# Mcdonnell Douglas DC-8-73F

- Type: Aircraft model (FAA registry)
- Registry code: 302199H
- Manufacturer (registry): MCDONNELL DOUGLAS
- Model: DC-8-73F
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-fan
- Seats: 272
- 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-8-73f

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 2006-03-04](https://openairdocs.org/ad/2006-03-04): Main cabin cargo door · Boeing DC-8-33, DC-8-51, DC-8-53 and 11 more. Effective Mar 13, 2006
- [AD 2005-18-07](https://openairdocs.org/ad/2005-18-07): Lower cargo doorjamb corners · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Oct 7, 2005
- [AD 2005-15-14](https://openairdocs.org/ad/2005-15-14): Upper inboard spar cap of the wing · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Sep 1, 2005
- [AD 2005-08-08](https://openairdocs.org/ad/2005-08-08): Engine fire extinguisher containers · Boeing DC-8-33, DC-8-43, DC-8-51 and 17 more. Effective May 26, 2005
- [AD 2005-06-05](https://openairdocs.org/ad/2005-06-05): Left and right elevator control tabs · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Apr 22, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-14-05](https://openairdocs.org/ad/2004-14-05): Seat locking pins · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Aug 13, 2004
- [AD 2003-03-15 R1](https://openairdocs.org/ad/2003-03-15-R1): Airplane Flight Manual (AFM) - oxygen masks · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 90 more. Effective Dec 22, 2003
- [AD 2003-17-07 R1](https://openairdocs.org/ad/2003-17-07-R1): Auxiliary power unit (APU) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 57 more. Effective Sep 24, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2002-14-19](https://openairdocs.org/ad/2002-14-19): Collins Air Data Computers (ADC) · Boeing DC-8-11, DC-8-12, DC-8-21 and 36 more. Effective Aug 23, 2002
- [AD 2002-03-05](https://openairdocs.org/ad/2002-03-05): Blue Ice · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Mar 19, 2002
- [AD 2001-26-04](https://openairdocs.org/ad/2001-26-04): Main Deck Cargo Door Structure and Fuselage Structure · Cargo door, cargo restraint bulkhead, heavy duty flooring… (Plattner STC SA1802SO or SA421NW). Effective Jan 30, 2002
- [AD 2001-26-03](https://openairdocs.org/ad/2001-26-03): Main Deck Cargo Door Structure and Fuselage Structure · Cargo door and cargo interior (Plattner STC SA1832SO). Effective Jan 30, 2002
- [AD 2001-26-02](https://openairdocs.org/ad/2001-26-02): Main Deck Cargo Door Structure and Fuselage Structure · Cargo door (Agro Air Associates STC SA1862SO or ST00309AT). Effective Jan 30, 2002
- [AD 2001-26-01](https://openairdocs.org/ad/2001-26-01): Main Deck Cargo Door Structure and Fuselage Structure · Forward cargo door (Aeronautical Engineers STC SA1063SO or SA1377SO). Effective Jan 30, 2002
- [AD 2001-24-28](https://openairdocs.org/ad/2001-24-28): Rudder Pedals Adjuster Hub Assembly · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Jan 16, 2002
- [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001
- [AD 2001-08-20](https://openairdocs.org/ad/2001-08-20): Flush Pump Motor · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-08-19](https://openairdocs.org/ad/2001-08-19): Transformer Ballast Assemblies · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-08-18](https://openairdocs.org/ad/2001-08-18): Cabin Electrical Service Panel · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-08-16](https://openairdocs.org/ad/2001-08-16): Circuit Breakers and Wiring · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-06-02](https://openairdocs.org/ad/2001-06-02): Front Spar Lower Cap · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Apr 27, 2001
- [AD 2000-20-08](https://openairdocs.org/ad/2000-20-08): Doorjambs Of Passenger And Service Doors · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Nov 13, 2000
- [AD 2000-15-11](https://openairdocs.org/ad/2000-15-11): Main Deck Cargo Door · Cargo door (Agro Air Associates STC SA1862SO). Effective Sep 7, 2000
- [AD 2000-13-03 R1](https://openairdocs.org/ad/2000-13-03-R1): Main Deck Cargo Door · Forward cargo door (Aeronautical Engineers STC SA1063SO). Effective Aug 1, 2000
- [AD 2000-09-01 R1](https://openairdocs.org/ad/2000-09-01-R1): Main Deck Cargo Door · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Jun 7, 2000
- [AD 2000-09-02](https://openairdocs.org/ad/2000-09-02): Main Deck Cargo Door · Cargo door and cargo interior (Plattner STC SA1832SO). Effective Jun 6, 2000
- [AD 2000-02-01](https://openairdocs.org/ad/2000-02-01): Lower Wing Skin · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Feb 29, 2000
- [AD 2000-01-18](https://openairdocs.org/ad/2000-01-18): Lower Cap of the Wing Front Spar · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Feb 23, 2000
- [AD 98-26-51](https://openairdocs.org/ad/98-26-51): Main Deck Cargo Door · Cargo door, cargo restraint bulkhead, heavy duty flooring… (Plattner STC SA1802SO). Effective Feb 3, 1999
- [AD 97-04-04](https://openairdocs.org/ad/97-04-04): Auxiliary Power Units · Airbus BAC 1-11 200 Series, BAC 1-11 400 Series, Auxiliary Power Units and 54 more. Effective Mar 24, 1997

Historical (superseded or no longer in force):

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2008-26-07](https://openairdocs.org/ad/2008-26-07) (historical): Lower skin and stringers · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Jan 28, 2009
- [AD 2008-09-04](https://openairdocs.org/ad/2008-09-04) (historical): Fuel tank systems · McDonnell Douglas DC-8-31, DC-8-32, DC-8-33 and 21 more. Effective May 27, 2008
- [AD 2007-02-02](https://openairdocs.org/ad/2007-02-02) (historical): Aft fuselage skin panel · McDonnell Douglas DC-8-55, DC-8-61, DC-8-61F and 12 more. Effective Feb 28, 2007
- [AD 2004-06-06](https://openairdocs.org/ad/2004-06-06) (historical): Lower cargo doorjamb corners · McDonnell Douglas DC-8-71, DC-8-71F, DC-8-72 and 3 more. Effective Apr 29, 2004
- [AD 2003-17-07](https://openairdocs.org/ad/2003-17-07) (historical): Fire Extinguishers for the Engine and Auxiliary Power Unit (APU) · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 60 more. Effective Sep 24, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2001-25-01](https://openairdocs.org/ad/2001-25-01) (historical): Engine Fire Extinguishing System Electrical Connectors · McDonnell Douglas DC-8-33, DC-8-43, DC-8-51 and 17 more. Effective Dec 20, 2001
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 95-04-01](https://openairdocs.org/ad/95-04-01) (historical): AFM - Limitations - Windshear · Boeing 727-100 Series, 727-200 Series, 737-100 Series and 54 more. Effective Mar 8, 1995
- [AD 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
- [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 140: https://openairdocs.org/model/mcdonnell-douglas-dc-8-73f/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 (1)

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 CHI80AA022](https://openairdocs.org/ntsb/CHI80AA022), Jan 23, 1980: Douglas DC-8 (N783FT), Chicago, IL, substantial damage

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19791211047189I](https://openairdocs.org/incident/19791211047189I), Dec 11, 1979: Doug DC8/ (N783FT), Boston, MA. Split flap condition during climb. Actuator frozen #5772691-3, porkchop fitting #5751152503 broken.

## Service difficulty reports (15,471, newest 50)

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

- [SDR E4EB2015112401](https://openairdocs.org/sdr/E4EB2015112401), May 28, 2015: FRAME. CRACKED. EXTERIOR FUSELAGE AFT LT LAVATORY, SERVICE PANEL CUT OUT WORN & GOUGED AT LATCH CONTACT POINTS. FOUND GOUGE TO BE OUT OF LIMITS & FOUND CRACK ON FRAME. REPAIRED
- [SDR IXXA20121215035O](https://openairdocs.org/sdr/IXXA20121215035O), Dec 15, 2012: WARNING LIGHT. FALSE ACTIVATION. DURING TAKEOFF, BELLY DOOR OPEN LIGHT ILUMINATED. TAKEOFF WAS ABORTED. RESET ALL CARGO DOORS IAW MM 52-70-0 ALL WARNING LIGHTS OUT.
- [SDR IXXA20121127032O](https://openairdocs.org/sdr/IXXA20121127032O), Nov 27, 2012: CONNECTOR. LOOSE. ON APPROACH, RT MLG DOWN GREEN LIGHT DID NOT ILLUMINATE, NO RED LIGHTS ILLUMINATED. CYCLED LANDING GEAR AND GREEN LIGHT ILLUMINATED. RESEATED CONNECTOR PLUG ON 
- [SDR DHLA20120413006](https://openairdocs.org/sdr/DHLA20120413006), Apr 13, 2012: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE. ACFT WAS GROUNDED. R & R EMERGENCY LIGHT BATTERY PACK. OPS CHECKED GOOD IAW MM 33-50-0.
- [SDR DHLA201200005](https://openairdocs.org/sdr/DHLA201200005), Apr 5, 2012: WARNING LIGHT. FALSE ACTIVATION. ON CLIMB OUT, NR 4 THRUST REVERSER LIGHT ILLUMINATED. RAN THRUST REVERSER EMERGENCY STOW CHECKLIST. LIGHT REMAINED ILLUMINATED. RAN ABNORMAL IN FLIGHT ENGINE SH
- [SDR DHLA201203140004](https://openairdocs.org/sdr/DHLA201203140004), Mar 14, 2012: CAP. LOOSE. NR 4 ENGINE SHUTDOWN DURING FLIGHT WITH OIL QTY AT 2 QUARTS. ACFT WAS GROUNDED. INSPECTED ENGINE FOUND OIL CAP TO BE LOOSE INSTALLED NEW CAP ASSY IAW MM 79-11-1
- [SDR IXXA20120306006S](https://openairdocs.org/sdr/IXXA20120306006S), Mar 5, 2012: RADOME. DAMAGED. NOSE RADOME DAMAGED. R & R NOSE RADOME IAW MM 53-50-1.
- [SDR IXXA20120223004S0](https://openairdocs.org/sdr/IXXA20120223004S0), Feb 23, 2012: DOOR. OUT OF RIG. L1 DOOR OUT OF RIG. R & R L1 DOOR AND ADJUSTED TO OPENING IAW MM 52-11-1, OPS CHECKED GOOD.
- [SDR DHLA201200003](https://openairdocs.org/sdr/DHLA201200003), Jan 31, 2012: BLADE. MISSING. NR 1 ENGINE FAILED WHEN ENCOUNTER OF CAT AT FL 370 OCCURED. PERFORMED ENGINE FAILURE CHECKLIST AND INFLIGHT AIRSTART ABNORMAL PROCEDURE AND ENGINE SHUTDOWN PROC
- [SDR DHLA2012010600001](https://openairdocs.org/sdr/DHLA2012010600001), Jan 6, 2012: FIRE DETECTOR. MALFUNCTIONED. NR 3 ENGINE FIRE WARNING, PHASE ONES COMPLETED & ENGINE CHECKLIST, FIRED BOTTLE, LIGHT WENT OUT. OIL PRESSURE WAS POSITIVE. ACFT DIVERTED, ACFT WAS GROUNDED. IN
- [SDR DHLA20120106002](https://openairdocs.org/sdr/DHLA20120106002), Jan 6, 2012: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE. ACFT GROUNDED. R & R EMERGENCY LIGHTS BATTERY PACK IAW MM 33-50-0 WORKING NORMAL.
- [SDR IXXA110082O](https://openairdocs.org/sdr/IXXA110082O), Dec 21, 2011: CONNECTOR. LOOSE. DURING UPLATCH CHECK, DOOR NOT LATCH LIGHT CAME ON. THE CREW CYCLED MAIN GEARS TWICE AND DOOR NOT LATCH LIGHT REMAINED ON. THE CREW LANDED WITHOUT FURTHER INCID
- [SDR IXXA110081O](https://openairdocs.org/sdr/IXXA110081O), Dec 20, 2011: CONNECTOR. DIRTY. DURING CLIMB OUT, AFTER GEAR RETRACTION, DOOR NOT LATCH LIGHT REMAINED ON. CREW CYCLED MAIN GEAR AND LIGHT REMAINED ON. LANDED WITHOUT FURTHER INCIDENT. MX INSP
- [SDR DHLA201100539](https://openairdocs.org/sdr/DHLA201100539), Nov 15, 2011: ACTUATOR. LEAKING. AFTER DEPARTURE, ACFT LOST HYDRAULIC LEVEL TO JUST ABOVE THE EMERGENCY LEVEL. ALL PROCEDURES COMPLIED AND ACFT RETURNED TO DEPARTURE. ACFT GROUNDED ON ARRIVAL. 
- [SDR IXXA110072O](https://openairdocs.org/sdr/IXXA110072O), Oct 27, 2011: ENGINE. FAILED. DURING TAKEOFF ROLL NR 2 ENGINE COMPRESSOR STALLED 3 TIMES. ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. FOUND N1 SEIZED. REPLACED NR 2 ENGI
- [SDR DHLA201100538](https://openairdocs.org/sdr/DHLA201100538), Oct 6, 2011: BATTERY PACK. INOPERATIVE. DURING PREFLIGHT FOUND EMERGENCY EXIT LIGHTS ARMED-NO POWER ON ACFT BATTERY DEAD. ACFT WAS GROUNDED. R & R EMERGENCY LIGHT BATTERY RACK ASSY IAW MMS 33-50-00. O
- [SDR IXXA110060O](https://openairdocs.org/sdr/IXXA110060O), Sep 11, 2011: ENGINE. SLOW. REJECTED TAKEOFF DUE TO ASSYMETRICAL THRUST ON TAKEOFF ROLL. THE NR 4 ENGINE SLOW TO ACCELERATE, DID NOT REACH MAX POWER. THE CREW RETURNED TO BLOCKS WITHOUT FU
- [SDR DHLA201100537](https://openairdocs.org/sdr/DHLA201100537), Aug 26, 2011: SKIN. CORRODED. LOWER FUSELAGE HAS CRACK IN SKIN AT STA 100 AT LONGERON 35 & 36R. CRACK IS PROBABLY INDUCED BY CORROSION. COMPLIED WITH STEPS 1-11 OF EVA D853-00412. FABRICATED
- [SDR DHLA2011F00187](https://openairdocs.org/sdr/DHLA2011F00187), Aug 25, 2011: SKIN. CRACKED. WHILE COMPLYING WITH VISUAL WALK AROUND INSP, A CRACK WAS FOUND IN THE LOWER FUSELAGE SKIN AT STA 100.5. UPON FURTHER INVESTIGATION THE CAUSE OF THE CRACK WAS C
- [SDR DHLA201100536](https://openairdocs.org/sdr/DHLA201100536), Aug 15, 2011: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS INOPERATIVE. ACFT GROUNDED. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AND OPS CHECKED GOOD IAW MM 33-50-1.
- [SDR DHLA201100534](https://openairdocs.org/sdr/DHLA201100534), Jul 28, 2011: ENGINE. FAILED. DURING DESCENT NR3 ENGINE AT IDLE, STARTED RUMBLING ENGINE N1 & N2 SPOOLED DOWN NO- OIL PRESSURE. ACFT WAS GROUNDED. REPLACED NR 3 ENGINE ASSY.
- [SDR DHLA201100533](https://openairdocs.org/sdr/DHLA201100533), Jul 26, 2011: LINE. LEAKING. AT FL 380 ENGINE NR 1 FAILED. COMPLETED ENGINE FAILURE CHECK LIST. TRIED RESTART AT 340 NO GOOD. AT FL 220 RESTART SUCCESSFUL. ALL PARAMETERS NORMAL. ACFT WAS G
- [SDR DHLA201100525](https://openairdocs.org/sdr/DHLA201100525), Jul 11, 2011: BATTERY. INOPERATIVE. EMERGENCY EXIT LIGHTS ONLY STAY ON FOR A FEW SECONDS. ACFT WAS GROUNDED. REPLACED EMERGENCY EXIT LIGHT BATTERY ASSY AND SYS. OPS CK GOOD IAW MM 33-50-1.
- [SDR IXXA110049O](https://openairdocs.org/sdr/IXXA110049O), Jun 27, 2011: DAMPER. DEFECTIVE. DURING CLIMB OUT, THE CREW NOTICED AT 250 KNOTS A PULSING IN BOTH CONTROL COLUMNS. THE PULSE INCREASED THROUGH ANY PITCH CHANGE WHETHER USING THE AUTOPILOT OR M
- [SDR DHLA201100531](https://openairdocs.org/sdr/DHLA201100531), Jun 23, 2011: FITTING. CORRODED. RT OUTER WING FWD BOTTOM PANEL.- FITTING HAS EXFOLIATION CORROSION S-62 (NR 4 ALT TANK) STA XW 408.000 PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, DWG 3640143. 
- [SDR DHLA201100530](https://openairdocs.org/sdr/DHLA201100530), Jun 23, 2011: FITTING. CORRODED. RT OUTER WING FWD BOTTOM PANEL.- FITTING HAS EXFOLIATION CORROSIOIN S-63, STA XW 408.000 (NR4 ALT TANK) PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, DWG 3640143.
- [SDR DHLA201100516](https://openairdocs.org/sdr/DHLA201100516), Jun 22, 2011: BATTERY PACK. INOPERATIVE. DURING PDC CK FOUND EMERGENCY LIGHTS INOPERATIVE. ACFT WAS GROUNDED. R & R EMER LIGHTS BATTERY PACK IAW MMS 33-50-10. OPS-CK-GOOD.
- [SDR IXXA110048O](https://openairdocs.org/sdr/IXXA110048O), Jun 10, 2011: CONNECTOR. DIRTY. ON FINAL APPROACH WITH LANDING GEAR LEVER DOWN, RT LANDING LIGHT DID NOT ILLUMINATE. THE CREW CYCLED THE GEAR AND GEAR LIGHT ILLUMINATED 10 SECONDS AFTER GEAR C
- [SDR DHLA201100532](https://openairdocs.org/sdr/DHLA201100532), Jun 7, 2011: STRINGER. CRACKED. RT INNER WING AFT TOP PANEL.- STRINGER NR4 CRACKED STA XRS 87.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 07-21-11, EVA D857-00408 REV IR DATED 07-06
- [SDR DHLA201100527](https://openairdocs.org/sdr/DHLA201100527), Jun 7, 2011: LONGERON. CORRODED. FWD ACCY COMPT- L33R SHOWS EXFOLIATION CORROSION AT STA 14.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 10 SHEET 1,3, TR 53-153 SHEET 4, TR 53-193. REMOVED F
- [SDR DHLA201100521](https://openairdocs.org/sdr/DHLA201100521), Jun 7, 2011: LONGERON. CORRODED. FWD ACCY COMPT- L33R SHOWS EXFOLIATION CORROSION AT STA 14.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 10 SHEET 1,3, TR 53-153, SHEET 4, TR 53-193. REMOVED 
- [SDR DHLA201100515](https://openairdocs.org/sdr/DHLA201100515), Jun 7, 2011: AMPLIFIER. INOPERATIVE. AMBER CARGO SMOKE LIGHT ILLUMINATED DURING DESCENT, LIGHT EXTINGUISHED ON SHORT FINAL APPROACH TO LANDING, NO SMOKE OR FIRE WAS NOTICED TO CREW. EMERGENCY WAS D
- [SDR DHLA201100524](https://openairdocs.org/sdr/DHLA201100524), Jun 6, 2011: FRAME. DEFORMED. MAIN CARGO BAY FRAME DEFORMED BS 1580.000 L19TO 21R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 6, SRM 53-4-1 FIG. 51 SHEET 21. REMOVED DEFORMED FRAME S
- [SDR DHLA201100523](https://openairdocs.org/sdr/DHLA201100523), Jun 6, 2011: FITTING. CORRODED. FWD ACCY COMPT FITTING CORRODED BY EXFOLIATION STA 8.000 L33R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 REMOVED CORROSION IAW SRM 51-1-8 PG 17-18 FOUND WITHIN
- [SDR IXXA110046O](https://openairdocs.org/sdr/IXXA110046O), Jun 5, 2011: LINK. FAILED. AFTER TAKEOFF, THE CREW HEARD A LOUD NOISE FROM NOSE GEAR AREA, THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX FOUND RT NOSE GEAR DOOR OPENED, NO FURTH
- [SDR IXXA110045O](https://openairdocs.org/sdr/IXXA110045O), Jun 5, 2011: LATCH. FAILED. AFTER TAKEOFF, THE CREW HEARD A LOUD NOISE FROM NOSE GEAR AREA, THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED NOSE GEAR AND FOUND RT NOSE GE
- [SDR DHLA201100529](https://openairdocs.org/sdr/DHLA201100529), Jun 3, 2011: TEE FITTING. CRACKED. R2 SERVICE DOOR INNER FITTING CRACKED 1". REMOVED CRACKED TEE FITTING IAW SRM 51-1-20D, SRM 51-1-21. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-8B. INSTALLED N
- [SDR DHLA201100520](https://openairdocs.org/sdr/DHLA201100520), Jun 2, 2011: SKIN. CORRODED. EXT FUS LWR SKIN CORRODED STA 1460.000 - 1480.000, L34L TO 35L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1, SRM 53-4-1, FIG. 17A SHEET 2. REMOVED LEVEL II CORR
- [SDR DHLA201100522](https://openairdocs.org/sdr/DHLA201100522), Jun 1, 2011: SKIN. CRACKED. RT WING UPPER SKIN 2" CRACK STA XRS 74.869 (BETWEEN CTR SPAR AND S-8). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-28-11, EVA D857-00406 REV IR, ASTAR D
- [SDR DHLA201100519](https://openairdocs.org/sdr/DHLA201100519), Jun 1, 2011: FRAME. DEFORMED. MAIN CARGO COMPT FRAME DEFORMED STA 1580.000 L21 TO 19L PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2, SHEET 6, SRM 53-4-1 FIG 51 SHEET 21. REMOVED DEFORMED FRAME
- [SDR DHLA201100528](https://openairdocs.org/sdr/DHLA201100528), May 31, 2011: ANGLE. CRACKED. NR 2 ENG TO PYLON ANGLE CRACK 10" STA YN 183.000 AT 12 O'CLOCK POS, LT SIDE. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATE 07-02-11, EVA D854-00407, REV IR D
- [SDR DHLA201100526](https://openairdocs.org/sdr/DHLA201100526), May 31, 2011: FITTING. CORRODED. RT MLG WHEEL WELL FITTING CORRODED AT STA 857.125, RBL 47 (EXFOLIATION). REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-20. FOUND OUT OF LIMITS IAW SRM 53-2-0 
- [SDR DHLA201100518](https://openairdocs.org/sdr/DHLA201100518), May 31, 2011: SKIN. CORRODED. RT AILERON SKIN LOWER PLATING CORRODED STA XA 737.000 - XA 775.000. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4. REMOVED LEVEL 2 CORROSION IAW SRM 51-1-8 PG 17-
- [SDR IXXA110043O](https://openairdocs.org/sdr/IXXA110043O), May 30, 2011: LOCK SENSOR. DEFECTIVE. AFTER TAKEOFF, NR 2 THRUST REVERSER LIGHT WAS BLINKING. THE CREW ACTUATED THE EMERGENCY STOW PUMP BUT NO HELP. THEY RETURNED TO DEPARTURE AND UPON LANDING THE L
- [SDR IXXA110040O](https://openairdocs.org/sdr/IXXA110040O), May 12, 2011: FUEL CONTROL. OUT OF ADJUST. DURING CRUISE, NR 4 ENGINE FLAMEDOUT. THE CREW ATTEMPTED RESTART, ENGINE WOULD NOT START. THEY LANDED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED FAULT TREE 51, C
- [SDR DHLA201100500](https://openairdocs.org/sdr/DHLA201100500), May 7, 2011: BATTERY PACK. INOPERATIVE. EMERGENCY BATTERY PACK DEAD. ACFT WAS GROUNDED. R & R EMERGENCY BATTERY PACK IAW MM 33-50-1. GROUND CKS GOOD.
- [SDR IXXA110037O](https://openairdocs.org/sdr/IXXA110037O), May 5, 2011: CONTROL TUBE. DIRTY. AT FLIGHT LEVEL 370, THE NR 2 ENGINE POWER ROLLED BACK FROM 94 PERCENT TO 87 PERCENT WITH A CORRESPONDING DROP IN EGT AND N2. THE PMC FOR NR 2 ENGINE WAS SWITCH
- [SDR DHLA201100049](https://openairdocs.org/sdr/DHLA201100049), May 4, 2011: BATTERY PACK. DISCHARGED. ALL 3 EMERGENCY EVAC LIGHTS DO NOT ILLUMINATE OR ARE VERY DIM WHEN PERFORMING A BATTERY CHECK. ACFT WAS GROUNDED. R & R EMERGENCY LIGHTS BATTERY RACK ASSY IAW D
- [SDR DHLA201100041](https://openairdocs.org/sdr/DHLA201100041), May 1, 2011: SKIN. CORRODED. FUSELAGE SKIN BULGING AND CRACKED AT FS 26.0, BETWEEN LONGERONS 35L AND 36. ACCOMPLISHED SKIN EXTERNAL DOUBLER REPAIR IAW EVA D853-0041 REV A, DWG D85300441-001
- [SDR DHLA201100048](https://openairdocs.org/sdr/DHLA201100048), Apr 11, 2011: SKIN. CRACKED. LT OTBD AIL LWR NOSE PLATING CRACKED 1" STA XA 734.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0, PG 1, SRM 57-8-1, FIG 4. REMOVED DAMAGED NOSE PLATING IAW SRM 57-

All 15,471: https://openairdocs.org/model/mcdonnell-douglas-dc-8-73f/reports.md

## STCs that may be installed (OpenAirDocs) (135, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC SA1315NM](https://openairdocs.org/stc/SA1315NM): Installation of overhead storage compartments, ceiling and wall linings and normal and emergency lights. Safran Cabin Inc
- [STC SA3169NM](https://openairdocs.org/stc/SA3169NM): Installation of floor proximity emergency escape marking system. Bruce Aerospace Inc
- [STC ST01078AT](https://openairdocs.org/stc/ST01078AT): Installation of an expanded, 17-parameters, Allied Signal, or Loral-Fairchild, Digital Flight Data Recorder (DFDR). Acron Aviation Inc
- [STC ST01174CH](https://openairdocs.org/stc/ST01174CH): Installation of UPS Aviation Technologies ADS-B provisions and Honeywell Mode-S System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC SA2534SW-D](https://openairdocs.org/stc/SA2534SW-D): Replacement of Switch assembly Int'l Inflatables Co. P/N 68748, with DME Corp. P/N L-140 in emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC SA2539SW-D](https://openairdocs.org/stc/SA2539SW-D): Replacement of light assembly, International Inflatables Co. P/N68555-1 with DME Corp. EL-104, EL-104A, and EL-104B in emergency slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC SA863EA](https://openairdocs.org/stc/SA863EA): Incorporation of DME Corporation emergency evacuation slide lighting system. Astronics Luminescent Systems Inc. Lists DC-8 Series
- [STC ST02580AT](https://openairdocs.org/stc/ST02580AT): Lithium cell battery pack to replace currently approved alkaline battery pack used in escape slide emergency light system. Astronics Luminescent Systems Inc
- [STC SA5720NM](https://openairdocs.org/stc/SA5720NM): Installation of the Mark VII ground proximity and windshear warning system. Honeywell International Inc
- [STC ST00375AT](https://openairdocs.org/stc/ST00375AT): Installation of a CAS-81 TCAS II and a TRA-67 Mode S transponder. Honeywell International Inc
- [STC SA9079SC-D](https://openairdocs.org/stc/SA9079SC-D): Recore of AiResearch Precooler, P/N 194430-1, -2 in accordance with Honeywell LORI Sealed Drawing List SDL3779-1, Revision A, dated 11 October 2005 or later FAA approved revision. Honeywell International Inc
- [STC SE00584AT](https://openairdocs.org/stc/SE00584AT): Installation of ELDEC fuel flow meter and Kollsman digital fuel flow/fuel used indicator. GDC Technics LLC
- [STC SA3421NM](https://openairdocs.org/stc/SA3421NM): Installation of Hughes-Avicom video entertainment system. Burrana Inc. Lists DC-8 Series
- [STC SA5059NM](https://openairdocs.org/stc/SA5059NM): Installation of Ancra cargo conveyor system, P/N's 81381-11, 81382-11. Ancra International LLC
- [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC
- [STC SA3140SO](https://openairdocs.org/stc/SA3140SO): Installation of a replacement coalescer filter, P/N 22D10 or 22D10-2. Purolator Facet, Inc
- [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic LLC
- [STC ST01067LA](https://openairdocs.org/stc/ST01067LA): Installation of Litton LTR-97 fiber optic gyro systems. Northrop Grumman Systems Corporation
- [STC ST01668LA](https://openairdocs.org/stc/ST01668LA): Installation of a single LTN-2012 Global Positioning Sensor Unit (GPSU) and dual LTN-92 Inertial Reference System (INS). Northrop Grumman Systems Corporation
- [STC ST01467LA-D](https://openairdocs.org/stc/ST01467LA-D): Installation of Universal Avionics Terrain Avoidance Warning System and MFD-640 Multi Function Display(s). Zalinka Aviation Support, LLC
- [STC ST01468LA-D](https://openairdocs.org/stc/ST01468LA-D): Installation of Universal Avionics Flight Management System. Zalinka Aviation Support, LLC
- [STC SA3420NM](https://openairdocs.org/stc/SA3420NM): Installation of Brownline Aft Stop, P/N 46443-102. Telair US LLC
- [STC SA1511GL](https://openairdocs.org/stc/SA1511GL): Installation of Type "C" containers. ABX Air Incorporated
- [STC SA1462GL](https://openairdocs.org/stc/SA1462GL): Installation of ABX Cargo Handling System. ABX Air Incorporated
- [STC SA3496NM](https://openairdocs.org/stc/SA3496NM): Installation of ABX-C Cargo Container assembly. Airborne Express Air Inc
- [STC SA7729SW](https://openairdocs.org/stc/SA7729SW): Installation of digital fuel quantity indicators, fuel totalizer, and capacitive fuel compensator units. Ontic Engineering and Manufacturing Inc
- [STC SA3168NM](https://openairdocs.org/stc/SA3168NM): Installation of ANCRA Corp. End Restraints in the cargo pallet positions number one or eighteen. Ancra International LLC
- [STC SA3957NM](https://openairdocs.org/stc/SA3957NM): Installation of cargo system P/N 80080-10, -11, or -12. Ancra International LLC
- [STC SA4560NM](https://openairdocs.org/stc/SA4560NM): Installation of ANCRA cargo system modification kit, P/N 81380-10. Ancra International LLC
- [STC SA4-918](https://openairdocs.org/stc/SA4-918): 1. Aircraft wiring in accordance with Douglas Aircraft Co. Service Change #17 (UAL COA-0-1456) to provide an operational Aircraft Flight Data Rrecorder conforming to CAR Amendment 40-6, paragraph 40.208 with the following additions to assure recording of data during takeoff and landing roll: a. Relay to provide automatic start of recording when nose landing gear reaches airborne condition on takeoff. b. Time delay relay to turn off recorder one minute after nose landing gear reaches "on ground" condition, on landing. c. Installation of standard toggle switch on Systems Engineer's Console, to permit Second Officer to turn on recorder at start of takeoff run. 2. Install Waste King Flight Data Recorder #5424, TSO-C51. United Airlines Inc
- [STC SA611WE](https://openairdocs.org/stc/SA611WE): Interior configuration - 120 passenger single class 5-abreast seating per United Air Lines approved drawing lists: COA 2-2083 (Sheet #1 Revision February 17, 1964, Sheet #2 dated December 4, 1963, Sheet #3 Revision dated February 27, 1964 and, COA 2-2099 Revision dated December 17, 1963). United Airlines Inc
- [STC SA65WE](https://openairdocs.org/stc/SA65WE): Installation of a cockpit hydraulic replenishing system. See 15F-2044 Chg. B, 9F-4813 Chg. C, 6F-8140 Chg. C, 6F-8130 Chg. B, 3F-9025 Chg. A, 3F-9022, 3F-9023 Chg. A, IF-9882, 6F-8141 Chg. C. COA-2-1534 (ERs 1 - 4), App. V(UAL) to AFM SM-23889, App. IV (UAL) to AFM SM-23891, App. VII(UAL) to AFM LB-30582 or later FAA approved revisions. United Airlines Inc
- [STC SA2825CE](https://openairdocs.org/stc/SA2825CE): Installation of B&D Instruments & Avionics, Inc. Electronic N2 Gas Compressor Indicator. Data required: (1) B&D Instruments & Avionics, Inc. Installation Manual Part No. 55006-003-011, Revision A, dated April 6, 1992, or later "FAA Approved" revision; and (2) copy of this certificate. Teledyne Controls
- [STC SA2826CE](https://openairdocs.org/stc/SA2826CE): Installation of optional set of B&D Instruments & Avionics, Inc. Electronic Exhaust Gas Temperature (EFT) Indicators. Teledyne Controls
- [STC ST01202WI-D](https://openairdocs.org/stc/ST01202WI-D): Modification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision. Rockwell Collins Inc
- [STC ST00746LA-D](https://openairdocs.org/stc/ST00746LA-D): Installation of smoke detection system, lower cargo compartment. Ontic Engineering and Manufacturing Inc
- [STC SA2082SO](https://openairdocs.org/stc/SA2082SO): Installation of fuselage window plugs. Kosola & Associates Inc
- [STC SA2216SO](https://openairdocs.org/stc/SA2216SO): Installation of an Ancra cargo loading system. Kosola & Associates Inc
- [STC ST01494CH](https://openairdocs.org/stc/ST01494CH): Installation of a Universal Avionics Terrain Awareness Warning System (TAWS) and a Universal Avionics GPS-1000 global positioning system. Airborne Maintenance & Engineering Services (AMES)
- [STC ST01930CH](https://openairdocs.org/stc/ST01930CH): Installation of Innovative Solutions & Support dual air data display unit. Airborne Maintenance & Engineering Services (AMES)
- [STC ST02123CH](https://openairdocs.org/stc/ST02123CH): Installation of Universal Aviionics Systems. Airborne Maintenance & Engineering Services (AMES)
- [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing
- [STC ST01256WI-D](https://openairdocs.org/stc/ST01256WI-D): Modification of a Collins TPR-720, TPR-900 or TPR-901 Mode S Transponder System installation with an ATC/TCAS Control Panel to an Elementary Surveillance Compliant Collins TPR-901 Mode S Transponder System installation with a Flight ID/ATC/TCAS Control Panel in accordance with Collins Drawing Index as listed on AML No. ST01256WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST01220AT](https://openairdocs.org/stc/ST01220AT): Installation of a Dual Trimble Model TNL-8100 Global Positioning System. Avionics Group Inc. Lists DC-8 Series
- [STC ST02069AT](https://openairdocs.org/stc/ST02069AT): Installation of a Dual Trimble TNL-8100 GPS Navigation System. Avionics Group Inc
- [STC SA1076NE](https://openairdocs.org/stc/SA1076NE): Installation of Aerofex livestock carrier P/N TS-QA-400 platform and panel system using size A or size M Class II pallet. Equine Air Transport Systems LLC
- [STC SA1343NM](https://openairdocs.org/stc/SA1343NM): Installation of an environmental control system. Airweld Inc

All 135: https://openairdocs.org/model/mcdonnell-douglas-dc-8-73f/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
- [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
- [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
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110795794120250923105918.0001): VOGT AERO · PMA PQ05310NM · 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
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101731757320260729202734.0001): Vogt Aero LLC · PMA PQ05310NM · 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
- [5002742AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187227990220230824131311.0001): Plate, Instruction. Aero Brake & Spares Inc · PMA PQ0694SW · Replaces 5002742 · May 26, 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
- [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
- [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
- [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

All of them: https://openairdocs.org/model/mcdonnell-douglas-dc-8-73f/pma.md

## The same model under other registry codes

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

- [Douglas DC-8-73F](https://openairdocs.org/model/douglas-dc-8-73f): 2 registered aircraft, registry code 302199F

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