# Douglas DC-8-72F

- Type: Aircraft model (FAA registry)
- Registry code: 302199E
- Manufacturer (registry): DOUGLAS
- Model: DC-8-72F
- 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-8-72f

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 2007-13-02](https://openairdocs.org/ad/2007-13-02): Sump heater, scavenge valve, and scavenge pump · Boeing DC-8-62, DC-8-62F, DC-8-63 and 4 more. Effective Jul 25, 2007
- [AD 2007-12-02](https://openairdocs.org/ad/2007-12-02): Left and right wing front spar · Boeing DC-8-33, DC-8-42, DC-8-43 and 16 more. Effective Jul 10, 2007
- [AD 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

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 138: https://openairdocs.org/model/douglas-dc-8-72f/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

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (257, newest 50)

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

- [SDR 2021FA0000325](https://openairdocs.org/sdr/2021FA0000325), Nov 18, 2021: RIB. CRACKED. L/ H HORZ. STAB I/B L/E SECTION LOWER RIB IS CRACKED AT STA. SFX.= 47.500, REF NRC B000153
- [SDR E4EB20151215005](https://openairdocs.org/sdr/E4EB20151215005), Dec 15, 2015: SKIN. CORRODED. REFERENCE NRC A016331, RT WING OTBD LE, OTBD SECTION HAS INTERGRANULAR CORROSION AROUND FASTENERS ON UPPER SKIN, BETWEEN XFS710.000 - 747.500. ITEM REPAIRED ON 
- [SDR E4EB20151215004](https://openairdocs.org/sdr/E4EB20151215004), Dec 15, 2015: SKIN. CORRODED. RT WING SKIN CTR LE HOIST POINT AT XFS 385.250 HAS INTERGRANULAR CORROSION. REPAIRED ON EA 008-5730-38-A5966.
- [SDR E4EB1215003](https://openairdocs.org/sdr/E4EB1215003), Dec 15, 2015: SKIN. DAMAGED. AFTER REMOVAL OF LT OTBD LE STUB WING, FOUND SKIN UPPER ATTACH SCREW HOLE COUNTERSINK DAMAGED. REPAIRED IAW EA 008-5730-38-A5967.
- [SDR E4EB20151215002](https://openairdocs.org/sdr/E4EB20151215002), Dec 15, 2015: SKIN. CORRODED. REFERENCE NRC A016593, LT WING CTR LE UPPER SKIN HAS INTERGRANULAR CORROSION AROUND FASTENERS AT XFS 347.750. ITEM REPAIRED IAW EA 008-5730-38-A6009.
- [SDR E4EB20151215001](https://openairdocs.org/sdr/E4EB20151215001), Dec 15, 2015: SKIN. CORRODED. REFERENCE NRC A016060, LT WING UPPER SURFACE HAS INTERGRANULAR CORROSION AROUND A FASTENER AT XW 761 & STRINGER 2. ITEM REPAIRED IAW EA 008-5710-38-A5879.
- [SDR E4EB20151214011](https://openairdocs.org/sdr/E4EB20151214011), Dec 14, 2015: SKIN. CORRODED. REFERENCE NRC A016333, RT WING OTBD LE, OTBD SECTION HAS INTERGRANULAR CORROSION AROUND FASTENERS ON UPPER SKIN BETWEEN XFS 778.750 - XW 761.695. ITEM REPAIRED 
- [SDR E4EB20151214010](https://openairdocs.org/sdr/E4EB20151214010), Dec 14, 2015: SKIN. CORRODED. LEFT HORIZ STAB INBD LE UPPER SURFACE HAS CORROSION AT OTBD HOIST ATTACH POINT. ITEM REPAIRED IAW EA 008-5530-38-A5938.
- [SDR E4EB20151214009](https://openairdocs.org/sdr/E4EB20151214009), Dec 14, 2015: SKIN. CORRODED. REFERENCE NRC A016797, RT WING CTR LE UPPER SKIN, TE HAS INTERGRANULAR CORROSION AROUND FASTENERS AT XOLD16.225 & XFS 429. REPAIR ACCOMPLISHED IAW EA 008-5730-3
- [SDR E4EB20151214008](https://openairdocs.org/sdr/E4EB20151214008), Dec 14, 2015: SKIN. CORRODED. REFERENCE NRC A016226, LT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN STRINGER 4 & CTR SPAR & XRS 358-393. ITEM REPAIRED IAW EA 008-5710-38-A5882.
- [SDR E4EB20151214007](https://openairdocs.org/sdr/E4EB20151214007), Dec 14, 2015: SKIN. CORRODED. REFERENCE NRC A016795, RT WING CTR LE UPPER SKIN, TE HAS INTERGRANULAR CORROSION AROUND FASTENER AT XFS 385.250. ITEM REPAIRED ON EA 008-5730-38-A5993.
- [SDR E4EB20151214006](https://openairdocs.org/sdr/E4EB20151214006), Dec 14, 2015: SKIN. CORRODED. REFERENCE NRC A016224, LT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN CTR & AFT SPAR & XRS 393 - 428. ITEM REPAIRED IAW EA 008-5710-38-A5885.
- [SDR E4EB20151214005](https://openairdocs.org/sdr/E4EB20151214005), Dec 14, 2015: WEB. CORRODED. REFERENCE NRC A017180, COCKPIT SUBFLOOR IS EXFOLIATED THROUGH SKIN AT STATION 133 RT CUSP AREA. REPAIR ACCOMPLISHED ON EA 008-5310-38-A5956.
- [SDR E4EB20151214004](https://openairdocs.org/sdr/E4EB20151214004), Dec 14, 2015: SKIN. CORRODED. REFERENCE NRC A016101, TAIL CONE SKIN CORRODED AT LOWER TAIL LIGHT ASSEMBLY. ITEM REPAIRED IAW EA 008-5330-38A5869.
- [SDR E4EB20151214003](https://openairdocs.org/sdr/E4EB20151214003), Dec 14, 2015: SKIN. CRACKED. REFERENCE NRC A019317, LT WING INBD LE, OTBD SECTION UPPER SKIN HAS SEVERAL CRACKS AT XILD 42. ITEM REPAIRED IAW EA 008-5730-38-A6019.
- [SDR E4EB20151214002](https://openairdocs.org/sdr/E4EB20151214002), Dec 14, 2015: SKIN. CORRODED. REFERENCE NRC A016084, EXTERIOR FUSELAGE HAS CORROSION ON SKIN AT WINDOW REPAIR DOUBLER, STATION 1340. REPAIR WAS ACCOMPLISHED ON EA 008-5320-38-A5955.
- [SDR E4EB20151214001](https://openairdocs.org/sdr/E4EB20151214001), Dec 14, 2015: WINDOW FRAME. CORRODED. REFERENCE NRC A017940, AFTER REMOVING RT CABIN WINDOW AT STATION 1410, FOUND CORROSION ON WINDOW FRAME & INSIDE FASTENER HOLES. ITEM REPAIRED ON EA 008-5320-38-
- [SDR E4EB20151213013](https://openairdocs.org/sdr/E4EB20151213013), Dec 13, 2015: DOUBLER. CORRODED. REFERENCE NRC A016097, EXTERIOR FUSELAGE, AFT RT LAVATORY SERVICE PANEL, CUT OUT HAS CORROSION INSIDE. REPAIR ACCOMPLISHED IAW EA 008-5330-38-A6035.
- [SDR E4EB20151213012](https://openairdocs.org/sdr/E4EB20151213012), Dec 13, 2015: SKIN. CORRODED. RIGHT WING, INBD LE, OTBD SECTION LOWER SKIN HAS INTERGRANULAR CORROSION AT XS 250.089. REPAIR ACTION ACCOMPLISHED IAW EA 008-5710-38-A6018.
- [SDR E4EB20151213011](https://openairdocs.org/sdr/E4EB20151213011), Dec 13, 2015: WINDOW FRAME. CORRODED. REFERENCE A017940, AFTER REMOVING RT CABIN WINDOW AT FS 1410, FOUND CORROSION ON WINDOW FRAME & INSIDE FASTENER. REPAIR ACCOMPLISHED IAW EA 008-5320-38-A5955.
- [SDR E4EB20151213010](https://openairdocs.org/sdr/E4EB20151213010), Dec 13, 2015: ANGLE. CORRODED. REFERENCE NRC A017102, AFT ACCESSORY COMPARTMENT, FS 1530, LONGERON 28L - 28R, AFT FACING SURFACES CORRODED.
- [SDR E4EB20151213009](https://openairdocs.org/sdr/E4EB20151213009), Dec 13, 2015: DOOR SEAL. TORN. REFERENCE NRC A016448 & A023498 INGRESS & EGRESS DOOR FROM FLIGHT DECK TO UPPER CARGO COMPARTMENT, MAIN CARGO DECK, HAS TORN & COMPRESSED FIRE SUPPRESSION SEALS
- [SDR E4EB20151213008](https://openairdocs.org/sdr/E4EB20151213008), Dec 13, 2015: SKIN. CORRODED. REFERENCE NRC A016309, LT HORIZONTAL STABILIZER INBD LE, UPPER SURFACE HAS CORROSION AT INBD HOIST ATTACH POINT. ITEM REPAIRED IAW EA 008-5530-38-A5929.
- [SDR E4EB20151213007](https://openairdocs.org/sdr/E4EB20151213007), Dec 13, 2015: PANEL. CORRODED. REFERENCE NRC A016937, RT INBD AILERON BALANCE PANEL HAS CORROSION. REPAIR ACCOMPLISHED IAW EA 008-5751-38-A5959.
- [SDR E4EB20151213006](https://openairdocs.org/sdr/E4EB20151213006), Dec 13, 2015: SKIN. CORRODED. REFERENCE NRC A016313, LT WING INBD STUB WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN XILD 42 - XW 257 AT FWD SPAR ATTACHMENT.
- [SDR E4EB20151213005](https://openairdocs.org/sdr/E4EB20151213005), Dec 13, 2015: PANEL. CORRODED. REFERENCE NRC A016695, LT WING INBD AILERON CTR & OTBD BALANCE PANELS HAVE RUST CORROSION. REPAIR ACCOMPLISHED IAW EA 008-5751-38-A5958.
- [SDR E4EB2015121310004](https://openairdocs.org/sdr/E4EB2015121310004), Dec 13, 2015: FLOORBEAM. CORRODED. AFTER REMOVAL OF AFT RT LAVATORY DUMP PAN & FASTENERS. MAIN CABIN FLOORBEAM FOUND EXFOLIATED.
- [SDR E4EB2015121300004](https://openairdocs.org/sdr/E4EB2015121300004), Dec 13, 2015: STRINGER. CORRODED. EXFOLIATED LOWER FWD STRINGER INBD END, INSIDE FUEL ACCESS PANEL 514D.
- [SDR E4EB20151213003](https://openairdocs.org/sdr/E4EB20151213003), Dec 13, 2015: SKIN. CORRODED. REFERENCE NRC A016056, LT WING LOWER SURFACE HAS CORROSION OTBD SIDE OF NR 1 PYLON AT STRINGER 52 28-034.
- [SDR E4EB20151213002](https://openairdocs.org/sdr/E4EB20151213002), Dec 13, 2015: DOUBLER. CORRODED. EXTERIOR FUSELAGE DOUBLER HAS CORROSION AT RT AFT DRAIN MAST, STATION 1552 32-015.
- [SDR E4EB7211213001](https://openairdocs.org/sdr/E4EB7211213001), Dec 13, 2015: SKIN. CORRODED. LEFT WING LOWER SURFACE HAS CORROSION AT STRINGER 53 & INBD OF PYLON, 28-023.
- [SDR E4EB2015120904](https://openairdocs.org/sdr/E4EB2015120904), Nov 6, 2015: ATTACH FITTING. CORRODED. FOUND FITTING THAT ATTACHES FRAME TO FLOORBEAM AT STATION 1480 RT SIDE WITH INTERGRANULAR CORROSION. REMOVED FITTING. FABRICATED & INSTALLED NEW FITTING IAW EA 
- [SDR E4EB2016F00010](https://openairdocs.org/sdr/E4EB2016F00010), Nov 2, 2015: FINGER DOUBLER. BROKEN. COCKPIT SUBFLOOR RT SIDE CUSP AREA BS 148, FINGER DOUBLER HAS MANY BROKEN OFF FASTENERS.
- [SDR E4EB2015FA0000533](https://openairdocs.org/sdr/E4EB2015FA0000533), Nov 2, 2015: SEAT TRACK. CORRODED. MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION AT SPLICE BS 590, RBL 60. 32-158.
- [SDR E4EB2015FA0000532](https://openairdocs.org/sdr/E4EB2015FA0000532), Nov 2, 2015: SEAT TRACK. CORRODED. MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION AT SPLICE STA 590, LBL 48. 32-155.
- [SDR E4EB2015FA0000531](https://openairdocs.org/sdr/E4EB2015FA0000531), Nov 2, 2015: SEAT TRACK. CORRODED. MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION AT SPLICE 995, LBL 45.32-152.
- [SDR E4EB2015FA0000530](https://openairdocs.org/sdr/E4EB2015FA0000530), Nov 2, 2015: SEAT TRACK. CORRODED. MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION AT SPLICE, BS 990, LBL 24, 32-151.
- [SDR E4EB2015FA0000529](https://openairdocs.org/sdr/E4EB2015FA0000529), Nov 2, 2015: TAB. DENTED. LEFT WING AILERON TRIM TAB IS DENTED ON UPPER AND LOWER SURFACES.
- [SDR E4EB2015FA0000528](https://openairdocs.org/sdr/E4EB2015FA0000528), Nov 2, 2015: TAB. DENTED. LEFT WING AILERON CONTROL TAB IS DENTED AND HAS DELAMINATION ON UPPER AND LOWER SURFACES.
- [SDR E4EB2015110200000](https://openairdocs.org/sdr/E4EB2015110200000), Nov 2, 2015: SKIN. CORRODED. RIGHT WING OTBD L/E INBD SECTION LOWER SKIN HAS INTER GRANULAR CORROSION AROUND FASTENERS AT XFS 685.
- [SDR E4EB2015FA0000526](https://openairdocs.org/sdr/E4EB2015FA0000526), Nov 2, 2015: SKIN. CORRODED. LEFT WING UPPER SKIN HAS CORROSION AROUND FASTENERS BETWEEN STR 10 AND FWD SPAR AND XRS 50-107 28-075.
- [SDR E4EB2016F00021](https://openairdocs.org/sdr/E4EB2016F00021), Nov 2, 2015: BULKHEAD WEB. CRACKED. CRACK FOUND AT RT OTBD SIDE OF AFT PRESSURE BULKHEAD WEB BETWEEN LONGHORN 10 AND 11 APPROXIMATELY 2" IN LENGTH . VERIFIED BY FPI AND HFEC INSPECTIONS.
- [SDR E4EB2016F00018](https://openairdocs.org/sdr/E4EB2016F00018), Nov 2, 2015: BULKHEAD WEB. CRACKED. CRACK FOUND AT LT INBD SIDE OF AFT PRESSURE BULKHEAD BETWEEN LONGHORN 10 AND 11 APPROXIMATELY 2.25" IN LENGTH. VERIFIED BY FPI AND HFEDC INSPECTION.
- [SDR E4EB2016F00017](https://openairdocs.org/sdr/E4EB2016F00017), Nov 2, 2015: BULKHEAD WEB. CRACKED. CRACK FOUND AT LT INBD SIDE OF AFT PRESSURE BULKHEAD BETWEEN LONGHORN 10 AND 11 APPROXIMATELY 2.25" IN LENGTH. VERIFIED BY FPI AND HFEDC INSPECTION.
- [SDR E4EB2015FA0000525](https://openairdocs.org/sdr/E4EB2015FA0000525), Nov 2, 2015: SEAT TRACK. CORRODED. MAIN DECK CARGO TRACK HAS CORROSION AT SPLICE BS 590, LBL 24.
- [SDR E4EB2015FA0000524](https://openairdocs.org/sdr/E4EB2015FA0000524), Nov 2, 2015: SKIN. CORRODED. LEFT WING CENTER L/E UPPER SKIN HAS INTERGRANULAR CORROSION AROUND FASTENER AT XFS 261.500 28-129, REF VT NRC 7000900968.
- [SDR E4EB20151029002](https://openairdocs.org/sdr/E4EB20151029002), Oct 29, 2015: SKIN. CORRODED. LT WING CTR UE UPPER SKIN HAS INTERGRANULAR CORROSION AROUND FASTENER AT XFS 261.500.
- [SDR E4EB20151029001](https://openairdocs.org/sdr/E4EB20151029001), Oct 29, 2015: SKIN. CORRODED. LEFT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN CTR SPAR & STRINGER 11 & XRS 204 & 238.052.
- [SDR E4EB2015120714](https://openairdocs.org/sdr/E4EB2015120714), Oct 27, 2015: LONGERON. DAMAGED. AFTER REMOVAL OF LOWER IFF ANTENNA, FOUND CORROSION, JUST AFT OF NLG INTERNAL STRUCTURE AROUND ANTENNA CUT OUT. GAINED ACCESS TO AREA & FOUND LONGERON 36L WITH 
- [SDR E4EB2015121205](https://openairdocs.org/sdr/E4EB2015121205), Oct 9, 2015: STRINGER. CORRODED. UPON OK TO CLOSE, FOUND EXFOLIATED LOWER FWD STRINGER INSIDE FUEL ACCESS PANEL 514D, INBOARD END. REMOVED STRINGER 59. FABRICATED STRINGER 59 REPAIR SPLICE FITT

All 257: https://openairdocs.org/model/douglas-dc-8-72f/reports.md

## STCs that may be installed (OpenAirDocs) (114, 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 ST01078AT](https://openairdocs.org/stc/ST01078AT): Installation of an expanded, 17-parameters, Allied Signal, or Loral-Fairchild, Digital Flight Data Recorder (DFDR). Acron Aviation Inc
- [STC ST01174CH](https://openairdocs.org/stc/ST01174CH): Installation of UPS Aviation Technologies ADS-B provisions and Honeywell Mode-S System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST02001AT](https://openairdocs.org/stc/ST02001AT): Installation of SAF-T-GLO Aerospace Limited's photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC 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 SA3140SO](https://openairdocs.org/stc/SA3140SO): Installation of a replacement coalescer filter, P/N 22D10 or 22D10-2. Purolator Facet, 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 SA3496NM](https://openairdocs.org/stc/SA3496NM): Installation of ABX-C Cargo Container assembly. Airborne Express Air 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 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 ST00984LA-D](https://openairdocs.org/stc/ST00984LA-D): Installation of smoke detection and fire suppression systems provisions. Securaplane Technologies LLC
- [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 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
- [STC SA2498NM](https://openairdocs.org/stc/SA2498NM): Installation of dual AiResearch GTCP85-98CK(D) Auxiliary Power Units (APU) in the forward baggage compartment. Airweld Inc
- [STC SA4225WE](https://openairdocs.org/stc/SA4225WE): Installation of 1 or 2 AiResearch GTCP85-98CK auxiliary power units in forward baggage compartment. Airweld Inc
- [STC SA3949NM](https://openairdocs.org/stc/SA3949NM): Installation of a Fairchild Model 800 Digital Flight Data Recorder. Flying Tiger Line Inc
- [STC ST127CH](https://openairdocs.org/stc/ST127CH): Installation of strobe upper anticollision light, P/N 30-1585-1. Honeywell International Inc
- [STC ST01738CH](https://openairdocs.org/stc/ST01738CH): Installation of a Honeywell Traffic Alert and Collision Avoidance System (TCAS II). Canard Aerospace Corporation
- [STC ST10503SC](https://openairdocs.org/stc/ST10503SC): Installation of a Universal Avionics Systems Corporation EFI-600 Flat Panel Electronic Flight Instrument system. Avionics & Systems Integration Group
- [STC ST00171LA-D](https://openairdocs.org/stc/ST00171LA-D): Modifications for combi configuration fire protection. Air Transport LLC
- [STC ST01073LA](https://openairdocs.org/stc/ST01073LA): Requirements for establishing group approval basis for Reduced Vertical Separation Minimum (RVSM) are contained in AeroMech Document No. AMI-QD-DC8-0006 dtd 9/15/00 or later approved FAA revisions. AeroMech Incorporated
- [STC ST01307WI-D](https://openairdocs.org/stc/ST01307WI-D): Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation. Rockwell Collins Inc
- [STC ST10268SC](https://openairdocs.org/stc/ST10268SC): Installation of a Universal Avionics Terrain Awareness Warning System (TAWS) in accordance with Aircraft Systems and Manufacturing Top Drawing List 5643-0001-00 A, dated July 20, 2004, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Document No. 5643-2160-00, Revision IR, dated July 22, 2004 is required. Aircraft Systems & Mfg
- [STC ST01791CH](https://openairdocs.org/stc/ST01791CH): Install reinforced flightdeck door and venting system as defined in Drawing List FDS-DL16 latest FAA approved revision per Cockpit Door System Installation Manual FDS-16 latest FAA approved revisions. National Aircraft Service Inc

All 114: https://openairdocs.org/model/douglas-dc-8-72f/stcs.md

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