Douglas DC-8-73F

Service difficulty reports · 15,471

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC873F'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS98828146Rib · crackedINSPECTION TYPE-C, L/E RIB CRACKED LT XFS785 UPPER RIB LT WING. REPAIRED IAW SRM 57-2-0.Nov 5, 1998 · N894UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS98828145Rib · crackedINSPECTION TYPE-C, L/E RIB CRACKED XFS 772.5 LT WING. REPAIRED IAW SRM 57-2-0.Nov 5, 1998 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS98828141Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 803.750 UPPER. REPAIRED IAW SRM 57-2-0.Nov 5, 1998 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS98828140Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 810 UPPER. REPAIRED IAW SRM 57-2-0.Nov 5, 1998 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS98828139Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 816.250 UPPER. REPAIRED IAW SRM 57-2-0.Nov 5, 1998 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS98828138Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT XFS 778.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.Nov 5, 1998 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS98828135Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.Nov 5, 1998 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS98828134Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG.Nov 5, 1998 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS98828133Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT XFS 622.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACKED AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.Nov 5, 1998 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS98828132Rib · crackedINSPECTION TYPE-C3, RT WING L/E RIB AT XFS 660.0 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.Nov 5, 1998 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR DHL9980136CSeat Track · wornAT C-CHECK, SEAT TRACK NR 5 WORN AT STA 239. REMOVED DAMAGED SECTION AND FABRICATED REPAIR PLUG PER SRM 53-2-3.Nov 5, 1998 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS98828222Skin · crackedINSPECTION TYPE-C, LT FUSELAGE SKIN AT STA 55 AT STR 21R IS CRACKED AT THE DOUBLER. REPAIRED IAW DC8-5330-0793-I.Nov 4, 1998 · N894UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS98828144Skin · crackedINSPECTION TYPE-C, RT WING L/E UPPER SKIN AT XFS 210 CRACKED. REPAIRED IAW SRM 57-2-0.Nov 4, 1998 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS98828143Skin · crackedINSPECTION TYPE-C, RT WING L/E UPPER SKIN AT XW 485 IS CRACKED IN 3 PLACES. REPAIRED IAW SRM 57-2-1.Nov 4, 1998 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS98828137Skin · crackedINSPECTION TYPE-C, RT WING L/E UPPER SKIN AT THE SPAR AT XS 433 HAS INTERGRANULAR CORROSION AND IS CRACKED. REPAIRED IAW SRM 57-2-1.Nov 4, 1998 · N894UP · Doug DC873F · Wing, Plate/SkinSDR DHL9980109CSkin · delaminatedAT C-CHECK, LT WING T/E LOWER PANEL STA 75 DELAMINATED. REPAIRED PANEL AND REINSTALLED PER SRM 51-1-8.Nov 4, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980142CSeat Track · damagedAT C-CHECK, SEAT TRACK 36 PLUG ELONGATED AT STA 1400. REMOVED AND INSTALLED FABRICATED PLUG PER SRM 53-2-3.Nov 3, 1998 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980137CSeat Track · damagedAT C-CHECK, SEAT TRACK NR 6 WORN AT STA 230. REMOVED AND REPLACED DAMAGED PLUG PER SRM 53-2-3.Nov 3, 1998 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL99801105Angle · crackedAT C-CHECK, AFT LOWER CARGO COMPT RT AT STA 1440 LONG R30 SHOWS CRACK DAMAGE ON ATTACH ANGLE. STOP DRILLED, FABRICATED ANGLE REPAIR AND INSTALLED PER SRM 51-1-21.Nov 3, 1998 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980107CSkin · delaminatedAT C-CHECK, LEFT WING T/E LOWER AREA AT STA 120 DELAMINATED. REPAIRED PER SRM 51-12-1.Nov 3, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR UPS98828052Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY BATTERY PACK.Nov 2, 1998 · N806UP · Doug DC873F · Emergency LightingSDR UPS98828050Container · damagedINSPECTION TYPE-N/A, ESCAPE SLIDE KEEPS FALLING OUT OF ITS CONTAINER. INSTALLED NEW CONTAINER AS REQUIRED, ESCAPE AND GRIP BAR OPS NORMAL.Nov 2, 1998 · N840UP · Doug DC873F · Escape SlideSDR UPS98828048Fitting · corrodedDURING AS/E INSP NOTED SUSPECTED CORROSION ABOVE MLG I/B TORQUE TUBE RT SIDE. UPON FURTHER INSP FOUND CORRISION AT MATING SURFACE OF 3 ATTACH FITTINGS OF I/B LONG 24 ABOVE MLG. RELEASED FOR FERRY FLIGHT TO SAT FOR REPAIR.Nov 1, 1998 · N801UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980190CBeam · corrodedAT C-CHECK, WHEELS NR 5 AND NR 6 BOGIE BEAM ASSY CORROSION. REMOVED AND REPLACED BOGIE BEAM PER MM 32-43-0.Nov 1, 1998 · N801DH · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR DHL9980126CSeat Track · damagedAT C-CHECK, SEAT TRACK NR 4 PLUG DAMAGED AT STA 151. REMOVED AND REPLACED PLUG PER SRM 53-2-3.Nov 1, 1998 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS98828106Fitting · corrodedINSPECTION TYPE-SP, FITTING AT FS 879.35 FOUND TO HAVE HEAVY CORROSION AROUND BOLT HOLES AND FLANGES BETWEEN LONGERON 24 AND CUSP RT W/W. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Oct 31, 1998 · N801UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98828105Longeron · corrodedINSPECTION TYPE-SP, TRANSFERED FROM LOG PAGE 709350 ITEM 1, CORROSION AT MATING FLANGE OF 3 ATTACH FITTINGS ON LONGERON 24 IN RT W/W AT STA 879, 902, AND 920. REMOVED AND REPLACED LONGERON 24 RT IAW DWG 5750198 AND SRM 51-1-20D AND SRM 51-3-1.Oct 31, 1998 · N801UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA99001Rod · brokenON WALKAROUND, FOUND NOSE GEAR RT AFT DOOR SUPPORT ROD BROKEN. ALSO, SKIN DAMAGE AROUND ATTACHMENT POINTS AT DOOR HINGES. REMOVED BROKEN NLG RT AFT DOOR ROD ASSY AND INSTALLED SERV ALT DOOR ROD ASSY (P/N 4648253) IAW MM 32-22-1. ADDITIONALLY INSPECTED LT AFOct 31, 1998 · N791FT · Doug DC873F · Landing Gear Door Retract SectionSDR DHL9980182CRib · crackedAT C-CHECK, LT WING CTR L/E INTERIOR LOWER I/B INTERNAL AREA STA 291.5 FOUND CRACK ON LOWER RIB. STOP DRILLED HOLE AND FABRICATED REPAIR DOUBLER PER SRM 51-1-21, 6 X 1.25.Oct 30, 1998 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR RRXA99731Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CABIN FLOORBEAM AT STA 1260 BL 40R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE REPAIR AND FILLER IAW DC-8 SRM 53-2-0, FIG 1B. (Oct 29, 1998 · N795FT · Doug DC873F · Fuselage Main, Floor BeamSDR DHL9980199CRib · crackedAT C-CHECK, RT WING CENTER LOWER INTERNAL AREA AT STA 300 FOUND CRACKD ON LOWER RIB. DRILLED TOP HOLE, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-1-21, 6 X 1.25.Oct 29, 1998 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR RRXA99733Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1250 BL 48R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3,Oct 28, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99732Floorbeam · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CABIN FLOORBEAM AT STA 1560 BL 16L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW DC-8 SRM 53-2-0, FIG 1B. (Oct 28, 1998 · N795FT · Doug DC873F · Fuselage Main, Floor BeamSDR DHL9980189CFairing · damagedAT C-CHECK, ELONGATED HOLES AND BARE METAL SPACERS ON FAIRING PANEL 5704072-403. FABRICATED DOUBLER PER SRM 53-2-0 AND INSTALLED PER SRM 51-1-21, 5 X 6.Oct 28, 1998 · N801DH · Doug DC873F · Empennage StructureSDR DHL9980188CAngle · crackedAT C-CHECK, LT WING LEADING EDGE INTERIOR UPPER O/B AREA AT XFS 520 FOUND CRACKED. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-21.Oct 28, 1998 · N801DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980187CAngle · crackedAT C-CHECK, LT CENTER WING LEADING EDGE UPPER O/B AREA STA XFS 520 FOUND CRACKED. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE PER SRM 51-1-21.Oct 28, 1998 · N801DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL99801100Tr Unit · dentedAT C-CHECK, LEFT T/R EXTERNAL SURFACE FOUND SEVERAL SCRATCHES AND DENTS AROUND NR 2 ENGINE. FABRICATED AND INSTALLED DOUBLER PER SRM 71-2-8, 4 DIA.Oct 27, 1998 · N801DH · Doug DC873F · Engine Thrust ReverserSDR RRXA99734Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1280 TO 1300 BL 48R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRMOct 24, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR DHL9980186CAngle · crackedAT C-CHECK, RT WING T/E INTERIOR AREA AT STA 463 JUST ABOVE NR 4 PYLON ON I/B SIDE FOUND CRACK ON VERTICAL ANGLE. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-1-21.Oct 24, 1998 · N801DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980185CShim · crackedAT C-CHECK, RT WING L/E LOWER AREA AT STA 463 JUST ABOVE NR 4 PYLON ON LT SIDE FOUND BROKEN SHIM ON LOWER SPAR MATING AREA. REMOVED AND FABRICATED LOWER SHIM PER SRM 51-1-21.Oct 24, 1998 · N801DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980184CAngle · crackedAT C-CHECK, LEFT WING L/E INTERIOR AREA AT STA 463 JUST ABOVE NR 1 PYLON ON I/B SIDE FOUND CRACKED ANGLE SUPPORT. FABRICATED ANGLE PER SRM 57-3-2.Oct 24, 1998 · N801DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980183CShim · crackedAT C-CHECK, LT WING L/E LOWER AREA AT STA 463 JUST ABOVE NR 1 PYLON LT SIDE FOUND BROKEN SHIM. TRIMMED AREA, WITHIN LIMITS.Oct 24, 1998 · N801DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980181CRib · crackedAT C-CHECK, RT WING CTR L/E INTERIOR LOWER I/B INTERNAL AREA AT STA 291.5 FOUND CRACK IN LOWER RIB. STOP DRILLED AND FABRICATED REPAIR DOUBLER PER SRM 57-2-0, 6 X 1.25.Oct 24, 1998 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL9980150CSkin · damagedAT C-CHECK, L/W UPPER SURFACE T/E BETWEEN STA XRS 391 AND XW 421 METAL SEAL STRIP DAMAGE. REMOVED METAL STRIP DAMAGE, FABRICATED NEW SEAL AND INSTALLED PER SRM 51-1-15, 5 X 1.Oct 24, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR RRXA99735Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1568 TO 1577 BL 2L TO 6L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-Oct 23, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR DHL9980179CSeat Track · damagedAT C-CHECK, FLIGHT ENGINEER FWD SEAT TRACK SHOWS HOLES ELONGATED. REMOVED AND REPLACED SEAT TRACK PER SRM 51-3-0.Oct 23, 1998 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980178CSkin · damagedAT C-CHECK, REPLACED SKIN FROM STA 210 TO 450 STR 21L TO 31L. REMOVED AND REPLACED SKIN PER DAC DRAWING 5755230.Oct 21, 1998 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL9980121CPanel · delaminatedAT C-CHECK, PANEL 162Q DELAMINATED INSIDE RT HAND CORNER. REMOVED DELAMINATED PANEL, REPAIRED AND REINSTALLED PER SRM 51-3-0.Oct 21, 1998 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL9980120CFairing · delaminatedAT C-CHECK, PANEL 261K SHOWS DELAMINATION. REMOVED AND REPAIRED PANEL PER SRM 51-3-0.Oct 21, 1998 · N801DH · Doug DC873F · Aerodynamic FairingsSDR 98ZZZX4212Beam · crackedAT C-CHECK, CRACKS WERE FOUND IN THE J-BEAM WHICH IS ATTACHED TO THE AFT FACE OF THE AFT PRESSURE BULKHEAD. THE CRACKS ORIGINATE IN THE RADII ADJACENT TO ATTACH BOLTS APPROXIMATELY ONE INCH EACH SIDE OF THE AIRCRAFT CENTERLINE. SUBMITTER STATED THE CRACKS APOct 21, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous Structure
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