS A BULGE AT FS315, LONGERON NR 33R. FOUND DOOR STRUCTURE FITTING CORRODED (FS 315, LONGERON 33R). REMOVED AND REPLACED FITTING IAW DC8
- [SDR ABXA030435](https://openairdocs.org/sdr/ABXA030435), Nov 7, 2003: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHT BATTERY DEAD. REPLACED EMERGENCY BATTERY PACK. SYSTEM CHECKED GOOD IAW DC8 MM 33.
- [SDR ABXA030394](https://openairdocs.org/sdr/ABXA030394), Oct 23, 2003: TRANSMITTER. DEFECTIVE. NR 4 ENGINE OIL PRESSURE INDICATED + 100 PSI AT TOP OF CLIMB. SECURED ENGINE AT 0325Z, RETURNED TO 22 PSI AT 0345. REPLACED NR 4 OIL PRESSURE TRANSMITTER, NR 4 
- [SDR ABXA030385](https://openairdocs.org/sdr/ABXA030385), Oct 8, 2003: SEAT. DEFECTIVE. FLIGHT ENGENEERS SEAT FELL DURING TAKE OFF AND INITIAL CLIMB. VERTICAL HOLD INOPERATIVE WITH SEAT POSITIONED FORWARD AT A 45 DEGREE ANGLE. SEAT NOT SAFE FOR FLI
- [SDR ABXA030386](https://openairdocs.org/sdr/ABXA030386), Oct 7, 2003: BRAKE ASSY. BROKEN. NR 8 BRAKE COMPENSATING LINK ATTACH POINT BROKE. REMOVED AND REPLACED BRAKE AND TIRE ASSEMBLY IN THE NR 8 POSITION IAW DC-8 MM 32-40-0.
- [SDR ARWA20030808](https://openairdocs.org/sdr/ARWA20030808), Aug 23, 2003: RETAINER. DAMAGED. MALFUNCTION OF PRESSURIZATION SYSTEM; CABIN CLIMB AT 2000 FT, A MIN UNABLE TO CONTROL. ADJUSTED SEAL RETAINER ON MAIN CARGO DOOR AT FORWARD LOWER AREA IAW MM 52
- [SDR ABXA030322](https://openairdocs.org/sdr/ABXA030322), Aug 4, 2003: ACTUATOR. BROKEN. DURING FLAP EXTENTION ON FINAL APPROACH AT APPROXIMATELY 5 DEGREES FLAPS, THE RIGHT AND LEFT FLAP INDICATORS SPLIT APPROXIMATELY 5-8 DEGREES WITH AN AIRCRAFT RO
- [SDR ABXA030321](https://openairdocs.org/sdr/ABXA030321), Aug 4, 2003: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY RACK ASSEMBLY IAW DC8 MM 33-50-01. CHECKED GOOD.
- [SDR ABXA030308](https://openairdocs.org/sdr/ABXA030308), Jul 22, 2003: SPRING. WORN. THE GEAR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY ACCOMPANIED WITH LEFT DOOR NOT LATCHED LIGHT AT FLIGHT ENGINEER'S PANEL. PERFORMED ABNORMAL CHECK, UNSAFE LIGHT

All 1,601: https://openairdocs.org/model/mcdonnell-douglas-dc-8-63/reports.md

## STCs that may be installed (OpenAirDocs) (194, 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 SA3180NM](https://openairdocs.org/stc/SA3180NM): Installation of Spacelite 8 Interior Retrofit Kits. Safran Cabin Inc
- [STC SA3169NM](https://openairdocs.org/stc/SA3169NM): Installation of floor proximity emergency escape marking system. Bruce Aerospace Inc
- [STC SA3166SO](https://openairdocs.org/stc/SA3166SO): Installation of an Expanded parameters Digital Flight Data Recorder. Acron Aviation Inc
- [STC ST01078AT](https://openairdocs.org/stc/ST01078AT): Installation of an expanded, 17-parameters, Allied Signal, or Loral-Fairchild, Digital Flight Data Recorder (DFDR). Acron Aviation Inc
- [STC ST01174CH](https://openairdocs.org/stc/ST01174CH): Installation of UPS Aviation Technologies ADS-B provisions and Honeywell Mode-S System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings 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-8 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-8 Series
- [STC SA863EA](https://openairdocs.org/stc/SA863EA): Incorporation of DME Corporation emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 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 SA5720NM](https://openairdocs.org/stc/SA5720NM): Installation of the Mark VII ground proximity and windshear warning system. Honeywell International Inc
- [STC SA502NE](https://openairdocs.org/stc/SA502NE): Installation of Inflight Services Video System, for Hawaiian Air. Burrana Inc
- [STC SA3421NM](https://openairdocs.org/stc/SA3421NM): Installation of Hughes-Avicom video entertainment system. Burrana Inc. Lists DC-8 Series
- [STC SA1066NM](https://openairdocs.org/stc/SA1066NM): Installation of a Video Projection System. Burrana Inc
- [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC
- [STC SA3140SO](https://openairdocs.org/stc/SA3140SO): Installation of a replacement coalescer filter, P/N 22D10 or 22D10-2. Purolator Facet, Inc
- [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic LLC
- [STC ST01067LA](https://openairdocs.org/stc/ST01067LA): Installation of Litton LTR-97 fiber optic gyro systems. Northrop Grumman Systems Corporation
- [STC ST01467LA-D](https://openairdocs.org/stc/ST01467LA-D): Installation of Universal Avionics Terrain Avoidance Warning System and MFD-640 Multi Function Display(s). Zalinka Aviation Support, LLC
- [STC ST01468LA-D](https://openairdocs.org/stc/ST01468LA-D): Installation of Universal Avionics Flight Management System. Zalinka Aviation Support, LLC
- [STC SA1511GL](https://openairdocs.org/stc/SA1511GL): Installation of Type "C" containers. ABX Air Incorporated
- [STC SA1775GL](https://openairdocs.org/stc/SA1775GL): Incorporate maximum permissible quick turn-around landing weight (flaps 35º). ABX Air Incorporated
- [STC SA1794GL](https://openairdocs.org/stc/SA1794GL): Incorporate anti-skid system inoperative and/or auto-ground spoilers inoperative landing field length data for Operations using 35° landing flaps. ABX Air Incorporated
- [STC SA2303SO](https://openairdocs.org/stc/SA2303SO): Installation of standard equipment as as required by AC120-29. ABX Air Incorporated
- [STC ST00670CH](https://openairdocs.org/stc/ST00670CH): Installation of single or dual II Morrow, Apollo 2101/2102 GPS Navigation Management Computer Systems. ABX Air Incorporated
- [STC SA1421GL](https://openairdocs.org/stc/SA1421GL): Installation of Supplemental Electric Heater. ABX Air Incorporated
- [STC SA1462GL](https://openairdocs.org/stc/SA1462GL): Installation of ABX Cargo Handling System. ABX Air Incorporated
- [STC SA3496NM](https://openairdocs.org/stc/SA3496NM): Installation of ABX-C Cargo Container assembly. Airborne Express Air Inc
- [STC ST369CH](https://openairdocs.org/stc/ST369CH): Approve autopilot and/or flight director coupled approach with 35 landing flap selection. ABX Air Incorporated
- [STC SA7729SW](https://openairdocs.org/stc/SA7729SW): Installation of digital fuel quantity indicators, fuel totalizer, and capacitive fuel compensator units. Ontic Engineering and Manufacturing Inc
- [STC SA2304SO](https://openairdocs.org/stc/SA2304SO): Installation of dual Bendix EFS-10 with MFD and dual Collins FDS-85 system. ABX Air Incorporated
- [STC SA2306SO](https://openairdocs.org/stc/SA2306SO): Installation of the Sperry directional gyro system. ABX Air Incorporated
- [STC SA2307SO](https://openairdocs.org/stc/SA2307SO): Installation of the third vertical gyro system. ABX Air Incorporated
- [STC SA2308SO](https://openairdocs.org/stc/SA2308SO): Installation of the dual IDC Series 35900 mach/airspeed indicator system. ABX Air Incorporated
- [STC SA2310SO](https://openairdocs.org/stc/SA2310SO): Installation of the dual Kollsman/IDC 28007-427 encoding altimeters with standby altimeter system. ABX Air Incorporated
- [STC SA2313SO](https://openairdocs.org/stc/SA2313SO): Installation of the Bendix RDR-4A radar system. ABX Air Incorporated
- [STC SA2318SO](https://openairdocs.org/stc/SA2318SO): Installation of the door warning system. ABX Air Incorporated
- [STC SA1360GL](https://openairdocs.org/stc/SA1360GL): Install Parker Hannifin Freon Air Conditioning System. ABX Air Incorporated
- [STC SA1616GL](https://openairdocs.org/stc/SA1616GL): Installation of Ametek digital fuel flow/fuel used indicator P/N10250N010F01. ABX Air Incorporated
- [STC SA1733GL](https://openairdocs.org/stc/SA1733GL): Installation of Vickers PV3-160-4B hydraulic pump. ABX Air Incorporated
- [STC SA1761GL](https://openairdocs.org/stc/SA1761GL): Installation of Kollsman P/N 35900-A2284 Mach airspeed indicator. ABX Air Incorporated
- [STC SA2320SO](https://openairdocs.org/stc/SA2320SO): Installation of the Fairchild F-800 digital flight data recorder system. ABX Air Incorporated
- [STC ST117CH](https://openairdocs.org/stc/ST117CH): Installation of expanded parameters. ABX Air Incorporated
- [STC ST125CH](https://openairdocs.org/stc/ST125CH): Installation of JET model AI-330 attitude indicator. ABX Air Incorporated
- [STC ST53CH](https://openairdocs.org/stc/ST53CH): Replacement of McD PN 4642526 compressor check valve flapper assembly with ABX Air, PN A04574. ABX Air Incorporated
- [STC SA2827WE-D](https://openairdocs.org/stc/SA2827WE-D): Installation of Collins FPC-75 part number 622-2615-012 or 622-2615-212 Ground Proximity Warning System Computer in conformance with United Airlines DAS-1-WE Approved Master List of drawings and documents for STC No. SA2827WE-D dated February 26, 1979 or later approved revisions. An alternate approved configuration consists of part number 622-2615-011 Rev. N or part number 622-2615-211 GPWS computer and a part number 622-2668-011 Barometric Altitude Computer installed in conformance with DAS-1-WE Approved Master List of drawings and related documents or later FAA approved revision (Continued on page 3.). United Airlines Inc
- [STC SA4-918](https://openairdocs.org/stc/SA4-918): 1. Aircraft wiring in accordance with Douglas Aircraft Co. Service Change #17 (UAL COA-0-1456) to provide an operational Aircraft Flight Data Rrecorder conforming to CAR Amendment 40-6, paragraph 40.208 with the following additions to assure recording of data during takeoff and landing roll: a. Relay to provide automatic start of recording when nose landing gear reaches airborne condition on takeoff. b. Time delay relay to turn off recorder one minute after nose landing gear reaches "on ground" condition, on landing. c. Installation of standard toggle switch on Systems Engineer's Console, to permit Second Officer to turn on recorder at start of takeoff run. 2. Install Waste King Flight Data Recorder #5424, TSO-C51. United Airlines Inc
- [STC SA611WE](https://openairdocs.org/stc/SA611WE): Interior configuration - 120 passenger single class 5-abreast seating per United Air Lines approved drawing lists: COA 2-2083 (Sheet #1 Revision February 17, 1964, Sheet #2 dated December 4, 1963, Sheet #3 Revision dated February 27, 1964 and, COA 2-2099 Revision dated December 17, 1963). United Airlines Inc

All 194: https://openairdocs.org/model/mcdonnell-douglas-dc-8-63/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.

- [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
- [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
- [WF334995](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108821019820250602133022.0001): Filter Element Lube Oil. Donaldson Company Inc · PMA PQ2432CE · Replaces Sundstrand 55956, AC-9649F-1… · May 23, 2025
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192694002020250923105634.0001): VOGT AERO · PMA PQ05310NM · Apr 22, 2025
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165781403520250923105628.0001): VOGT AERO · PMA PQ05310NM · Apr 22, 2025
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178263063620250923105931.0001): VOGT AERO · PMA PQ05310NM · Mar 4, 2025
- [3575-1251-07-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172611889620260729202728.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1251-07 · Mar 4, 2025
- [3575-1480-01-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170852615820260729202754.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1480-01 · Mar 4, 2025
- [3575-1251-01-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169467633820260729202723.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1251-01 · Mar 4, 2025
- [440-0150-5-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128051330520260729202746.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 440-0150-5 · Mar 4, 2025
- [3575-1480-07-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122566397220260729202800.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1480-07 · Mar 4, 2025
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110795794120250923105918.0001): VOGT AERO · PMA PQ05310NM · Mar 4, 2025
- [440-0150-3-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106234740920260729202739.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 440-0150-3 · Mar 4, 2025
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101731757320260729202734.0001): Vogt Aero LLC · PMA PQ05310NM · Mar 4, 2025
- [DEC31-027-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146178353220250304142404.0001): Shaft Drive Fuel Pump. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces Airesearch P/N 3603685-1 · Feb 27, 2025
- [103154-909-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118409506520230727204617.0001): Safety Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 103154-909-2 · Apr 20, 2023
- [122618-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156194142520230907183534.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 122618-1-1 · Feb 24, 2023
- [320362-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152527095020230907183533.0001): Solenoid Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 320362-2 · Feb 24, 2023
- [383342-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133028187220230907183536.0001): Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 383342-1-1 · Feb 24, 2023
- [105984-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119902323020230907183537.0001): Anti-Ice Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105984-2 · Feb 24, 2023
- [392900-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189455606920230907183331.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 392900-1-1 · Feb 23, 2023
- [398018-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163636197720230907183315.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 398018-1-1 · Feb 23, 2023
- [108742-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159430638720230907183327.0001): Pressure Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 108742-2 · Feb 23, 2023
- [105976-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152035340520230907183326.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105976-1 · Feb 23, 2023
- [122546-2-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145869651920230907183329.0001): Pressure Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 122546-2-1 · Feb 23, 2023
- [105980-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140197898520230907183328.0001): Butterfly Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105980-2 · Feb 23, 2023
- [105982-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110550695020230907183313.0001): Pneumatic Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105982-2 · Feb 23, 2023
- [525254-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108708698020230907183333.0001): Actuator Assy Fuel Dump Chute. Honeywell International Inc. · PMA PQ1222NM · Replaces 525254-1 · Feb 23, 2023
- [392160-4-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108409609920230907183330.0001): Pressure Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 392160-4-1 · Feb 23, 2023
- [SM600BA100N22-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189709749720221130144515.0001): Remote Control Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces BAN7016-607 · Oct 31, 2022
- [160-066-80](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185108580520221130144357.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0012-80 · Oct 31, 2022
- [1526-066-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166131476020221130144341.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0002-3 · Oct 31, 2022
- [1200-066-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164799404820221130144328.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0009-15 · Oct 31, 2022
- [H20-9B](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139073107020221130144509.0001): Switch. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces H20-9B · Oct 31, 2022
- [SM600BA20N25](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123850243020221130144521.0001): Remote Control Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces SM600BA20N25 · Oct 31, 2022
- [160-083-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123725710320221130144400.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0012-70P · Oct 31, 2022
- [1200-066-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115243180520221130144326.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0009-10 · Oct 31, 2022
- [3755705-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192798688420220929114601.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3755705-1 · Sep 27, 2022
- [3718232-504](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188697278020220929114502.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-504 · Sep 27, 2022
- [3718232-503](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188413757320220929114501.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-503 · Sep 27, 2022
- [3718232-505](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183899181420220929114502.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-505 · Sep 27, 2022
- [3718232-516](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181531934020220929114509.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-516 · Sep 27, 2022
- [3889142-510](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180513779620220929113517.0001): PANEL A. AmSafe Bridport · PMA PQ2482NM · Replaces 3889142-510 · Sep 27, 2022
- [3889142-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179267638820220929113509.0001): PANEL A. AmSafe Bridport · PMA PQ2482NM · Replaces 3889142-1 · Sep 27, 2022
- [3718232-511](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178457873520220929114507.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-511 · Sep 27, 2022
- [3718231-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168988236720220929113547.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718231-1 · Sep 27, 2022
- [3755704-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162454280820220929114510.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3755704-1 · Sep 27, 2022

All of them: https://openairdocs.org/model/mcdonnell-douglas-dc-8-63/pma.md

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