# Mcdonnell Douglas DC-8-71

- Type: Aircraft model (FAA registry)
- Registry code: 302199A
- Manufacturer (registry): MCDONNELL DOUGLAS
- Model: DC-8-71
- 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/mcdonnell-douglas-dc-8-71

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 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 2002-16-01](https://openairdocs.org/ad/2002-16-01): Main cargo door area · Forward cargo door (Aeronautical Engineers STC SA1063SO or 2 others). Effective Aug 22, 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 2001-24-34](https://openairdocs.org/ad/2001-24-34): Generator Power Feeder Cables, Supporting Brackets, and Clamps at all the Engine Pylons · Boeing DC-8-71, DC-8-72 and DC-8-73. Effective Jan 16, 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

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 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 146: https://openairdocs.org/model/mcdonnell-douglas-dc-8-71/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 (3)

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 20010610011369I](https://openairdocs.org/incident/20010610011369I), Jun 10, 2001: Doug DC871 (N811AL), Pittsburgh, PA. (-23)On June 10, 2001, a DC-8-71, s/n 46099, registered as N811AL, and operating as rrxa flight 1321, was enroute from "ewr" to "ind" when the #1 engine fire…
- [Incident 19920106001249I](https://openairdocs.org/incident/19920106001249I), Jan 6, 1992: Doug DC871 (N744UP), Des Moines, IA. Lost hydraulic pressure en route. Landed safely at destination. Replaced NR2 engine hydraulic pump case drain line.
- [Incident 19890213022899I](https://openairdocs.org/incident/19890213022899I), Feb 13, 1989: Doug DC871 (N744UP), Dallas-Ft Worth, TX. Lost hydraulic pressure. Aileron and rudder control light came on. Found reservoir head pressure valve open.

## Service difficulty reports (341, newest 50)

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

- [SDR ASMF 20081204](https://openairdocs.org/sdr/ASMF%2020081204), Dec 21, 2008: LINE. LEAKING. DURING TRANSIT CHECK, A HYD LEAK ON THE LT WHEEL WELL LANDING GEAR WAS DETECTED. MX REPLACED AND TESTED THE HYDRAULIC LINE IAW AMM 20-50-00, ALL CORRECT.
- [SDR UPS06847672](https://openairdocs.org/sdr/UPS06847672), Aug 11, 2006: LAMP. INOPERATIVE. EMERGENCY EXIT LIGHT, DISARM CHECK LIGHT INTERMITTENT INOP. RELAMPED EMERGENCY EXIT LIGHT PER M/M 33-10-00. OPS CHECK GOOD.
- [SDR UPS06847532](https://openairdocs.org/sdr/UPS06847532), Jul 28, 2006: SLIDE. UNWANTED DEPLOY. L1 DOOR SLIDE INOP. ENTERED DEFERRAL M330219. INSTALLED EVACUATION SLIDE IN L-1 DOOR PER AMM 25-60-01-2. OPS CHECK OK. THIS CLEARS DEFERRAL.
- [SDR UPS05845053](https://openairdocs.org/sdr/UPS05845053), Aug 4, 2005: BATTERY. MALFUNCTIONED. EMERG EXIT LIGHTS ARE SLOW TO DISARM WHEN ACTIVATED. REMOVED AND REPLACED EMERG BATTERY AND RELAY UNIT SYS OPS CHECK NORMAL PER MM 33-50-01-2 PARA 2,4 & 5.
- [SDR UPS05843866](https://openairdocs.org/sdr/UPS05843866), Feb 1, 2005: FRAME. CORRODED. FRAME AND SPLICE CORRODED BEYOND LIMITS AT STA 1420 L34R-L36. REMOVED SPLICE FTG AND CUT OUT CORRODED FRAME SECTION BETWEEN L36 AND L34R. FAB REPLACMENT SPLICE 
- [SDR IXXA0500001O](https://openairdocs.org/sdr/IXXA0500001O), Jan 13, 2005: TRANSCEIVER. INOPERATIVE. DURING CLIMBOUT FROM KIAH THE WEATHER RADAR WOULD NOT COME OUT OF TEST PATTERN WITH FAIL LIGHT ON. CREW RETURNED TO KIAH AND LANDED WITHOUT INCIDENT. MAINTENANC
- [SDR UPS04843546](https://openairdocs.org/sdr/UPS04843546), Nov 18, 2004: RIB. CRACKED. C3 RT WING CENTER L/E RIB CRACKED AT AFT END, STA XFS347. STOP DRILLED CRACK, NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6 .
- [SDR UPS04841888](https://openairdocs.org/sdr/UPS04841888), Feb 1, 2004: RIB. CRACKED. INSPECTION TYPE: C3, RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 847.5, XFS 791.25. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILL TERMINATES CRACKS, FABRICATED AN
- [SDR IXXA0400005O](https://openairdocs.org/sdr/IXXA0400005O), Jan 12, 2004: CURTAIN. UNSECURE. DURING TAKEOFF AND UPON GEAR RETRACTION, A NOISE WAS HEARD FROM NOSE GEAR AREA. CREW RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED GEAR DOOR BRACK
- [SDR IXXA0300075O](https://openairdocs.org/sdr/IXXA0300075O), Nov 15, 2003: ODOR. DETECTED. DURING CRUISE AN ELECTRICAL ODOR WAS IN THE CEILING AREA OF THE FLT STATION DOOR AND COURIER COMPARTMENT. CREW TURNED OFF THE CIRCUIT BREAKER LIGHT SWITCH ON TH
- [SDR IXXA060562S](https://openairdocs.org/sdr/IXXA060562S), Sep 22, 2003: RIB. CRACKED. DURING ROUTINE C CHECK, FOUND RIGHT WING CENTER LEADING EDGE LOWER SURFACE RIB CRACKED AT STATION 341. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRI
- [SDR IXXA0300008O](https://openairdocs.org/sdr/IXXA0300008O), Jan 28, 2003: CONNECTOR. DIRTY. AFTER DEPARTURE FROM LRD DURING CRUISE CREW NOTED NR 3 ENGINE EGT ROSE ABNORMALLY. CREW SHUTDOWN NR 3 ENG PER COMPANY POLICY. AIRCRAFT RETURNED TO LRD FOR AN UN
- [SDR IXXA0200159O](https://openairdocs.org/sdr/IXXA0200159O), Dec 3, 2002: WING. CRACKED. AFTER LANDING AT SEA THE FLIGHT CREW NOTICED A SLOW FUEL LEAK COMING FROM THE #1 PYLON INBOARD SIDE. MAINTENANCE INSPECTED THE AIRCRAFT AND CATORGIZED IT AS A S
- [SDR IXXA0200027O](https://openairdocs.org/sdr/IXXA0200027O), May 22, 2002: STATOR VANE. MALFUNCTIONED. AFTER TAKEOFF FROM TOL, THE FLIGHT CREW EXPERIENCED A WINDSHEAR WARNING ALERT. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND THE NUMBER THREE ENGINE EXCEEDED 
- [SDR IXXA0200018O](https://openairdocs.org/sdr/IXXA0200018O), Apr 18, 2002: COWLING. DAMAGED. DURING A ROUTINE MAINTENANCE PREFLIGHT IN TER, MINOR EVIDENCE OF DAMAGE TO #1 ENGINE OUTBOARD COWLING. MAINTENANCE INSPECTED THE ENGINE IN ACCORDANCE WITH AN AP
- [SDR IXXA0200025O](https://openairdocs.org/sdr/IXXA0200025O), Apr 17, 2002: PUMP. LEAKING. EN ROUTE FROM SEA TO ANC, THE FLT CREW NOTICED A DECLINE IN THE MAIN HYD SYS QUANTITY. THE FLT CREW NOTICED WHILE FOLLOWING COMPANY PROCEDURES THE HORIZONTAL ST
- [SDR IXXA0200015O](https://openairdocs.org/sdr/IXXA0200015O), Apr 16, 2002: WARNING LIGHT. ILLUMINATED. AFTER TAKE OFF FROM ANC, THE LANDING GEAR UPLATCH CHECK FAILED AND THE LANDING GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR BUT THE WARNING INDICATIO
- [SDR IXXA0200014O](https://openairdocs.org/sdr/IXXA0200014O), Apr 15, 2002: BRACKET. LOOSE. AFTER TAKE OFF FROM ANC, THE LANDING GEAR UPLATCH CHECK FAILED AND THE LANDING GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR SEVERAL TIMES BEFORE THE 
- [SDR IXXA0100076O](https://openairdocs.org/sdr/IXXA0100076O), Dec 12, 2001: ENGINE. LEAKING. EN ROUTE FROM JFK TO BDL. WHEN LEFT AIR CONDITION PACK WAS TURNED ON SMOKE WAS EMITTING FROM THE VENTS. THE FLIGHT CREW SECURED THE PACK AND THE SMOKE SUBSIDED.
- [SDR UPS01836770](https://openairdocs.org/sdr/UPS01836770), Sep 6, 2001: GENERATOR. SMOKE. DURING TAXI OUT NR 2 BUS POWER FAIL LIGHT ILLUMINATED NR 2 GEN UNPAR'LD LIGHT ILLUMINATED AND LEFT EMERG AC BUS POWER FAIL LIGHT ILLUMINATED ATTEMPTED TO PERFOR
- [SDR UPS01836725](https://openairdocs.org/sdr/UPS01836725), Aug 28, 2001: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHTS CIRCUIT BREAKER OPENED IN FLIGHT. PERFORMED EMERGENCY LIGHT BATTERY TEST PER MM REF 33-50-01 EMERGENCY LIGHTING CHECKS GOOD
- [SDR RRXA010055](https://openairdocs.org/sdr/RRXA010055), Jun 27, 2001: WARNING SYSTEM. ACTIVATED. JUST PRIOR TO STARTING APPROACH EXPERIENCE FIRE WARNING ON NR 1 ENGINE FOLLOWED QRH. SHUT DOWN ENGINE AND BOTH BOTTLES FIRED. REPAIRED DAMAGED WIRING AT P10-700
- [SDR RRXA011047](https://openairdocs.org/sdr/RRXA011047), Jun 13, 2001: ELEMENT. FAULTY. INTERMITTENT FIRE INDICATION ON NR 1 ENG FIRED BOTH BOTTLES AND SHUT DOWN ENG FIRE INDICATIONS STILL WERE INTERMITTENT. WHEN FIRE LIGHT IN HANDLE INTERMITTENT W
- [SDR RRXA010008](https://openairdocs.org/sdr/RRXA010008), Feb 6, 2001: TIRE. FAILED. RIGHT MAIN GEAR TIRES BLEW ON LANDING. REMOVED AND REPLACED RT MLG WHEEL AND TIRE ASSYS IAW M/M 32-40-1 (TIRE POSITIONS 4, 5, 7, 8).
- [SDR RRXA001084](https://openairdocs.org/sdr/RRXA001084), Dec 6, 2000: LANDING GEAR. VIBRATION. AFTER RETRACTION OF GEAR LOUD NOISE AND VIBRATION FROM NOSE GEAR AREA CYCLED GEAR NO NOISE WHEN EXTENDED. JACKED AIRCRAFT IAW DC-8 M/M CH 7-11-0 PERFORMED GEAR 
- [SDR RRXA001080](https://openairdocs.org/sdr/RRXA001080), Nov 8, 2000: FIRE LOOP. MALFUNCTIONED. AT TOP WHEN RETARDED THROTTLES #3 ENG HAD STEADY FIRE WARNING (BELL & LIGHT) SHUT DOWN ENG. AFTER SHUT DOWN AND DISCHARGING AGENT, FIRE WARNING CONTINUED. ***CO
- [SDR RRXA001064](https://openairdocs.org/sdr/RRXA001064), Oct 10, 2000: WARNING SYSTEM. MALFUNCTIONED. REJECTED T/O DUE TO NO ELEVATOR CHECK, ASKED FOR FREIGHT REWEIGH (120 KNOTS). PERFORMED REJECTED T/O INSPECTION IAW EWA WORK CARD SP001. NO DEFECTS NOTED. INSPE
- [SDR RRXA003051](https://openairdocs.org/sdr/RRXA003051), Sep 15, 2000: TRUNNION. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK AND CORROSION DAMAGE TO THE NOSE W/W RT. TUNNEL NOSE GEAR TRUNNION ATTACH FITTING AT STA X=+20, Y=-12 Z=-25, DAMAGE EXC
- [SDR RRXA003053](https://openairdocs.org/sdr/RRXA003053), Sep 8, 2000: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND BROKEN OFF SCREWS AND CORROSION DAMAGE TO THE SEAT TRACK FLANGE AT STA Y=70-280 & X=+60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S
- [SDR RRXA003766](https://openairdocs.org/sdr/RRXA003766), Sep 6, 2000: DOUBLER. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT SURFACE REAR SPAR LWR CAP AT STA XRS -578, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIV
- [SDR RRXA003055](https://openairdocs.org/sdr/RRXA003055), Sep 6, 2000: SPLICE. CRACKED. DURING A MAINTENANCE VISIT FOUND A 1/2 INCH CRACK LEADING FROM FASTENER HOLE ON THE THROUGH ACCESS HOLE 506A AT STA XW 408 AND XW 393 NR 8 UPPER STRINGER SPLICE
- [SDR RRXA003054](https://openairdocs.org/sdr/RRXA003054), Sep 6, 2000: RETAINER. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACKED, BROKEN AND CORROSION DAMAGE TO THE MAIN CARGO DOR SEAL RETAINERS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRE
- [SDR RRXA003052](https://openairdocs.org/sdr/RRXA003052), Sep 6, 2000: PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE SUB-FLOOR PANEL AT STA 220-360 FROM RBL 45 TO RBL 49, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////COR
- [SDR RRXA002983](https://openairdocs.org/sdr/RRXA002983), Aug 31, 2000: PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE SUB FLOOR PANEL AT STA 80-220 AND LBL 25 - LBL 45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAM
- [SDR RRXA002982](https://openairdocs.org/sdr/RRXA002982), Aug 31, 2000: PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE SUB FLOOR PANEL FROM STA 220-360 AND RBL 25 - RBL 45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED 
- [SDR RRXA002991](https://openairdocs.org/sdr/RRXA002991), Aug 29, 2000: THRESHOLD. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACKED, BENT AND RIVET DRILLED OFF THE LT L3 DOOR SILL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002990](https://openairdocs.org/sdr/RRXA002990), Aug 29, 2000: FASTENER. DAMAGED. DURING A MAINTENANCE VISIT FOUND A PARTIAL HI-LOK DRILLED AT RT LWR WING I/B NR 4 PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002989](https://openairdocs.org/sdr/RRXA002989), Aug 29, 2000: BOSS. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MLG SHOCK STRUT ASSY RETRACT PIN BOSS WHICH MEANS MA-AI-3210-01:03 NEEDS TO BE C/W, DAMAGE EXCEEDED LIM
- [SDR RRXA002987](https://openairdocs.org/sdr/RRXA002987), Aug 29, 2000: ANGLE. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACKED TO THE CUSP KICK PLATE LT ANGLE AT STA 1560 - 1580, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002986](https://openairdocs.org/sdr/RRXA002986), Aug 29, 2000: SPAR. DAMAGED. DURING A MAINTENANCE VISIT FOUND 7 DEFORMED BOLT HOLES TO THE RT CENTER AUX TANK AFT LT INNER ACCESS HOLE UPPER REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 
- [SDR RRXA002985](https://openairdocs.org/sdr/RRXA002985), Aug 29, 2000: SPAR. DAMAGED. DURING A MAINTENANCE VISIT FOUND 4 DEFORMED BOLT HOLES TO THE LT CENTER AUX TANK AFT RT INNER ACCESS HOLE UPPER REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 
- [SDR RRXA002984](https://openairdocs.org/sdr/RRXA002984), Aug 29, 2000: THRESHOLD. DAMAGED. DURING A MAINTENANCE VISIT FOUND SEVERAL ELONGATED HOLES TO THE THRESHOLD ON THE B PIT DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002999](https://openairdocs.org/sdr/RRXA002999), Aug 28, 2000: DOOR. MISREPAIRED. DURING A MAINTENANCE VISIT FOUND A BAD REPAIR TO THE LT MAIN LANDING GEAR DOOR AFT LWR CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002998](https://openairdocs.org/sdr/RRXA002998), Aug 28, 2000: FRAME. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME UNDER PRESSURE DECK AT STA -99 AND LBL 60 BELOW L22L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002997](https://openairdocs.org/sdr/RRXA002997), Aug 28, 2000: PANEL. DAMAGED. DURING A MAINTENANCE VISIT FOUND A TORN CAMLOCK HOLE AT STA 683A, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002996](https://openairdocs.org/sdr/RRXA002996), Aug 28, 2000: SEAT TRACK. BROKEN. DURING A MAINTENANCE VISIT FOUND A BROKEN SEAT TRACK AT STA 680 AND RBL 25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002995](https://openairdocs.org/sdr/RRXA002995), Aug 28, 2000: SEAT TRACK. BROKEN. DURING A MAINTENANCE VISIT FOUND A BROKEN SEAT TRACK AT STA 1040 AND RBL 25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002994](https://openairdocs.org/sdr/RRXA002994), Aug 28, 2000: SEAT TRACK. BROKEN. DURING A MAINTENANCE VISIT FOUND A BROKEN SEAT TRACK AT STA 1450 AND RBL 25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002993](https://openairdocs.org/sdr/RRXA002993), Aug 28, 2000: LONGERON. CRACKED. DURING A MAINTENANCE VISIT FOUND A POSSIBLE CRACK TO THE LONGERON AT STA 857 AND L4R AFT SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002992](https://openairdocs.org/sdr/RRXA002992), Aug 28, 2000: SEAT TRACK. BROKEN. DURING A MAINTENANCE VISIT FOUND A BROKEN SEAT TRACK AT X=0 Y=1477 Z=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.

All 341: https://openairdocs.org/model/mcdonnell-douglas-dc-8-71/reports.md

## STCs that may be installed (OpenAirDocs) (151, 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 ST03450AT](https://openairdocs.org/stc/ST03450AT): Installation of a horse stall system. Gregory Jackson
- [STC SA3180NM](https://openairdocs.org/stc/SA3180NM): Installation of Spacelite 8 Interior Retrofit Kits. 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 ST00375AT](https://openairdocs.org/stc/ST00375AT): Installation of a CAS-81 TCAS II and a TRA-67 Mode S transponder. Honeywell International Inc
- [STC ST00761SE](https://openairdocs.org/stc/ST00761SE): Installation of the MK VII Enhanced Ground Proximity Warning System (EGPWS). 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 ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic LLC
- [STC ST01067LA](https://openairdocs.org/stc/ST01067LA): Installation of Litton LTR-97 fiber optic gyro systems. Northrop Grumman Systems Corporation
- [STC ST01668LA](https://openairdocs.org/stc/ST01668LA): Installation of a single LTN-2012 Global Positioning Sensor Unit (GPSU) and dual LTN-92 Inertial Reference System (INS). Northrop Grumman Systems Corporation
- [STC ST01467LA-D](https://openairdocs.org/stc/ST01467LA-D): Installation of Universal Avionics Terrain Avoidance Warning System and MFD-640 Multi Function Display(s). Zalinka Aviation Support, LLC
- [STC ST01468LA-D](https://openairdocs.org/stc/ST01468LA-D): Installation of Universal Avionics Flight Management System. Zalinka Aviation Support, LLC
- [STC SA1511GL](https://openairdocs.org/stc/SA1511GL): Installation of Type "C" containers. ABX Air Incorporated
- [STC SA1462GL](https://openairdocs.org/stc/SA1462GL): Installation of ABX Cargo Handling System. ABX Air Incorporated
- [STC SA3496NM](https://openairdocs.org/stc/SA3496NM): Installation of ABX-C Cargo Container assembly. Airborne Express Air Inc
- [STC SA7729SW](https://openairdocs.org/stc/SA7729SW): Installation of digital fuel quantity indicators, fuel totalizer, and capacitive fuel compensator units. Ontic Engineering and Manufacturing Inc
- [STC SA1926NW-D](https://openairdocs.org/stc/SA1926NW-D): Installation of a flight attendant seat at RH floor level exit door. United Airlines Inc
- [STC SA1933NW-D](https://openairdocs.org/stc/SA1933NW-D): Three video projectors and their associated wiring and controls are installed throughout the cabin. Video installation was done according to United Air Lines, DAS-1-WE, Approved Drawing List No.1933 dated May 25, 1983, or later FAA approved revisions. United Airlines Inc
- [STC SA1946NW-D](https://openairdocs.org/stc/SA1946NW-D): Dual class seat mix change - increase coach section capacity from 165 passengers to 174 passengers. Installation in accordance with United Air Lines, DAS-1-WE, Drawing List No. 1946 dated August 16, 1984, or later FAA approved revisions. United Airlines Inc
- [STC SA2713NM-D](https://openairdocs.org/stc/SA2713NM-D): Install emergency escape path lighting. United Airlines Inc
- [STC SA2741NM-D](https://openairdocs.org/stc/SA2741NM-D): Installation of a Bendix model DCA-80A data recorder and other passive equipment. 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 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 SA8011SW](https://openairdocs.org/stc/SA8011SW): Installation of Collins DLC-800 ACARS and number 3 VHF transceiver. United Parcel Service
- [STC ST00794AT](https://openairdocs.org/stc/ST00794AT): Increase in aircraft operating weights(max takeoff weight - 328,000 lbs., max landing weight - 258,000 lbs., max zero fuel weiht - 245,000 lbs.) (DC-8-71 SN 46099 only). Aircraft Modification Design Services
- [STC SA1063SO](https://openairdocs.org/stc/SA1063SO): Installation of forward cargo door. Aeronautical Engineers Inc
- [STC SA1377SO](https://openairdocs.org/stc/SA1377SO): Installation of a cargo interior. Aeronautical Engineers Inc
- [STC ST00746LA-D](https://openairdocs.org/stc/ST00746LA-D): Installation of smoke detection system, lower cargo compartment. Ontic Engineering and Manufacturing Inc
- [STC SA2082SO](https://openairdocs.org/stc/SA2082SO): Installation of fuselage window plugs. Kosola & Associates Inc
- [STC SA1123NW-D](https://openairdocs.org/stc/SA1123NW-D): Installation of an underwing fueling panel. United Air Lines Inc
- [STC SA2709NM-D](https://openairdocs.org/stc/SA2709NM-D): Installation of an Airfone Air-to-Ground Passenger Telephone System. United Air Lines Inc
- [STC SA2716NM-D](https://openairdocs.org/stc/SA2716NM-D): Installation of Bendix Model TRA-66A Mode S transponder. United Air Lines Inc
- [STC SA2717NM-D](https://openairdocs.org/stc/SA2717NM-D): Installation of TCAS and data recording provisions, consisting of equipment mounting trays, antenna systems and cables, circuit breakers, and complete system interwiring. United Air Lines Inc

All 151: https://openairdocs.org/model/mcdonnell-douglas-dc-8-71/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
- [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
- [AAP-358474-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127843643720240311212403.0001): Bearing. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N 358474-1 · Mar 6, 2024
- [AAP- 358991-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132389091720231010203037.0001): Bearing. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N 358991-1 · Sep 29, 2023
- [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
- [3202208-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193407306420240306163316.0001): Valve Check. Honeywell International Inc. · PMA PQ1222NM · Replaces 3202208-1 · Apr 14, 2023
- [123994-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172749283720240306163315.0001): Valve Check. Honeywell International Inc. · PMA PQ1222NM · Replaces 123994-1 · Apr 14, 2023
- [398444-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171059642320240306163315.0001): Valve Butterfly Mix. Honeywell International Inc. · PMA PQ1222NM · Replaces 398444-2 · Apr 14, 2023
- [123674-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166044694720240306163315.0001): Valve Check. Honeywell International Inc. · PMA PQ1222NM · Replaces 123674-1 · Apr 14, 2023
- [396420-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142749110120240306163315.0001): Valve Flow Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 396420-1 · Apr 14, 2023
- [3224714-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132434227720240306163316.0001): Valve Emergency Vent. Honeywell International Inc. · PMA PQ1222NM · Replaces 3224714-1 · Apr 14, 2023
- [321942-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113693947020240306163315.0001): Valve Shutoff. Honeywell International Inc. · PMA PQ1222NM · Replaces 321942-1 · Apr 14, 2023
- [8-782-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146241388520230321112327.0001): Percs Sensor. Eldec Corporation · PMA PQ0079NM · Replaces 8-782-01 · Mar 10, 2023
- [3224714-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179410552920230907183523.0001): Emergency Vent Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 3224714-2 · Feb 24, 2023
- [107464-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179340808820230907183516.0001): Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 107464-3 · Feb 24, 2023
- [108032-10-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178796345920230907183514.0001): Pressure Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 108032-10-1 · Feb 24, 2023
- [397892-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175214220920230907183528.0001): Valve S/O. Honeywell International Inc. · PMA PQ1222NM · Replaces 397892-1 · Feb 24, 2023
- [979908-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172000509320230907183532.0001): Precooler Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 979908-5 · Feb 24, 2023
- [3505154-20-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171420521520230907183529.0001): Air Turbine Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505154-20-1 · Feb 24, 2023
- [396420-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168908831420230907183519.0001): Valve Flow Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 396420-2 · Feb 24, 2023
- [121668-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168847377220230907183531.0001): Flexshaft. Honeywell International Inc. · PMA PQ1222NM · Replaces 121668-2 · Feb 24, 2023
- [3202160-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159982332020230907183527.0001): Valve Bleed Air. Honeywell International Inc. · PMA PQ1222NM · Replaces 3202160-1 · Feb 24, 2023
- [3214326-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153188892920230907183518.0001): Valve Bleed Air. Honeywell International Inc. · PMA PQ1222NM · Replaces 3214326-2 · 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
- [3505154-18](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149563448620230907183523.0001): Starter Air Turbine. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505154-18 · Feb 24, 2023
- [979904-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137143215420230907183520.0001): Valve Shutoff. Honeywell International Inc. · PMA PQ1222NM · Replaces 979904-1 · Feb 24, 2023
- [3505154-19](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136786638620230907183524.0001): Starter Air Turbine. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505154-19 · Feb 24, 2023
- [3505154-21](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134907274720230907183525.0001): Starter Air Turbine. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505154-21 · Feb 24, 2023
- [3505154-22](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133594149620230907183530.0001): Air Turbine Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505154-22 · Feb 24, 2023
- [979908-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131583983320230907183526.0001): Valve Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 979908-4 · Feb 24, 2023
- [3214324-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109909264220230907183517.0001): Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 3214324-2 · Feb 24, 2023
- [979906-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108057837420230907183521.0001): Valve Shutoff. Honeywell International Inc. · PMA PQ1222NM · Replaces 979906-1 · Feb 24, 2023
- [398444-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104517825520230907183522.0001): Electric 3-Way Mixing Butterfly Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 398444-2 · Feb 24, 2023
- [129552-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104209779020230907183515.0001): Pneu, Thermostat. Honeywell International Inc. · PMA PQ1222NM · Replaces 129552-1-1 · Feb 24, 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
- [105982-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110550695020230907183313.0001): Pneumatic Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105982-2 · Feb 23, 2023

All of them: https://openairdocs.org/model/mcdonnell-douglas-dc-8-71/pma.md

---
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.