# Douglas DC-8-62F

- Type: Aircraft model (FAA registry)
- Registry code: 3021972
- Manufacturer (registry): DOUGLAS
- Model: DC-8-62F
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-jet
- Seats: 152
- Weight class: 20,000 lb and over
- Cruise speed: 444 mph
- Certification: Type certificated
- Data sheet: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Holder: The Boeing Company
- Registered aircraft: 0
- Page: https://openairdocs.org/model/douglas-dc-8-62f

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 2007-04-06](https://openairdocs.org/ad/2007-04-06): Engine thrust brake circuit · Boeing DC-8-62, DC-8-62F, DC-8-63 and 1 more. Effective Mar 21, 2007
- [AD 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

Historical (superseded or no longer in force):

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2008-26-07](https://openairdocs.org/ad/2008-26-07) (historical): Lower skin and stringers · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Jan 28, 2009
- [AD 2008-09-04](https://openairdocs.org/ad/2008-09-04) (historical): Fuel tank systems · McDonnell Douglas DC-8-31, DC-8-32, DC-8-33 and 21 more. Effective May 27, 2008
- [AD 2007-02-02](https://openairdocs.org/ad/2007-02-02) (historical): Aft fuselage skin panel · McDonnell Douglas DC-8-55, DC-8-61, DC-8-61F and 12 more. Effective Feb 28, 2007
- [AD 2006-07-25](https://openairdocs.org/ad/2006-07-25) (historical): Rudder pedal bracket · McDonnell Douglas DC-8-11, DC-8-12, DC-8-21 and 44 more. Effective May 16, 2006
- [AD 2003-17-07](https://openairdocs.org/ad/2003-17-07) (historical): Fire Extinguishers for the Engine and Auxiliary Power Unit (APU) · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 60 more. Effective Sep 24, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2001-25-01](https://openairdocs.org/ad/2001-25-01) (historical): Engine Fire Extinguishing System Electrical Connectors · McDonnell Douglas DC-8-33, DC-8-43, DC-8-51 and 17 more. Effective Dec 20, 2001
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 95-04-01](https://openairdocs.org/ad/95-04-01) (historical): AFM - Limitations - Windshear · Boeing 727-100 Series, 727-200 Series, 737-100 Series and 54 more. Effective Mar 8, 1995
- [AD 93-20-02](https://openairdocs.org/ad/93-20-02) (historical): AFM Changes - Cargo Door Inspection · Cargo door, cargo restraint bulkhead, heavy duty flooring… (Plattner STC SA1802SO or SA421NW). Effective Nov 17, 1993

All 151: https://openairdocs.org/model/douglas-dc-8-62f/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 ANC11CA101](https://openairdocs.org/ntsb/ANC11CA101), Sep 10, 2011: Douglas DC-8-62F (N71CX), Yakota, Japan, no damage. Probable cause: The passenger's decision to ignore the fasten seatbelt sign, resulting in serious injury to the passenger during a turbulence encounter.
- [NTSB MIA95WA067](https://openairdocs.org/ntsb/MIA95WA067), Jan 29, 1995: Douglas DC8-62 (N791AL), Manaus, Brazil, incident, minor damage

## FAA accident and incident reports (1)

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.

- [Accident 20110910026389A](https://openairdocs.org/incident/20110910026389A), Sep 10, 2011: Douglas DC-8-62F (N71CX), No damage. While enroute cruising at flight level 270 in the vicinty of thunderstorms, the aircraft encountered turbulence. The captain had previously illuminated the…

## Service difficulty reports (1,163, newest 50)

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

- [SDR IXXA201312040450](https://openairdocs.org/sdr/IXXA201312040450), Dec 4, 2013: PRESSURE SWITCH. MALFUNCTIONED. AFTER TAKEOFF AT 1545Z NR 1 ENG LOW OIL PRESS LIGHT ILLUMINATED, PERFORMED APPROPRIATE CHECK LIST, LOW PRESS LIGHT STAYED ON SHUT ENG DOWN. R & R NR 1 LOW OIL P
- [SDR IXXA20130107001O](https://openairdocs.org/sdr/IXXA20130107001O), Jan 7, 2013: TRANSCEIVER. INOPERATIVE. AFTER DEPARTURE, NR 1 HF RADIO TUNES, BUT IS WEAK AND UNREADABLE AND NR 2 HF RADIO WILL NOT CHANNELIZE OR TUNE. ACFT RETURNED TO PREVIOUS STATION. R & R CAPTAIN
- [SDR IXXA20121210033O](https://openairdocs.org/sdr/IXXA20121210033O), Dec 10, 2012: CONTROLLER. INOPERATIVE. ACFT ENROUTE AND AIR RETURNED BACK TO DEPARTURE DUE TO F/O WINDSHIELD CRACKED AND ARCING. PILOT STATED F/O VISION IMPAIRED. R & R RT SIDE WINDSHIELD IAW MM 56-1
- [SDR IXXA20121121031O](https://openairdocs.org/sdr/IXXA20121121031O), Nov 21, 2012: VALVE. STUCK. ACFT RETURNED TO DEPARTURE, DUE TO NO HEAT IN THE PASSENGER COMPARTMENT. TROUBLESHOT AND FOUND NASI MIX VALVE STUCK IN THE FULL COLD POSITION. R & R MIX VALVE I
- [SDR IXXA20121001028O](https://openairdocs.org/sdr/IXXA20121001028O), Oct 1, 2012: BATTERY. INOPERATIVE. F/A EMERGENCY FLASHLIGHTS FOUND INOPERATIVE. R & R THE RT EMERGENCY FLASHLIGHT AND BATTERIES IAW MM 16.02. OPS CHECK GOOD.
- [SDR IXXA20120922027O](https://openairdocs.org/sdr/IXXA20120922027O), Sep 22, 2012: CONTROL VALVE. LEAKING. DURING FLIGHT, HYDRAULIC QUANTITY LEVEL STARTED SLOWLY DECREASING. ACFT RETURNED TO ORIGINATING STATION. FOUND SLOT CONTROL VALVE LEAKING. R & R PACKING AND O-R
- [SDR IXXA20120907023O](https://openairdocs.org/sdr/IXXA20120907023O), Sep 7, 2012: ENGINE. STALLED. DURING TAKEOFF ROLL, CREW EXPERIENCED A COMPRESSOR STALL ON THE NR 3 ENGINE. TAKEOFF WAS REJECTED AT 85 KIAS AND 1.96 EPR. RETURNED BACK TO GATE. MX PERSONNEL P
- [SDR IXXA20120618016O](https://openairdocs.org/sdr/IXXA20120618016O), Jun 18, 2012: CONNECTOR. DIRTY. NR 1 EGT FLUCTUATED RAPIDLY AND THEN DROPPED TO ZERO DURING TAKEOFF ROLL. TAKEOFF ABORTED AT APPROX 40 KNOTS. ACFT RETURNED TO BLOCKS. INSPECTED THERMOCOUPLE HA
- [SDR IXXA20120605015](https://openairdocs.org/sdr/IXXA20120605015), Jun 5, 2012: AMPLIFIER. FAILED. CAPTAINS HSI AND ADI FAILED AFTER TAKEOFF. RETURNED TO ORIGINATING STATION. PERFORMED OVERWEIGHT LANDING INSP IAW MM 5-50-0 AND MM 13.01.05. NO DISCREPANCIES NO
- [SDR IXXA20120605014](https://openairdocs.org/sdr/IXXA20120605014), Jun 5, 2012: GYRO. FAILED. CAPTAINS HSI AND ADI FAILED AFTER INITIAL CLIMBOUT AND LEVEL OFF AT CRUISE ALTITUDE. RETURNED TO ORIGINATING STATION. R & R NR 1 FOG GYRO IAW MM 34-11-25. OPS C
- [SDR IXXA20120322009O](https://openairdocs.org/sdr/IXXA20120322009O), Mar 20, 2012: GROUND WIRE. DAMAGED. PASSENGER COMPARTMENT FORWARD BULKHEAD EMERGENCY EXIT IDENTIFIER DOES NOT ILLUMINATE. REPAIRED GROUND WIRE TO IDENTIFIER IAW MM 20-50-1 AND RELAMPED SIGN. OPS C
- [SDR IXXA20120228005O](https://openairdocs.org/sdr/IXXA20120228005O), Feb 28, 2012: SWITCH. LEAKING. NR 3 ENGINE STARTED SLOWLY LEAKING OIL. AT 1418Z WITH NR 3 OIL QUANTITY INDICATION OF 1 GALLON AND NR 3 OIL TEMP SLOWLY STARTING TO INCREASE, NR 3 ENGINE WAS SH
- [SDR IXXA20120218003O](https://openairdocs.org/sdr/IXXA20120218003O), Feb 18, 2012: BATTERY. INOPERATIVE. DURING PREFLIGHT INSPECTION, FOUND RT EMERGENCY FLASHLIGHT INOPERATIVE. MX REPLACED EMERGENCY FLASHLIGHT BATTERY. OPS CHECKED GOOD IAW MM 25-60-0.
- [SDR IXXA1100770](https://openairdocs.org/sdr/IXXA1100770), Nov 28, 2011: SLIDE. LOW PRESSURE. LEFT HAND PASSENGER DOOR ESCAPE SLIDE PRESSURE LOW AND IN RED RANGE (2600 PSI AT 22 DEGREES CELCIUS) - DISCOVERED DURING POSTFLIGHT INSPECTION. MX R & R EMERGEN
- [SDR IXXA1100740](https://openairdocs.org/sdr/IXXA1100740), Nov 2, 2011: FAN. FAILED. DURING DESCENT, FLIGHT CREW SWITCHED ON RT RECIRCULATION FAN AND NOTICED A STRONG ELECTRICAL ODOR. FAN WAS SUBSEQUENTLY TURNED OFF AND ELECTRICAL ODOR DISSIPATE
- [SDR IXXA110069O](https://openairdocs.org/sdr/IXXA110069O), Oct 13, 2011: TRANSCEIVER. DEFECTIVE. DURING CLIMB OUT, THE WEATHER RADAR FAILED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED WEATHER RADAR TRANSCEIVER, OPS CHECK GOOD IAW M
- [SDR IXXA110065O](https://openairdocs.org/sdr/IXXA110065O), Oct 6, 2011: UNKNOWN. UNKNOWN. AFTER TAKEOFF, WHEN GEARS WERE BEING RETRACTED THE CREW A HEARD LOUD NOISE IN NOSE GEAR AREA. THEY CYCLED NOSE GEAR AND NOISE CONTINUED. THEY RETURNED TO WITHOU
- [SDR IXXA110062O](https://openairdocs.org/sdr/IXXA110062O), Sep 25, 2011: GROUND WIRE. LOOSE. AIR TURN BACK, DUE TO AUTO PILOT WILL NOT STAY ENGAGED WITH ELEVATOR SERVO ON. THE ACFT PITCHES UP AND DOWN AND DISENGAGED IN VERTICAL SPEED OR ALT HOLD MODES. 
- [SDR IXXA20110925001](https://openairdocs.org/sdr/IXXA20110925001), Sep 25, 2011: FAN. FAILED. DURING CRUISE, THE LT RECIRCULATION FAN HAS A SMELL OF SMOKE. THE CREW TURNED OFF LT RECIRCULATION FAN AND SMOKE, SMELL WENT AWAY. THEY LANDED WITHOUT FURTHER I
- [SDR IXXA110058O](https://openairdocs.org/sdr/IXXA110058O), Sep 4, 2011: FAN. ODOR. DURING CRUISE, THE OVERHEAD COCKPIT CLIMATE CONTROL UNIT EMITS A BURNING ODOR WHEN TURNED ON. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND CLEANED
- [SDR IXXA110059O](https://openairdocs.org/sdr/IXXA110059O), Sep 3, 2011: BATTERY. INOPERATIVE. DURING PREFLIGHT INSPECTUIN, FOUND EMERGENCY FLASHLIGHT INOPERATIVE. MX REPLACED BATTERY IAW MM 33-50-0.
- [SDR IXXA110056O](https://openairdocs.org/sdr/IXXA110056O), Sep 2, 2011: FAN. FAILED. DURING CRUISE, WHEN THE CREW TURNED ON LT RECIRCULATION FAN IT EMITTED A BURNING SMELL. THEY TURNED THE LT RECIRCULATION FAN OFF AND SMELL WENT AWAY. THEY LANDE
- [SDR IXXA110054O](https://openairdocs.org/sdr/IXXA110054O), Aug 19, 2011: CONTROLLER. MALFUNCTIONED. DURING CRUISE, 30 MIN INTO FLIGHT, AUTOPILOT DISCONNECTED AND WOULD NOT RECONNECT. THE CREW RETURNED . MX REPLACED AUTOPILOT CONTROLLER. OPS CHECKED GOOD IAW MM
- [SDR IXXA110055O](https://openairdocs.org/sdr/IXXA110055O), Aug 18, 2011: OXYGEN MASK. TORN. DURING POST FLIGHT INSP, FOUND F/A DEMO KIT O2 MASK TORN. MX REPLACED O2 MASK IN F/A DEMO KIT IAW MM 16.02.
- [SDR IXXA20110813001](https://openairdocs.org/sdr/IXXA20110813001), Aug 13, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK INSP, FOUND VERTICAL STABILIZER RT LATERAL SKIN CORRODED AT STA ZR 35.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. 
- [SDR IXXA20110812001](https://openairdocs.org/sdr/IXXA20110812001), Aug 12, 2011: SPAR. CORRODED. DURING ROUTINE C-CHECK INSP FOUND RT VERTICAL STABILIZER REAR SPAR CORRODED AT STA ZR 45.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERF
- [SDR IXXA20110811001](https://openairdocs.org/sdr/IXXA20110811001), Aug 11, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK INSP, FOUND LT WING T/E UPPER SKIN CORRODED AT STA XW 761.695 - 736.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FA
- [SDR IXXA20110810003](https://openairdocs.org/sdr/IXXA20110810003), Aug 10, 2011: SKIN. CRACKED. DURING ROUTINE C-CHECK INSP, FOUND RT INBD AILERON UPPER SKIN CRACKED AT STATION XA 603.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDE
- [SDR IXXA20110810002](https://openairdocs.org/sdr/IXXA20110810002), Aug 10, 2011: SKIN. CRACKED. DURING ROUTINE C-CHECK INSP, FOUND RT OTBD AILERON LOWER SKIN CRACKED AT STA XA 610.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PA
- [SDR IXXA20110810001](https://openairdocs.org/sdr/IXXA20110810001), Aug 10, 2011: ANGLE. CRACKED. DURING ROUTINE C-CHECK, INSP FOUND NR 60 ACCESS DOOR BEAM AFT PRESS BULKHEAD CRACKED BOTTOM LINE-0. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STO
- [SDR IXXA11SMN103S](https://openairdocs.org/sdr/IXXA11SMN103S), Aug 9, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK, FOUND EXTERNAL SKIN CORRODED AT BS 902.00- 910.000 LONGERON 19 - 21RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PER
- [SDR IXXA20110809004](https://openairdocs.org/sdr/IXXA20110809004), Aug 9, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK INSP FOUND EXTERNAL SKIN CORRODED AT STA 1100.000 LONGERON 21 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED
- [SDR IXXA20110809003](https://openairdocs.org/sdr/IXXA20110809003), Aug 9, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK INSP FOUND LT WING UPPER SKIN CORRODED AT STATION XRS 358.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED ND
- [SDR IXXA20110809001](https://openairdocs.org/sdr/IXXA20110809001), Aug 9, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK INSP FOUND LT WING UPPER SKIN AFT PART CORRODED AT STA XRS 70.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORME
- [SDR IXXA20110808002](https://openairdocs.org/sdr/IXXA20110808002), Aug 8, 2011: SKIN. CORRODED. DURING ROUTINE C-CHECK INSP FOUND FORWARD CARGO COMPARTMENT INTERNAL SKIN CORRODED AT STA 600.000, LONGERON 36. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED 
- [SDR IXXA20110808001A](https://openairdocs.org/sdr/IXXA20110808001A), Aug 8, 2011: SKIN. CRACKED. DURING ROUTINE C-CHECK INSP FOUND FUSELAGE NOSE SECTION LOWER SKIN CRACKED AT STA 260.000, LONGERON 34 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVE
- [SDR IXXA20110808001](https://openairdocs.org/sdr/IXXA20110808001), Aug 8, 2011: SKIN. CRACKED. DURING ROUTINE C-CHECK INSP, FOUND NLG CORNER LOWER SKIN CRACKED AT STATION 208.000, LONGERON 33 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMA
- [SDR IXXA20110801002](https://openairdocs.org/sdr/IXXA20110801002), Aug 1, 2011: STRUCTURE. MISREPAIRED. DURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT STA FS 255 LONGERON 33.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORME
- [SDR IXXA201108SMN095S](https://openairdocs.org/sdr/IXXA201108SMN095S), Aug 1, 2011: ANGLE. CRACKED. DURING ROUTINE C-CHECK INSP, FOUND ANGLE CRACKED AT STA FS 975 LONGERON 24 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED R
- [SDR IXXA110051O](https://openairdocs.org/sdr/IXXA110051O), Jul 26, 2011: LIGHT. UNSECURE. DURING PREFLIGHT INSP, FOUND GALLEY SERVICE DOOR EMERGENCY EXIT LIGHTING INTERMITTENT. MX RESECURED LIGHTING ASSY. OPERATIONAL CHECK GOOD IAW MM 33-50-0. ACFT R
- [SDR IXXA110050S](https://openairdocs.org/sdr/IXXA110050S), Jul 23, 2011: STRINGER. DELAMINATED. DURING ROUTINE B-CHECK INSPECTION FOUND NR 1 ENGINE LOWER STRINGER DELAMINATED. R & R DAMAGED STRINGER IAW MM 78-10-2.
- [SDR IXXA110042O](https://openairdocs.org/sdr/IXXA110042O), May 29, 2011: FAN. DEFECTIVE. DURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ELECTRICAL ODOR. THE CREW TURNED OFF THE LT RECIRCULATION FAN THE BURNED ODOR WENT AWAY. THEY LANDED WI
- [SDR IXXA110041O](https://openairdocs.org/sdr/IXXA110041O), May 18, 2011: FAN. DEFECTIVE. DURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ODOR. THE CREW SHUT OFF THE LT RECIRCULATION FAN AND BURNED ODOR WENT AWAY. THEY LANDED WITHOUT FURTHER
- [SDR IXXA0041O](https://openairdocs.org/sdr/IXXA0041O), May 18, 2011: FAN. ODOR. DURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ODOR IN COCKPIT. THE CREW SHUTOFF LT RECIRCULATION FAN AND ODOR WENT AWAY. OPEN
- [SDR IXXA110038O](https://openairdocs.org/sdr/IXXA110038O), May 4, 2011: CONNECTOR. SHORTED. WHILE INCREASING THE INTENSITY OF THE ENGINE INSTRUMENT LIGHTS, THE CREW SMELLED AN ELECTRICAL ODOR COMING FROM THE ENGINE INSTRUMENT LIGHT PANEL. THEY TURNED O
- [SDR IXXA110036O](https://openairdocs.org/sdr/IXXA110036O), Apr 30, 2011: SMOKE DETECTOR. DEFECTIVE. DURING CLIMBOUT, THE NR 2 CARGO SMOKE DETECTOR FLASHED ON MOMENTARLY SEVERAL TIMES WITH ASSOCIATED AUDIBLE WARNING. THE CREW INSPECTED THE CARGO COMPARTMENT FOR
- [SDR IXXA110034O](https://openairdocs.org/sdr/IXXA110034O), Apr 20, 2011: FAN. DEFECTIVE. DURING CRUISE, THE RT RECIRCULATION FAN EMMITTING A BURNING ODOR, TURNED OFF THE RT RECIRCULATION FAN AND ODOR WENT AWAY, LANDED WITHOUT FURTHER INCIDENT. MX RE
- [SDR IXXA1100330](https://openairdocs.org/sdr/IXXA1100330), Apr 18, 2011: ACTUATOR. DEFECTIVE. AT FL 320 CABIN PRESSURIZATION CONTROL WAS SET TO 340 FOR FOR A SELECTED CABIN 4,500 FT CABIN CLIMBED TO 8500 FT. CABIN PRESS CONTROL LEVER PHYSICALLY LIMITED T
- [SDR IXXA110032O](https://openairdocs.org/sdr/IXXA110032O), Apr 13, 2011: FAN. FAILED. DURING CRUISE THE RT RECIRCULATION FAN EMMITTING AN ELECTRICAL ODOR. THE CREW TURNED OFF FAN AND SMELL WENT AWAY. THE CREW LANDED WITHOUT FURTHER INCIDENT.
- [SDR IXXA110030O](https://openairdocs.org/sdr/IXXA110030O), Mar 22, 2011: CSD. DEFECTIVE. DURING CLIMB OUT, NR 4 GENERATOR BREAKER CYCLED OPEN AND CLOSED SEVERAL TIMES, GENERATOR WOULD NOT CARRY ITS OWN BUSS, VOLTS AND FREQUENCYS OK. THE CREW RETURNE

All 1,163: https://openairdocs.org/model/douglas-dc-8-62f/reports.md

## STCs that may be installed (OpenAirDocs) (146, 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 SA3166SO](https://openairdocs.org/stc/SA3166SO): Installation of an Expanded parameters Digital Flight Data Recorder. Acron Aviation Inc
- [STC ST01078AT](https://openairdocs.org/stc/ST01078AT): Installation of an expanded, 17-parameters, Allied Signal, or Loral-Fairchild, Digital Flight Data Recorder (DFDR). Acron Aviation Inc
- [STC ST01174CH](https://openairdocs.org/stc/ST01174CH): Installation of UPS Aviation Technologies ADS-B provisions and Honeywell Mode-S System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST02001AT](https://openairdocs.org/stc/ST02001AT): Installation of SAF-T-GLO Aerospace Limited's photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC SA2076SO](https://openairdocs.org/stc/SA2076SO): Installation of emergency escape path lighting system. Astronics Luminescent Systems Inc
- [STC SA2534SW-D](https://openairdocs.org/stc/SA2534SW-D): Replacement of Switch assembly Int'l Inflatables Co. P/N 68748, with DME Corp. P/N L-140 in emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC SA2539SW-D](https://openairdocs.org/stc/SA2539SW-D): Replacement of light assembly, International Inflatables Co. P/N68555-1 with DME Corp. EL-104, EL-104A, and EL-104B in emergency slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC SA863EA](https://openairdocs.org/stc/SA863EA): Incorporation of DME Corporation emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC ST02580AT](https://openairdocs.org/stc/ST02580AT): Lithium cell battery pack to replace currently approved alkaline battery pack used in escape slide emergency light system. Astronics Luminescent Systems Inc
- [STC SA5720NM](https://openairdocs.org/stc/SA5720NM): Installation of the Mark VII ground proximity and windshear warning system. Honeywell International Inc
- [STC 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 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 SA2785WE](https://openairdocs.org/stc/SA2785WE): Installation of dual Litton LTN-51 or LTN-72 Inertial Navigation System. Northrop Grumman Systems Corporation
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic LLC
- [STC ST01067LA](https://openairdocs.org/stc/ST01067LA): Installation of Litton LTR-97 fiber optic gyro systems. Northrop Grumman Systems Corporation
- [STC ST01467LA-D](https://openairdocs.org/stc/ST01467LA-D): Installation of Universal Avionics Terrain Avoidance Warning System and MFD-640 Multi Function Display(s). Zalinka Aviation Support, LLC
- [STC ST01468LA-D](https://openairdocs.org/stc/ST01468LA-D): Installation of Universal Avionics Flight Management System. Zalinka Aviation Support, LLC
- [STC SA1511GL](https://openairdocs.org/stc/SA1511GL): Installation of Type "C" containers. ABX Air Incorporated
- [STC SA1775GL](https://openairdocs.org/stc/SA1775GL): Incorporate maximum permissible quick turn-around landing weight (flaps 35º). ABX Air Incorporated
- [STC SA1794GL](https://openairdocs.org/stc/SA1794GL): Incorporate anti-skid system inoperative and/or auto-ground spoilers inoperative landing field length data for Operations using 35° landing flaps. ABX Air Incorporated
- [STC ST09378SC](https://openairdocs.org/stc/ST09378SC): Installation of a dual Honeywell/ Trimble HT9000 global navigation system. LB Aircraft Engineering Inc
- [STC SA1421GL](https://openairdocs.org/stc/SA1421GL): Installation of Supplemental Electric Heater. ABX Air Incorporated
- [STC SA1462GL](https://openairdocs.org/stc/SA1462GL): Installation of ABX Cargo Handling System. ABX Air Incorporated
- [STC SA3496NM](https://openairdocs.org/stc/SA3496NM): Installation of ABX-C Cargo Container assembly. Airborne Express Air Inc
- [STC ST369CH](https://openairdocs.org/stc/ST369CH): Approve autopilot and/or flight director coupled approach with 35 landing flap selection. ABX Air Incorporated
- [STC SA1360GL](https://openairdocs.org/stc/SA1360GL): Install Parker Hannifin Freon Air Conditioning System. ABX Air Incorporated
- [STC SA1616GL](https://openairdocs.org/stc/SA1616GL): Installation of Ametek digital fuel flow/fuel used indicator P/N10250N010F01. ABX Air Incorporated
- [STC SA1733GL](https://openairdocs.org/stc/SA1733GL): Installation of Vickers PV3-160-4B hydraulic pump. ABX Air Incorporated
- [STC SA1761GL](https://openairdocs.org/stc/SA1761GL): Installation of Kollsman P/N 35900-A2284 Mach airspeed indicator. ABX Air Incorporated
- [STC ST117CH](https://openairdocs.org/stc/ST117CH): Installation of expanded parameters. ABX Air Incorporated
- [STC ST125CH](https://openairdocs.org/stc/ST125CH): Installation of JET model AI-330 attitude indicator. ABX Air Incorporated
- [STC ST53CH](https://openairdocs.org/stc/ST53CH): Replacement of McD PN 4642526 compressor check valve flapper assembly with ABX Air, PN A04574. ABX Air Incorporated
- [STC 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 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 SA2308WE](https://openairdocs.org/stc/SA2308WE): Installation of cargo barrier net. Boeing Company
- [STC ST02032AT](https://openairdocs.org/stc/ST02032AT): Increase in aircraft operating weights (Maximum landing weight to 265000 lbs and maximum zero fuel weight to 241500 lbs). Aircraft Modification Design Services
- [STC ST00746LA-D](https://openairdocs.org/stc/ST00746LA-D): Installation of smoke detection system, lower cargo compartment. Ontic Engineering and Manufacturing 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 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

All 146: https://openairdocs.org/model/douglas-dc-8-62f/stcs.md

## The same model under other registry codes

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

- [Mcdonnell Douglas DC-8-62F](https://openairdocs.org/model/mcdonnell-douglas-dc-8-62f): 0 registered aircraft, registry code 302197D

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