# Douglas DC-8-63F - Type: Aircraft model (FAA registry) - Registry code: 302198F - Manufacturer (registry): DOUGLAS - Model: DC-8-63F - 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-8-63f 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 2008-16-11](https://openairdocs.org/ad/2008-16-11): Forward and aft service doors · Boeing DC-8-61, DC-8-61F, DC-8-63 and 3 more. Effective Sep 17, 2008 - [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 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 152: https://openairdocs.org/model/douglas-dc-8-63f/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 DCA71AZ002](https://openairdocs.org/ntsb/DCA71AZ002-79683), Jul 27, 1970: Douglas DC-8 (N785FT), Naha Ab, JA, destroyed, 4 fatal - [NTSB OAK70A0028](https://openairdocs.org/ntsb/OAK70A0028), Oct 16, 1969: Douglas DC-8 (N8634), Stockton, CA, destroyed ## FAA accident and incident reports (6) 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 20001208030589I](https://openairdocs.org/incident/20001208030589I), Dec 8, 2000: Doug DC863F (N867BX), East Tawan, MI. (-23)All three crew members were given reexaminations of their pilot certificates on 12-21-00 by the principal operations inspector for air transport, intl'… - [Incident 20000817028769I](https://openairdocs.org/incident/20000817028769I), Aug 17, 2000: Doug DC863F (N906R), Omaha, NE. (-23)On post flight crew found right gear retract bolt broken at the strut connector. The aircraft was ferried for repairs. - [Incident 19950913035579I](https://openairdocs.org/incident/19950913035579I), Sep 13, 1995: Doug DC863 (N661AV), Cali, CP, Minor damage. During taxi for takeoff aircraft stopped and leaned to right. Shutdown to investigate. No more info follows. - [Incident 19900202009719I](https://openairdocs.org/incident/19900202009719I), Feb 2, 1990: Doug DC863F (N867BX), Fort Wayne, IN. While turning at end of runway the main gear tires left the pavement and sank in the ground. - [Incident 19890920061229I](https://openairdocs.org/incident/19890920061229I), Sep 20, 1989: Doug DC863F (N867BX), Fort Wayne, IN. Aircraft blew six tires during attempt to turn around on runway. Tried to blow fog away and increase RVR for takeoff - [Incident 19821108064089I](https://openairdocs.org/incident/19821108064089I), Nov 8, 1982: Doug DC8* (N29180), Tulsa, OK, Minor damage. Post flight inspection revealed loss of right main landing gear strut fairing door. Pilot on test flight. ## Service difficulty reports (1,883, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR U2RA464AML5501](https://openairdocs.org/sdr/U2RA464AML5501), Mar 31, 2011: BULB. BURNED OUT. EMERGENCY EXIT DISARM LIGHT INOP. - [SDR U2RA464M85463](https://openairdocs.org/sdr/U2RA464M85463), Mar 4, 2011: ACCESS PANEL. CRACKED. NR 4 PYLON UPPER L/E CAP FAIRING HINGE IS CRACKED 2 PLACES ON OTBD SIDE. - [SDR U2RA464OSC18858](https://openairdocs.org/sdr/U2RA464OSC18858), Aug 26, 2010: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT FS 8.000 AIR CONDITIONING CONDENSER EXHAUST DOOR CUTOUT UPPER AFT CORNER CRACK LENGTH APPROX 2". - [SDR U2RA464OSC18837](https://openairdocs.org/sdr/U2RA464OSC18837), Aug 25, 2010: LONGERON. CRACKED. LONGERON 35RIS CRACKED FROM STA 1343-1348 (5"). - [SDR U2RA464OSC18449](https://openairdocs.org/sdr/U2RA464OSC18449), Aug 20, 2010: ATTACH FITTING. CRACKED. FUSELAGE FRAME TO CUSP FITTING CRACKED APPROX 5" AT STA 717.75. - [SDR U2RA464OSC18836](https://openairdocs.org/sdr/U2RA464OSC18836), Aug 19, 2010: LONGERON. CRACKED. LONGERON 34R IS CRACKED FROM STA 1343-1349. - [SDR U2RA865FLP3376](https://openairdocs.org/sdr/U2RA865FLP3376), Sep 19, 2009: SKIN. CRACKED. FOUND 2 EACH CRACKS IN FUSELAGE SKIN APPROX AT STA 1760 LT SIDE MID POINT VERTICALLY. ONE CRACK APPROX 2 INCHES LONG BETWEEN L13L AND L14L AND ONE CRACK APPROX - [SDR U2RA865FLP3371](https://openairdocs.org/sdr/U2RA865FLP3371), Sep 13, 2009: SKIN. DAMAGED. FUSELAGE DAMAGED BY FORKLIFT BETWEEN LONGERON 26 AND 27 AT STA 370. REPAIRED IAW DWG 53-09382-1. - [SDR 22AA20090505](https://openairdocs.org/sdr/22AA20090505), May 9, 2009: SPAR. CRACKED. ON PRE FLIGHT FOUND FUEL LEAK BY LEFT WING ROOT FORWARD OF WHEEL WELL. UPON FURTHER INVESTIGATION THE LEFT REAR SPAR WAS FOUND CRACKED. - [SDR 22AA20081203](https://openairdocs.org/sdr/22AA20081203), Dec 31, 2008: BLEED VALVE. STUCK. LOG PAGE NR 128276. NR 1 ENGINE WOULD NOT ACCELERATE TO TAKE-OFF POWER; REJECTED TAKE OFF AT 80 KTS. - RETURNED TO GATE. FOUND NR 1 COMPRESSOR BLEED VALVE STUCK - [SDR 22AA20081102](https://openairdocs.org/sdr/22AA20081102), Dec 1, 2008: CONTROL CABLE. BROKEN. ON DESCENT LONG TRIM SUITCASE HANDLE, RIGHT SUITCASE HANDLE JAMMED. FOUND BROKEN CABLE RUNNING NR 49B. REMOVED AND REPLACED 1/16 CONTROL CABLE RUNNING NR 49B IN - [SDR 22AA20081002](https://openairdocs.org/sdr/22AA20081002), Oct 15, 2008: CYLINDER. MALFUNCTIONED. ON APPROACH INTO MROC THE FLAPS WOULD NOT EXTEND BEHOND 23 DEGREES. FOUND OUTBOARD FLAP LOCKOUT CYLINDER RETRACTED; SERVICE FLAP LOCKOUT CYLINDERS IAW MM 27-51- - [SDR ARWA20080802](https://openairdocs.org/sdr/ARWA20080802), Aug 14, 2008: UNKNOWN. SPARKS. AIR TURNBACK REPORTED SPARKS COMING FROM RT MAIN GEAR. DECLARED EMERGENCY AND RETURNED TO MIA. (S) - [SDR ARWA20080707](https://openairdocs.org/sdr/ARWA20080707), Jul 31, 2008: FUEL CONTROL. MALFUNCTIONED. ENG NR 1 FAILED TO ACCELERATE BEYOND GROUND IDLE. REMOVED AND REPLACED FUEL CONTROL UNIT AT NR 1 ENG IAW DC8 MM 73-20-1. PERFORMED ENG RUN UP IAW DC8 MM 77-00. - [SDR ARWA20080705](https://openairdocs.org/sdr/ARWA20080705), Jul 24, 2008: GYRO. MALFUNCTIONED. NR 2 COMPASS PROCESSES 10 DEGREES. REMOVED AND REPLACED NR 2 DIRECTIONAL GYRO IN ACCORDANCE WITH DC8 M/M 34-21-1; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH DC - [SDR 865FLP2936](https://openairdocs.org/sdr/865FLP2936), Mar 28, 2008: COMPRESSOR. STALLED. NR 1 ENGINE COMPRESSOR STALLED AT 1000 FT AND WAS SECURED. ENGINE WAS RELIT PRIOR TO LANDING. ENGINE POWER ASSURANCE RUN ON GROUND DETECTED NO DISCREPANCIES. - [SDR ARWA20080304](https://openairdocs.org/sdr/ARWA20080304), Mar 23, 2008: COMPASS. INOPERATIVE. FIRST OFFICER'S COMPASS INOPERATIVE. REMOVED AND REPLACED DIRECTIONAL GYRO NR 2 (DG-2) IN ACCORDANCE WITH M/M 34-21-1 AND RADIO DIRECTION INDICATOR NR 2 (RDI NR - [SDR ARWA20080201](https://openairdocs.org/sdr/ARWA20080201), Feb 3, 2008: LIMIT SWITCH. MALFUNCTIONED. DURING TAKEOFF ROLL, TAKEOFF WARNING HORN CAME ON. REMOVED AND REPLACED SI-278 FLAP UPLIMIT SWITCH IN ACCORDANCE WITH M/N 27-52-1 AND SI-177 AND 176 SPOILERS SW - [SDR IXXA08SMN020S](https://openairdocs.org/sdr/IXXA08SMN020S), Jan 19, 2008: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP LOWER SURFACE HAS IMPROPER REPAIR AT STATION XW 59.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAI - [SDR ARWA20071205](https://openairdocs.org/sdr/ARWA20071205), Dec 18, 2007: SNAP RING. LOOSE. DURING CLIMB-OUT, UNABLE TO CONTROL THE CABIN PRESSURIZATION, NEITHER WITH AUTO OR MANUAL (WITH 4 T.C. ON). FOUND NR 2 TC DISFUSER SNAP RING LOOSE. REINSTALLED - [SDR N921RM81664](https://openairdocs.org/sdr/N921RM81664), Oct 26, 2007: SKIN. CRACKED. "D" PIT DOOR DAMAGED FORWARD UPPER SKIN AT CORNER. APPROX .375 INCH CRACK RADIATED FROM EDGE OF FUSELAGE SKIN IN DOOR RADIUS AND TERMINATED AT FIRST FASTENER. - [SDR ARWA20070901](https://openairdocs.org/sdr/ARWA20070901), Sep 23, 2007: ENGINE. POWER LOSS. ABORT TAKEOFF DUE TO NR 1 ENGINE UNABLE TO MAKE MAXIMUM TAKEOFF POWER EPR I-68 AT FIREWALL. ABORTED PRIOR REACHING 80 KNOTS. OPERATIONAL CHECKED NR 1 ENGINE AT - [SDR ARWA20070802](https://openairdocs.org/sdr/ARWA20070802), Aug 18, 2007: INDICATOR. MALFUNCTIONED. POWER REDUCTION REQUIRED ON NR 2 ENGINE AFTER TAKEOFF IN ORDER TO MAINTAIN EGT LIMIT. 09-04-07 REMOVED AND REPLACED NR 2 EGT INDICATOR IN ACCORDANCE WITH MM 77- - [SDR ABXA070265](https://openairdocs.org/sdr/ABXA070265), Aug 2, 2007: HINGE PIN. SHEARED. DURING MAINTENANCE ON WO 600267980, UPPER FORWARD CARGO DOOR FORWARD HINGE PIN WAS SHEARED. REMOVED AND REPLACED FORWARD HINGE PIN IAW DC8 AMM 20-10-0. - [SDR ARWA20070703](https://openairdocs.org/sdr/ARWA20070703), Jul 10, 2007: BLEED VALVE. MALFUNCTIONED. ABORTED TAKE-OFF AT 118 KTS, UNABLE TO MAINTAIN TAKEOFF POWER WITHOUT EXCEEDING NR 3 ENGINE EGT LIMIT. REMOVED NR 3 ENGINE SURGE VALVE IN ACCORDANCE WITH M/M 75 - [SDR ARWA20070702](https://openairdocs.org/sdr/ARWA20070702), Jul 5, 2007: BRAKE ASSY. DAMAGED. WHILE TAXING TO RAMP, AFTER LANDING, BRAKES LOCKED UP. NR 5 BRAKE ASSEMBLY LOCKED UP ON TAXI WAY. REMOVED AND REPLACED NR 5 ANTI-SKID WHEEL SPEED TRANSDUCER IAW - [SDR ARWA20070701](https://openairdocs.org/sdr/ARWA20070701), Jul 4, 2007: BRAKE ASSY. LOCKED. AFTER LANDING, ON TAXI TO RAMP, BRAKES "LOCKED UP". REMOVED AND REPLACED BRAKE ASSEMBLY NR 2 IN ACCORDANCE WITH DC-8 M/M 32-42-1. OPERATIONAL CHECK FOR LEAKS OK - [SDR ARWA20070607](https://openairdocs.org/sdr/ARWA20070607), Jun 17, 2007: CONTROL UNIT. UNKNOWN. L/F I/B ANTI-SKID LIGHT ILLUMINATED. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT IN ACCORDANCE WITH M/M 32-43-1; CHECK GOOD IN ACCORDANCE WITH M/M 32-43-0. - [SDR ARWA20070611](https://openairdocs.org/sdr/ARWA20070611), Jun 15, 2007: ACCESS DOOR. CRACKED. DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; RT WING UPPER SURFACE MAIN FUEL TANK ACC DOOR NR 505C WT OUT WITH 02 CRACKS. REPAIR ACC DOOR NR 505C OF RT - [SDR ARWA20070610](https://openairdocs.org/sdr/ARWA20070610), Jun 15, 2007: ACCESS DOOR. CRACKED. DURING "C" CHECK INSPECTIONS, THE FOLLOWING WAS FOUND; RT WING UPPER SURFACE MAIN FUEL TANK ACCESS DOOR NR 505E CUT OUT WITH CRACK. REPAIRED RT WING UPPER SURFA - [SDR ARWA20070609](https://openairdocs.org/sdr/ARWA20070609), Jun 15, 2007: SKIN. CORRODED. DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STATION 260 L-21L SKIN WITH CORROSION. REPAIRED FUSELAGE EXTERIOR SKIN ATW FS 200 AND FS - [SDR ARWA20070608](https://openairdocs.org/sdr/ARWA20070608), Jun 15, 2007: SKIN. DENTED. DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND LT HORIZONTAL STABILIZER XH 285.00 L/E LOWER SURFACE WITH DENT. REPAIRED L/E PLATING OF LT HORIZONTAL STABI - [SDR ARWA20070606](https://openairdocs.org/sdr/ARWA20070606), Jun 13, 2007: TRANSDUCER. INOPERATIVE. PRIOR TO TAKEOFF ANTI-SKID INOPERATIVE LIGHT REMAINED ILLUMINATED; RETURN TO BLOCK. REMOVED AND REPLACED NR 8 MAIN LANDING GEAR WHEEL SPEED TRANSDUCER IN ACCORD - [SDR ABXA070184](https://openairdocs.org/sdr/ABXA070184), Jun 12, 2007: BATTERY. DISCHARGED. EMERGENCY EXIT LIGHT BATTERY PACK DEAD UNABLE TO CHANGE. REMOVED AND REPLACED EMERGENCY LIGHT PACK ASSEMBLY IAW DC8 AMM 33-50-01. - [SDR ARWA20070604](https://openairdocs.org/sdr/ARWA20070604), Jun 7, 2007: UNKNOWN. UNKNOWN. BEFORE TAKEOFF ANTI-SKID INOPERATIVE LIGHT PLUS RAI (F/W) LIGHTS BOTH ILLUMINATED. - [SDR ARWA20070602](https://openairdocs.org/sdr/ARWA20070602), Jun 5, 2007: BYPASS VALVE. BROKEN. AILERON MANUAL REVERSER LIGHT STAYS ON WHILE AILERON IS POWERED AND CONTROL CHECK UNSATISFACTORY. REMOVED AND REPLACED BROKEN BYPASS VALVE TURNBUCKLE AND ADJUST - [SDR N865F1480010](https://openairdocs.org/sdr/N865F1480010), Apr 30, 2007: PANEL. CORRODED. COCKPIT SUBFLOOR PRESSURE PANEL EXISTING REPAIR WITH CORROSION STA -17.00 LBL 50". - [SDR N865F1479009](https://openairdocs.org/sdr/N865F1479009), Apr 30, 2007: STRINGER. CORRODED. COCKPIT SUB FLOOR STRINGER DOUBLER WITH CORROSION AT STA -117.00 CPCP 455R 0552. - [SDR ABXA070149](https://openairdocs.org/sdr/ABXA070149), Apr 30, 2007: TRANSMITTER. DEFECTIVE. DURING CRUISE NR 2 ENGINE OIL PRESSURE WENT TO OFF SCALE LOW MOMENTARILY AND RECOVERED. FIFTEEN MINUTES LATER, AGAIN OFF SCALE LOW AND STAYED. SECURED NR 2 ENGI - [SDR ABXA070107](https://openairdocs.org/sdr/ABXA070107), Apr 17, 2007: TRANSMITTER. DEFECTIVE. AT TOP OF CLIMB, NR 1 ENGINE OIL PRESSURE STARTED DROPPING OFF INTO CAUTIONARY RANGE. RAN ABNORMAL CHECK LIST, REDUCED POWER TO IDLE. OIL PRESSURE DROPPED BELOW - [SDR N865F1134011](https://openairdocs.org/sdr/N865F1134011), Mar 26, 2007: UNKNOWN. CORRODED. FOUND COCKPIT SUBFLOOR WITH CORROSION AT STA.-67.00 L21L CPCP455L 0552. - [SDR N865R1125006](https://openairdocs.org/sdr/N865R1125006), Mar 26, 2007: UNKNOWN. CORRODED. COCKPIT SUBFLOOR INNER AREA WITH CORROSION AT STA 67 L-21R CPCP 455R 0552. - [SDR N865R1124005](https://openairdocs.org/sdr/N865R1124005), Mar 26, 2007: ANGLE. CORRODED. COCKPIT SUBFLOOR ANGLE WITH CORROSION AT STA 32.000 L-21R CPCP455R 0552. - [SDR N865R1076007](https://openairdocs.org/sdr/N865R1076007), Mar 23, 2007: ACCESS DOOR. CORRODED. LT WING XFS 836 OUTBD L/E INNER LOWER SECTION ACCESS DOOR NR 517B JAMB WITH CORROSION CPCP 107L 0552. - [SDR ARWA20070306](https://openairdocs.org/sdr/ARWA20070306), Mar 22, 2007: HOSE. LEAKING. IN FLIGHT EN COUNTER A LOSS OF HYDRAULIC PRESSURE; PERFORMED EMERGENCY CHECKLIST. T/S AND FOUND RT MAIN LANDING GEAR BOGIE TRIM CYLINDER HYDRAULIC HOSE LEAKING; - [SDR N865F753008](https://openairdocs.org/sdr/N865F753008), Mar 19, 2007: SKIN. CORRODED. RUDDER ZR 168.656 LT EXTERNAL SKIN WITH CORROSION CPCP 6820 0551. - [SDR N865R623002](https://openairdocs.org/sdr/N865R623002), Mar 15, 2007: BULKHEAD. CRACKED. AFT FLAT PRESSURE BULKHEAD WEB STA 1766 L11L CRACK CPCP 5730 0551. - [SDR ABXA070072](https://openairdocs.org/sdr/ABXA070072), Mar 15, 2007: WIRE. DAMAGED. DURING SERVICE CHECK FOUND ELECTRICAL ODOR COMING FROM OVERHEAD LIGHT. FOUND ONE FLUORESCENT LIGHT RECEPTACLE CORRODED AT TERMINAL ENDS AND SHORTING. CLEANED RE - [SDR N865F624003](https://openairdocs.org/sdr/N865F624003), Mar 13, 2007: BULKHEAD. CRACKED. AFT FLAT PRESSURE BULKHEAD WEB STA 1766 L-11R-12R CRACK CPCP 5730 0551. - [SDR ABXA070069](https://openairdocs.org/sdr/ABXA070069), Mar 13, 2007: WIRE. CHAFED. ACRID ODOR OF ELECTRICAL SMOKE BY ALL 3 CREW MEMBERS, SOURCE NOT IDENTIFIED. ODOR COMES AND GOES. FOUND LOAD CALCULATOR WIRES CHAFING ON PANEL. ROUTED PANEL ARE All 1,883: https://openairdocs.org/model/douglas-dc-8-63f/reports.md ## STCs that may be installed (OpenAirDocs) (189, 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 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 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 SA2616WE](https://openairdocs.org/stc/SA2616WE): Installation of Trans Com Model 1144 movie projector, screen assemblies and sound system. Burrana Inc - [STC SA3421NM](https://openairdocs.org/stc/SA3421NM): Installation of Hughes-Avicom video entertainment system. Burrana Inc. Lists DC-8 Series - [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 SA2582WE](https://openairdocs.org/stc/SA2582WE): Installation of Litton Systems, Inc. LTN-72 Inertial Navigation System installed in the number two position and two LTN-51inertial navigation systems. Northrop Grumman Systems Corporation - [STC SA2634WE](https://openairdocs.org/stc/SA2634WE): Installation of three Litton 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 SA630CE](https://openairdocs.org/stc/SA630CE): Installation of cargo pallets. Telair US 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 ST00670CH](https://openairdocs.org/stc/ST00670CH): Installation of single or dual II Morrow, Apollo 2101/2102 GPS Navigation Management Computer Systems. ABX Air Incorporated - [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 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 SA2318SO](https://openairdocs.org/stc/SA2318SO): Installation of the door warning system. 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 SA2320SO](https://openairdocs.org/stc/SA2320SO): Installation of the Fairchild F-800 digital flight data recorder system. 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 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 SA2827WE-D](https://openairdocs.org/stc/SA2827WE-D): Installation of Collins FPC-75 part number 622-2615-012 or 622-2615-212 Ground Proximity Warning System Computer in conformance with United Airlines DAS-1-WE Approved Master List of drawings and documents for STC No. SA2827WE-D dated February 26, 1979 or later approved revisions. An alternate approved configuration consists of part number 622-2615-011 Rev. N or part number 622-2615-211 GPWS computer and a part number 622-2668-011 Barometric Altitude Computer installed in conformance with DAS-1-WE Approved Master List of drawings and related documents or later FAA approved revision (Continued on page 3.). United Airlines Inc - [STC 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 ST00746LA-D](https://openairdocs.org/stc/ST00746LA-D): Installation of smoke detection system, lower cargo compartment. Ontic Engineering and Manufacturing Inc All 189: https://openairdocs.org/model/douglas-dc-8-63f/stcs.md ## PMA parts (OpenAirDocs) (over 1,000, first 50) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first. - [AF300P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191275281320260717175324.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026 - [AF302](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178154048320260717175326.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026 - [AF300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172513122320260717175322.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026 - [M840105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154219509420260325172403.0001): Cylinder Assembly. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 840105 · Feb 17, 2026 - [M840105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140279722720260325180521.0001): Cylinder Assembly. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 840105 · Feb 17, 2026 - [WF334995](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108821019820250602133022.0001): Filter Element Lube Oil. Donaldson Company Inc · PMA PQ2432CE · Replaces Sundstrand 55956, AC-9649F-1… · May 23, 2025 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192694002020250923105634.0001): VOGT AERO · PMA PQ05310NM · Apr 22, 2025 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165781403520250923105628.0001): VOGT AERO · PMA PQ05310NM · Apr 22, 2025 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178263063620250923105931.0001): VOGT AERO · PMA PQ05310NM · Mar 4, 2025 - [3575-1251-07-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172611889620260729202728.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1251-07 · Mar 4, 2025 - [3575-1480-01-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170852615820260729202754.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1480-01 · Mar 4, 2025 - [3575-1251-01-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169467633820260729202723.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1251-01 · Mar 4, 2025 - [440-0150-5-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128051330520260729202746.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 440-0150-5 · Mar 4, 2025 - [3575-1480-07-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122566397220260729202800.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1480-07 · Mar 4, 2025 - [440-0150-3-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106234740920260729202739.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 440-0150-3 · Mar 4, 2025 - [DEC31-027-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146178353220250304142404.0001): Shaft Drive Fuel Pump. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces Airesearch P/N 3603685-1 · Feb 27, 2025 - [103154-909-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118409506520230727204617.0001): Safety Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 103154-909-2 · Apr 20, 2023 - [122618-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156194142520230907183534.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 122618-1-1 · Feb 24, 2023 - [320362-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152527095020230907183533.0001): Solenoid Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 320362-2 · Feb 24, 2023 - [383342-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133028187220230907183536.0001): Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 383342-1-1 · Feb 24, 2023 - [105984-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119902323020230907183537.0001): Anti-Ice Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105984-2 · Feb 24, 2023 - [392900-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189455606920230907183331.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 392900-1-1 · Feb 23, 2023 - [398018-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163636197720230907183315.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 398018-1-1 · Feb 23, 2023 - [108742-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159430638720230907183327.0001): Pressure Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 108742-2 · Feb 23, 2023 - [105976-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152035340520230907183326.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105976-1 · Feb 23, 2023 - [122594-3-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147106652220230907183318.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 122594-3-1 · Feb 23, 2023 - [122546-2-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145869651920230907183329.0001): Pressure Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 122546-2-1 · Feb 23, 2023 - [105980-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140197898520230907183328.0001): Butterfly Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105980-2 · Feb 23, 2023 - [105982-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110550695020230907183313.0001): Pneumatic Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105982-2 · Feb 23, 2023 - [525254-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108708698020230907183333.0001): Actuator Assy Fuel Dump Chute. Honeywell International Inc. · PMA PQ1222NM · Replaces 525254-1 · Feb 23, 2023 - [392160-4-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108409609920230907183330.0001): Pressure Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 392160-4-1 · Feb 23, 2023 - [SM600BA100N22-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189709749720221130144515.0001): Remote Control Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces BAN7016-607 · Oct 31, 2022 - [160-066-80](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185108580520221130144357.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0012-80 · Oct 31, 2022 - [1526-066-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166131476020221130144341.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0002-3 · Oct 31, 2022 - [1200-066-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164799404820221130144328.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0009-15 · Oct 31, 2022 - [H20-9B](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139073107020221130144509.0001): Switch. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces H20-9B · Oct 31, 2022 - [SM600BA20N25](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123850243020221130144521.0001): Remote Control Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces SM600BA20N25 · Oct 31, 2022 - [160-083-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123725710320221130144400.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0012-70P · Oct 31, 2022 - [1200-066-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115243180520221130144326.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0009-10 · Oct 31, 2022 - [3755705-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192798688420220929114601.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3755705-1 · Sep 27, 2022 - [3718232-504](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188697278020220929114502.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-504 · Sep 27, 2022 - [3718232-503](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188413757320220929114501.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-503 · Sep 27, 2022 - [3718232-505](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183899181420220929114502.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-505 · Sep 27, 2022 - [3718232-516](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181531934020220929114509.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-516 · Sep 27, 2022 - [3889142-510](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180513779620220929113517.0001): PANEL A. AmSafe Bridport · PMA PQ2482NM · Replaces 3889142-510 · Sep 27, 2022 - [3889142-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179267638820220929113509.0001): PANEL A. AmSafe Bridport · PMA PQ2482NM · Replaces 3889142-1 · Sep 27, 2022 - [3718232-511](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178457873520220929114507.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-511 · Sep 27, 2022 - [3718231-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168988236720220929113547.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718231-1 · Sep 27, 2022 - [3755704-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162454280820220929114510.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3755704-1 · Sep 27, 2022 - [3889142-502](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161896863520220929113512.0001): PANEL A. AmSafe Bridport · PMA PQ2482NM · Replaces 3889142-502 · Sep 27, 2022 All of them: https://openairdocs.org/model/douglas-dc-8-63f/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Mcdonnell Douglas DC-8-63F](https://openairdocs.org/model/mcdonnell-douglas-dc-8-63f): 1 registered aircraft, registry code 302198H --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.