# Douglas DC-8-71F

- Type: Aircraft model (FAA registry)
- Registry code: 302199D
- Manufacturer (registry): DOUGLAS
- Model: DC-8-71F
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-jet
- Seats: 152
- Weight class: 20,000 lb and over
- 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-8-71f

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 2003-17-07 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 2001-08-16](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 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
- [AD 97-04-04](https://openairdocs.org/ad/97-04-04): Auxiliary Power Units · Airbus BAC 1-11 200 Series, BAC 1-11 400 Series, Auxiliary Power Units and 54 more. Effective Mar 24, 1997
- [AD 96-17-07](https://openairdocs.org/ad/96-17-07): Main Landing Gear Swivel Bogie Beam Lugs · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Sep 23, 1996
- [AD 96-02-06](https://openairdocs.org/ad/96-02-06): AFM - Limitations - Windshear · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 59 more. Effective Feb 26, 1996

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 2004-06-06](https://openairdocs.org/ad/2004-06-06) (historical): Lower cargo doorjamb corners · McDonnell Douglas DC-8-71, DC-8-71F, DC-8-72 and 3 more. Effective Apr 29, 2004
- [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 88-11-03](https://openairdocs.org/ad/88-11-03) (historical): Generator Cables · McDonnell Douglas DC-8-71, DC-8-71F, DC-8-72 and 3 more. Effective Jun 3, 1988
- [AD 83-02-05](https://openairdocs.org/ad/83-02-05) (historical): Exhaust Nozzle Plug · McDonnell Douglas DC-8-71, DC-8-71F, DC-8-72 and 3 more. Effective Feb 7, 1983

All 136: https://openairdocs.org/model/douglas-dc-8-71f/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 (8)

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 DCA06MA022](https://openairdocs.org/ntsb/DCA06MA022), Feb 8, 2006: Douglas DC-8 (N748UP), Philadelphia, PA, destroyed. Probable cause: an in-flight cargo fire that initiated from an unknown source, which was most likely located within cargo container 12, 13, or 14. Contributing to the loss of the aircraft were the inadequate…
- [NTSB ANC02IA007](https://openairdocs.org/ntsb/ANC02IA007), Dec 14, 2001: Douglas DC-8-71F (N825BX), Anchorage, AK, incident, no damage. Probable cause: The asymmetrical activation of the left wing spoiler due to a broken retraction cable during takeoff. A factor associated with the incident was the operator's inadequate inspection of the cable.
- [NTSB MIA01IA129](https://openairdocs.org/ntsb/MIA01IA129), Apr 26, 2001: McDonnell Douglas DC-8-71F (N8076U), Nashville, TN, incident, minor damage. Probable cause: The failure of company maintenance personnel to install the correct hydraulic landing gear extension component, and the failure of company maintenance inspection personnel to comply with proper post…
- [NTSB SEA97IA071](https://openairdocs.org/ntsb/SEA97IA071), Mar 12, 1997: McDonnell Douglas DC-8-71F (N830BX), Portland, OR, incident, no damage. Probable cause: improper installation of four attach bolts on the elevator drive torque tube.
- [NTSB NYC95IA106](https://openairdocs.org/ntsb/NYC95IA106), May 13, 1995: Douglas DC-8-71 (N707UP), Louisville, KY, incident, minor damage. Probable cause: preexisting crack(s) on the inside surface of the right main landing gear cylinder, and the subsequent fracture of the cylinder, which resulted in a collapse of the right main landing gear.
- [NTSB CHI95LA049](https://openairdocs.org/ntsb/CHI95LA049), Nov 30, 1994: Douglas DC-8-71F (N826BX), Chicago, IL, minor damage. Probable cause: the failure of the ground crew to maintain an appropriate center of gravity while downloading cargo from the airplane. A factor was the ground crew's failure to follow established downloading…
- [NTSB MIA92IA166](https://openairdocs.org/ntsb/MIA92IA166), Aug 22, 1992: Douglas DC-8-71F (N748UP), Miami, FL, incident, minor damage. Probable cause: FAILURE OF THE AIRCRAFT OPERATOR MAINTENANCE PERSONNEL TO ADEQUATELY LUBRICATE AND SEAL THE MAIN LANDING GEAR BOGIE BEAM SWIVEL JOINT AS REQUIRED BY MANUFACTURER AND OPERATOR MAINTENANCE PROGRAM…
- [NTSB CHI83IA162](https://openairdocs.org/ntsb/CHI83IA162), Apr 11, 1983: Douglas DC-8-71 (N8085U), Minneapolis, MN, incident, minor damage

## FAA accident and incident reports (43)

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 20080319012469I](https://openairdocs.org/incident/20080319012469I), Mar 19, 2008: Doug DC871F (N730UP), Louisville, KY, No damage. (-23) (1) The reason for evacuation: crew was notified of tail fire in the #3 engine. Crew discharged fire bottle in #3 engine. Through the investigation the…
- [Accident 20060207001809A](https://openairdocs.org/incident/20060207001809A), Feb 7, 2006: Doug DC871F (N748UP), Philadelphia, PA, Destroyed. (-23) On February 7, 2006, at 2359 eastern standard time, a Douglas DC-8-71, N748UP, operated by united parcel service company, as flight 1307, was…
- [Incident 20020925031489I](https://openairdocs.org/incident/20020925031489I), Sep 25, 2002: Doug DC871F (N825BX), El Paso, TX. (-23) Enroute from stl to elp, the light panel for the flap quadrant, located on the left hand side of the center console, shorted out, producing smoke and…
- [Incident 20020214004369I](https://openairdocs.org/incident/20020214004369I), Feb 14, 2002: Doug DC871F (N830BX), Orlando, FL, Minor damage. (-23) On 02/14/2002, ixxa mechanics removed and replaced the #2 engine bleed air regulator valve in order to correct a deferral on that system. The new valve…
- [Accident 20011214033549A](https://openairdocs.org/incident/20011214033549A), Dec 14, 2001: Doug DC871F (N825BX), Anchorage, AK, No damage. (-23) After takeoff (anc) aircraft began to roll hard left. Crew input opposite aileron & rudder to maintain control. Emergency declared. Aircraft returned to…
- [Incident 20010426006779I](https://openairdocs.org/incident/20010426006779I), Apr 26, 2001: Doug DC871F (N8076U), Nashville, TN, Minor damage. (.19)On April 26, 2001, at about 0629 central daylight time, a boeing/mcdonnell Douglas DC-8-71F, N8076U, registered to emery worldwide airlines, inc.,…
- [Incident 20001019031449I](https://openairdocs.org/incident/20001019031449I), Oct 19, 2000: Doug DC871F (N825BX), Omaha, NE. (-23)During approach in Omaha, NE, the crew noticed the #2 engine hydraulic quanitty drop to stand pipe level crew performed loss of hydraulic quantity…
- [Incident 20000525016589I](https://openairdocs.org/incident/20000525016589I), May 25, 2000: Doug DC871F (N708UP), Des Moines, IA, Minor damage. (-23)On taxi in after normal landing the tower reported right engine on fire. Confirmed smoke form right side. Check list run and engines 3 and 4 shtudown…
- [Incident 19991123033759I](https://openairdocs.org/incident/19991123033759I), Nov 23, 1999: Doug DC871F (N703UP), Des Moines, IA, Minor damage. (-23) Aircraft landed on runway 31R. Wind reported to crew as 3616 with no gusts. ATIS wx reported as 33013KT 7SM OVC008 A2983. Crew reported a 10 kt decrease…
- [Incident 19990817039319I](https://openairdocs.org/incident/19990817039319I), Aug 17, 1999: Doug DC871F (N797UP), Chicago, IL, Substantial damage. A/c landed 32R, brakes locked up on rt gear & ground off tires & wheels causing gear fire. Fire department put out fire. Unsafe nose gear lite was caused to…
- [Incident 19990622014279I](https://openairdocs.org/incident/19990622014279I), Jun 22, 1999: Doug DC871F (N779UP), Ontario, CA. #1 Engine was lost when relay R2-7035 became inoperative. This relay controls the starter control valve. Starter controllight illuminated. Relay was changed,…
- [Incident 19990428017369I](https://openairdocs.org/incident/19990428017369I), Apr 28, 1999: Doug DC871F (N700UP), Ontario, CA. Crew reported fumes in the cockpit, while taxing to spot. Crew decided to evacuate via excape slide, five people on board, all escaped with no injuries. It was…
- [Incident 19980312009289I](https://openairdocs.org/incident/19980312009289I), Mar 12, 1998: Doug DC871F (N828BX), Toledo, OH, Minor damage. Narrative: a meeting with the captain sweeney, fo kevin molden, and fe bill choate, the crew on 826BX, was held in Toledo, Ohio on March 13. Also present was…
- [Incident 19980212006349I](https://openairdocs.org/incident/19980212006349I), Feb 12, 1998: Doug DC871F (N824BX), Toledo, OH, Minor damage. Narrative: number one engine pod struck runway first officer was executing a low visibility landing. Number one engine cowling and transfer gear box damaged as…
- [Incident 19970708024629I](https://openairdocs.org/incident/19970708024629I), Jul 8, 1997: Doug DC871F (N825BX), Ontario, CA. Ammonia fumes from cargo area on climbout. Returned. Ammonia container inside container spilled. Cleaned up.
- [Incident 19970311017339I](https://openairdocs.org/incident/19970311017339I), Mar 11, 1997: Doug DC871F (N830BX), Portland, OR. Narrative: on March 11, 1997 at approximately 2000, the pilot of a DC-8-71F, N830BX, aborted a take-off at Portland International Airport. According to the…
- [Incident 19950513011479I](https://openairdocs.org/incident/19950513011479I), May 13, 1995: Doug DC871F (N707UP), Louisville, KY, Minor damage. Right main landing gear folded on landing. Skidded to stop dragging right engine on runway.
- [Incident 19950217008429I](https://openairdocs.org/incident/19950217008429I), Feb 17, 1995: Doug DC871F (N705UP), Atlanta, GA. Narrative: aircraft exited the end of the runway, due to excessive rollout speed.
- [Incident 19950123002859I](https://openairdocs.org/incident/19950123002859I), Jan 23, 1995: Doug DC871F (N706UP), Philadelphia, PA. Narrative: flight crew reported enroute and inbound of a possible chemical spill. Their exposure time to unrecognizable fumes was approximately 30 minutes…
- [Accident 19941130044059A](https://openairdocs.org/incident/19941130044059A), Nov 30, 1994: Doug DC871F (N826BX), Chicago, IL, Minor damage. Unloaded forward cargo first contrary to instructions. Failed lock rack. Rolled aft. Tail hit ramp. Damage door.
- [Incident 19940615022059I](https://openairdocs.org/incident/19940615022059I), Jun 15, 1994: Doug DC871 (N820BX), Rochester, NY. Compressor stall left engine on takeoff.NR2 spool seized.FOD shavings in NR5 compressor boroscope plug.
- [Incident 19930719030289I](https://openairdocs.org/incident/19930719030289I), Jul 19, 1993: Doug DC871F (N797UP), Dallas-Ft Worth, TX. Pilot misjudged the turn from high speed taxiway. Right main gear rolled off concrete onto unstressed asphault.
- [Incident 19930318008429I](https://openairdocs.org/incident/19930318008429I), Mar 18, 1993: Doug DC871F (N703UP), Miami, FL, Minor damage. Pilot struck a lamp post while taxiing to ramp. Marshaller and wing walker directing aircraft.
- [Incident 19920721032279I](https://openairdocs.org/incident/19920721032279I), Jul 21, 1992: Doug DC871F (N730UP), Raleigh-Durham, NC. Fire warning on NR1 engine on approach. Shut it down. Fired bottle. Landed safely. No fire.
- [Incident 19911227061899I](https://openairdocs.org/incident/19911227061899I), Dec 27, 1991: Doug DC871F (N706UP), Syracuse, NY. NR1 engine flamed out in flight. Completed flight. Unable to restart engine on ground.
- [Incident 19910221006329I](https://openairdocs.org/incident/19910221006329I), Feb 21, 1991: Doug DC871F (N701UP), Minneapolis, MN, Minor damage. Pilot made a hard landing and the NR3 and NR4 engines contacted the runway. NR3 and NR4 engines replaced.
- [Incident 19900927048999I](https://openairdocs.org/incident/19900927048999I), Sep 27, 1990: Doug DC871F (N705UP), Wichita, KS. Forward cargo door warning at cruise. Some pressure lost. Landed safely.
- [Incident 19891019054439I](https://openairdocs.org/incident/19891019054439I), Oct 19, 1989: Doug DC871F (N701UP), San Francisco, CA. Lost hydraulic pressure on climb. Able to lower gear. Diverted and landed. Door sequencing valve had failed.
- [Incident 19890609027499I](https://openairdocs.org/incident/19890609027499I), Jun 9, 1989: Doug DC871F (N798UP), Louisville, KY. Engine shut down due to fire warning. Fire warning on rollout. Fire bottles used. Faulty wire in detection system.
- [Incident 19881208053159I](https://openairdocs.org/incident/19881208053159I), Dec 8, 1988: Doug DC871F (N700UP), Ontario, CA, Minor damage. During hard landing all 4 engines contacted runway at some time. 2 had damage to accessory gear box areas.
- [Incident 19870306015429I](https://openairdocs.org/incident/19870306015429I), Mar 6, 1987: Doug DC871F (N752UP), Louisville, KY. Deflection of rudder on liftoff. Returned with yaw damper off. Replaced rudder power control unit, shut off valve.
- [Incident 19870126003539I](https://openairdocs.org/incident/19870126003539I), Jan 26, 1987: Doug DC871F (N748UP), Memphis, TN. On gear extension right main indicated unsafe. Safe landing. Malfunction not reported.
- [Incident 19860522034139I](https://openairdocs.org/incident/19860522034139I), May 22, 1986: Doug DC871F (N798UP), Ontario, CA, Minor damage. Split flap condition existed on approach. Safe landing. Found left inboard flap actuator link broken.
- [Incident 19860205014239I](https://openairdocs.org/incident/19860205014239I), Feb 5, 1986: Doug DC871F (N702UP), Houston, TX. Crew misunderstood clearance altitude and ATC did not correct incorrect readback. Loss of standard separation.
- [Incident 19860125004099I](https://openairdocs.org/incident/19860125004099I), Jan 25, 1986: Doug DC871 (N8085U), Omaha, NE. Returned with no indication of gear up after takeoff. Ferried gear down to investigate problem.
- [Incident 19860103006139I](https://openairdocs.org/incident/19860103006139I), Jan 3, 1986: Doug DC861F (N750UP), Huntingburg, IN. Climbed above assigned altitude due to malfunction as autopilot was engaged. Less than standard separation.
- [Incident 19840606032069I](https://openairdocs.org/incident/19840606032069I), Jun 6, 1984: Doug DC861 (N8085U), Las Vegas, NV, Minor damage. Lost oil quantity and pressure at cruise altitude. Engine shut down. Loss of oil undetermined.
- [Incident 19830410028879I](https://openairdocs.org/incident/19830410028879I), Apr 10, 1983: Doug DC861 (N8085U), Minneapolis, MN, Minor damage. Tire exploded at cruise altitude. Tire caught on fire during landing. Previous aborted takeoff a possible factor.
- [Incident 19830304011969I](https://openairdocs.org/incident/19830304011969I), Mar 4, 1983: Doug DC861 (N8076U), Reno, NV, Minor damage. #1 Engine failed. Visible damage to engine cowling. Declared emergency. Diverted to Reno. C1 disc failure.
- [Incident 19820528023979I](https://openairdocs.org/incident/19820528023979I), May 28, 1982: Doug DC861 (N8076U), Cheyenne, WY. Flight attendant temporarily incapacitated when thrown to floor in moderate turbulance.
- [Incident 19811112080389I](https://openairdocs.org/incident/19811112080389I), Nov 12, 1981: Doug DC861 (N8085U), Philadelphia, PA, Minor damage. Returned to airport when number 4 engine fire warning came on. Found bleed air valve open and starter destroyed.
- [Incident 19800907082129I](https://openairdocs.org/incident/19800907082129I), Sep 7, 1980: Doug DC861 (N8076U), Chicago, IL. Flight returned due to a hydraulic problem. A brake line fitting had broken.
- [Incident 19800625048899I](https://openairdocs.org/incident/19800625048899I), Jun 25, 1980: Doug DC861 (N8085U), Greensboro, NC, Minor damage. Pilot made hard landing and bounced once. Weather at minimums.

## Service difficulty reports (8,938, newest 50)

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

- [SDR IXXA1100520](https://openairdocs.org/sdr/IXXA1100520), Aug 9, 2011: WIRE HARNESS. DAMAGED. DURING CLIMBOUT, NR 3 MAIN TANK BOOST PUMP C/B`S POPPED. THE CREW PERFORMED COM PROCEDURES, BUT NO HELP. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT
- [SDR IXXA110052O](https://openairdocs.org/sdr/IXXA110052O), Aug 9, 2011: WIRE HARNESS. DAMAGED. DURING CLIMB OUT, NR 3 MAIN TANK BOOST PUMP C/B'S POPPED. THE CREW PERFORMED COM PROCEDURES, BUT NO HELP. THE CREW RETURNED TO DEPARTUE WITHOUT FURTHER INCIDENT
- [SDR IXXA11SMN094S](https://openairdocs.org/sdr/IXXA11SMN094S), Jun 14, 2011: SKIN. DENTED. DURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR LOWER SKIN PANEL DENTED AT SEVERAL POINTS AT STA XE 246.000 - XH 285.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKI
- [SDR IXXA11SMN093S](https://openairdocs.org/sdr/IXXA11SMN093S), Jun 10, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK INSP FOUND RT MLG INBD DOOR INNER SKIN CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEAN
- [SDR IXXA11SMN092S](https://openairdocs.org/sdr/IXXA11SMN092S), Jun 8, 2011: SKIN. CRACKED. DURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR UPPER SKIN DENTED AND CRACKED AT STATION XE 246.000 - 285.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGE
- [SDR IXXA11SMN091S](https://openairdocs.org/sdr/IXXA11SMN091S), Jun 8, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK INSP, FOUND RT HORIZ STABILIZER T/E UPPER SKIN CORRODED AT STA XE 29.000 - 77.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE
- [SDR IXXA11SMN090S](https://openairdocs.org/sdr/IXXA11SMN090S), Jun 8, 2011: WEB. WORN. DURING ROUTINE C-CHECK INSP FOUND NR 3 ENGINE THRUST REVERSER RT COWL FIXED STRUCTURE WEB FLANGE WORN AT STA YN 203.000. REMOVED FASTENERS AS NEEDED TO PERFORM 
- [SDR IXXA11SMN089S](https://openairdocs.org/sdr/IXXA11SMN089S), Jun 8, 2011: WEB. WORN. DURING ROUTINE C-CHECK INSP, FOUND NR 3 ENGINE THRUST REVERSER LT COWL FIXED STRUCTURE WEB FLANGE WORN AT STA YN 203.000. REMOVED FASTENERS AS NEEDED TO PERFORM
- [SDR IXXA11SMN088S](https://openairdocs.org/sdr/IXXA11SMN088S), Jun 8, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK INSP FOUND RT WING UPPER SKIN CORRODED AT STA XW 55.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKI
- [SDR IXXA11SMN086S](https://openairdocs.org/sdr/IXXA11SMN086S), Jun 8, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK INSP FOUND LT WING T/E PANEL CORRODED AT STATION XW 55.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. CLEANED, TREAT
- [SDR IXXA11SMN085S](https://openairdocs.org/sdr/IXXA11SMN085S), Jun 8, 2011: FITTING. CRACKED. DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FWD BATHTUB FITTING CRACKED AT STA 680.000, LONGERON 9 RT. REMOVED CRACKED BATHTUB FITTING. CLEANED, TR
- [SDR IXXA11SMN084S](https://openairdocs.org/sdr/IXXA11SMN084S), Jun 8, 2011: FITTING. CRACKED. DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 798.000, LONGERON 19 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED 
- [SDR IXXA11SMN087S](https://openairdocs.org/sdr/IXXA11SMN087S), Jun 7, 2011: SKIN. DENTED. DURING ROUTINE C-CHECK INSP FOUND RT OTBD FLAP UPPER EXTERNAL SKIN DENTED AT SEVERAL POINTS AT STA XF 415.000 - 440.000. REMOVED DAMAGED SKIN. FABRICATED NEW SK
- [SDR IXXA11SMN083S](https://openairdocs.org/sdr/IXXA11SMN083S), Jun 7, 2011: SUPPORT FITTING. CRACKED. DURING ROUTINE C-CHECK INSP, FOUND RT WING FLAP LINK SUPPORT LT SIDE CRACKED AT STA XF 409.000. REMOVED HINGE CRACKED SUPPORT FITTING. CLEANED, TREATED AND PRIM
- [SDR IXXA11SMN082S](https://openairdocs.org/sdr/IXXA11SMN082S), Jun 6, 2011: FITTING. CRACKED. DURING ROUTINE C-CHECK INSP FOUND RT MLG WHEEL WELL FITTING CRACKED AT STATION 879.375. REMOVED CRACKED FRAME FITTING. FABRICATED NEW FITTING, SPLICERS, SHIMS A
- [SDR IXXA11SMN081S](https://openairdocs.org/sdr/IXXA11SMN081S), Jun 6, 2011: SKIN. MISREPAIRED. DURING ROUTINE C-CHECK INSP FOUND, IMPROPER REPAIR AT FWD BASKET DOOR OPENING FWD CTR LIP AT STATION FS 290, LONGERON 34.5 RT. REMOVED FASTENERS AS NEEDED TO PE
- [SDR IXXA11SMN080S](https://openairdocs.org/sdr/IXXA11SMN080S), Jun 6, 2011: STRAP. CORRODED. DURING ROUTINE C-CHECK INSPECTION, FOUND NLG WHEEL WELL LT TUNNEL COMPARTMENT STRAP CORRODED AT STA 8.000. REMOVED CORROSION. REMOVED DAMAGED STRAP SEGEMENT. FA
- [SDR IXXA11SMN079S](https://openairdocs.org/sdr/IXXA11SMN079S), Jun 6, 2011: SUPPORT FITTING. CRACKED. DURING ROUTINE C-CHECK INSP FOUND NR 1 ALT TANK NR 6 FUEL PROBE FITTING SUPPORT CRACKED. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED N
- [SDR IXXA11SMN078S](https://openairdocs.org/sdr/IXXA11SMN078S), Jun 6, 2011: ANGLE. CRACKED. DURING ROUTINE C-CHECK INSP FOUND NR 4 PYLON INTERNAL ANGLE CRACKED AT STATION YN 321.397 AND STA XRS 495.665. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. RE
- [SDR IXXA11SMN077](https://openairdocs.org/sdr/IXXA11SMN077), Jun 6, 2011: FITTING. CRACKED. DURING ROUTINE C-CHECK INSP, FOUND RT MLG WHEEL WELL DOG HOUSE FITTING CRACKED AT STA 855.000, RT BOTTOM LINE 46. REMOVED CRACKED FITTING. CLEANED, TREATED, AND
- [SDR IXXA11SMN076S](https://openairdocs.org/sdr/IXXA11SMN076S), Jun 6, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK INSPECTION, FOUND LT MLG INBD DOOR INNER SKIN CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN
- [SDR IXXA110044O](https://openairdocs.org/sdr/IXXA110044O), Jun 4, 2011: STRIKER. BENT. DURING CRUISE, THE MLG DOOR LIGHT REMAINED ON. THE CREW CYCLED THE MAIN LANDING GEAR AND LIGHT REMAINED ON. WHEN AIRSPEED INCREASED TO 210 IAS LIGHT WENT OUT. T
- [SDR IXXA11SMN075S](https://openairdocs.org/sdr/IXXA11SMN075S), Jun 3, 2011: STRUCTURE. MISREPAIRED. DURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT SMALL DRAIN DOUBLER FWD LOWER CENTER FUSELAGE FORWARD OF CENTER EQUIP DOOR AT STA FS 615 LONGERON 36. REMO
- [SDR IXXA11SMN072S](https://openairdocs.org/sdr/IXXA11SMN072S), Jun 2, 2011: SKIN. MISREPAIRED. DURING ROUTINE C-CHECK INSP FOUND IMPROPER DOUBLER REPAIR AT LT FWD FUSELAGE EMERGENCY EXIT DOOR AT STA FS 404 LONGERON 15.5 LT. REMOVED EXISTING REPAIR. FABRIC
- [SDR IXXA11SMN071S](https://openairdocs.org/sdr/IXXA11SMN071S), Jun 2, 2011: SKIN. MISREPAIRED. DURING ROUTINE C-CHECK INSPECTUIN FOUND IMPROPER DOUBLER REPAIR AT RT FWD FUSELAGE EMERGENCY EXIT DOOR AT STATION FS 392, LONGERON 16.5 RT. REMOVED FASTENERS AS
- [SDR IXXA11SMN070S](https://openairdocs.org/sdr/IXXA11SMN070S), Jun 2, 2011: SKIN. MISREPAIRED. DURING ROUTINE C-CHECK INSP, FOUND IMPROPER DOUBLER REPAIR, RT FWD FUSELAGE, 2 WINDOWS FWD OF EMERGENCY EXIT DOOR AT STATION FS 300 LONGERON 16 RT. REMOVED EXIS
- [SDR IXXA110035O](https://openairdocs.org/sdr/IXXA110035O), Apr 28, 2011: CONTROL CABLE. OUT OF RIG. DURING LEVEL OFF, NR 3 ENGINE COMPRESSOR STALLED WHEN THROTTLES WERE RETARDED,(N1-93 PERCENT, N2-91 PERCENT, F/F-3100, OAT-44 DEGREES AND M-.80/300KIAS). THE CR
- [SDR IXXAIXXA110031O](https://openairdocs.org/sdr/IXXAIXXA110031O), Mar 30, 2011: ENGINE. POWER LOSS. DURING CRUISE AT FL 380 IN CALM AIR, NR 2 ENG N1 RPM AND NR 2 RPM ROLLED BACKED TO 50 PERCENT N1 AND 85 PERCENT N2. EGT WAS 530°C FUEL FLOW DECREASED TO APPROX 
- [SDR IXXA11SMN028S](https://openairdocs.org/sdr/IXXA11SMN028S), Mar 4, 2011: SKIN. DENTED. DURING ROUTINE C-CHECK INSP, FOUND RT WING OTBD FLAP LOWER SKIN SCRATCH AND DENTS XF AT STA 174.000 TO XF 219.000. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND 
- [SDR IXXA110023O](https://openairdocs.org/sdr/IXXA110023O), Feb 18, 2011: WIRE HARNESS. DEFECTIVE. DURING CLIMBOUT FROM KTOL NR ONE EGT ANALOG AND DIGITAL READ OUTS DROPPED FROM 700 DEGREE TO 420 DEGREE WITH FLUCTUATION PLUS/ MINUS 5 DEGREE, N1 AND N2 SIMILAR
- [SDR IXXA110022S](https://openairdocs.org/sdr/IXXA110022S), Feb 14, 2011: SKIN. DENTED. DURING PREFLIGHT FOUND LT SIDE BELLY SKIN TO BE (DENTED AND CRACKED) AT STA 55 BETWEEN 15" TO 19.2500" FROM CTR LINE. OPEN
- [SDR IXXA11SMN048S](https://openairdocs.org/sdr/IXXA11SMN048S), Feb 11, 2011: SPAR CAP. CRACKED. DURING ROUTINE C-CHECK INSP FOUND RT WING FRONT SPAR L/E LOWER CAP CRACKED AT STA XFS 500.233. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSP
- [SDR U2RA449SPIM003](https://openairdocs.org/sdr/U2RA449SPIM003), Feb 11, 2011: SKIN. CORRODED. RT HORIZ STAB BETWEEN XE 75.672 AND XE 147.906 T/E UPPER PANEL SKIN WITH CORROSION AROUND FASTENERS.
- [SDR IXXA110019O](https://openairdocs.org/sdr/IXXA110019O), Feb 10, 2011: CONNECTOR. DIRTY. DURING TAKEOFF, NR 1 ENG OIL PRESSURE LIGHT CAME ON INTERMITTENTLY, OIL TEMP AND PRESSURE GOOD ON FLIGHT ENGINEER PANEL. THE CREW ABORTED TAKEOFF AND RETURNED T
- [SDR IXXA11SMN047S](https://openairdocs.org/sdr/IXXA11SMN047S), Feb 8, 2011: FITTING. CRACKED. DURING ROUTINE C-CHECK INSP, FOUND RT MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 680.000 LONGERON 6, RT. REMOVED CRACKED FITTING. CLEANED AND APPLIED PRIMER 
- [SDR IXXA11SMN044S](https://openairdocs.org/sdr/IXXA11SMN044S), Feb 7, 2011: FLOORBEAM. CRACKED. DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FLOORBEAM WEB CRACKED AT STA 960.000 LT BOTTOM LINE 56. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. 
- [SDR IXXA11SMN043S](https://openairdocs.org/sdr/IXXA11SMN043S), Feb 7, 2011: FITTING. CORRODED. DURING ROUTINE C CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CORRODED AT STA 879.000, LONGERON-19 RT TO LONGERON-22 RT. REMOVED CORROSION. FOUND OUT OF LIMI
- [SDR IXXA11SMN041S](https://openairdocs.org/sdr/IXXA11SMN041S), Feb 7, 2011: RIB. CRACKED. DURING ROUTINE C-CHECK INSP, FOUND RT WING INBD FLAP RIB CRACKED AT STA XF 129.000. REMOVED DAMAGED RIB. FABRICATED NEW RIB. PERFORMED HEAT TREATMENT. CLEANED, 
- [SDR IXXA11SMN038S](https://openairdocs.org/sdr/IXXA11SMN038S), Feb 7, 2011: SKIN. CRACKED. DURING ROUTINE C-CHECK INSPECTION, FOUND SKIN CRACKED AT STA 55.000, 70.000 LONGERON 33 RT AND LONGERON 34 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED D
- [SDR IXXA11SMN046S](https://openairdocs.org/sdr/IXXA11SMN046S), Feb 7, 2011: FITTING. CRACKED. DURING ROUTINE C-CHECK INSP, FOUND EMPENNAGE NR 60 ACCESS RT FITTING CRACKED AT STA 1766.000, LONGERON 19. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED 
- [SDR IXXA11SMN045S](https://openairdocs.org/sdr/IXXA11SMN045S), Feb 7, 2011: FITTING. CRACKED. DURING ROUTINE C-CHECK INSP FOUND EMPENNAGE NR 60 ACCESS LT FITTING CRACKED AT STA 1766.000 LONGERON 19. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AR
- [SDR IXXA11SMN042S](https://openairdocs.org/sdr/IXXA11SMN042S), Feb 7, 2011: FITTING. CRACKED. DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 702.000 LONGERON 19 RT. REMOVED CRACKED FITTING.INSTALLED NEW FITTING IAW SR
- [SDR IXXA11SMN040S](https://openairdocs.org/sdr/IXXA11SMN040S), Feb 7, 2011: ANGLE. CORRODED. DURING ROUTINE C-CHECK INSP, FOUND FWD LOWER CARGO FWD DOOR AND JAMB INTERIOR CORRODED AT STA 335.000, LONGERON 36 TO LONGERON 35 RT. REMOVED DAMAGED ANGLE. FAB
- [SDR IXXA11SMN037S](https://openairdocs.org/sdr/IXXA11SMN037S), Feb 7, 2011: FITTING. CRACKED. DURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STA 1160.000. R & R AFT CARGO COMPARTMENT FITTING IAW SRM 51-1-20D.
- [SDR U2RA449SPIM004](https://openairdocs.org/sdr/U2RA449SPIM004), Feb 7, 2011: DRIVE ASSY. CRACKED. RUDDER TAB DRIVE SECTOR BROKEN.
- [SDR IXXA11SMN039S](https://openairdocs.org/sdr/IXXA11SMN039S), Feb 6, 2011: SKIN. DENTED. DURING ROUTINE C-CHECK INSP, FOUND LT INBD FLAP UPPÈR SKIN SHOWS DENTS AT DIFFERENT LOCATIONS AT STATION XW 3.000 - XW 92.000. REMOVED DAMAGED SKIN. FABRICATED 
- [SDR IXXA11SMN030S](https://openairdocs.org/sdr/IXXA11SMN030S), Feb 5, 2011: DOOR FRAME. CRACKED. DURING ROUTINE C-CHECK INSP FOUND LOWER FWD CARGO COMPARTMENT FRAME CRACKED AT STA 200.000 BETWEEN LONGERON-32 RT AND LONGERON -33 RT. REMOVED FASTENERS AS NEED
- [SDR IXXA11SMN036S](https://openairdocs.org/sdr/IXXA11SMN036S), Feb 5, 2011: CARGO TRACK. BROKEN. DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 2 TRACK LUGS BROKEN AT STA 1580.000 - STA 1600.000. REMOVED DAMAGED TRACK SEGMENT. CLEANED, TREATED,
- [SDR IXXA11SMN035S](https://openairdocs.org/sdr/IXXA11SMN035S), Feb 5, 2011: CARGO TRACK. BROKEN. DURING ROUTINE C-CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT NR 4 TRACK LUGS BROKEN AT STA 320.000 - STA 340.000. REMOVED DAMAGED TRACK SEGMENT. CLEANED, TREA
- [SDR IXXA11SMN034S](https://openairdocs.org/sdr/IXXA11SMN034S), Feb 5, 2011: FITTING. CRACKED. DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 1690.000, LONGERON 21 LT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED A

All 8,938: https://openairdocs.org/model/douglas-dc-8-71f/reports.md

## STCs that may be installed (OpenAirDocs) (129, 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 SA3169NM](https://openairdocs.org/stc/SA3169NM): Installation of floor proximity emergency escape marking system. Bruce Aerospace Inc
- [STC ST01078AT](https://openairdocs.org/stc/ST01078AT): Installation of an expanded, 17-parameters, Allied Signal, or Loral-Fairchild, Digital Flight Data Recorder (DFDR). Acron Aviation Inc
- [STC ST01174CH](https://openairdocs.org/stc/ST01174CH): Installation of UPS Aviation Technologies ADS-B provisions and Honeywell Mode-S System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC SA2534SW-D](https://openairdocs.org/stc/SA2534SW-D): Replacement of Switch assembly Int'l Inflatables Co. P/N 68748, with DME Corp. P/N L-140 in emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC SA2539SW-D](https://openairdocs.org/stc/SA2539SW-D): Replacement of light assembly, International Inflatables Co. P/N68555-1 with DME Corp. EL-104, EL-104A, and EL-104B in emergency slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC SA863EA](https://openairdocs.org/stc/SA863EA): Incorporation of DME Corporation emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC ST02580AT](https://openairdocs.org/stc/ST02580AT): Lithium cell battery pack to replace currently approved alkaline battery pack used in escape slide emergency light system. Astronics Luminescent Systems Inc
- [STC SA5720NM](https://openairdocs.org/stc/SA5720NM): Installation of the Mark VII ground proximity and windshear warning system. Honeywell International Inc
- [STC ST00375AT](https://openairdocs.org/stc/ST00375AT): Installation of a CAS-81 TCAS II and a TRA-67 Mode S transponder. Honeywell International Inc
- [STC SA9079SC-D](https://openairdocs.org/stc/SA9079SC-D): Recore of AiResearch Precooler, P/N 194430-1, -2 in accordance with Honeywell LORI Sealed Drawing List SDL3779-1, Revision A, dated 11 October 2005 or later FAA approved revision. Honeywell International Inc
- [STC SE00584AT](https://openairdocs.org/stc/SE00584AT): Installation of ELDEC fuel flow meter and Kollsman digital fuel flow/fuel used indicator. GDC Technics LLC
- [STC SA3421NM](https://openairdocs.org/stc/SA3421NM): Installation of Hughes-Avicom video entertainment system. Burrana Inc. Lists DC-8 Series
- [STC SA3905NM](https://openairdocs.org/stc/SA3905NM): Installation of ANCRA cargo handling system P/N 80900-10 or -11, respectively. Ancra International LLC
- [STC SA5059NM](https://openairdocs.org/stc/SA5059NM): Installation of Ancra cargo conveyor system, P/N's 81381-11, 81382-11. Ancra International 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 ST01668LA](https://openairdocs.org/stc/ST01668LA): Installation of a single LTN-2012 Global Positioning Sensor Unit (GPSU) and dual LTN-92 Inertial Reference System (INS). 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 SA3420NM](https://openairdocs.org/stc/SA3420NM): Installation of Brownline Aft Stop, P/N 46443-102. Telair US LLC
- [STC SA1511GL](https://openairdocs.org/stc/SA1511GL): Installation of Type "C" containers. ABX Air Incorporated
- [STC ST09378SC](https://openairdocs.org/stc/ST09378SC): Installation of a dual Honeywell/ Trimble HT9000 global navigation system. LB Aircraft Engineering Inc
- [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 SA7729SW](https://openairdocs.org/stc/SA7729SW): Installation of digital fuel quantity indicators, fuel totalizer, and capacitive fuel compensator units. Ontic Engineering and Manufacturing Inc
- [STC SA3168NM](https://openairdocs.org/stc/SA3168NM): Installation of ANCRA Corp. End Restraints in the cargo pallet positions number one or eighteen. Ancra International LLC
- [STC SA3957NM](https://openairdocs.org/stc/SA3957NM): Installation of cargo system P/N 80080-10, -11, or -12. Ancra International LLC
- [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 SA2825CE](https://openairdocs.org/stc/SA2825CE): Installation of B&D Instruments & Avionics, Inc. Electronic N2 Gas Compressor Indicator. Data required: (1) B&D Instruments & Avionics, Inc. Installation Manual Part No. 55006-003-011, Revision A, dated April 6, 1992, or later "FAA Approved" revision; and (2) copy of this certificate. Teledyne Controls
- [STC SA2826CE](https://openairdocs.org/stc/SA2826CE): Installation of optional set of B&D Instruments & Avionics, Inc. Electronic Exhaust Gas Temperature (EFT) Indicators. Teledyne Controls
- [STC ST01202WI-D](https://openairdocs.org/stc/ST01202WI-D): Modification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision. Rockwell Collins Inc
- [STC ST00746LA-D](https://openairdocs.org/stc/ST00746LA-D): Installation of smoke detection system, lower cargo compartment. Ontic Engineering and Manufacturing Inc
- [STC SA2082SO](https://openairdocs.org/stc/SA2082SO): Installation of fuselage window plugs. Kosola & Associates Inc
- [STC ST01494CH](https://openairdocs.org/stc/ST01494CH): Installation of a Universal Avionics Terrain Awareness Warning System (TAWS) and a Universal Avionics GPS-1000 global positioning system. Airborne Maintenance & Engineering Services (AMES)
- [STC ST01930CH](https://openairdocs.org/stc/ST01930CH): Installation of Innovative Solutions & Support dual air data display unit. Airborne Maintenance & Engineering Services (AMES)
- [STC ST02123CH](https://openairdocs.org/stc/ST02123CH): Installation of Universal Aviionics Systems. Airborne Maintenance & Engineering Services (AMES)
- [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing
- [STC ST01256WI-D](https://openairdocs.org/stc/ST01256WI-D): Modification of a Collins TPR-720, TPR-900 or TPR-901 Mode S Transponder System installation with an ATC/TCAS Control Panel to an Elementary Surveillance Compliant Collins TPR-901 Mode S Transponder System installation with a Flight ID/ATC/TCAS Control Panel in accordance with Collins Drawing Index as listed on AML No. ST01256WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [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 ST02069AT](https://openairdocs.org/stc/ST02069AT): Installation of a Dual Trimble TNL-8100 GPS Navigation System. Avionics Group Inc
- [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 SA1343NM](https://openairdocs.org/stc/SA1343NM): Installation of an environmental control system. Airweld Inc
- [STC SA1387NM](https://openairdocs.org/stc/SA1387NM): Installation of a single or dual AiResearch GTCP85-98CK and/or GTCP-85-98CK(D) Auxiliary Power Units in the forward baggage compartment. Airweld Inc

All 129: https://openairdocs.org/model/douglas-dc-8-71f/stcs.md

## The same model under other registry codes

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

- [Mcdonnell Douglas DC-8-71F](https://openairdocs.org/model/mcdonnell-douglas-dc-8-71f): 0 registered aircraft, registry code 302199G

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