# Mcdonnell Douglas DC-8-62

- Type: Aircraft model (FAA registry)
- Registry code: 302197B
- Manufacturer (registry): MCDONNELL DOUGLAS
- Model: DC-8-62
- 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-8-62

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 2008-22-01](https://openairdocs.org/ad/2008-22-01): Auxiliary fuel tanks · Boeing 727-100 Series, 727-200 Series, 727 Series and 17 more. Effective Nov 26, 2008
- [AD 2008-06-23](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 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
- [AD 2000-09-02](https://openairdocs.org/ad/2000-09-02): Main Deck Cargo Door · Cargo door and cargo interior (Plattner STC SA1832SO). Effective Jun 6, 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 150: https://openairdocs.org/model/mcdonnell-douglas-dc-8-62/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)

- [N995CF](https://openairdocs.org/aircraft/N995CF): [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 1968, S/N 46024

## NTSB investigations (6)

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 CHI00LA047](https://openairdocs.org/ntsb/CHI00LA047), Dec 17, 1999: Douglas DC-8-62 (N995CF), Indianapolis, IN, substantial damage. Probable cause: the flight crew misjudged the clearance between their right wing and the radome of the parked aircraft. A factor associated with the accident was the ground handling contractor failed to identify the…
- [NTSB DCA89RA056](https://openairdocs.org/ntsb/DCA89RA056), Jun 7, 1989: McDonnell Douglas DC-8-62 (N1809E), Paramaribo, Suriname, destroyed, 174 fatal
- [NTSB MIA80RA003](https://openairdocs.org/ntsb/MIA80RA003), Oct 14, 1979: Douglas DC-8 (N1809E), Panama Cty, St. Pierre & Miquelon, substantial damage
- [NTSB MIA77IA057](https://openairdocs.org/ntsb/MIA77IA057), May 10, 1977: Douglas DC-8 (N810BN), Miami, FL, incident, minor damage
- [NTSB FTW75AF040](https://openairdocs.org/ntsb/FTW75AF040), Dec 5, 1974: Douglas DC-8 (N1803), Bogota, Colombia, no damage
- [NTSB FTW70AF060](https://openairdocs.org/ntsb/FTW70AF060), Mar 18, 1970: Douglas DC-8 (N1803), Guayaquil, Ecuador, no damage

## FAA accident and incident reports (23)

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 20000111003289I](https://openairdocs.org/incident/20000111003289I), Jan 11, 2000: Doug DC862 (N801MG), Fort Wayne, IN. Aircraft hydraulic press dropped to mid-scale. Found cracked pump housing on standby rudder pump.
- [Accident 19991217046279A](https://openairdocs.org/incident/19991217046279A), Dec 17, 1999: Doug DC862 (N995CF), Indianapolis, IN, No damage. (-23) Aircraft was parked on spot B4C. Evergreen ground control gave taxi instructions to taxi off spot B4C to box 2 following the greeen dotted line. Ground…
- [Incident 19991208041639I](https://openairdocs.org/incident/19991208041639I), Dec 8, 1999: Doug DC862 (N31CX), Jacksonville, FL, Minor damage. (-23) During ground taxi operations flight crew performed an uncommanded right turn, and struck a building. Right hand turn wing tip damaged and right hand…
- [Incident 19991103038659I](https://openairdocs.org/incident/19991103038659I), Nov 3, 1999: Doug DC862 (N802MG), Fort Wayne, IN. #3 Engine shut down due to fire warning light. Found lower fire loop connector had broken wires.
- [Incident 19990417026069I](https://openairdocs.org/incident/19990417026069I), Apr 17, 1999: Doug DC862 (N993CF), Minneapolis, MN, Minor damage. While parking at gate, marshaler failed to observe instructions from wingwalkers for aircraft to stop. Pilot was on centerline and following marchallers…
- [Incident 19980714025809I](https://openairdocs.org/incident/19980714025809I), Jul 14, 1998: Doug DC862 (N993CF), Newburgh, NY. After takeoff pilot experienced #4 engine warning. Discharged fire bottle and fire warning light extinguished. On landing roll out, fire warning indication…
- [Incident 19980613036149I](https://openairdocs.org/incident/19980613036149I), Jun 13, 1998: Doug DC862F (N995CF), Dayton, OH, Substantial damage. (-5) On the above date and time emery 024 (heavy) was departing day when the main cargo door opened for unknown reasons. According to statements by the flight…
- [Incident 19980320026969I](https://openairdocs.org/incident/19980320026969I), Mar 20, 1998: Doug DC862 (N181SK), Wilmington, OH. Acft descended below minimum safe altitude on ILS 4L approach to iln. Acft desended to 1500' MSL in area that was charted as 2800' MSL minimum alt. With…
- [Incident 19980205005809I](https://openairdocs.org/incident/19980205005809I), Feb 5, 1998: Doug DC862 (N802BN), Dayton, OH. Narrative: on the above date and time inspectors, mark m. mcconaughy and James l. jackson responded to the Dayton international airport on the complaint of a…
- [Incident 19970919030319I](https://openairdocs.org/incident/19970919030319I), Sep 19, 1997: Doug DC862 (N801MG), Buffalo, NY. Narrative: on Friday, September 19, 1997 at 11:53 local time, a Mcdonnell Douglas DC-8-63, s/n 45986, registered to American international airways, heard a…
- [Incident 19960613029389I](https://openairdocs.org/incident/19960613029389I), Jun 13, 1996: Doug DC862 (N772CA), Philadelphia, PA, Minor damage. Narrative: during a maintenance nighttime taxi operation the aircraft's left wing tip and closure rib was damaged after striking the right wing tip of a world…
- [Incident 19960609017419I](https://openairdocs.org/incident/19960609017419I), Jun 9, 1996: Doug DC862 (N51CX), Rochester, NY. Narrative: #4 engine had an overheat condition after take-off at Rochester. Pilot shut down engine and dumped 10,000 lbs of fuel over lake ontario. Aircraft…
- [Incident 19960306007059I](https://openairdocs.org/incident/19960306007059I), Mar 6, 1996: Doug DC862 (N993CF), Peoria, IL. Narrative: on March 6, 1996, at approximately 2240 CST, emery worldwide airlines DC-8 aircraft, N993CF, was taxiing on taxiway a. the aircraft slid sideways…
- [Incident 19951021038329I](https://openairdocs.org/incident/19951021038329I), Oct 21, 1995: Doug DC862 (N801AX), Pittsburgh, PA. Narrative: after departure from rochester, new york, and during the climb-out phase of the flight, #3 engine fire light illuminated and the appropriate…
- [Incident 19910121003939I](https://openairdocs.org/incident/19910121003939I), Jan 21, 1991: Doug DC862 (N993CF), Dover, DE. Co-pilot became sick en route. Removed from co-pilots position. Transported to hospital at airport.
- [Accident 19890607014469A](https://openairdocs.org/incident/19890607014469A), Jun 7, 1989: Doug DC862 (N1809E), Paramaribo, Destroyed, 14 fatal. Crashed short of runway . Appeared airport was shrouded in thick fog.
- [Incident 19881027067129I](https://openairdocs.org/incident/19881027067129I), Oct 27, 1988: Doug DC862 (N995CF), Indianapolis, IN, Minor damage. Aircraft hit light pole while being directed by ground personnel to gate. No guide line for large aircraft.
- [Incident 19870917076229I](https://openairdocs.org/incident/19870917076229I), Sep 17, 1987: Doug DC862 (N1803), Philadelphia, PA. Allegedly taxied within 5 feet of a DC9. Wing went over cockpit, wing walkers. Airborne express word against ups.
- [Incident 19851104058839I](https://openairdocs.org/incident/19851104058839I), Nov 4, 1985: Doug DC862 (N1803), Ypsilanti, MI. On touchdown hydraulic quantity and pressure went to zero. Hydraulic accumulator exploded. Mounting bracket cracked
- [Incident 19840429021789I](https://openairdocs.org/incident/19840429021789I), Apr 29, 1984: Doug DC862 (N1803), Honolulu, HI, Minor damage. Left wing hit a portable stand while taxiing to gate. A mechanic was guiding aircraft to the gate.
- [Incident 19800124017269I](https://openairdocs.org/incident/19800124017269I), Jan 24, 1980: Doug DC862 (N1803), Washington, DC. Ice patches on runway. Ok after normal landing and attempting to turn off the runway, nose gear slid off runway.
- [Incident 19790723021169I](https://openairdocs.org/incident/19790723021169I), Jul 23, 1979: Doug DC863 (N1809E), Los Angeles, CA, Minor damage. Aircraft was pushed back before passenger door was closed. Door made contact with jetway.
- [Incident 19781228020179I](https://openairdocs.org/incident/19781228020179I), Dec 28, 1978: Doug DC862 (N810BN), Miami, FL. Flight hit unexpected turbulance during descent causing injuries to cabin crew and passengers.

## Service difficulty reports (2,778, newest 50)

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

- [SDR IXXA201308180280](https://openairdocs.org/sdr/IXXA201308180280), Aug 18, 2013: BLEED VALVE. MALFUNCTIONED. COMPRESSOR STALL AT APPROX 75 KNOTS. SUSPECT NR 1 AND 2 ENGINES. RAN NR 1 AND 2 ENGINES IAW ENGINE RUN HANDBOOK 70.01. FOUND NR 1 ENGINE PRESSURE RATIO BLEED CO
- [SDR IXXA20130202002O](https://openairdocs.org/sdr/IXXA20130202002O), Feb 2, 2013: LINK. INOPERATIVE. ON CLIMBOUT, AFTER A GOOD UPLATCH CHECK, HEARD A LOUD NOISE IN NOSE GEAR AREA. (SOUNDED LIKE A NOSE GEAR DOOR POPPED OPEN). R & R RT NLG DOOR FORWARD LINK ASSY 
- [SDR IXXA2013020700006](https://openairdocs.org/sdr/IXXA2013020700006), Dec 5, 2012: SKIN. CRACKED. RT WING UPPER SKIN CRACKED AT XRS 22.750 S17. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIGURE 8. TRIMMED OUT CRACK ON RT WING UPPER SKIN IAW SRM 57-2-1. FABRICATED
- [SDR IXXA2013020700005](https://openairdocs.org/sdr/IXXA2013020700005), Nov 23, 2012: PANEL. DAMAGED. RT WING OTBD FLAP LOWER PANEL WITH SEVERAL DENTS AND SCRATCHES XF 415 - 452. PERFORMED MAJOR REPAIR IAW SRM 57-7-1, FIG 4, TR 57-94. REMOVED OTBD FLAP LOWER PAN
- [SDR IXXA2013020700004](https://openairdocs.org/sdr/IXXA2013020700004), Nov 12, 2012: FITTING. CORRODED. AFTER CARGO COMPARTMENT - INTERIOR BATHTUB FITTING CORRODED AT STA 1530.000, L-32R (AFTER PART). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, NOV 15, 2012, DWG E
- [SDR IXXA2013020700003](https://openairdocs.org/sdr/IXXA2013020700003), Nov 12, 2012: FITTING. CORRODED. AFTER ACCESSORY COMPARTMENT INTERIOR BATHTUB FITTING CORRODED AT STA 1530.000 L-34R (AFTER PART). PERFORMED MAJOR REPAIR IAW FORM 8110-3 DWG NR ED-5546 NOV 15,2
- [SDR IXXA2013020700002](https://openairdocs.org/sdr/IXXA2013020700002), Nov 9, 2012: SKIN. CORRODED. RUDDER SKIN-LT PANEL SHOWS CORROSION FROM STA ZR 140.750 TO STA ZR 150.750. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED EXISTING DAMAGED PANEL IAW SRM
- [SDR IXXA121109SMN026S](https://openairdocs.org/sdr/IXXA121109SMN026S), Nov 9, 2012: LONGERON. CRACKED. LONGERON 24R, HORIZONTAL LEG CRACKED 2 INCHES AT FS 879.375. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 5 TR 53-123. REMOVED FASTENERS FROM REPAIRED AREA IAW SR
- [SDR IXXA121109SMN025S](https://openairdocs.org/sdr/IXXA121109SMN025S), Nov 9, 2012: LONGERON. CRACKED. LONGERON 24L, HORIZONTAL LEG CRACKED 1 INCH AT FS 879.375. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 5, TR 53-123.
- [SDR IXXA2013020700001](https://openairdocs.org/sdr/IXXA2013020700001), Nov 6, 2012: SKIN. DAMAGED. RT WING L/E NR 4 STUB WING CORRODED, XW 454 - XW 485. REMOVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-21. REMOVED CORROSION FROM DAMAGED AREA IAW SRM 51-1-8. 
- [SDR IXXA20120706017O](https://openairdocs.org/sdr/IXXA20120706017O), Jul 6, 2012: LOCK. LACK OF LUBE. HAD A DOOR NOT LATCH LAMP ON DURING UPLATCH CHECK. UNSATISFACTORY UP LATCH, BOTH ALTERNATE DOOR LIGHTS DID NOT COME ON AFTER RECYCLE OF THE LANDING GEAR. JACKED
- [SDR RRXA001532](https://openairdocs.org/sdr/RRXA001532), Jan 21, 2008: FRAME. DAMAGED. DURING A MAINT VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT. FS 1340 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW SRM. REMOVED DAMAGE, TREATED AN
- [SDR IXXA08SMN013S](https://openairdocs.org/sdr/IXXA08SMN013S), Jan 15, 2008: FRAME. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT CRACK ON FRAME FLANGE AT STATION 240.000 LONGERON 21RIGHT. REMOVED FASTENERS AS NEEDED TO PERFOR
- [SDR IXXA08SMN012S](https://openairdocs.org/sdr/IXXA08SMN012S), Jan 15, 2008: DOOR. DELAMINATED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING (MLG/FUSELAGE) UPPER DOOR DELAMINATED SKIN. REMOVED DAMAGED DOOR. INSTALLED NEW DOOR. PERFORMED OPS CHECK FOR
- [SDR IXXA08SMN011S](https://openairdocs.org/sdr/IXXA08SMN011S), Jan 15, 2008: SKIN. DELAMINATED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING (MLG/FUSELAGE) MIDDLE DOOR DELAMINATED SKIN. REMOVED DELAMINATED DOOR. INSTALLED NEW MID DOOR. PERFORMED OPS 
- [SDR IXXA08SMN010S](https://openairdocs.org/sdr/IXXA08SMN010S), Jan 15, 2008: DOOR. DELAMINATED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING (MLG/FUSELAGE) UPPER DOOR DELAMINATED SKIN. REMOVED RIGHT MAIN LANDING GEAR OUTBOARD DOOR. INSTALLED NEW DOO
- [SDR IXXA08SMN009S](https://openairdocs.org/sdr/IXXA08SMN009S), Jan 15, 2008: SKIN. DELAMINATED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING (MLG/FUSELAGE) MIDDLE DOOR, DELAMINATED SKIN. REMOVED DAMAGED SKIN. INSTALLED NEW SKIN CENTER DOOR ON RIGHT 
- [SDR IXXA08SMN008S](https://openairdocs.org/sdr/IXXA08SMN008S), Jan 15, 2008: SKIN. DELAMINATED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 SPOILER DELAMINATED. REMOVED DAMAGED SPOILER. INSTALLED NEW RIGHT SPOILER IAW DC8 MAINTENANCE MANUA
- [SDR IXXA08SMN004S](https://openairdocs.org/sdr/IXXA08SMN004S), Jan 14, 2008: PANEL. DELAMINATED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LOWER PANEL DELAMINATED AT STATION XF 219 TO XF 339.000. REMOVED DAMAGED PANEL. INSTALLED NEW PANEL IAW DC8 S
- [SDR IXXA070043O](https://openairdocs.org/sdr/IXXA070043O), Aug 23, 2007: B-NUT. LOOSE. DURING CRUISE FROM KBWI NUMBER THREE ENGINE OIL QUANITY SLOWLY DECREASED UNTIL INDICATING ZERO. PRESSURE AND TEMPERATURE REMAINED NORMAL UNTIL THE OIL PRESSURE 
- [SDR IXXA070036O](https://openairdocs.org/sdr/IXXA070036O), Aug 1, 2007: FUEL CONTROL. MALFUNCTIONED. DURING CRUISE FROM WSAP TO RJTY NR 1 ENGINE LOST POWER EPR REDUCED 1.2 AND FUEL FLOW DECREASED 1000 POUNDS PER HOUR. THE CREW PERFORMED THE ENGINE SHUTDOWN CHEC
- [SDR IXXA07SMN106S](https://openairdocs.org/sdr/IXXA07SMN106S), Feb 8, 2007: DOOR FRAME. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE "A" DOOR AFT LOWER JAMB CORNER CRACKED. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR C
- [SDR IXXA07SMN105S](https://openairdocs.org/sdr/IXXA07SMN105S), Feb 8, 2007: VANE. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE SLOT VANE HAS A NON STANDARD REPAIR, BETWEEN STATION XS 515.720 AND XS 520.168. REMOVED 
- [SDR IXXA07SMN104S](https://openairdocs.org/sdr/IXXA07SMN104S), Feb 8, 2007: VANE. DAMAGED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE SLOT VANE HOLES ELONGATED, BETWEEN STATION XOLDI 6.225 AND XS 435.789. REMOVED EXISTING 
- [SDR IXXA07SMN103S](https://openairdocs.org/sdr/IXXA07SMN103S), Feb 8, 2007: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING EDGE OUTER SECTION HAS A NON STANDARD REPAIR, BETWEEN STATION XFS 710.000 AND XFS 716.250. 
- [SDR IXXA07SMN102S](https://openairdocs.org/sdr/IXXA07SMN102S), Feb 8, 2007: SKIN. BROKEN. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP, UPPER SKIN BROKEN AT STATION XCW 64.000. REMOVED DAMAGED PANEL PLATING. FABRICATED NEW SKIN AND
- [SDR IXXA07SMN101S](https://openairdocs.org/sdr/IXXA07SMN101S), Feb 8, 2007: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP LOWER SKIN HAS A NON STANDARD REPAIR, AT STATION XW 115.000. REMOVED PLATING WITH EXISTING NON S
- [SDR IXXA07SMN100S](https://openairdocs.org/sdr/IXXA07SMN100S), Feb 8, 2007: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING, OUTBORD FLAP UPPER SKIN NON STANDARD REPAIR, AT STATION XF 210.000. REMOVED PANEL PLATING WITH EXISTING NON 
- [SDR IXXA07SMN099S](https://openairdocs.org/sdr/IXXA07SMN099S), Feb 8, 2007: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER. LEADING EDGE OUTER SKIN NON STANDARD REPAIR AT STATION XFS 178.750. REMOVED EXISTING NON ST
- [SDR IXXA07SMN098S](https://openairdocs.org/sdr/IXXA07SMN098S), Feb 8, 2007: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING FRAME, CRACKED AT STATION 759.000, LONGERON 18 LEFT. REMOVED FASTENERS. PERFORMED STOP H
- [SDR IXXA07SMN097S](https://openairdocs.org/sdr/IXXA07SMN097S), Feb 8, 2007: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT STATION XOLDI 6.225. REMOVED EXISTING NON
- [SDR IXXA07SMN096S](https://openairdocs.org/sdr/IXXA07SMN096S), Feb 8, 2007: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT STATION XS 520.000. REMOVED EXISTING NON 
- [SDR IXXA07SMN094S](https://openairdocs.org/sdr/IXXA07SMN094S), Feb 8, 2007: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER.- LEADING EDGE OUTER SKIN NON STANDARD REPAIR AND CORROSION AT STATION XFS 178.750. REMOVED
- [SDR IXXA07SMN095S](https://openairdocs.org/sdr/IXXA07SMN095S), Feb 8, 2007: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER FITTING ANGLE CRACKED AT STATION XFS 60.000. REMOVED DAMAGED FITTING ANGLE. CLEANED, 
- [SDR IXXA07SMN093S](https://openairdocs.org/sdr/IXXA07SMN093S), Feb 8, 2007: SKIN. CORRODED. DURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER. UPPER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATION XFS 178.750. REMOVED EXISTING NON STANDA
- [SDR IXXA07SMN092S](https://openairdocs.org/sdr/IXXA07SMN092S), Feb 8, 2007: SKIN. CORRODED. DURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATION XFS 47.500. REMOVED CORROSION. FOUND OUT OF LIM
- [SDR IXXA07SMN091S](https://openairdocs.org/sdr/IXXA07SMN091S), Feb 8, 2007: PANEL. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, LEFT WING OUTBORD AILERON LOWER PANEL NON STANDARD REPAIR, BETWEEN STATION XA 650.000 AND XA 693.000. REMOVED SKIN WITH EXIST
- [SDR IXXA07SMN090S](https://openairdocs.org/sdr/IXXA07SMN090S), Feb 8, 2007: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, LEFT OUTBOARD AILERON UPPER SKIN NON STANDARD REPAIR, STATION XA 646.000. REMOVED SKIN WITH EXISTING REPAIR. FABRICATED NEW S
- [SDR IXXA07SMN089S](https://openairdocs.org/sdr/IXXA07SMN089S), Feb 8, 2007: SKIN. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT UPPER SKIN CORRODED AT STATION 1730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND O
- [SDR IXXA07SMN088S](https://openairdocs.org/sdr/IXXA07SMN088S), Feb 8, 2007: SKIN. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER SKIN CORRODED AT STATION XFS1730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOU
- [SDR IXXA070004O](https://openairdocs.org/sdr/IXXA070004O), Jan 26, 2007: FIBER OPTIC GYRO. PRECESSES. APPROXIMATELY 1.5 HOURS AFTER TAKEOFF FROM WSAP THE NR 2 COMPASS STARTED PROCESSING AT THE RATE OF 60° TO 70° PER HOUR, DG MODE PROCESSING AT THE RATE OF 25° PE
- [SDR IXXA06SMN418S](https://openairdocs.org/sdr/IXXA06SMN418S), Nov 17, 2006: FITTING. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND FITTING CORRODED AT STATION 530.000 RBL 45. REMOVED CORRODED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING 
- [SDR IXXA06SMN373S](https://openairdocs.org/sdr/IXXA06SMN373S), Nov 10, 2006: SKIN. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN CORRODED AT STATION XE127.960. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN PA
- [SDR IXXA06SMN355S](https://openairdocs.org/sdr/IXXA06SMN355S), Nov 10, 2006: SKIN. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD STUB WING UPPER SKIN CORRODED AT STATION XFS246.000 REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRA
- [SDR IXXA06SMN350S](https://openairdocs.org/sdr/IXXA06SMN350S), Nov 4, 2006: SKIN. DAMAGED. DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER FASTENERS INSTALLED ON THE LEFT OUTBOARD AILERON EXTERNAL LOWER SKIN FROM STATION XA542.000 TO STATION XA566.0
- [SDR IXXA06SMN347S](https://openairdocs.org/sdr/IXXA06SMN347S), Nov 4, 2006: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION FOUND FITTING CRACKED AT STATION 742.000 LONGERON 11 RIGHT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW 
- [SDR IXXA06SMN346S](https://openairdocs.org/sdr/IXXA06SMN346S), Nov 4, 2006: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 857.000, LONGERON 19 RIGHT. REMOVED CRACK FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALL
- [SDR IXXA06SMN339S](https://openairdocs.org/sdr/IXXA06SMN339S), Nov 4, 2006: SKIN. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SKIN CORROSION AT STATION XF803.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED 
- [SDR IXXA06SMN352S](https://openairdocs.org/sdr/IXXA06SMN352S), Nov 4, 2006: SKIN. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS341.500. REMOVED FASTENERS AS NEEDED TO REMOVE CORROSI
- [SDR IXXA06SMN351S](https://openairdocs.org/sdr/IXXA06SMN351S), Nov 4, 2006: SKIN. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD AILERON LOWER SKIN DENTED AT STATION XA558.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUB

All 2,778: https://openairdocs.org/model/mcdonnell-douglas-dc-8-62/reports.md

## STCs that may be installed (OpenAirDocs) (227, 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 SA1315NM](https://openairdocs.org/stc/SA1315NM): Installation of overhead storage compartments, ceiling and wall linings and normal and emergency lights. Safran Cabin 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 ST02001AT](https://openairdocs.org/stc/ST02001AT): Installation of SAF-T-GLO Aerospace Limited's photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC SA2076SO](https://openairdocs.org/stc/SA2076SO): Installation of emergency escape path lighting system. Astronics Luminescent Systems 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-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 ST00094AT](https://openairdocs.org/stc/ST00094AT): Installation of TRA-67 Mode S transponder and CAS-81 Traffic Alert and Collision Avoidance System (TCAS II). Honeywell International Inc
- [STC SA480NE](https://openairdocs.org/stc/SA480NE): Installation of Inflight Services Video system, for Hawaiian Air. Burrana Inc
- [STC SA993EA](https://openairdocs.org/stc/SA993EA): Installation of Inflight Motion Pictures, Inc. 16mm Movie Projection System 1R4000 and Screen Assemblies. Burrana Inc
- [STC SA3421NM](https://openairdocs.org/stc/SA3421NM): Installation of Hughes-Avicom video entertainment system. Burrana Inc. Lists DC-8 Series
- [STC SA1959WE](https://openairdocs.org/stc/SA1959WE): Installation of Movie 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 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 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 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 SA1133NW-D](https://openairdocs.org/stc/SA1133NW-D): Seat mix change from dual class 144 passenger to 189 passenger all coach charter configuration. Installation in accordance with DAS-1-WE United Air Lines Drawing List No. 1133 dated January 20, 1982, or later FAA approved revisions. United Airlines Inc
- [STC SA1136NW-D](https://openairdocs.org/stc/SA1136NW-D): Installs 88 passenger seating arrangement with 20 executive passengers and 68 coach passengers and provides an alternate 75 passenger seating arrangements with 19 executive passengers and 56 coach passengers and two televisions. Installation is in accordance with DAS-1-WE United Air Lines Drawing List No. 1135 dated March 11, 1982, or later FAA approved revision. United Airlines Inc
- [STC SA1138NW-D](https://openairdocs.org/stc/SA1138NW-D): Seat mix change from charter all coach configuration of 189 passenger to 204 passenger all coach charter configuration. Installation in accordance with DAS-1-WE United Air Lines Drawing List No. 1138 dated June 18, 1982, or later FAA approved revisions. United Airlines Inc
- [STC SA1140NW-D](https://openairdocs.org/stc/SA1140NW-D): Seat mix change from charter all coach configuration of 204 passenger to 180 passenger all coach charter configuration. Installation in accordance with DAS-1-WE United Air Lines Drawing List No. 1140 dated October 15, 1982, or later FAA approved revisions. United Airlines Inc
- [STC SA2146WE](https://openairdocs.org/stc/SA2146WE): Alternate Seating Configuration in accordance with FAA Approved United Air Lines Drawing List No. COA 2-3736, or later FAA approved revisions. United Airlines Inc
- [STC SA2211WE](https://openairdocs.org/stc/SA2211WE): Installation of Bendix Third Attitude Indicator to meet the requirements of 14 CFR 121.305(j). United Airlines Inc
- [STC SA2237WE](https://openairdocs.org/stc/SA2237WE): Alternate seating configuration. United Airlines Inc
- [STC SA2296WE](https://openairdocs.org/stc/SA2296WE): Alternate seating and galley arrangement in accordance with FAA Approved United Air Lines Drawing Lists C0A-2-4081 and C0A-2-4088 or later FAA approved revisions. United Airlines Inc

All 227: https://openairdocs.org/model/mcdonnell-douglas-dc-8-62/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
- [SG9344](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189396641220231023182456.0001): Polycarbonate Marker Insert Vertical Exit Arrow. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9344 · Sep 15, 2023
- [SG9444](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179992853720231023182624.0001): Test Coupon. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9444 · Sep 15, 2023
- [SG9341](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175380655620231023182449.0001): Polycarbonate Insert Marker Exit L/Arrow. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9341 · Sep 15, 2023
- [SG9345](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174931531420231023182503.0001): Polycarbonate Insert Marker Double Dot. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9345 · Sep 15, 2023
- [SG9442](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167467075320231023182544.0001): Standard Bottom Track. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9442 · Sep 15, 2023
- [SG9445](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159414889720231023182646.0001): Stopped End Cap. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9445 · Sep 15, 2023
- [SG9422](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154937719720231023182523.0001): Photoluminescent Insert. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9422 · Sep 15, 2023
- [SG9603](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149090788120231023182830.0001): Flush End Piece. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9603 · Sep 15, 2023
- [SG9443](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146612570920231023182604.0001): Test Procedure Blank. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9443 · Sep 15, 2023
- [SG9501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145758793420231023182728.0001): Standard Top Track. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9501 · Sep 15, 2023
- [SG9342](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139981626320231023182455.0001): Polycarbonate Insert Marker Exit R/Arrow. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9342 · Sep 15, 2023
- [SG9601](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127490108820231023182749.0001): Flush Cover. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9601 · Sep 15, 2023
- [SG9446](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124139484720231023182706.0001): Ramped End Cap. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9446 · Sep 15, 2023
- [SG9602](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110530356120231023182810.0001): Flush Track Base. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9602 · Sep 15, 2023
- [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
- [122666-2-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127534894520230907183535.0001): 1st Spool Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 122666-2-1 · 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
- [122594-3-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147106652220230907183318.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 122594-3-1 · 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
- [397592-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153705427520230907183636.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 397592-1-1 · Feb 14, 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

All of them: https://openairdocs.org/model/mcdonnell-douglas-dc-8-62/pma.md

## The same model under other registry codes

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

- [Douglas DC-8-62](https://openairdocs.org/model/douglas-dc-8-62): 0 registered aircraft, registry code 3021970

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