# Douglas DC-8-61F

- Type: Aircraft model (FAA registry)
- Registry code: 3021953
- Manufacturer (registry): DOUGLAS
- Model: DC-8-61F
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-jet
- Seats: 152
- Weight class: 20,000 lb and over
- Cruise speed: 444 mph
- Certification: Type certificated
- Data sheet: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Holder: The Boeing Company
- Registered aircraft: 0
- Page: https://openairdocs.org/model/douglas-dc-8-61f

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 2007-12-02](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 2005-18-07](https://openairdocs.org/ad/2005-18-07): Lower cargo doorjamb corners · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Oct 7, 2005
- [AD 2005-15-14](https://openairdocs.org/ad/2005-15-14): Upper inboard spar cap of the wing · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Sep 1, 2005
- [AD 2005-08-08](https://openairdocs.org/ad/2005-08-08): Engine fire extinguisher containers · Boeing DC-8-33, DC-8-43, DC-8-51 and 17 more. Effective May 26, 2005
- [AD 2005-06-05](https://openairdocs.org/ad/2005-06-05): Left and right elevator control tabs · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Apr 22, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-14-05](https://openairdocs.org/ad/2004-14-05): Seat locking pins · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Aug 13, 2004
- [AD 2003-03-15 R1](https://openairdocs.org/ad/2003-03-15-R1): Airplane Flight Manual (AFM) - oxygen masks · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 90 more. Effective Dec 22, 2003
- [AD 2003-21-02](https://openairdocs.org/ad/2003-21-02): Lower inboard auxiliary spar cap · Boeing DC-8-11, DC-8-12, DC-8-21 and 21 more. Effective Nov 20, 2003
- [AD 2003-17-07 R1](https://openairdocs.org/ad/2003-17-07-R1): Auxiliary power unit (APU) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 57 more. Effective Sep 24, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2002-14-19](https://openairdocs.org/ad/2002-14-19): Collins Air Data Computers (ADC) · Boeing DC-8-11, DC-8-12, DC-8-21 and 36 more. Effective Aug 23, 2002
- [AD 2002-03-05](https://openairdocs.org/ad/2002-03-05): Blue Ice · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Mar 19, 2002
- [AD 2001-26-04](https://openairdocs.org/ad/2001-26-04): Main Deck Cargo Door Structure and Fuselage Structure · Cargo door, cargo restraint bulkhead, heavy duty flooring… (Plattner STC SA1802SO or SA421NW). Effective Jan 30, 2002
- [AD 2001-26-03](https://openairdocs.org/ad/2001-26-03): Main Deck Cargo Door Structure and Fuselage Structure · Cargo door and cargo interior (Plattner STC SA1832SO). Effective Jan 30, 2002
- [AD 2001-26-02](https://openairdocs.org/ad/2001-26-02): Main Deck Cargo Door Structure and Fuselage Structure · Cargo door (Agro Air Associates STC SA1862SO or ST00309AT). Effective Jan 30, 2002
- [AD 2001-26-01](https://openairdocs.org/ad/2001-26-01): Main Deck Cargo Door Structure and Fuselage Structure · Forward cargo door (Aeronautical Engineers STC SA1063SO or SA1377SO). Effective Jan 30, 2002
- [AD 2001-24-28](https://openairdocs.org/ad/2001-24-28): Rudder Pedals Adjuster Hub Assembly · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Jan 16, 2002
- [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001
- [AD 2001-08-20](https://openairdocs.org/ad/2001-08-20): Flush Pump Motor · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-08-19](https://openairdocs.org/ad/2001-08-19): Transformer Ballast Assemblies · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-08-18](https://openairdocs.org/ad/2001-08-18): Cabin Electrical Service Panel · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-08-17](https://openairdocs.org/ad/2001-08-17): Heating or Antifogging Wiring · Boeing DC-8-11, DC-8-12, DC-8-21 and 18 more. Effective May 31, 2001
- [AD 2001-08-16](https://openairdocs.org/ad/2001-08-16): Circuit Breakers and Wiring · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective May 31, 2001
- [AD 2001-06-02](https://openairdocs.org/ad/2001-06-02): Front Spar Lower Cap · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Apr 27, 2001
- [AD 2001-04-15](https://openairdocs.org/ad/2001-04-15): Pitot Tube Lines · Pneumatic flow control system (National Aircraft Service STC ST466CH). Effective Mar 21, 2001
- [AD 2000-20-08](https://openairdocs.org/ad/2000-20-08): Doorjambs Of Passenger And Service Doors · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Nov 13, 2000
- [AD 2000-15-11](https://openairdocs.org/ad/2000-15-11): Main Deck Cargo Door · Cargo door (Agro Air Associates STC SA1862SO). Effective Sep 7, 2000
- [AD 2000-13-03 R1](https://openairdocs.org/ad/2000-13-03-R1): Main Deck Cargo Door · Forward cargo door (Aeronautical Engineers STC SA1063SO). Effective Aug 1, 2000
- [AD 2000-09-01 R1](https://openairdocs.org/ad/2000-09-01-R1): Main Deck Cargo Door · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Jun 7, 2000
- [AD 2000-09-02](https://openairdocs.org/ad/2000-09-02): Main Deck Cargo Door · Cargo door and cargo interior (Plattner STC SA1832SO). Effective Jun 6, 2000
- [AD 2000-02-01](https://openairdocs.org/ad/2000-02-01): Lower Wing Skin · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more. Effective Feb 29, 2000
- [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 2003-17-07](https://openairdocs.org/ad/2003-17-07) (historical): Fire Extinguishers for the Engine and Auxiliary Power Unit (APU) · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 60 more. Effective Sep 24, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2001-25-01](https://openairdocs.org/ad/2001-25-01) (historical): Engine Fire Extinguishing System Electrical Connectors · McDonnell Douglas DC-8-33, DC-8-43, DC-8-51 and 17 more. Effective Dec 20, 2001
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 95-04-01](https://openairdocs.org/ad/95-04-01) (historical): AFM - Limitations - Windshear · Boeing 727-100 Series, 727-200 Series, 737-100 Series and 54 more. Effective Mar 8, 1995
- [AD 93-20-02](https://openairdocs.org/ad/93-20-02) (historical): AFM Changes - Cargo Door Inspection · Cargo door, cargo restraint bulkhead, heavy duty flooring… (Plattner STC SA1802SO or SA421NW). Effective Nov 17, 1993

All 141: https://openairdocs.org/model/douglas-dc-8-61f/ads.md

## Information bulletins (advisory) (4)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (82, newest 50)

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

- [SDR COOSDR040042](https://openairdocs.org/sdr/COOSDR040042), Oct 11, 2004: LONGERON. CORRODED. FWD CARGO COMPT AT Y STA 360.0, LONGERON 28R CORRODED.
- [SDR ARWA0010805](https://openairdocs.org/sdr/ARWA0010805), Aug 13, 2001: STRINGER. CRACKED. DURING SCHEDULED MAINTENANCE:FOUND 2 INCH CRACK AT STATION 940 STRINGER 23R.REPAIRED IAW EO DRAWING NR AS11300 DATED 08/09/01
- [SDR ARWA0010804](https://openairdocs.org/sdr/ARWA0010804), Aug 13, 2001: STRINGER. CRACKED. DURING SCHEDULED MAINTENANCE:FOUND 2 INCH CRACK AT STATION 940 STRINGER 23R.CORRECTIVE ACTION:REPAIRED I.A.W. E.O. DRAWING # AS11300 DATED 08/09/01
- [SDR TC8A99015](https://openairdocs.org/sdr/TC8A99015), Apr 24, 1999: FUEL CONTROL. MALFUNCTIONED. TRIP NR 03295 LATI-EINN, NR 1 ENGINE FLAMEOUT AT 22:05 Z, ON DESCENT. ENGINE FLAMEOUT CHECKLIST COMPLETED, 35 PERCENT N2, OIL PRESSURE 20 PSI AND 25 PERCENT N1.
- [SDR TC8A99013](https://openairdocs.org/sdr/TC8A99013), Apr 17, 1999: P & D VALVE. FAILED. NR 1 ENGINE FLAME-OUT AFTER ENGINE START. FUEL FLOW INDICATOR SHOWING FLUCTUATION OF 1,000 +/- 500 PSI. FUEL PRESSURE ENGINE DRIVEN PUMP. NORMAL RANGE - FUEL PR
- [SDR 99ZZZX675](https://openairdocs.org/sdr/99ZZZX675), Jan 22, 1999: WHEEL. CRACKED. NDT SPECS MIL-I-6870 DETECTED CRACK IN TUBEWALL WEB AREA DRIVE KEY HOLE. NO CRACKS PERMITTED THIS AREA. BENDIX OHM 32-40-05 REV 15 DATED 10-15-96. CHECK SECTION
- [SDR 99ZZZX555](https://openairdocs.org/sdr/99ZZZX555), Jan 13, 1999: WHEEL. CRACKED. VISUALLY DETECTED LEAKING AREA BETWEEEN TIE BOLTS. CONFIRMED CRACK TUBE WALL ROTOR DRIVE KEY HOLE. NO CRACKS PERMITTED THIS AREA. BENDIX OHM 32-40-05 REV 15 DAT
- [SDR 99ZZZX554](https://openairdocs.org/sdr/99ZZZX554), Jan 13, 1999: WHEEL. CRACKED. VISUALLY DETECTED LEAKING AREA BETWEEEN TIE BOLTS. CONFIRMED CRACK TUBE WALL ROTOR DRIVE KEY HOLE. NO CRACKS PERMITTED THIS AREA. BENDIX OHM 32-40-05 REV 15 DAT
- [SDR CKSA99002](https://openairdocs.org/sdr/CKSA99002), Jan 1, 1999: FUEL PUMP. FAILED. DURING CRUISE FL 340, NR 1 ENG BEGAN TO LOSE PWR AS EVIDENCED BY DECREASING EPR AND RPM IND. APPLIED ENG AND SCOOP ANTI-ICE, EPR AND RPM'S CONTINUED TO DROP. AF
- [SDR TC8A98085](https://openairdocs.org/sdr/TC8A98085), Dec 17, 1998: FUEL CONTROL. OUT OF ADJUST. NR 4 ENGINE WOULD NOT DEVELOPE TAKEOFF POWER, (1.87 EPR). REJECTED T/O AT 100 KTS. ADJUSTED NR 4 ENGINE FUEL CONTROL IAW DMM, CH 73-20-1. PERFORMED ENGINE RUN-U
- [SDR TC8A98080](https://openairdocs.org/sdr/TC8A98080), Nov 11, 1998: FITTING. LOOSE. SLOW HYDRAULIC FLUID DOWN TO STANDPIPE, MANUAL REVERSION LIGHT ON. ACCOMPLISHED ABNORMAL HYDRAULIC CHECKLIST. FOUND LOOSE FITTING PRESSURE SIDE OF NR 3 ENGINE H
- [SDR TC8A98079](https://openairdocs.org/sdr/TC8A98079), Nov 11, 1998: O-RING. BROKEN. HYDRAULIC LOSS TO STANDPIPE IN FLIGHT. PERFORMED CHECKLIST, OPERATED IN MANUAL REVERSION. FOUND HYDRAULIC LEAD NR 3 ENGINE, HYDRAULIC PUMP INLET. REMOVED AND RE
- [SDR TC8A98067](https://openairdocs.org/sdr/TC8A98067), Oct 7, 1998: ENGINE. FAILED. DFW-DAY. TRIP# 02617 DISCREP: #1 ENGINE LOSS OF POWER ON CLIMBOUT 240-330. ENGINE SURGING FROM CLIMB EPR TO 1.6 THEN 1.3 SHUTDOWN, ALL PARAMETERS NORMAL. FERRIE
- [SDR TC8A98065](https://openairdocs.org/sdr/TC8A98065), Oct 3, 1998: FITTING. FAILED. DURING DESCENT, LOSS OF HYDRAULIC FLUID. QUANTITY DROPPED DOWN TO AUX MARK. PERFORMED IMMEDIATE ACTION ITEMS THEN ABNORMAL HYDRAULIC PROCEDURES. REPLACED NR 10 
- [SDR TC8A98051](https://openairdocs.org/sdr/TC8A98051), Aug 25, 1998: CYLINDER. FAILED. AFTER PUSHBACK, AIRCRAFT WOULD ONLY TURN SEVERAL DEGREES LEFT WITH NOSE WHEEL STEERING. FOUND RT STEERING CYLINDER FAILED DURING PUSHBACK. REPLACED RT STEERING 
- [SDR ABXA9800714](https://openairdocs.org/sdr/ABXA9800714), Jul 12, 1998: FITTING. CRACKED. STATION 980-1000 STRINGER 22R END FITTING WAS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-8 AND DWG 37532351.
- [SDR TC8A98038](https://openairdocs.org/sdr/TC8A98038), Jul 2, 1998: ENGINE. MALFUNCTIONED. ABORTED T/O AT IAH DUE TO HIGH EGT ON ENGINE NR 2, 1.85 EPR, EGT GOES 555 REDLINE AND CONTINUE TO CLIMB, SHUT DOWN ENGINE, TAXI BACK. ENGINE NR 2 EXCEEDS MAX EG
- [SDR ABXA9800670](https://openairdocs.org/sdr/ABXA9800670), Jun 27, 1998: STRAP. CRACKED. RIGHT WING LEADING EDGE AT STATION XFS 610.000, UPPER RIB TRAILING EDGE STRAP IS CRACKED. REPLACED STRAP IAW DWG 5655441 AND DC8 SRM 51-1-21A.
- [SDR ABXA9800712](https://openairdocs.org/sdr/ABXA9800712), Jun 26, 1998: ANGLE. CRACKED. 680 BULKHEAD UPPER ATTACH FITTING TO FLOOR BOARD FRAME CRACKED AT RBL24. REPLACED FLOOR SUPPORT ANGLE IAW DWG 4645517 AND DC8 SRM 51-1-20D.
- [SDR ABXA9800669](https://openairdocs.org/sdr/ABXA9800669), Jun 24, 1998: WEB. CORROSION. HEAVY CORROSION ON TORQUE BOX WEB AT STATION 1210-1250. REPAIRED WEB IAW DWG 9754945, DC8 SRM 53-2-0 AND 51-1-21.
- [SDR ABXA9800717](https://openairdocs.org/sdr/ABXA9800717), Jun 23, 1998: RIB. CRACKED. LEFT WING LEADING EDGE LOWER RIB ARM CRACKED BY AFT FASTENER AT STATION XFS 816.250. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-21.
- [SDR ABXA9800716](https://openairdocs.org/sdr/ABXA9800716), Jun 23, 1998: ANGLE. CRACKED. RIGHT WING LEADING EDGE AT STATION XFS 766.250, THE INTERNAL DOUBLER ANGLE FORWARD OF ACCESS HOLE HAS A 5 CRACK. REPAIRED IAW DC8 SRM 51-1-8 AND 51-1-20D.
- [SDR ABXA9800703](https://openairdocs.org/sdr/ABXA9800703), Jun 23, 1998: RIB. CRACKED. RIGHT WING LEADING EDGE AT STATION XOLDI 6.225, UPPER LEADING EDGE RIB HAS A 4 CRACK. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-21.
- [SDR ABXA9800702](https://openairdocs.org/sdr/ABXA9800702), Jun 23, 1998: FITTING. CRACKED. FLOORBOARD ATTACH ANGLE CRACKED AT STATION 1140, RBL 55. REPAIRED IAW ABX REA NR D853-22888 AND DC8 SRM 51-3-0.
- [SDR ABXA9800552](https://openairdocs.org/sdr/ABXA9800552), Jun 22, 1998: FLANGE. CRACKED. AFT PRESSURE BULKHEAD AFT SIDE HORIZONTAL BEAM HAS 3 CRACK ON LOWER FLANGE AT AIRCRAFT CENTERLINE. REPAIRED IAW ABX REA D853-23407MR.
- [SDR ABXA9800706](https://openairdocs.org/sdr/ABXA9800706), Jun 21, 1998: FITTING. CRACKED. SPLICE FITTING CRACKED AT STATION 1300 - 1320 STRINGER 31L. REPLACED FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA9800705](https://openairdocs.org/sdr/ABXA9800705), Jun 21, 1998: WEB. CRACKED. LEFT WHEEL WELL AFT TORQUE BOX WEB CRACKED. REPAIRED IAW DC8 SRM 53-2-0, 51-1-8 AND 51-1-21.
- [SDR ABXA9800704](https://openairdocs.org/sdr/ABXA9800704), Jun 21, 1998: FITTING. CRACKED. LEFT LOWER FRAME TO CUSP FITTING CRACKED AT STATION 1070. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 9755584.
- [SDR ABXA9800713](https://openairdocs.org/sdr/ABXA9800713), Jun 20, 1998: FITTING. CRACKED. STATION 1040-1060 LONGERON 35L SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-21.
- [SDR ABXA9800674](https://openairdocs.org/sdr/ABXA9800674), Jun 20, 1998: SKIN. CRACKED. CRACK IN TRAILING EDGE SKIN FORWARD OF NR 2 SPOILER BOARD OUTBOARD CENTER HINGE. REPAIRED IAW DC8 SRM 57-2-0.
- [SDR ABXA9800709](https://openairdocs.org/sdr/ABXA9800709), Jun 19, 1998: FITTING. CRACKED. LONGERON 31L SPLICE FITTING IS CRACKED AT STATION 180 - 200. REPLACED SPLICE FITTING IAW DC8 SRM 51-11-20D.
- [SDR ABX9800711](https://openairdocs.org/sdr/ABX9800711), Jun 19, 1998: LONGERON. CORROSION. LONGERON 31R AT STATION 640-680 HAS CORROSION. REPAIRED IAW ABX REA D853-22883MR.
- [SDR ABXA9800683](https://openairdocs.org/sdr/ABXA9800683), Jun 18, 1998: RIB. CRACKED. LEFT WING LEADING EDGE RIB AT STATION XFS 778.750 IS CRACKED AT THE AFT LOWER END. REPAIRED RIB IAW DRAWING K05056.
- [SDR ABXA9800682](https://openairdocs.org/sdr/ABXA9800682), Jun 18, 1998: RIB. CRACKED. LEFT WING LEADING EDGE RIB AT STATION XFS 716.250 IS CRACKED AT AFT LOWER END. REPAIRED RIB IAW DRAWING K05056.
- [SDR ABXA9800681](https://openairdocs.org/sdr/ABXA9800681), Jun 18, 1998: MEMBRANE. CRACKED. LEFT CUSP MEMBRANE AT STATION 1480 TO 1500 IS CRACKED. REPAIRED CUSP MEMBRANE IAW DC8 SRM 53-2-0.
- [SDR ABXA9800680](https://openairdocs.org/sdr/ABXA9800680), Jun 18, 1998: FITTING. CRACKED. LONGERON 31R SPLICE FITTING BETWEEN STATION 440 TO 460 IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 53-1-0 AND 51-1-20D.
- [SDR ABXA9800679](https://openairdocs.org/sdr/ABXA9800679), Jun 18, 1998: FITTING. CRACKED. LONGERON 31R BETWEEN STATION 1040 TO 1060 SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 53-1-0 AND 51-1-20D.
- [SDR ABXA9800678](https://openairdocs.org/sdr/ABXA9800678), Jun 18, 1998: SKIN. CRACKED. RIGHT WING LEADING EDGE LOWER SKIN AT STATION XOLDI 6.225 IS CRACKED. REPAIRED LEADING EDGE SKIN IAW DC8 SRM 57-2-1.
- [SDR ABXA9800677](https://openairdocs.org/sdr/ABXA9800677), Jun 18, 1998: WEB. CRACKED. LEFT FORWARD ENTRY DOOR WEB IS CRACKED BELOW LOWER HINGE CUTOUT. REPLACED LOWER WEB IAW DRAWING 5615463 AND DC8 SRM 51-1-21.
- [SDR ABXA9800676](https://openairdocs.org/sdr/ABXA9800676), Jun 18, 1998: WEB. CRACKED. LEFT AFT ENTRY DOOR LOWER FORWARD CORNER WEB IS CRACKED. REPAIRED WEB IAW DC8 SRM 52-01 FIG 8.
- [SDR ABXA9800675](https://openairdocs.org/sdr/ABXA9800675), Jun 18, 1998: WEB. CRACKED. LEFT MAIN GEAR WHEEL WELL LOWER SUPPORT WEB CRACKED AT FS 870. REPAIRED WEB IAW DC8 SRM 53-2-0 AND 51-1-21.
- [SDR ABXA9800661](https://openairdocs.org/sdr/ABXA9800661), Jun 18, 1998: SKIN. CRACKED. RIGHT WING TOP SKIN AT STATION XRS 74 IS CRACKED AT STRINGER 9, 10, AND 11. REPAIRED RIGHT WING SKIN DC-8 SRM 57-2-1.
- [SDR ABXA9800715](https://openairdocs.org/sdr/ABXA9800715), Jun 17, 1998: FITTING. CRACKED. STATION 980-1000 STRINGER 23R END FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 3753306.
- [SDR ABXA9800710](https://openairdocs.org/sdr/ABXA9800710), Jun 17, 1998: FITTING. CRACKED. 680 BULKHEAD SEAT TRACK ATTACH FITTING CRACKED AT BL-0. REPLACED FITTING IAW DWG 4645517 AND DC8 SRM 51-1-20D.
- [SDR ABXA9800664](https://openairdocs.org/sdr/ABXA9800664), Jun 17, 1998: ANGLE. CRACKED. DRIVE LINK FITTING STIFFENER ANGLE CRACKED, LEFT WING, FLAP STATION 3.00. REPAIRED IAW DC8 SRM 53-8-1 AND 51-1-20.
- [SDR ABXA9800663](https://openairdocs.org/sdr/ABXA9800663), Jun 17, 1998: FITTING. CRACKED. STATION 980 - 1000 LONGERON 23L END FITTING CRACKED. REPLACED END FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA9800662](https://openairdocs.org/sdr/ABXA9800662), Jun 17, 1998: FITTING. CRACKED. LONGERON 31L SPLICE FITTING BETWEEN STATION 440 AND 460 CRACKED. REPLACED LONGERON SPLICE FITTING IAW DC8 SRM 53-1-0 AND 51-1-20D.
- [SDR ABXA9800665](https://openairdocs.org/sdr/ABXA9800665), Jun 16, 1998: FITTING. CRACKED. FS 960 FITTING CRACKED BETWEEN LONGERON 24L AND THE PRESSURE WEB. REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-3-0.
- [SDR ABXA9800667](https://openairdocs.org/sdr/ABXA9800667), Jun 14, 1998: SPLICE. CRACKED. LONGERON 34R CRACKED STATION 1140-1160. REPAIRED IAW DC8 SRM 53-2-2.
- [SDR ABXA9800668](https://openairdocs.org/sdr/ABXA9800668), Jun 13, 1998: FITTING. CRACKED. LONGERON 31L SPLICE FITTING CRACKED STATION 600-620. REPAIRED IAW DC8 SRM 51-1-20D.

All 82: https://openairdocs.org/model/douglas-dc-8-61f/reports.md

## STCs that may be installed (OpenAirDocs) (147, 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 SA2481WE](https://openairdocs.org/stc/SA2481WE): Installation of Trans Com Model 1357 movie projector and screen assemblies. Burrana Inc
- [STC SA3421NM](https://openairdocs.org/stc/SA3421NM): Installation of Hughes-Avicom video entertainment system. Burrana Inc. Lists DC-8 Series
- [STC SA5059NM](https://openairdocs.org/stc/SA5059NM): Installation of Ancra cargo conveyor system, P/N's 81381-11, 81382-11. Ancra International LLC
- [STC SA3140SO](https://openairdocs.org/stc/SA3140SO): Installation of a replacement coalescer filter, P/N 22D10 or 22D10-2. Purolator Facet, Inc
- [STC SA2800WE](https://openairdocs.org/stc/SA2800WE): Installation of dual Litton LTN-51 or LTN-72 Inertial Navigation System. Northrop Grumman Systems Corporation
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic LLC
- [STC ST01067LA](https://openairdocs.org/stc/ST01067LA): Installation of Litton LTR-97 fiber optic gyro systems. Northrop Grumman Systems Corporation
- [STC ST01467LA-D](https://openairdocs.org/stc/ST01467LA-D): Installation of Universal Avionics Terrain Avoidance Warning System and MFD-640 Multi Function Display(s). Zalinka Aviation Support, LLC
- [STC ST01468LA-D](https://openairdocs.org/stc/ST01468LA-D): Installation of Universal Avionics Flight Management System. Zalinka Aviation Support, LLC
- [STC SA630CE](https://openairdocs.org/stc/SA630CE): Installation of cargo pallets. Telair US LLC
- [STC SA1511GL](https://openairdocs.org/stc/SA1511GL): Installation of Type "C" containers. ABX Air Incorporated
- [STC SA1794GL](https://openairdocs.org/stc/SA1794GL): Incorporate anti-skid system inoperative and/or auto-ground spoilers inoperative landing field length data for Operations using 35° landing flaps. ABX Air Incorporated
- [STC SA1421GL](https://openairdocs.org/stc/SA1421GL): Installation of Supplemental Electric Heater. ABX Air Incorporated
- [STC SA1462GL](https://openairdocs.org/stc/SA1462GL): Installation of ABX Cargo Handling System. ABX Air Incorporated
- [STC SA1559GL](https://openairdocs.org/stc/SA1559GL): Installation of dual 20 Joule engine ignition system when powered by P&W JT3D-3B engines. ABX Air Incorporated
- [STC SA3496NM](https://openairdocs.org/stc/SA3496NM): Installation of ABX-C Cargo Container assembly. Airborne Express Air Inc
- [STC ST369CH](https://openairdocs.org/stc/ST369CH): Approve autopilot and/or flight director coupled approach with 35 landing flap selection. ABX Air Incorporated
- [STC SA7729SW](https://openairdocs.org/stc/SA7729SW): Installation of digital fuel quantity indicators, fuel totalizer, and capacitive fuel compensator units. Ontic Engineering and Manufacturing Inc
- [STC SA1360GL](https://openairdocs.org/stc/SA1360GL): Install Parker Hannifin Freon Air Conditioning System. ABX Air Incorporated
- [STC SA1616GL](https://openairdocs.org/stc/SA1616GL): Installation of Ametek digital fuel flow/fuel used indicator P/N10250N010F01. ABX Air Incorporated
- [STC SA1733GL](https://openairdocs.org/stc/SA1733GL): Installation of Vickers PV3-160-4B hydraulic pump. ABX Air Incorporated
- [STC SA1761GL](https://openairdocs.org/stc/SA1761GL): Installation of Kollsman P/N 35900-A2284 Mach airspeed indicator. ABX Air Incorporated
- [STC SA2320SO](https://openairdocs.org/stc/SA2320SO): Installation of the Fairchild F-800 digital flight data recorder system. ABX Air Incorporated
- [STC ST117CH](https://openairdocs.org/stc/ST117CH): Installation of expanded parameters. ABX Air Incorporated
- [STC ST125CH](https://openairdocs.org/stc/ST125CH): Installation of JET model AI-330 attitude indicator. ABX Air Incorporated
- [STC ST53CH](https://openairdocs.org/stc/ST53CH): Replacement of McD PN 4642526 compressor check valve flapper assembly with ABX Air, PN A04574. ABX Air Incorporated
- [STC SA3168NM](https://openairdocs.org/stc/SA3168NM): Installation of ANCRA Corp. End Restraints in the cargo pallet positions number one or eighteen. Ancra International LLC
- [STC SA3957NM](https://openairdocs.org/stc/SA3957NM): Installation of cargo system P/N 80080-10, -11, or -12. Ancra International LLC
- [STC SA2827WE-D](https://openairdocs.org/stc/SA2827WE-D): Installation of Collins FPC-75 part number 622-2615-012 or 622-2615-212 Ground Proximity Warning System Computer in conformance with United Airlines DAS-1-WE Approved Master List of drawings and documents for STC No. SA2827WE-D dated February 26, 1979 or later approved revisions. An alternate approved configuration consists of part number 622-2615-011 Rev. N or part number 622-2615-211 GPWS computer and a part number 622-2668-011 Barometric Altitude Computer installed in conformance with DAS-1-WE Approved Master List of drawings and related documents or later FAA approved revision (Continued on page 3.). United Airlines Inc
- [STC SA4-918](https://openairdocs.org/stc/SA4-918): 1. Aircraft wiring in accordance with Douglas Aircraft Co. Service Change #17 (UAL COA-0-1456) to provide an operational Aircraft Flight Data Rrecorder conforming to CAR Amendment 40-6, paragraph 40.208 with the following additions to assure recording of data during takeoff and landing roll: a. Relay to provide automatic start of recording when nose landing gear reaches airborne condition on takeoff. b. Time delay relay to turn off recorder one minute after nose landing gear reaches "on ground" condition, on landing. c. Installation of standard toggle switch on Systems Engineer's Console, to permit Second Officer to turn on recorder at start of takeoff run. 2. Install Waste King Flight Data Recorder #5424, TSO-C51. United Airlines Inc
- [STC SA611WE](https://openairdocs.org/stc/SA611WE): Interior configuration - 120 passenger single class 5-abreast seating per United Air Lines approved drawing lists: COA 2-2083 (Sheet #1 Revision February 17, 1964, Sheet #2 dated December 4, 1963, Sheet #3 Revision dated February 27, 1964 and, COA 2-2099 Revision dated December 17, 1963). United Airlines Inc
- [STC SA65WE](https://openairdocs.org/stc/SA65WE): Installation of a cockpit hydraulic replenishing system. See 15F-2044 Chg. B, 9F-4813 Chg. C, 6F-8140 Chg. C, 6F-8130 Chg. B, 3F-9025 Chg. A, 3F-9022, 3F-9023 Chg. A, IF-9882, 6F-8141 Chg. C. COA-2-1534 (ERs 1 - 4), App. V(UAL) to AFM SM-23889, App. IV (UAL) to AFM SM-23891, App. VII(UAL) to AFM LB-30582 or later FAA approved revisions. United Airlines Inc
- [STC ST01202WI-D](https://openairdocs.org/stc/ST01202WI-D): Modification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision. Rockwell Collins Inc
- [STC SA1341NM](https://openairdocs.org/stc/SA1341NM): Installation of CFMI CFM-56 engines and related changes. Boeing Company
- [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 ST01487CH](https://openairdocs.org/stc/ST01487CH): Installation of a Traffic Collision and Avoidance System (TCAS) TTR-921 and Models TPR901 system. Airborne Maintenance & Engineering Services (AMES)
- [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)

All 147: https://openairdocs.org/model/douglas-dc-8-61f/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [AF300P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191275281320260717175324.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [AF302](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178154048320260717175326.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [AF300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172513122320260717175322.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [M840105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154219509420260325172403.0001): Cylinder Assembly. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 840105 · Feb 17, 2026
- [M840105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140279722720260325180521.0001): Cylinder Assembly. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 840105 · Feb 17, 2026
- [WF334995](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108821019820250602133022.0001): Filter Element Lube Oil. Donaldson Company Inc · PMA PQ2432CE · Replaces Sundstrand 55956, AC-9649F-1… · May 23, 2025
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192694002020250923105634.0001): VOGT AERO · PMA PQ05310NM · Apr 22, 2025
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165781403520250923105628.0001): VOGT AERO · PMA PQ05310NM · Apr 22, 2025
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178263063620250923105931.0001): VOGT AERO · PMA PQ05310NM · Mar 4, 2025
- [3575-1251-07-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172611889620260729202728.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1251-07 · Mar 4, 2025
- [3575-1480-01-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170852615820260729202754.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1480-01 · Mar 4, 2025
- [3575-1251-01-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169467633820260729202723.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1251-01 · Mar 4, 2025
- [440-0150-5-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128051330520260729202746.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 440-0150-5 · Mar 4, 2025
- [3575-1480-07-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122566397220260729202800.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1480-07 · Mar 4, 2025
- [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
- [103154-909-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118409506520230727204617.0001): Safety Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 103154-909-2 · Apr 20, 2023
- [122618-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156194142520230907183534.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 122618-1-1 · Feb 24, 2023
- [320362-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152527095020230907183533.0001): Solenoid Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 320362-2 · Feb 24, 2023
- [383342-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133028187220230907183536.0001): Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 383342-1-1 · Feb 24, 2023
- [122666-2-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127534894520230907183535.0001): 1st Spool Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 122666-2-1 · Feb 24, 2023
- [105984-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119902323020230907183537.0001): Anti-Ice Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105984-2 · Feb 24, 2023
- [392900-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189455606920230907183331.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 392900-1-1 · Feb 23, 2023
- [108742-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159430638720230907183327.0001): Pressure Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 108742-2 · Feb 23, 2023
- [105976-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152035340520230907183326.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105976-1 · Feb 23, 2023
- [122594-3-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147106652220230907183318.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 122594-3-1 · Feb 23, 2023
- [122546-2-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145869651920230907183329.0001): Pressure Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 122546-2-1 · Feb 23, 2023
- [105980-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140197898520230907183328.0001): Butterfly Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 105980-2 · Feb 23, 2023
- [392160-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121943223620230907183325.0001): Differential Regulator & Shutoff. Honeywell International Inc. · PMA PQ1222NM · Replaces 392160-1 · 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
- [525254-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108708698020230907183333.0001): Actuator Assy Fuel Dump Chute. Honeywell International Inc. · PMA PQ1222NM · Replaces 525254-1 · Feb 23, 2023
- [392160-4-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108409609920230907183330.0001): Pressure Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 392160-4-1 · Feb 23, 2023
- [SM600BA100N22-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189709749720221130144515.0001): Remote Control Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces BAN7016-607 · Oct 31, 2022
- [160-066-80](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185108580520221130144357.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0012-80 · Oct 31, 2022
- [1526-066-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166131476020221130144341.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0002-3 · Oct 31, 2022
- [1200-066-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164799404820221130144328.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0009-15 · Oct 31, 2022
- [H20-9B](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139073107020221130144509.0001): Switch. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces H20-9B · Oct 31, 2022
- [SM600BA20N25](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123850243020221130144521.0001): Remote Control Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces SM600BA20N25 · Oct 31, 2022
- [160-083-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123725710320221130144400.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0012-70P · Oct 31, 2022
- [1200-066-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115243180520221130144326.0001): Circuit Breaker. SAFRAN Power USA LLC · PMA PQ1478CE · Replaces 5D0009-10 · Oct 31, 2022
- [3755705-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192798688420220929114601.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3755705-1 · Sep 27, 2022
- [3718232-504](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188697278020220929114502.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-504 · Sep 27, 2022
- [3718232-503](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188413757320220929114501.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-503 · Sep 27, 2022
- [3718232-505](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183899181420220929114502.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-505 · Sep 27, 2022
- [3718232-516](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181531934020220929114509.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-516 · Sep 27, 2022
- [3889142-510](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180513779620220929113517.0001): PANEL A. AmSafe Bridport · PMA PQ2482NM · Replaces 3889142-510 · Sep 27, 2022
- [3889142-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179267638820220929113509.0001): PANEL A. AmSafe Bridport · PMA PQ2482NM · Replaces 3889142-1 · Sep 27, 2022
- [3718232-511](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178457873520220929114507.0001): NET ASSY. AmSafe Bridport · PMA PQ2482NM · Replaces 3718232-511 · Sep 27, 2022

All of them: https://openairdocs.org/model/douglas-dc-8-61f/pma.md

## The same model under other registry codes

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

- [Mcdonnell Douglas DC-8-61F](https://openairdocs.org/model/mcdonnell-douglas-dc-8-61f): 0 registered aircraft, registry code 302195D

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