# Douglas DC-8F-54

- Type: Aircraft model (FAA registry)
- Registry code: 3021926
- Manufacturer (registry): DOUGLAS
- Model: DC-8F-54
- 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-8f-54

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 2008-06-23](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 2007-12-02](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 2006-03-04](https://openairdocs.org/ad/2006-03-04): Main cabin cargo door · Boeing DC-8-33, DC-8-51, DC-8-53 and 11 more. Effective Mar 13, 2006
- [AD 2005-18-07](https://openairdocs.org/ad/2005-18-07): Lower cargo doorjamb corners · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Oct 7, 2005
- [AD 2005-15-14](https://openairdocs.org/ad/2005-15-14): Upper inboard spar cap of the wing · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Sep 1, 2005
- [AD 2005-08-08](https://openairdocs.org/ad/2005-08-08): Engine fire extinguisher containers · Boeing DC-8-33, DC-8-43, DC-8-51 and 17 more. Effective May 26, 2005
- [AD 2005-06-05](https://openairdocs.org/ad/2005-06-05): Left and right elevator control tabs · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Apr 22, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-14-05](https://openairdocs.org/ad/2004-14-05): Seat locking pins · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Aug 13, 2004
- [AD 2003-03-15 R1](https://openairdocs.org/ad/2003-03-15-R1): Airplane Flight Manual (AFM) - oxygen masks · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 90 more. Effective Dec 22, 2003
- [AD 2003-21-02](https://openairdocs.org/ad/2003-21-02): Lower inboard auxiliary spar cap · Boeing DC-8-11, DC-8-12, DC-8-21 and 21 more. Effective Nov 20, 2003
- [AD 2003-17-07 R1](https://openairdocs.org/ad/2003-17-07-R1): Auxiliary power unit (APU) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 57 more. Effective Sep 24, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2002-14-19](https://openairdocs.org/ad/2002-14-19): Collins Air Data Computers (ADC) · Boeing DC-8-11, DC-8-12, DC-8-21 and 36 more. Effective Aug 23, 2002
- [AD 2002-03-05](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
- [AD 2000-02-01](https://openairdocs.org/ad/2000-02-01): Lower Wing Skin · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Feb 29, 2000
- [AD 2000-01-18](https://openairdocs.org/ad/2000-01-18): Lower Cap of the Wing Front Spar · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Feb 23, 2000
- [AD 98-26-51](https://openairdocs.org/ad/98-26-51): Main Deck Cargo Door · Cargo door, cargo restraint bulkhead, heavy duty flooring… (Plattner STC SA1802SO). Effective Feb 3, 1999

Historical (superseded or no longer in force):

- [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 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

All 132: https://openairdocs.org/model/douglas-dc-8f-54/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 (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 MIA95RA121](https://openairdocs.org/ntsb/MIA95RA121), Apr 28, 1995: Douglas DC-8F-54 (N43UA), Guatemala Cty., Guatemala, 6 fatal
- [NTSB BFO95IA023](https://openairdocs.org/ntsb/BFO95IA023), Dec 25, 1994: Douglas DC-8-54F (N427FB), New York, NY, incident, minor damage. Probable cause: THE FAILURE OF THE RIGHT MAIN LANDING GEAR'S SHOCK STRUT PISTON LUG DUE TO STRESS CORROSION.
- [NTSB FTW93IA067](https://openairdocs.org/ntsb/FTW93IA067), Jan 15, 1993: Mcdonnell Douglas DC8-55 (N8041U), Dfw Airport, TX, incident, minor damage. Probable cause: FAILURE OF AN ENGINE TURBINE WHEEL FOR UNDETERMINED REASONS.
- [NTSB DCA78AA005](https://openairdocs.org/ntsb/DCA78AA005), Dec 18, 1977: Douglas DC-8F (N8047U), Kaysville, UT, destroyed, 3 fatal
- [NTSB IAD70II053](https://openairdocs.org/ntsb/IAD70II053), Mar 26, 1970: Douglas DC-8F (N8047U), Dulles Int Apt, VA, incident, minor damage
- [NTSB DCA65I0002](https://openairdocs.org/ntsb/DCA65I0002), Sep 14, 1964: Douglas DC8F (N109RD), Pacific Ocean (Pacific Ocean), incident, no damage

## FAA accident and incident reports (17)

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 19981103041519I](https://openairdocs.org/incident/19981103041519I), Nov 3, 1998: Doug DC8F54 (N992CF), Indianapolis, IN. (-5) The #2 engine hydraulic pump seal failed, allowing the hydraulic fluid to enter the engine gear box. The crew declared an emergency and diverted the…
- [Incident 19980602019929I](https://openairdocs.org/incident/19980602019929I), Jun 2, 1998: Doug DC8F54 (N7046H), San Juan, Puerto Rico, Minor damage. Aircraft struck loaded with number 4 engine while parking. Ground crew failed to signal flight crew of hazard.
- [Incident 19970610022409I](https://openairdocs.org/incident/19970610022409I), Jun 10, 1997: Doug DC8F54 (N802CK), Miami, FL. Fire warning left engine on climbout. Shutdown. Returned. Fire loop worn and loose. Replaced. Cured problem.
- [Incident 19950815029199I](https://openairdocs.org/incident/19950815029199I), Aug 15, 1995: Doug DC8F54 (N8041U), Rochester, NY. On climbout catastrophic failure of NR1 engine. Returned. Found destroyed fan blades. Engine was destroyed.
- [Accident 19950428013029A](https://openairdocs.org/incident/19950428013029A), Apr 28, 1995: Doug DC8F54 (N43UA), Guatemala City, GT, Destroyed, 6 fatal. (.19) See preliminary report for complete narrative.
- [Incident 19941225046479I](https://openairdocs.org/incident/19941225046479I), Dec 25, 1994: Doug DC8F54 (N427FB), New York, NY, Minor damage. Aborted takeoff due vibration. Right gear broke at bogie pivot. All four tires blown.
- [Incident 19940315000619I](https://openairdocs.org/incident/19940315000619I), Mar 15, 1994: Doug DC8F54 (N802CK), Dallas-Ft Worth, TX, Minor damage. Narrative: aircraft was parked on the east end of the east freight ramp. The aircraft was loaded with crew on board, waiting on door safety check and push back…
- [Incident 19931223049539I](https://openairdocs.org/incident/19931223049539I), Dec 23, 1993: Doug DC8F54 (N991CF), Washington, DC. NR4 engine failed after takeoff from baltimore. Diverted to Washington. Landed safely. Machanical fuel pump had failed
- [Incident 19930114001609I](https://openairdocs.org/incident/19930114001609I), Jan 14, 1993: Doug DC8F54 (N8041U), Dallas-Ft Worth, TX. NR4 engine shut down on climb. Returned. Landed safely. Engine had a turbine failure.
- [Incident 19920707026989I](https://openairdocs.org/incident/19920707026989I), Jul 7, 1992: Doug DC8F54 (N8041U), Kansas City, MO. NR2 engine low oil pressure light on. Shut engine down. Landed safely. Found metal in NR2 engine oil screen.
- [Incident 19920303008579I](https://openairdocs.org/incident/19920303008579I), Mar 3, 1992: Doug DC8F54 (N992CF), Cleveland, OH. Crew smelled smoke in cockpit. Diverted to Cleveland. Landed safely. Found unseated arcing light bulb in cargo bay.
- [Incident 19911212060789I](https://openairdocs.org/incident/19911212060789I), Dec 12, 1991: Doug DC8F54 (N992CF), Indianapolis, IN, Minor damage. Experienced two blown tires on rollout. Maintenance found an anti-skid control valve had failed.
- [Incident 19911018052179I](https://openairdocs.org/incident/19911018052179I), Oct 18, 1991: Doug DC8F54 (N8041U), Las Vegas, NV, Minor damage. NR1 engine compressor stall after takeoff. Returned. Engine tail cone parts found on runway.
- [Incident 19890721039699I](https://openairdocs.org/incident/19890721039699I), Jul 21, 1989: Doug DC8F54 (N802CK), Baltimore, MD, Minor damage. Aborted takeoff due to noise in cargo area. Aborted again due to landing gear smoke. Had heat build up on tires.
- [Incident 19881228066829I](https://openairdocs.org/incident/19881228066829I), Dec 28, 1988: Doug DC8F54 (N991CF), Indianapolis, IN. Lost hydraulic fluid. Used emergency brake system. Lost steering. Veered off runway. Hole in flap actuator.
- [Incident 19880617038779I](https://openairdocs.org/incident/19880617038779I), Jun 17, 1988: Doug DC8F54 (N8042U), Kansas City, MO. Hydraulic system pressure dropped to zero on climb. Returned. Had a double engine driven hydraulic pump failure.
- [Incident 19871021074689I](https://openairdocs.org/incident/19871021074689I), Oct 21, 1987: Doug DC8F54 (N802CK), Covington - Cin, OH, Minor damage. Marshaller signaled chocks set. Brakes set. Engine shutdown. Brakes released. Plane moved forward. Hit a k loader.

## Service difficulty reports (194, newest 50)

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

- [SDR DHL2001806509](https://openairdocs.org/sdr/DHL2001806509), Mar 8, 2001: LIGHT. CRACKED. C-CHECK-FWD CARGO BAY LIGHT BASE CRACKED 1 INCH AT STA.100 LBL.17. REMOVED FASTENER IAW.SRM.51-1-21. FABRICATED DOUBLER IAW SRM 53-2-0 FIG.2 CLEANED,TREATED & P
- [SDR ARWA0010101](https://openairdocs.org/sdr/ARWA0010101), Jan 18, 2001: HYDRAULIC LINE. LEAKING. DURING DESCENT AT THE INITIAL PHASE OF THE APPROACH LOSS HYDRAULIC FLUID AND PRESSURE. INITIATED PHASE I AND ABNORMAL IAW PROCEDURES. AFTER CLEARING THE ACTIVE 
- [SDR ARWA0001004](https://openairdocs.org/sdr/ARWA0001004), Nov 3, 2000: PIN. BROKEN. FLIGHT LEAVING OUT OF MIA TO KM, WHEN LANDING GEAR SELECTED UP; CREW HEARD LOUD BANG IN AFT AIRCRAFT; FOLLOWED BY UNSAFE RED GEAR LIGHT AND LOSS OF HYDRAULIC FL
- [SDR ARWA0001003](https://openairdocs.org/sdr/ARWA0001003), Oct 23, 2000: PANEL. CORRODED. DURING B CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON LT WING UPPER INNER WING L/E SLANT PANEL. REPAIR CORROSION CRACK IAW EO 0010181.
- [SDR ARWA0001002](https://openairdocs.org/sdr/ARWA0001002), Oct 23, 2000: LONGERON. CORRODED. DURING B CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION CRACK AT LONGERON L-24 BETWEEN FS 960 AND 980. REPAIRED CORROSION CRACK IAW BOEING MESSAGE INW-LIM-00-
- [SDR ARWA0001001](https://openairdocs.org/sdr/ARWA0001001), Oct 23, 2000: SKIN. CORRODED. DURING B CHECK INSPECTION FOUND THE FOLLOWING:CORRODED C3 CARGO DOOR LOWER EDGE OUTER SKIN BETWEEN BS 1130 AND BS 1160. REPAIRED CORROSION CRACK IAW DRAWING AS1
- [SDR ARAWA000901](https://openairdocs.org/sdr/ARAWA000901), Sep 16, 2000: FUEL CONTROL. MALFUNCTIONED. ON APPROACH TO SKCL, NR 4 ENGINE FAILED. PERFORMED EMERGENCY PROCEDURES AS PER FINE AIR PROCEDURES. LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 ENGINE F
- [SDR 20001208AP006](https://openairdocs.org/sdr/20001208AP006), Jul 6, 2000: FITTING. CRACKED. DURING AN INSPECTION FOUND THE FOLLOWING, CRACKED LEFT MLG AUXILIARY SPAR FITTING. REPLACED AUXILIARY SPAR FITTING IAW DOUGLAS DRAWING NR 5802630. (M)
- [SDR 20001208AP002](https://openairdocs.org/sdr/20001208AP002), Jul 6, 2000: SPAR CAP. CRACKED. DURING AN INSPECTION OF THE PYLON FOUND FORWARD SPAR CRACK AT STATION XFS 550. REPAIRED FORWARD PYLON IAW DOUGLAS DRAWING NR 5802712. (M)
- [SDR 20001208AP001](https://openairdocs.org/sdr/20001208AP001), Jul 6, 2000: FITTING. CRACKED. DURING AN INSPECTION FOUND THE FOLLOWING, CRACKED FITTING LEFT SIDE LONGERON 24. REPLACED CRACK LONGERON FITTING IAW DOUGLAS DRAWING NR 5802709. (M)
- [SDR 20001208AP003](https://openairdocs.org/sdr/20001208AP003), May 30, 2000: BALLAST. OVERHEATED. SHORTLY AFTER TAKEOFF FROM MGA EN ROUTE TO MIA CREW NOTICED STRANGE SMELL IN COCKPIT, SMOKE WAS DETECTED IN COCKPIT AND MAIN CARGO COMPARTMENT. RETURNED BACK TO
- [SDR 2000ZZZX465](https://openairdocs.org/sdr/2000ZZZX465), Nov 11, 1999: SKIN. CORRODED. DURING B-CHECK INSPECTION, FOUND THE FOLLOWING: 4.5 INCH CRACK IN RIGHT INBOARD FORWARD LOWER WING SKIN AT STA XRS 210 BETWEEN 66 AND 67. REPAIRED CRACK IAW BOE
- [SDR 2000ZZZX459](https://openairdocs.org/sdr/2000ZZZX459), Nov 2, 1999: BALLAST. FAILED. AFTER TAKEOFF FROM MIA, EXPERIENCED SMOKE AND ELECTRICAL ODOR IN THE COCKPIT; RETURNED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED THE BALLAST FOR T
- [SDR 2000ZZZX472](https://openairdocs.org/sdr/2000ZZZX472), Oct 21, 1999: FCU. INOPERATIVE. DURING SHORT FINAL, NR 3 ENGINE FLAMEOUT; FUEL ON NR 3 TANK WAS 5800; SUSPECT FCU MALFUNCTION. CHANGED AND TESTED FCU UNIT IAW PW MM 72-0. (X)
- [SDR 2000ZZZX473](https://openairdocs.org/sdr/2000ZZZX473), Sep 23, 1999: LINE. LEAKING. FLT 790 - ON DESCENT INTO MIA FROM POS, REPORTED LOSS OF HYDRAULIC FLUID DOWN TO STANDPIPE. PERFORMED EMERGENCY CHECKLIST. DECLARED EMERGENCY AND LANDED FULL FL
- [SDR 2000ZZZM231](https://openairdocs.org/sdr/2000ZZZM231), Aug 31, 1999: SPAR. CRACKED. DURING D-CHECK INSPECTION, FOUND 4 INCH CRACK IN RIGHT LOWER SPAR CAP AT XCW 69.5. REPAIRED ACCOMPLISH IAW BOEING SERVICE ENGINEERING FAX FAS-MIA-99-0010RR AND 
- [SDR 2000ZZZX464](https://openairdocs.org/sdr/2000ZZZX464), Aug 27, 1999: FLOORBEAM. CORRODED. DURING B-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORROSION DAMAGE UPPER FLANGE AT STA FS 1380 RBL 38. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA G5
- [SDR 2000ZZZX461](https://openairdocs.org/sdr/2000ZZZX461), Aug 27, 1999: FLOORBEAM. CORRODED. DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORROSION DAMAGE STA FS 1480. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA G5310-03:00. (X)
- [SDR 2000ZZZX460](https://openairdocs.org/sdr/2000ZZZX460), Aug 27, 1999: FLOORBEAM. CORRODED. DURING B-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORROSION DAMAGE STA FS 1480. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA G5310-01:00. (X)
- [SDR 2000ZZZM248](https://openairdocs.org/sdr/2000ZZZM248), Apr 21, 1999: SKIN. CRACKED. DURING D-CHECK INSPECTION, FOUND LEADING UPPER CAP CRACKED. REPAIRED CRACK ON WING RIGHT IAW FINE AIRLINES EA NR G5711-02:00. (M)
- [SDR TC8A99005](https://openairdocs.org/sdr/TC8A99005), Mar 18, 1999: LINE. LEAKING. NO FLIGHT, RETURN TO RAMP TO SERVICE HYDRAULICS. HYDRAULICS DROPPED APPROXIMATELY 5 GALLONS ON TAXI OUT. SERVICED HYDRAULICS, FIXED LEAK ON NR 3 ENGINE.
- [SDR 99ZZZM231](https://openairdocs.org/sdr/99ZZZM231), Jan 13, 1999: SWITCH. FAILED. DURING CRUISE GEAR UNSAFE LIGHT ILLUMINATED. CYCLED GEAR AND RECEIVED THREE GREEN LIGHTS FOR LANDING GEAR. LANDED AT MIA WITHOUT INCIDENT. GROUND INSPECTION REV
- [SDR 2000ZZZX463](https://openairdocs.org/sdr/2000ZZZX463), Dec 8, 1998: SKIN. CORRODED. DURIGN C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE AT STA XE149 HORIZONTAL STABILIZER, LEFT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EO 980007
- [SDR 2000ZZZX462](https://openairdocs.org/sdr/2000ZZZX462), Dec 8, 1998: SKIN. CORRODED. DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE AT STA XE 133 TO 246 ELEVATOR LEFT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EO 9811091. (X)
- [SDR 2000ZZZX467](https://openairdocs.org/sdr/2000ZZZX467), Nov 11, 1998: FLOORBEAM. CORRODED. DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORRROSION DAMAGE AT STA FS 940. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EO 9810211. (X)
- [SDR 2000ZZZX466](https://openairdocs.org/sdr/2000ZZZX466), Nov 11, 1998: FLOORBEAM. CORRODED. DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORRROSION DAMAGE AT STA FS 820 - FS 859, LEFT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EO 9810161
- [SDR RRXA98506](https://openairdocs.org/sdr/RRXA98506), Nov 4, 1998: PUMP. FAILED. HYD QUANTITY LOSS INFLIGHT. FOUND NR 2 ENG HYD PUMP INTERNAL SEALS ALLOWING FLUID TO FLOW INTO NR 2 ENG OIL SUPPLY. DRAINED, FLUSHED ENG OIL TANK 2 TIMES. REMOV
- [SDR TC8A98076](https://openairdocs.org/sdr/TC8A98076), Oct 30, 1998: BLADE. DENTED. COMPRESSOR STALL NR 3 ENGINE DURING TAKEOFF ROLL, APPROXIMATELY 60 KNOTS, ANTI-ICE OFF. INSPECTED COMPRESSOR AND TURBINE IAW PW 72-0, PG 118, NO DEFECTS NOTED. 
- [SDR TC8A98069](https://openairdocs.org/sdr/TC8A98069), Oct 22, 1998: VOLTAGE REG. FAILED. TRIP# 02707. DISCREP: #2 GENERATOR SHOWS UNBALANCED LOAD. CORR. ACTION: TRANSFERRED TO DMI 8809 AS PER MEL 24-1 CAT C. PLACARD INSTALLED, SPECIAL PROCEDURES COM
- [SDR TC8A98068](https://openairdocs.org/sdr/TC8A98068), Oct 20, 1998: TERMINAL. DAMAGED. TRIP NR 02692, DURING TAXI, NR 1 AND NR 3 GENERATOR UNPARALLELED, VOLTS AND FREQS OK. AIRCRAFT FERRIED TO KYIP. TROUBLESHOT SYSTEM, REPLACED TERMINALS AT WIRE N
- [SDR 99ZZZM29](https://openairdocs.org/sdr/99ZZZM29), Oct 19, 1998: STRUT. CRACKED. CREW REPORTED FINDING A HYDRAULIC LEAK ON NOSE LANDING GEAR DURING PRE-FLIGHT GYE. FOUND CRACK IN NLG OLEO OUTER CYLINDER APPROX 6 INCH FROM TOP, APPROX 1.5 INC
- [SDR ZIAA98039](https://openairdocs.org/sdr/ZIAA98039), Oct 3, 1998: SKIN. CORRODED. YIP - BELLY AT APPROXIMATELY FS 600, REINFORCING PLATE HAS SEVERAL POPPED RIVETS. REMOVED PLATE DUE TO CORROSION. REMOVED SKIN DAMAGE DUE TO CORROSION. REPAIRED
- [SDR TC8A98053](https://openairdocs.org/sdr/TC8A98053), Aug 22, 1998: BLEED VALVE. REPLACED. MULTIPLE COMPRESSOR STALLS ON CLIMBOUT, 6,000 FT ON NR 1 ENG. REMOVED AND REPLACED NR 1 PRBC VALVE, OPS CHECKS OK IAW 75-30-3.
- [SDR TC8A98046](https://openairdocs.org/sdr/TC8A98046), Aug 6, 1998: CONNECTOR. DIRTY. TRIP NR 02268, NR 1 TURBO COMPRESSOR WOULD NOT TEST. CLEANED CANNON PLUG AND RESET, OPS CHECK GOOD IAW M/M 21-10-2.
- [SDR 98ZZZM564](https://openairdocs.org/sdr/98ZZZM564), Jul 20, 1998: FITTING. CRACKED. FOUND RIGHT MAIN LANDING GEAR SUPPORT FITTING CRACKED. REMOVED AND REPLACED RIGHT MAIN GEAR FITTING PER IAW DOUGLAS DC8 MLG FITTING REPLACEMENT GUIDE AND RECOVE
- [SDR TC8A98042](https://openairdocs.org/sdr/TC8A98042), Jul 18, 1998: FITTING. CRACKED. ON TAXI UPON FLIGHT CONTROL CHECK, SPOILER PUMP PRESSURE INDICATION WENT TO ZERO. FOUND FITTING AT SPOILER SUPPLY LINE CRACKED. REPLACED FITTING IAW MM 27-62-0,
- [SDR TC8A98041](https://openairdocs.org/sdr/TC8A98041), Jul 15, 1998: COMPRESSOR. STALLED. LOUD, PRONOUNCED, SUSPECTED ENGINE COMPRESSOR STALL ON RT SIDE DURING TAKEOFF PASSING 70 KIAS, ABORT INITIATED. INSPECTED NR 3 AND NR 4 ENGINES FOR DAMAGE, NONE
- [SDR 98ZZZM870](https://openairdocs.org/sdr/98ZZZM870), Jul 14, 1998: UNKNOWN. ODOR. ON ARRIVAL GYE, REPORTED SMOKE ODOR FROM UNKNOWN SOURCE IN COCKPIT AND CABIN. ON GROUND, RAN ENGINES AND PRESSURIZED AIRCRAFT TO CHECK NASI PNEUMATIC FLOW CONTR
- [SDR TC8A98040](https://openairdocs.org/sdr/TC8A98040), Jul 10, 1998: COMPRESSOR. STALLED. INITIATED ABORT PASSING 80 KNOTS BECAUSE OF SUSPECTED COMPRESSOR STALL OR BLOWN TIRE. RETURNED TO THE BLOCKS, LET BRAKES COOL, INSPECTED BRAKES AND TIRES IAW M/
- [SDR TC8A98036](https://openairdocs.org/sdr/TC8A98036), Jun 25, 1998: OIL TANK. LOOSE. ON CLIMB-OUT AT APPROX 10000 FEET, NR 3 ENGINE FIRE WARNING BELL AND LIGHTS. PERFORMED ENGINE SHUTDOWN. FOUND MIDDLE STRAP ON ENGINE OIL TANK LOOSE AND IN CONTA
- [SDR 98ZZZM498](https://openairdocs.org/sdr/98ZZZM498), Jun 25, 1998: LINE. BROKEN. IN CRUISE BOG TO MIA EXPERIENCED LOSS OF HYDRAULIC QTY. EXECUTED ABNORMAL PROCEDURES AND LANDED MIA WITHOUT INCIDENT. AIRCRAFT TOWED OFF RUNWAY. INSPECTION REVE
- [SDR CKSA98349](https://openairdocs.org/sdr/CKSA98349), Jun 18, 1998: PLUG. MISLOCATED. ON CLIMBOUT, BURNING SMELL NOTED IN COCKPIT. FO'S AUDIO PANEL CB POPPED. AFTER 5 MIN COOL DOWN, CB RESET AN IMMEDIATELY POPPED AGAIN. BURNING SMELL DISIPATED. F
- [SDR 98ZZZM686](https://openairdocs.org/sdr/98ZZZM686), Jun 13, 1998: LINE. BROKEN. ON TAXI AFTER LANDING MIA, FLT 364 - REPORTED LOSS OF HYDRAULIC QUANTITY TO AUX LEVEL WITH LOW BRAKE PRESSURE LIGHT ILLUMINATED AND NO EFFECTIVE BRAKING OR STEE
- [SDR RRXA98225](https://openairdocs.org/sdr/RRXA98225), Jun 4, 1998: NUT. MISSING. FLAP SPLIT ON APPROACH. A/C ROLLS TO LEFT AT 10 DEG PERFORMED A ZERO FLAP LNDG. REPLACED MISSING NUTS ON FLAP TRACK ON LEFT FLAP, OPS CHECKS NORMAL, NO SPLIT NO
- [SDR TC8A98027](https://openairdocs.org/sdr/TC8A98027), May 22, 1998: BRAKE. LOCKED UP. ON TAXI OUT, AIRPLANE SHUDDERED AND CAME TO A STOP, WOULD NOT MOVE. REMOVED AND REPLACED NR 6 BRAKE ASSY, LEAK CHECK OPS CHECKED OK PER M/M 32-42-1.
- [SDR CKSA98336](https://openairdocs.org/sdr/CKSA98336), May 21, 1998: HYDRAULIC LINE. LEAKING. DURING CRUISE, LOSS OF HYDRAULIC FLUID ON QUANTITY INDICATOR (5.8 GALLONS). ACCOMPLISHED AIA EMERGENCY PROCEDURES. ON POSTFLIGHT, DISCOVERED NR 2 ENGINE LEAKING
- [SDR RRXA98082](https://openairdocs.org/sdr/RRXA98082), Apr 28, 1998: ENGINE. FAILED. NR 4 ENG LOUD BANG, HEAVY VIBRATION, DECAYING N1, N2 AND INCREASING EGT, ACCOMPANIED BY VIOLENT YAW TO THE RIGHT. HEAVY VIBRATION FELT WITH THROTTLE ADVANCEMENT
- [SDR RRXA98079](https://openairdocs.org/sdr/RRXA98079), Apr 21, 1998: STATIC HOSE. COLLAPSED. CAPT'S ALTIMETER IS STUCK AT 500 FEET. FOUND STATIC HOSE ASSY FROM CAPTS STATIC SOURCE SELECTOR TO MANIFOLD MOUNTED ON BACK OF INSTRUMENT PANEL TO BE PARTIALLY 
- [SDR RRXA98078](https://openairdocs.org/sdr/RRXA98078), Apr 17, 1998: HYD LINE. FAILED. AT FL 35.0 LOST HYD FLUID TO STAND PIPE AUX LEVEL. PERFORMED HYD FLUID OR PRESS LOSS CHECKLIST. FOUND PRESSURE LINE ON NR 3 ENGINE RUPTURED. REMOVED AND REPLACE
- [SDR RRXA98073](https://openairdocs.org/sdr/RRXA98073), Mar 24, 1998: FIRE ELEMENT. SHORTED. CLIMBING THROUGH 13000 FT, NR 2 ENG FIRE WARNING CAME ON. SHUT DOWN ENGINE AND FIRE WARNING WENT OUT. TESTED FIRE WARNING AND TEST WAS INOP, DISCHARGED AGENT AF

All 194: https://openairdocs.org/model/douglas-dc-8f-54/reports.md

## STCs that may be installed (OpenAirDocs) (143, 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 SA3169NM](https://openairdocs.org/stc/SA3169NM): Installation of floor proximity emergency escape marking system. Bruce Aerospace Inc
- [STC ST01174CH](https://openairdocs.org/stc/ST01174CH): Installation of UPS Aviation Technologies ADS-B provisions and Honeywell Mode-S System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC SA2534SW-D](https://openairdocs.org/stc/SA2534SW-D): Replacement of Switch assembly Int'l Inflatables Co. P/N 68748, with DME Corp. P/N L-140 in emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC SA2539SW-D](https://openairdocs.org/stc/SA2539SW-D): Replacement of light assembly, International Inflatables Co. P/N68555-1 with DME Corp. EL-104, EL-104A, and EL-104B in emergency slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC SA863EA](https://openairdocs.org/stc/SA863EA): Incorporation of DME Corporation emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC ST02580AT](https://openairdocs.org/stc/ST02580AT): Lithium cell battery pack to replace currently approved alkaline battery pack used in escape slide emergency light system. Astronics Luminescent Systems Inc
- [STC SA804EA](https://openairdocs.org/stc/SA804EA): Installation of Inflight Motion Picture system. Burrana Inc
- [STC SA3421NM](https://openairdocs.org/stc/SA3421NM): Installation of Hughes-Avicom video entertainment system. Burrana Inc. Lists DC-8 Series
- [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 SA4088WE](https://openairdocs.org/stc/SA4088WE): Installation of single or dual Litton LTN-72 INS. Northrop Grumman Systems Corporation
- [STC SA633CE](https://openairdocs.org/stc/SA633CE): Make and install cargo pallets. Telair US LLC
- [STC SA813CE](https://openairdocs.org/stc/SA813CE): Install Brooks & Perkins cargo pallet P/N 17430-100-2. Telair US LLC
- [STC SA843CE](https://openairdocs.org/stc/SA843CE): Installation of cargo-pallet17469-500-1. Telair US LLC
- [STC SA1511GL](https://openairdocs.org/stc/SA1511GL): Installation of Type "C" containers. ABX Air Incorporated
- [STC SA1462GL](https://openairdocs.org/stc/SA1462GL): Installation of ABX Cargo Handling System. ABX Air Incorporated
- [STC ST369CH](https://openairdocs.org/stc/ST369CH): Approve autopilot and/or flight director coupled approach with 35 landing flap selection. ABX Air Incorporated
- [STC SA1033WE](https://openairdocs.org/stc/SA1033WE): Installation of either single or dual Collins AL-101 Radio Altimeter System(s) in accordance with FAA Approved United Air Lines Report Nos. F-1038 and No. F-1054. United Airlines Inc
- [STC SA1034WE](https://openairdocs.org/stc/SA1034WE): Installation control and annunciation circuitry to implement Flight Director "Go-Around" command modes in accordance with the UAL FAA approved drawing list dated August 11, 1965, revised August 16, 1965. UAL FAA approved Airplane Flight Manual Supplementary Log of pages as listed. Type Manual Approved Dated Appendix DC-8-21, 31, 32, 33 SM 23889 1-19-60, 3-60, 2-1-60 and V 11-28-60 respectively DC-8-51, 52, 53 LB 30582 10-10-61, 4-28-61 and 4-28-61 resp. VII DC-8-51, 52, 53 LB 30757 1-26-62 IV DC-8F-54, 55 LB 31180 1-29-63, 6-19-64 respectively IV. United Airlines Inc
- [STC SA1120NW-D](https://openairdocs.org/stc/SA1120NW-D): Replacement of NAS3610-2AIP cargo pallets and NAS3610-2AIN nets with L size pallets and nets in accordance with DAS-1-WE Approved Drawing List No.1120 dated May 8, 1981, or later FAA approved revisions. United Airlines Inc
- [STC SA1184WE](https://openairdocs.org/stc/SA1184WE): Installation - Cockpit Voice Recorder, United Data Control, Inc., per approved United Air Lines Report No. F-1067 for the DC-8F-54 and DC-8F-55 and Report No. F-1015 for DC-8-12, -21, -31, -32, -33, -51, -52. United Airlines Inc
- [STC SA1220WE](https://openairdocs.org/stc/SA1220WE): Substitution of Brownline pallet P/N 23118-51 for Douglas pallet P/N 5776662-505 and use of Brownline pallet net P/N 22672-51 on Brownline pallet P/N 23118-51 and Douglas pallet P/N 5776662-505. United Airlines Inc
- [STC SA1395WE](https://openairdocs.org/stc/SA1395WE): Substitution of Brownline Pallet P/N 23640-51 and P/N 23224-51 for Douglas Pallet P/N 5776662-505. United Airlines Inc
- [STC SA1522WE](https://openairdocs.org/stc/SA1522WE): Substitution of Brownline cargo container assembly P/N 24026-51 for Douglas pallet assembly P/N 5776662-505 and net P/N 7778335 in accordance with FAA Approved United Air Lines Drawing List No. COA 2-3160 revised October 11, 1967, or later FAA approved revisions. United Airlines Inc
- [STC SA1538WE](https://openairdocs.org/stc/SA1538WE): Installation of Fairchild Model 13920-301 or 15630-601 Flight Data Recorder and Honeywell P/N 180 VI Central Air Data Computer in accordance with FAA Approved United Air Lines Report F-1174 dated September 8, 1967, revised November 13, 1967, or later FAA approved revision. United Airlines Inc
- [STC SA1603WE](https://openairdocs.org/stc/SA1603WE): Replacement of DC-8 reverser system - primary reverser cover door - JT3D engine with improved door designed and fabricated by United Air Lines. 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 SA2584WE](https://openairdocs.org/stc/SA2584WE): Installation of Aeroquip cargo net P/N 3950020 with any TSO-C90 approved NAS 3610-2A1, 2A3, or 2A4 cargo pallet. United Airlines Inc
- [STC SA2745WE-D](https://openairdocs.org/stc/SA2745WE-D): This modification provides seats, oxygen, cockpit communications, emergency equipment and other items necessary to carry six couriers or other persons authorized aft of Station 1370. United Airlines Inc
- [STC SA2827WE-D](https://openairdocs.org/stc/SA2827WE-D): Installation of Collins FPC-75 part number 622-2615-012 or 622-2615-212 Ground Proximity Warning System Computer in conformance with United Airlines DAS-1-WE Approved Master List of drawings and documents for STC No. SA2827WE-D dated February 26, 1979 or later approved revisions. An alternate approved configuration consists of part number 622-2615-011 Rev. N or part number 622-2615-211 GPWS computer and a part number 622-2668-011 Barometric Altitude Computer installed in conformance with DAS-1-WE Approved Master List of drawings and related documents or later FAA approved revision (Continued on page 3.). United Airlines Inc
- [STC SA3189WE](https://openairdocs.org/stc/SA3189WE): Installation of United Air Lines NLG orifice support tube assembly P/N 6F13548-501 and -502 per FAA Approved United Air Lines Drawing No. 6F13548, Rev. "B" dated January 10, 1977, or later FAA approved revisions as an equivalent replacement for McDonnell Douglas NLG orifice support tube P/N 5598184 and 5717019. United Airlines Inc
- [STC SA3357WE-D](https://openairdocs.org/stc/SA3357WE-D): Retrofit of fuel quantity indicators and totalizers, Gull Airborne, Instruments, Inc. part numbers 206-009 and 206-016 series. United Airlines Inc
- [STC SA3586WE-D](https://openairdocs.org/stc/SA3586WE-D): Installation of a removable dual Delco C-IV inertial navigation system for navigation only. United Airlines Inc
- [STC SA4-918](https://openairdocs.org/stc/SA4-918): 1. Aircraft wiring in accordance with Douglas Aircraft Co. Service Change #17 (UAL COA-0-1456) to provide an operational Aircraft Flight Data Rrecorder conforming to CAR Amendment 40-6, paragraph 40.208 with the following additions to assure recording of data during takeoff and landing roll: a. Relay to provide automatic start of recording when nose landing gear reaches airborne condition on takeoff. b. Time delay relay to turn off recorder one minute after nose landing gear reaches "on ground" condition, on landing. c. Installation of standard toggle switch on Systems Engineer's Console, to permit Second Officer to turn on recorder at start of takeoff run. 2. Install Waste King Flight Data Recorder #5424, TSO-C51. United Airlines Inc
- [STC SA611WE](https://openairdocs.org/stc/SA611WE): Interior configuration - 120 passenger single class 5-abreast seating per United Air Lines approved drawing lists: COA 2-2083 (Sheet #1 Revision February 17, 1964, Sheet #2 dated December 4, 1963, Sheet #3 Revision dated February 27, 1964 and, COA 2-2099 Revision dated December 17, 1963). United Airlines Inc
- [STC SA65WE](https://openairdocs.org/stc/SA65WE): Installation of a cockpit hydraulic replenishing system. See 15F-2044 Chg. B, 9F-4813 Chg. C, 6F-8140 Chg. C, 6F-8130 Chg. B, 3F-9025 Chg. A, 3F-9022, 3F-9023 Chg. A, IF-9882, 6F-8141 Chg. C. COA-2-1534 (ERs 1 - 4), App. V(UAL) to AFM SM-23889, App. IV (UAL) to AFM SM-23891, App. VII(UAL) to AFM LB-30582 or later FAA approved revisions. United Airlines Inc
- [STC SA833WE](https://openairdocs.org/stc/SA833WE): Installation of two triple seats in the main cabin and associated changes per United Air Lines Drawing No. 6F-8882 "E" change, "DC-8F Interior Arrangement" and the following drawings: (see Continuation Sheet). United Airlines Inc
- [STC SA293EA](https://openairdocs.org/stc/SA293EA): Tray carrier. Lockheed Aircraft Service Co
- [STC ST00850AT](https://openairdocs.org/stc/ST00850AT): Increase in aircraft operating weights as substantiated by the design data. (DC-8F-54 S/Ns 45802, 45886, 46012 only)). Aircraft Modification Design Services
- [STC ST00924AT](https://openairdocs.org/stc/ST00924AT): Increase in aircraft operating weights(maximum landing weight - 240,000 lbs., maximum zero fuel weight - 224,000 lbs.) (DC-8F-54 S/N 45637). Aircraft Modification Design Services
- [STC SA2082SO](https://openairdocs.org/stc/SA2082SO): Installation of fuselage window plugs. Kosola & Associates Inc
- [STC SA1405WE](https://openairdocs.org/stc/SA1405WE): Structural installation of Dorne and Margolin DMC 33-2 Satcom VHF radio antenna. United Air Lines Inc
- [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing
- [STC ST01220AT](https://openairdocs.org/stc/ST01220AT): Installation of a Dual Trimble Model TNL-8100 Global Positioning System. Avionics Group Inc. Lists DC-8 Series
- [STC ST01380AT](https://openairdocs.org/stc/ST01380AT): Installation of QTV Stage 3 Plus Hushkit. Quiet Technology Venture Ltd
- [STC SA1076NE](https://openairdocs.org/stc/SA1076NE): Installation of Aerofex livestock carrier P/N TS-QA-400 platform and panel system using size A or size M Class II pallet. Equine Air Transport Systems LLC
- [STC ST127CH](https://openairdocs.org/stc/ST127CH): Installation of strobe upper anticollision light, P/N 30-1585-1. Honeywell International Inc
- [STC SA523NE](https://openairdocs.org/stc/SA523NE): Installation of two Turbomach (solar) T-62T-40C gas turbine auxiliary powerplants. Limited to installation on serial number 45881 ONLY. PATS Aircraft LLC

All 143: https://openairdocs.org/model/douglas-dc-8f-54/stcs.md

## The same model under other registry codes

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

- [Mcdonnell Douglas DC-8F-54](https://openairdocs.org/model/mcdonnell-douglas-dc-8f-54): 0 registered aircraft, registry code 302192H

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