# Douglas DC-8F-55

- Type: Aircraft model (FAA registry)
- Registry code: 3021928
- Manufacturer (registry): DOUGLAS
- Model: DC-8F-55
- 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-55

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 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

All 133: https://openairdocs.org/model/douglas-dc-8f-55/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 (2)

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 MIA98IA035](https://openairdocs.org/ntsb/MIA98IA035), Nov 20, 1997: Douglas DC-8F-55 (N55FB), Miami, FL, incident, minor damage. Probable cause: The inadequate overhaul of the No. 4 engine start valve resulting in the valve remaining open after engine start; and the subsequent free run state of the starter resulting in a starter overheat,…
- [NTSB NYC68I0068](https://openairdocs.org/ntsb/NYC68I0068), Nov 2, 1967: Douglas DC-8F (N801SW), Jamaica, NY, incident, minor damage

## FAA accident and incident reports (5)

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 19981125043539I](https://openairdocs.org/incident/19981125043539I), Nov 25, 1998: Doug DC855 (N801CK), El Paso, TX. (-5)DC-8, operated by gaia, on 11/25/98 had #3 engine oil loss, engine shot down and windmill oil press. Nas 20-60 p.s.I. Aircraft landed El Paso, TX. Without…
- [Incident 19971120045769I](https://openairdocs.org/incident/19971120045769I), Nov 20, 1997: Doug DC8F55 (N55FB), Miami, FL, Minor damage. (-5) On November 20, 1997, about 1312 eastern standard time, a Douglas DC-8F-55, N55FB, registered to agro air associates, inc., operated by fine air services,…
- [Incident 19970610022399I](https://openairdocs.org/incident/19970610022399I), Jun 10, 1997: Doug DC8F55 (N801CK), Miami, FL. Problems yaw damper. Placarded not to use. Put on MEL. Problems using autopilot. Replaced auto pilot disconnect.
- [Incident 19960904030629I](https://openairdocs.org/incident/19960904030629I), Sep 4, 1996: Doug DC855 (N809CK), Atlanta, GA, Minor damage. Narrative: phase of operation was taxi to ramp position. Wing walker did not get a/c stopped in time to miss N901SJ Lockheed L-382E aircraft l/wing tip and…
- [Incident 19900215064919I](https://openairdocs.org/incident/19900215064919I), Feb 15, 1990: Doug DC8F55 (N855BC), Fort Wayne, IN. Cargo door opened and dumped cargo on takeoff. Returned and landed. Microswitch was broken and striker bent.

## Service difficulty reports (238, newest 50)

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

- [SDR 20001208AP007](https://openairdocs.org/sdr/20001208AP007), Aug 28, 2000: LONGERON. CRACKED. DURING B-CHECK INSPECTION, FOUND THE FOLLOWING, CRACKED LONGERON AT STATION 248, RECORDED ON NON-ROUTINE ITEM NR 3222. REPAIRED CRACKED LONGERON IAW SRM 53-2-2.
- [SDR 20001208AP005](https://openairdocs.org/sdr/20001208AP005), Aug 28, 2000: FITTING. CORRODED. DURING B-CHECK INSPECTION, FOUND THE FOLLOWING, CORRODED LONGERON FITTING AT BS 248, L-33R, RECORDED ON NON-ROUTINE ITEM NR 3257. REPLACED LONGERON SPLICE FITTI
- [SDR 20001208AP004](https://openairdocs.org/sdr/20001208AP004), Aug 28, 2000: DOOR. OPEN. JUST AFTER TAKEOFF FROM KINGSTON CREW NOTICED THAT THE NLG DOOR STAYED OPEN. RETURNED FLIGHT BACK TO KINGSTON AND LANDED WITH A GROSS WEIGHT OF 190,000 LBS. UPO
- [SDR 2000ZZZX690](https://openairdocs.org/sdr/2000ZZZX690), Nov 18, 1999: FITTING. CRACKED. LEFT HAND STA 98 FLAP ACTUATOR ATTACH FITTING (INSIDE PANEL 562L) HAS APPROXIMATELY 1 INCH CRACK IN IT. REMOVED AND REPLACED FITTING IAW DC-8 SRM'S 57-3-0, 51-3
- [SDR 2000ZZZX684](https://openairdocs.org/sdr/2000ZZZX684), Nov 17, 1999: DOOR. DAMAGED. REPLACED COCKPIT DOOR. FABRICATED NEW COCKPIT DOOR PER EO 99-136 WITH APPROVED 8110-3 DATED 8-3-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX697](https://openairdocs.org/sdr/2000ZZZX697), Nov 16, 1999: FLOOR PANEL. CORRODED. CORROSION EXISTS ON THE SURFACE OF ALL FLOOR PLANKS FROM STA 280 TO STA 1490 L21L TO L21R. REMOVED CORROSION BY CHEMICAL METHOD. TREATED AND PRIMED. IT IS ACCEP
- [SDR 2000ZZZX708](https://openairdocs.org/sdr/2000ZZZX708), Nov 11, 1999: FILLER. MISSING. DUE TO EXISTING REPAIR, DOUBLER ON LT FRONT SPAR (XRS 69.5) LOWER WING PLANK, TAPER FILLERS NEED TO BE FABRICATED TO COMPLETE SB 57-2OR5. FABRICATED FILLERS AND
- [SDR 2000ZZZX676](https://openairdocs.org/sdr/2000ZZZX676), Nov 11, 1999: SKIN. CRACKED. DURING C-CHECK, FOUND .50 INCH LOWER L/E SURFACE AT INBOARD SLOT APPROXIMATELY XFS 213.5 LT WING. NDT TO ASSURE CRACK HAD BEEN STOPPED. FABRICATED EXTERNAL DOUB
- [SDR 2000ZZZX675](https://openairdocs.org/sdr/2000ZZZX675), Nov 11, 1999: SKIN. CRACKED. FOUND DURING C-CHECK. CRACK LOCATED AT INBOARD SLOT LOWER L/E, 1.50 INCHES LONG ON RT WING XFS 214.25. NDT CRACK TO ASSURE THAT CRACK HAD BEEN STOPPED. FABRICAT
- [SDR 2000ZZZX694](https://openairdocs.org/sdr/2000ZZZX694), Nov 8, 1999: SPAR. CRACKED. LOWER FRONT SPAR HORIZONTAL LEG 10 INCH CRACK BS 680 - 26.5 INCHES TO 36.50 INCHES RBL CENTER WING TANK. CUT OUT DAMAGE. FABRICATED FILLER, DOUBLERS, AND INSTAL
- [SDR 2000ZZZX671](https://openairdocs.org/sdr/2000ZZZX671), Nov 8, 1999: SPAR. CRACKED. LOWER FRONT SPAR 1.50 INCH CRACK FS 680 LBL 34 INCHES Z AXIS -47 AND .50 INCH CRACK BS 680 LBL XCW 39 INCHES AND XCW 43 INCHES Z AXIS -47 INCH. CUT OUT DAMAGE. 
- [SDR 2000ZZZM213](https://openairdocs.org/sdr/2000ZZZM213), Nov 8, 1999: SPAR. CRACKED. LOWER FRONT SPAR HORIZ LEG 10 INCHES CRACK FS 680 - 26.5 TO 36.5 INCH RBL CENTER WING TANK. CUT OUT DAMAGE. FABRICATED FILLERS, DOUBLERS AND INSTALLED IAW DC-8 
- [SDR 2000ZZZX681](https://openairdocs.org/sdr/2000ZZZX681), Nov 5, 1999: FAIRING. DAMAGED. PANEL 162V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED WITH DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATI
- [SDR 2000ZZZX680](https://openairdocs.org/sdr/2000ZZZX680), Nov 5, 1999: FAIRING. DAMAGED. PANEL 161V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL 
- [SDR 2000ZZZX679](https://openairdocs.org/sdr/2000ZZZX679), Nov 5, 1999: SKIN. DAMAGED. RT MLG DOOR CENTER STRUT/SEVERAL SCREWS STARTING TO PULL THROUGH SKIN. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-
- [SDR 2000ZZZM260](https://openairdocs.org/sdr/2000ZZZM260), Nov 5, 1999: SKIN. DAMAGED. SCREWS PULLING THROUGH SKIN L/E CENTER SECTION LOWER SURFACE XW454 LEFT WING. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO NR 99-136 WITH APPROVED 8110-3
- [SDR 2000ZZZX670](https://openairdocs.org/sdr/2000ZZZX670), Nov 4, 1999: TEE. CORRODED. THROUGH ACCESS HOLE 506C AND THROUGH INBOARD RIB CUT-OUT, INBOARD LOWER WING STR 63-72 AT STA XW.000 IN NR 3 MAIN TANK HAS CORROSION BETWEEN STRINGER. REMOVED C
- [SDR 2000ZZZX711](https://openairdocs.org/sdr/2000ZZZX711), Nov 2, 1999: WEB. CRACKED. FOUND DURING C-CHECK. RT FLAP EXHAUST GATE INBOARD END WEB CRACKED. CUT OUT INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 10-29-99. REF: ZANTOP INTERNATION
- [SDR 2000ZZZX688](https://openairdocs.org/sdr/2000ZZZX688), Nov 2, 1999: GILLINER. DAMAGED. REPLACED MAIN CABIN GILLINER AND STRAPS PER EO NR 99-136 WITH APPROVED 8110-3 DATED 7-24-99. REF: ZANTOP INTERNAL AIRLINES, INC. ZIAA.
- [SDR 2000ZZZX682](https://openairdocs.org/sdr/2000ZZZX682), Nov 2, 1999: FITTING. CORRODED. PANEL 162V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED WITH DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATI
- [SDR 2000ZZZX677](https://openairdocs.org/sdr/2000ZZZX677), Nov 2, 1999: SKIN. CRACKED. INBOARD AILERON L/E PLATING AT STA XA 503.5 HAS A 2.5 INCH CRACK (EO). ROUTED OUT CRACK. FABRICATED DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DAT
- [SDR 2000ZZZM215](https://openairdocs.org/sdr/2000ZZZM215), Nov 2, 1999: WEB. CRACKED. FOUND DURING C-CHECK, RIGHT FLAP EXHAUST GATE INBOARD END WEB CRACKED. CUT OUT CRACKED SECTION. FABRICATED NEW WEB AND INSTALLED PER EO NR 99-136 WITH APPROVED 
- [SDR 2000ZZZX695](https://openairdocs.org/sdr/2000ZZZX695), Oct 29, 1999: SPAR. CRACKED. FOUND DURING C-CHECK. A 4.75 INCH CORROSION CRACK APPROXIMATE STA XCW 31.0 LT IN FRONT SPAR LOWER T-CAP VERTICAL LEG. ROUTED OUT CRACK, BLENDED, NDT CONFIRMED C
- [SDR 2000ZZZM214](https://openairdocs.org/sdr/2000ZZZM214), Oct 29, 1999: SPAR. CRACKED. FOUND DURING C-CHECK, A 4.75 INCH CORROSION CRACK APPROX STATION XCW 31 LEFT IN FRONT SPAR LOWER T-CAP VERTICAL LEG. ROUTED OUT CRACK, BLENDED, NDT CONFIRMED CR
- [SDR 2000ZZZX703](https://openairdocs.org/sdr/2000ZZZX703), Oct 28, 1999: SKIN. CRACKED. AFT LEFT COWL DOOR HAS 3 INCH CRACK OUTSIDE SKIN AT INLET SCOOP NR 3 ENGINE. STOP DRILLED, NDT CONFIRMED CRACK HAS BEEN STOPPED. WELDED CRACK AND NDT NO FLAWS. 
- [SDR 2000ZZZX709](https://openairdocs.org/sdr/2000ZZZX709), Oct 25, 1999: GEAR TAB. DENTED. RT ELEVATOR GEAR TAB DAMAGED DENT/CREASE. REPAIRED RT ELEVATOR GEAR TAB PER EO 99-136 WITH APPROVED 8110-3 DATED 10-15-99. REF: ZANTOP INTERNATIONAL AIRLINES, I
- [SDR 2000ZZZX669](https://openairdocs.org/sdr/2000ZZZX669), Oct 21, 1999: RING. MISSING. FOUND DURING C-CHECK. DOUBLER AROUND CIRCUMFERENCE OF FORWARD SIDE OF WIND SOCK HAS SECTION MISSING. NR 4 ENGINE. FABRICATED NEW SECTION, WELDED IN PLACE NDT WE
- [SDR 2000ZZZX704](https://openairdocs.org/sdr/2000ZZZX704), Oct 19, 1999: DUCT. CRACKED. NR 2 ENGINE INBOARD SIDE 1 O'CLOCK POSITION. FIRE EXTINGUISHER DUCT CRACKED AT ATTACH ANGLE. REMOVED DUCT, REPAIRED PER BOEING MEMO 99-00006 H AND EO 99-136 WIT
- [SDR 2000ZZZM235](https://openairdocs.org/sdr/2000ZZZM235), Oct 18, 1999: DRAIN. CRACKED. FOUND DURING C-CHECK, LEFT MAIN GEAR WELL FORWARD DRAIN SPOUT CRACKED. NDT TO DETERMINE END OF CRACK, STOP DRILLED AND WELDED PER MIL-STD-2219. NDT NO FLAWS PER
- [SDR 2000ZZZX696](https://openairdocs.org/sdr/2000ZZZX696), Oct 14, 1999: SKIN. MISREPAIRED. LEFT HAND AFT ENTRY DOOR FUSELAGE SKIN CUT-OUT, PREVIOUS REPAIR IMPROPER STA 1400 - L21L. REMOVED EXISTING DOUBLER. FABRICATED NEW DOUBLER AND INSTALLED PER EO 
- [SDR 2000ZZZX689](https://openairdocs.org/sdr/2000ZZZX689), Oct 14, 1999: FRAME. CRACKED. FUSELAGE STATION 460 LONGERON 21R FRAME BENT AND FRAME CAP CRACKED. REMOVED DAMAGED SECTION OF FRAME. FABRICATED FRAME SPLICES IAW DC-8 SRM 53-2-0. TREATED AND 
- [SDR 2000ZZZX702](https://openairdocs.org/sdr/2000ZZZX702), Oct 9, 1999: RIVET. SHEARED. NR 1 ENGINE RIVET HEAD SHEARED IN INTAKE FOR PNEUMATIC HEAT EXCHANGER. IT IS ACCEPTABLE TO USE AS IS, IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH A
- [SDR 2000ZZZX699](https://openairdocs.org/sdr/2000ZZZX699), Oct 6, 1999: HEAT SHIELD. CRACKED. NR 1 ENGINE HEAT SHIELD FOR MAIN FUEL LINE CRACKED. STOP DRILLED CRACK, NDT TO ASSURE CRACK HAD BEEN STOPPED. WELDED ACCORDING TO MIL-STD-2219. NDT WELD NO FLAW
- [SDR 2000ZZZX687](https://openairdocs.org/sdr/2000ZZZX687), Oct 5, 1999: PIPE. CHAFED. FOUND DURING C-CHECK. NR 3 PYLON VENTILATION PIPE CHAFED. FABRICATED DOUBLERS AND WELDED IN PLACE IAW BOEING MESSAGE M-7200-99-07969 WITH APPROVED 8110-3 DATED 
- [SDR 2000ZZZX678](https://openairdocs.org/sdr/2000ZZZX678), Sep 27, 1999: SKIN. CRACKED. LEFT WING OUTBOARD FLAP SKIN JUST BELOW HINGE FITTING IS CRACKED STA XR 219. STOP DRILLED CRACKS, NDT TO ASSURE CRACKS HAD BEEN STOPPED. FABRICATED DOUBLER AND 
- [SDR 2000ZZZX672](https://openairdocs.org/sdr/2000ZZZX672), Sep 23, 1999: FITTING. CRACKED. RIGHT ELEVATOR NR 2 A-FRAME CRACKED. REMOVED AND REPLACED NR 2 POSITION A-FRAME RT ELEVATOR IAW DC-8 OHM 27-30-1. (X)
- [SDR 2000ZZZX691](https://openairdocs.org/sdr/2000ZZZX691), Sep 16, 1999: LONGERON. CORRODED. LONGERON 6R STA 1490 TO STA 1600, HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED, AND REPAIRED PER DC-8 SRM 53-2-2 PAGES 59/60
- [SDR 2000ZZZM210](https://openairdocs.org/sdr/2000ZZZM210), Sep 16, 1999: LONGERON. CORRODED. LONGERON 6R STATION 1490 TO 1600 HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED AND REPAIR PER DC-8 SRM 53-2-2 PAGE 59/60 PER 
- [SDR 2000ZZZX700](https://openairdocs.org/sdr/2000ZZZX700), Sep 15, 1999: SPINNER. CRACKED. NOSE COWL CRACKED AT 6:00 O'CLOCK POSITION NR 4 ENGINE. CUT OUT PREVIOUS WELD, NDT TO ASSURE ALL CRACKS STOPPED. FABRICATED PLUG AND WELDED IN PLACE. NDT WELD N
- [SDR 2000ZZZX692](https://openairdocs.org/sdr/2000ZZZX692), Sep 15, 1999: RING. CRACKED. LONGERON 6R STA 1490 TO STA 1600, HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED, AND REPAIRED PER DC-8 SRM 53-2-2 PAGES 59/60
- [SDR 2000ZZZX683](https://openairdocs.org/sdr/2000ZZZX683), Sep 15, 1999: LEG. BROKEN. LEFT MAIN W/W SAFETY NET LEG BROKEN OFF. WELDED NEW SECTION OF TUBING PER MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO 99-136 WITH APPROVED 8110-3 DATED 9-10-99
- [SDR 2000ZZZM211](https://openairdocs.org/sdr/2000ZZZM211), Sep 15, 1999: RING. CRACKED. INBOARD TOP SIDE OF TRANSLATING RING HAS CRACK NR 4 ENGINE. STOP DRILLED CRACK, NDT TO ASSURE CRACK STOPPED. FABRICATED DOUBLER AND INSTALLED PER EO NR 99-136 W
- [SDR 2000ZZZX673](https://openairdocs.org/sdr/2000ZZZX673), Sep 14, 1999: LONGERON. CORRODED. LONGERON 30, 31 RIGHT AT STA 320 HAD CORROSION. REMOVED CORROSION. FABRICATED FILLER, DOUBLER, AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 9-1-99. RE
- [SDR 2000ZZZX686](https://openairdocs.org/sdr/2000ZZZX686), Sep 10, 1999: PANEL. CORRODED. LEFT OUTBOARD MOST UPPER SLOT DOOR BOTTOM INBOARD OF INBOARD ADJ SCREW HAS CORROSION XS 503.789. BLENDED OUT CORROSION, TREATED AND PRIMED. MAXIMUM UNDER CUT IN
- [SDR 2000ZZZX701](https://openairdocs.org/sdr/2000ZZZX701), Sep 9, 1999: RIVET. SHEARED. NR 1 ENGINE RIVET HEAD SHEARED IN INTAKE FOR OIL COOLER. IT IS ACCEPTABLE TO USE AS IS. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3
- [SDR 2000ZZZX706](https://openairdocs.org/sdr/2000ZZZX706), Sep 8, 1999: OUTFLOW VALVE. CORRODED. SUGAR SCOOP CORRODED (OUTFLOW VALVE) STA 1323. REMOVED CORROSION IAW DC-8 SRM 51-1-8. WELDED AREA, NDT TO ASSURE NO FLAWS (NONE FOUND) BLEND SMOOTH AND FINISHED
- [SDR 2000ZZZM229](https://openairdocs.org/sdr/2000ZZZM229), Sep 2, 1999: FITTING. CRACKED. DURING B-CHECK INSPECTION, FOUND 20 INCH CRACK AT LEFT INBOARD CANOE FITTING AT STATION 98. REPLACED FITTING AT LEFT CANOE IAW MM 27-27-7. (M)
- [SDR 2000ZZZM245](https://openairdocs.org/sdr/2000ZZZM245), Aug 31, 1999: SKIN. CORRODED. DURING D-CHECK INSPECTION, FOUND THE FOLLOWING, CORROSION DAMAGE AT LEFT AND RIGHT RUDDER SKIN. REPAIRED CORROSION DAMAGE IAW FINE AIR EO NR 9808131, SRM 51-1-2
- [SDR 2000ZZZX685](https://openairdocs.org/sdr/2000ZZZX685), Aug 30, 1999: PANEL. CORRODED. OUTBOARD SLOT LEFT WING L/E HAS AREA OF EXFOLIATION XW 454. CUT OUT AREA OF EXFOLIATION. FABRICATED FILLER, DOUBLER, AND INSTALLED PER EO 99-136 WITH APPROVED 8
- [SDR 2000ZZZX674](https://openairdocs.org/sdr/2000ZZZX674), Aug 26, 1999: SKIN. CRACKED. LEFT WING CENTER L/E OTBD EDGE XFS 291.500 FWD VERTICAL PLATE CRACKED APPROXIMATELY 3 INCHES. REMOVED OUTBOARD END WEB. FABRICATED NEW SECTION AND SPLICE PLATE 

All 238: https://openairdocs.org/model/douglas-dc-8f-55/reports.md

## STCs that may be installed (OpenAirDocs) (112, 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 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 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 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 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 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 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 ST09247SC](https://openairdocs.org/stc/ST09247SC): Installation of dual Universal UNS-1D FMS/GPS navigation systems. Aircraft Systems & Mfg
- [STC ST01163CH](https://openairdocs.org/stc/ST01163CH): Installation of an AlliedSignal CAS67A traffic alert and collision avoidance system (TCAS II). EAD Inc
- [STC ST01004NY](https://openairdocs.org/stc/ST01004NY): Installation of cargo restraint straps. Airline Container Manufacturing Co Inc. Lists DC-8 Series
- [STC ST01188LA](https://openairdocs.org/stc/ST01188LA): Installation of upper and lower red anti-collision light. Responsible ACO is Los Angeles, NM-L. BF Goodrich Aerospace. Lists DC-8 Series
- [STC SA1296GL](https://openairdocs.org/stc/SA1296GL): Installation of Norton Radome kit No. 4784CX. Saint-Gobain Performance Plastics Corp
- [STC ST09336SC](https://openairdocs.org/stc/ST09336SC): Installation of Innovative System and Support, Inc, Altitude Control System (ACS), Digital Air Data Computer, Altimeter, Airspeed Indicator, and Altitude Alerter. Aircraft Systems & Mfg
- [STC ST01253CH](https://openairdocs.org/stc/ST01253CH): Installation of a Pneumatic Air Cycle system. National Aircraft Service Inc
- [STC SA2539WE](https://openairdocs.org/stc/SA2539WE): Installation of emblem light. DeVore Aviation Corporation of America, a New Mexico Corporation
- [STC ST00792CH](https://openairdocs.org/stc/ST00792CH): Installation of National Aircraft Services, Inc Supplemental Floor Heat. National Aircraft Service Inc
- [STC ST09534SC](https://openairdocs.org/stc/ST09534SC): Installation of the ARINC 542A DFDR 18 sensor upgrade. Aircraft Systems & Mfg. Lists DC-8 Series
- [STC ST09495SC](https://openairdocs.org/stc/ST09495SC): Installation of a Universal Avionics Radio Reference Sensor (RRS) unit. Aircraft Systems & Mfg
- [STC ST00791CH](https://openairdocs.org/stc/ST00791CH): Installation of a dual GPS, Trimble 2101 I/O Approach Plus System. American Intl Airways
- [STC SA3915NM](https://openairdocs.org/stc/SA3915NM): Modification of DC-8 airplanes by installation of engine inlet and exhaust noise attenuation treatment. Topeka Management, Inc
- [STC SA4071SW](https://openairdocs.org/stc/SA4071SW): Modification of Janitrol heat exchangers. Limco-Airepair, Inc
- [STC ST01079AT](https://openairdocs.org/stc/ST01079AT): Installation of global positioning system monitoring unit. ARINC Inc. Lists DC-8 Series
- [STC SA1327NM](https://openairdocs.org/stc/SA1327NM): Installation of heavy duty Universal pallet system. (DC-8 series refer to PEMCO engineers index list PDC-8). Pemco Engineers Inc. Lists DC-8 Series
- [STC ST179CH](https://openairdocs.org/stc/ST179CH): Installation of cargo container curtain. Plastic Composites Corp. Lists DC-8 Series
- [STC ST466CH](https://openairdocs.org/stc/ST466CH): Installation of a pneumatic flow control system. National Aircraft Service Inc
- [STC ST145CH](https://openairdocs.org/stc/ST145CH): Installation of air conditioning system. Tech Air Corporation
- [STC ST00625AT](https://openairdocs.org/stc/ST00625AT): Installation of a Trimble TNL-8100 GPS navigation system. Rich Intl Airways. Lists DC-8 Series
- [STC ST258CH](https://openairdocs.org/stc/ST258CH): Install ballast assembly according to drawing lists. ABX Air Incorporated

All 112: https://openairdocs.org/model/douglas-dc-8f-55/stcs.md

## The same model under other registry codes

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

- [Mcdonnell Douglas DC-8F-55](https://openairdocs.org/model/mcdonnell-douglas-dc-8f-55): 0 registered aircraft, registry code 302192M

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