# Douglas DC-8-62 - Type: Aircraft model (FAA registry) - Registry code: 3021970 - Manufacturer (registry): 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: 0 - Page: https://openairdocs.org/model/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/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 None registered with this model now. ## 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 DEN00FA078](https://openairdocs.org/ntsb/DEN00FA078), Apr 28, 2000: Douglas DC-8-62F (N990CF), Denver, CO, substantial damage. Probable cause: The failure of the clamp that secured the high-pressure bleed air duct to the high-pressure relief valve. Factors were the resulting excessive pressurization of the engine nacelle, and the subsequent… - [NTSB MIA97IA050](https://openairdocs.org/ntsb/MIA97IA050), Dec 31, 1996: Douglas DC8-62 (N804AX), Orlando, FL, incident, minor damage. Probable cause: The failure of the captain to center the rudder and close all engine throttles during an aborted takeoff resulting in an uncontrolled turn to the right due to nose wheel steering through the rudder… - [NTSB IAD96LA052](https://openairdocs.org/ntsb/IAD96LA052), Mar 20, 1996: Douglas DC-8-62 (N803AX), Wilmington, OH, substantial damage. Probable cause: The pilot-in-command's inadequate visual lookout and the company/operator's inadequate crew/group coordination and communication during taxi and snow removal operations. Related factors were the… - [NTSB NYC91FA086](https://openairdocs.org/ntsb/NYC91FA086), Mar 12, 1991: Douglas DC-8-62 (N730PL), Jamaica, NY, destroyed. Probable cause: IMPROPER PREFLIGHT PLANNING/PREPARATION, IN THAT THE FLIGHT ENGINEER MISCALCULATED (MISJUDGED) THE AIRCRAFT'S GROSS WEIGHT BY 100,000 LBS AND PROVIDED THE CAPTAIN WITH IMPROPER TAKEOFF SPEEDS; AND… - [NTSB CHI72AC010](https://openairdocs.org/ntsb/CHI72AC010), Jul 26, 1971: Douglas DC-8 (N8975U), No.Pacific Ocean (Pacific Ocean), no damage - [NTSB MIA69I0007](https://openairdocs.org/ntsb/MIA69I0007), Aug 5, 1968: Douglas DC-8 (N1804), No.Atlantic Ocean (Atlantic Ocean), incident, no damage - [NTSB UNK68X0135](https://openairdocs.org/ntsb/UNK68X0135), Apr 23, 1968: Douglas DC-8 (N1804), Quito, Ecuador, substantial damage ## FAA accident and incident reports (31) 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 20000427017119I](https://openairdocs.org/incident/20000427017119I), Apr 27, 2000: Doug DC862 (N990CF), Denver, CO, Minor damage. (-23)On April 28, 2000, emery flight 025, enroute form sea to day was over eastern Montana. At approxiamtely 0330Z in cruise at FL370, the crew heard a loud… - [Incident 19981124045799I](https://openairdocs.org/incident/19981124045799I), Nov 24, 1998: Doug DC862 (N8968U), Ashland, KY. [privacy data omitted](PIC & check airmen)was giving[privacy data omitted]his operating experience in the DC-8. Center gave them a descent to FL 240. [privacy… - [Incident 19980617024759I](https://openairdocs.org/incident/19980617024759I), Jun 17, 1998: Doug DC862 (N803AX), Salt Lake City, UT, Minor damage. On approach hit several small birds damaging NR3 engine. - [Incident 19970116012659I](https://openairdocs.org/incident/19970116012659I), Jan 16, 1997: Doug DC862 (N803CK), Terre Haute, IN, Minor damage. Narrative: on January 16, 1997, at 0839 EST, a Douglas DC-8-62, N803CK, registered to American international airways (cksa), slid off runway 23 during… - [Incident 19961230045369I](https://openairdocs.org/incident/19961230045369I), Dec 30, 1996: Doug DC862 (N804AX), Orlando, FL, Minor damage. Narrative: on December 30, 1996, at about 2227 EST, a Douglas DC-8-62, N804AX, operated by abx air inc. dba airborne express, as a cargo flight under 14 CFR… - [Accident 19960320040759A](https://openairdocs.org/incident/19960320040759A), Mar 20, 1996: Doug DC862 (N803AX), Wilmington, OH, Substantial damage. Wing struck a snowplow truck during taxi for takeoff. Poor ground crew coordination and company dispatch procedures (-23) a day sort DC-8 taxiing for departure… - [Incident 19960217021369I](https://openairdocs.org/incident/19960217021369I), Feb 17, 1996: Doug DC862 (N1805), Keflavik, IC, Minor damage. Narrative: this incident investigated by the iceland caa and national air safety board. Report is attached. - [Incident 19950728031169I](https://openairdocs.org/incident/19950728031169I), Jul 28, 1995: Doug DC862 (N735PL), Miami, FL, Minor damage. Lost NR4 engine cowl on takeoff. Indicates maintenance failed to fasten cowling. - [Incident 19950406008809I](https://openairdocs.org/incident/19950406008809I), Apr 6, 1995: Doug DC862 (N803CK), San Francisco, CA. Narrative: 1.) Kalitta flight 879 when enroute at 1315Z, lost all main hydraulic pressure. Lost quantity but was still in normal range. Flight crew declared an… - [Incident 19930921050139I](https://openairdocs.org/incident/19930921050139I), Sep 21, 1993: Doug DC862 (N808AX), Ft Lauderdale, FL. Crew experienced eye irritation on climbout. Returned. Found irritation substance in upper cargo area. - [Incident 19930909043419I](https://openairdocs.org/incident/19930909043419I), Sep 9, 1993: Doug DC862 (N735PL), Chicago, IL, Minor damage. Appears aircraft struck an unknown object while taxiing to park. Had a leading guide and three wing walkers. - [Incident 19930714030709I](https://openairdocs.org/incident/19930714030709I), Jul 14, 1993: Doug DC862 (N1808E), Miami, FL. Aircraft blew NR3 and NR4 main tires while taxiing to gate. Found anti skid unit faulty. - [Incident 19920513019229I](https://openairdocs.org/incident/19920513019229I), May 13, 1992: Doug DC862 (N735PL), Kansas City, MO, Minor damage. Low hydraulic light on descent. Landed safely. Replaced r and r slot control valve. - [Incident 19920127005409I](https://openairdocs.org/incident/19920127005409I), Jan 27, 1992: Doug DC862 (N994CF), Salt Lake City, UT, Minor damage. Pilot lost both the inboard and outboard engine cowling off NR4 engine. Continued to destination. Landed safely. - [Accident 19910312005259A](https://openairdocs.org/incident/19910312005259A), Mar 12, 1991: Doug DC862 (N730PL), New York, NY, Destroyed. Flight engineer incorrectly figured vr speed. Pilot unable rotate. Aborted. Hit ILS off runway avoiding overrun. - [Incident 19890723054159I](https://openairdocs.org/incident/19890723054159I), Jul 23, 1989: Doug DC862F (N996CF), Tokyo, JA. After landing it was determined there was insufficient number of seats and oxygen masks for passengers onboard. - [Incident 19890629051079I](https://openairdocs.org/incident/19890629051079I), Jun 29, 1989: Doug DC862 (N8969U), Honolulu, HI, Minor damage. Experienced loss of cabin pressurization. Emergency descent to lower altitude. Pressurization duct was ruptured. - [Incident 19890311026929I](https://openairdocs.org/incident/19890311026929I), Mar 11, 1989: Doug DC862 (N994CF), Phoenix, AZ, Minor damage. Cargo door warning light was on at rotation. Returned. Found a lock sequence valve control micro switch inoperative - [Incident 19890123005839I](https://openairdocs.org/incident/19890123005839I), Jan 23, 1989: Doug DC862 (N8970U), Honolulu, HI, Minor damage. NR2 engine oil and pressure drop. Engine shutdown. Landed safely. Found a hole in top of oil pressure transmitter. - [Incident 19881130064019I](https://openairdocs.org/incident/19881130064019I), Nov 30, 1988: Doug DC862 (N8970U), Honolulu, HI, 1 fatal. Mechanic was electrocuted while replacing fuel flow power supply. His head contacted a power relay terminal. - [Incident 19871231082069I](https://openairdocs.org/incident/19871231082069I), Dec 31, 1987: Doug DC862 (N8969U), Pacific Ocean, HI. Passenger assaulted flight attendant en route to honolulu. Arrested by fbi on arrival. Company did not report assault - [Incident 19821118065649I](https://openairdocs.org/incident/19821118065649I), Nov 18, 1982: Doug DC863 (N8968U), Fairbanks, AK. Lost directional control on takeoff, over corrected, struck runway lights and snowbank. Left without checking damage - [Incident 19800629056799I](https://openairdocs.org/incident/19800629056799I), Jun 29, 1980: Doug DC862 (N1805), Los Angeles, CA, Minor damage. Open door struck jetway during pushback. Door hinges broken. - [Incident 19800228027869I](https://openairdocs.org/incident/19800228027869I), Feb 28, 1980: Doug DC8/ (N1805), Carupano Grande, Minor damage. Engine shutdown due to power loss and vibration. Tach generator housing had been ingested. - [Incident 19800225027229I](https://openairdocs.org/incident/19800225027229I), Feb 25, 1980: Doug DC862 (N8974U), Beggs Reporting, HI. Flight encountered severe updraft at FL390. Minor injury to flight engineer only. - [Incident 19790530028539I](https://openairdocs.org/incident/19790530028539I), May 30, 1979: Doug DC8* (N1805), Panama, PN. Aircraft ran off side of runway after aborting takeoff. - [Incident 19790428200641I](https://openairdocs.org/incident/19790428200641I), Apr 28, 1979: Doug DC862 (N1805), Miami, FL, Minor damage. During taxi onto the runway, wingtip struck holding aircraft. Wingtip damage. - [Incident 19790210006229I](https://openairdocs.org/incident/19790210006229I), Feb 10, 1979: Doug DC862 (N8969U), Laramie, WY. Four people injured due to turbulence in flight. - [Incident 19781223021049I](https://openairdocs.org/incident/19781223021049I), Dec 23, 1978: Doug DC8/ (N8968U), Des Moines, IA. Pilot lost directional control on takeoff due to slow spool up of one engine. - [Incident 19781117026499I](https://openairdocs.org/incident/19781117026499I), Nov 17, 1978: Doug DC862 (N8969U), Chicago, IL, Minor damage. Engine nacelle struck runway on landing. - [Incident 19781020029199I](https://openairdocs.org/incident/19781020029199I), Oct 20, 1978: Doug DC862 (N8969U), Fresno, CA, Minor damage. Nightly runway construction going on. Pilot was cleared for departure and told all obstructions moved. Hit a pole. ## 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/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/douglas-dc-8-62/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Mcdonnell Douglas DC-8-62](https://openairdocs.org/model/mcdonnell-douglas-dc-8-62): 1 registered aircraft, registry code 302197B --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.