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 RRXA991342Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 33 RIGHT END TIE FITTING AT STA 8.00. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW FAA APPROVED TENNESSEE TECHNICAApr 21, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829660Stringer · corrodedINSPECTION TYPE:N/A, STR 24 AT STA 1667 HEAVLY CORRODED. REMOVED SECTION OF STRINGER SPLICED IN NEW SECTION PER 53-2-2.Apr 20, 1999 · N814UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829657Rib · crackedINSPECTION TYPE:C2, LT WING L/E RIB AT FS 603.75 IS CRACKED AT THE AFT LOWER FASTENER. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Apr 20, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829592Intercostal · corrodedINSPECTION TYPE:C3, FS 1260-1280 AT LONG 33R, THE INTERCOSTAL UPPER FLANGE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9754949 AND SRM 51-1-20D.Apr 20, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829589Frame · corrodedINSPECTION TYPE:C3 FS 1060 FRAME AT LONG 35L TO 35R IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND REPAIRED FRAME IAW SRM 53-2-0.Apr 20, 1999 · N840UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829580Rib · crackedINSPECTION TYPE:C2 LEFT WING INBOARD RIB AT XOLDI 6.225 IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.Apr 20, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829486Fitting · crackedINSPECTION TYPE:C2, INTERCOSTAL AT LONG 35R ATTACH FITTING IS CRACKED AT FS 1240. REMOVED, AND REPLACED FITTING IAW SRM 51-1-20D.Apr 20, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991359Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, RT UPPER CUSP FRAME AT STA 560 ATTACH ANGLE, LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DAC DWG 5753488 AND DCApr 20, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991347Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTTOM OF FUSELAGE MARKER BEACON ANTENNA FROM BASE AROUND SKIN BETWEEN STA 680 AND STA 702 AT LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATApr 20, 1999 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991333Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, IN SCREW HOLES, LEADING EDGE CENTER SECTION LOWER SURFACE, 46 FORWARD OF FRONT SPAR AT STA XFS 286.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATEDApr 20, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR UPS99829600Fitting · corrodedINSPECTION TYPE:C3, LONG 35R SPLICE AT FS 1270 IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Apr 19, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829578Angle · crackedINSPECTION TYPE:C2, THE RT STA 98 FLAP ACTUATOR ATTACH FITTING INBD MOUNT ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 3643319 AND SRM 51-1-20D AND 51-3-0.Apr 19, 1999 · N880UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99829576Rib · crackedINSPECTION TYPE:C2 RT WING L/E, INBD STA XOLDI 6.225 RIB IS CRACKED ABOVE THE PNEU DUCT. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.Apr 19, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829569Fitting · crackedINSPECTION TYPE:C2, RT WING FLAP HINGE SUPPORT FITTING I/B SIDE GAVE CRACK INDICATION. REPLACED BRACKET.Apr 19, 1999 · N819UP · Doug DC873F · Wing, Control Surface Attach FittingsSDR UPS99829546Rib · crackedINSPECTION TYPE:C2, RT WING L/E RIB AT XS 491.193 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 19, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829530Fitting · crackedINSPECTION TYPE:C2 LEFT HORIZONTAL STAB AT STA X 70 APPROX 18 INCHS IN FRONT OF SPAR VERTICAL SUPPORY FITTING CRACKED. REMOVED AND REPLACED FITTING DOUBLER IAW DC-8 SRM 55-2-0.Apr 19, 1999 · N819UP · Doug DC873F · Horizontal Stabilizer StructureSDR UPS99829521Fitting · crackedINSPECTION TYPE:C2 RT LONG 24 UPPER FITTING AT FS 879 HAS CRACK AT ATTACHMENT HOLES. REMOVED CRACK FITTING, LOCATE NEW FITTING, DRILL, AND REAM EXISTING HOLES IN FITTING IAW DC-8 SRM 51-3-2 AND INSTALLED IAW DC-8 SRM 51- 1-20D.Apr 19, 1999 · N819UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99829520Fitting · corrodedINSPECTION TYPE:C2 LONG 24 RT UPPER FITTING AT FS 940 HAS CORROSION AT BOTTOM ATTACHMENT HOLES. REMOVED CORRODED FITTING, LOCATE NEW FITTING DRILL REAMED EXISTING HOLES IN FITTING IAW DC-8 SRM 51-3-2 AND INSTALLED IAW DC-8 SRM 51-1 -20D,CPCP.Apr 19, 1999 · N819UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99829500Rib · crackedINSPECTION TYPE:C2, LT WING L/E RIB AT XFS 635.0 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 19, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829499Rib · crackedINSPECTION TYPE:C2, LT WING L/E RIB AT XFS 628.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 19, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829498Rib · crackedINSPECTION TYPE:C2, LT WING L/E RIB AT XFS 628.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 19, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829497Rib · crackedINSPECTION TYPE:C2, LT WING L/E RIB AT XFS 622.5 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 19, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829496Rib · crackedINSPECTION TYPE:C2, LT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 19, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829494Rib · crackedINSPECTION TYPE:C2, LT WING L/E RIB AT XFS 641.25 IS CRACKED AT THE AFT UPPER FASTENER STOP DRILLED AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 19, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829491Fitting · crackedINSPECTION TYPE:C2, THE RT STA 410 FLAP CANOE FITTING, OTBD SIDE FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-3-0.Apr 19, 1999 · N880UP · Doug DC873F · Trailing Edge FlapsSDR UPS99829474Rib · crackedINSPECTION TYPE:C2 RT WING L/E RIB AT XFS 691.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.Apr 19, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829451Skin · crackedINSPECTION TYPE:C1, LT WING L/E SKIN AT FS 710 IS CRACKED AT THE AFT LWR CORNER. REPAIRED SKIN IAW SRM 51-2-1.Apr 19, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR RRXA991358Shim · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LT UPPER CUSP FRAME AT STA 360 FROM SHIM AT ATTACH ANGLE, LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SHIM AND FITTIApr 19, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991356Shim · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LT UPPER CUSP AT STA 400 FRAME ATTACH ANGLE SHIM FROM UNDER SHIM MARKED 12 NR 83. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SHIM IAWApr 19, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991355Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SPLICE, LONGERON 36, BETWEEN STA 1726 AND STA 1745. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE AND LONGERON SECTION IAWApr 19, 1999 · N606AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829658Angle · crackedINSPECTION TYPE:C2, CABIN FLOORBEAM SUPPORT ATTACH ANGLE IS CRACKED FS 680, RBL 24. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 4645517 AND SRM 51-1-20D.Apr 18, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829616Skin · corrodedINSPECTION TYPE:C2, LT I/B SLOT VANE I/B END HAS MODERATE CORROSION. CUT OUT DAMAGED AREA AND REPAIRED IAW EO DC8-5720-7767A.Apr 18, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS99829584Longeron · crackedINSPECTION TYPE:C2 LONGERON 27R IS CRACKED BETWEEN FS 55 AND 70. REMOVED DAMAGED LONGERON, FABRICATED, AND REPLACED IAW DWG 3648666 AND SRM 51-1-20D.Apr 18, 1999 · N880UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829577Frame · crackedINSPECTION TYPE:C2 FS 55 FRAME IS CRACKED AT LONGERON 24L, AROUND THE ROD ATTACHMENT. CUT OUT DAMAGED AREA AND REPAIRED SRM 53-2-0 FIG 2.Apr 18, 1999 · N880UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829544Frame · crackedINSPECTION TYPE:C2, FS 55 FRAME IS CRACKED AT LONG 24R, AROUND THE ROD ATTACHMENT. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 2.Apr 18, 1999 · N880UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829542Fitting · crackedINSPECTION TYPE:C2 FRAME 660 ATTACH FITTING AT LONG 36 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Apr 18, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829529Skin · crackedINSPECTION TYPE:C2 EXTERIOR FUSELAGE SKIN CRACKED AT FS 40, LONGERON 30L AT DOOR CUTOUT. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 13.Apr 18, 1999 · N880UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829527Fitting · corrodedINSPECTION TYPE:C2, HEAVY CORROSION ON T FITTING, FS 660 AT LONG 36. REPAIRED FITTING IAW DHC SK880-110. CPCPApr 18, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829519Base · crackedINSPECTION TYPE:C CRACKED BASE FOR LEFT GEAR WELL HYD. RESERVOIR OUTBOARD FWD SIDE CRACK PREVIOUSLY REPAIRED IAW DC-8 SRM57-2-0, DOUBLER WAS INSTALLED.Apr 18, 1999 · N819UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829501Seat Track · corrodedINSPECTION TYPE:C3 MAIN CABIN SEAT TRACK, FS 370 TO 530, RBL 60, LWR FLANGE IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK FROM FS 370 TO 530, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-2-3.Apr 18, 1999 · N840UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99829495Skin · crackedINSPECTION TYPE:C2, LT WING L/E UPPER SKIN AT XFS 660 IS CRACKED AT 1 FASTENER. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.Apr 18, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS99829493Skin · crackedINSPECTION TYPE:C2, RT WING L/E LWR SKIN AT XFS 710 IS CRACKED AT 1 FASTENER HOLE. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 57-2-0 FIG 24.Apr 18, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS99829487Skin · crackedINSPECTION TYPE:C2, RT WING L/E UPPER SKIN AT XFS 710.0 IS CRACKED AT 1 SCREW HOLE. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.Apr 18, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS99829473Skin · corrodedINSPECTION TYPE:C2 RT WING L/E, LWR SKIN AT XFS 708 IS CORRODED OUT OF LIMITS AT 1 EA SCREW HOLE. REPAIRED SKIN IAW EO DC8-5720-7787.Apr 18, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS99829471Skin · crackedINSPECTION TYPE:C2 RT WING L/E LWR SKIN AT XW 761.695 IS CRACKED AT 1 SCREW HOLE. REPAIRED SKIN IAW EO DC8-5720-4087.Apr 18, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS99829357Floorbeam · corrodedINSPECTION TYPE:A/CK, CORROSION FOUND AT THE FLOORBEAM BY THE LT SERVICE DOOR. UPON FURTHER INVESTIGATION THE LT CIRCUMFERENTIAL FRAME AT STA 1667 FROM STR 21 TO STR 23 TO HAVE EXTENSIVE CORRISION. *S/D* REMOVED LOWER SECTION OF FRAME, FABED SPLICES AND INSApr 18, 1999 · N814UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS99829356Floorbeam · crackedINSPECTION TYPE:A/CK, CRACK AT FLOORBEAM AFT OF SERVICE DOOR. UPON FURTHER INVESTIGATION FOUND CRACK AT CIRCUMFERENTIAL FRAME AT STA 1680 STR 21 NOT AT FLOORBEAM AS FIRST REPORTED. *S/D* REMOVED DAMAGED SECTION OF FRAME, FABED SPLICES AND INSTALLED REPAIR PApr 18, 1999 · N814UP · Doug DC873F · Fuselage Main, Floor BeamSDR DHL99807002Panel · fireON FINAL APPROACH TO MIA , HEARD LOUD POPPING NOISE BEHIND S/O PANEL, F/O REPORTED SMOKE AND S/O SAW FLAMES BEHIND PANEL. USED HALON EXTINGUISHER TO PUT OUT FIRE. ACCOMPLISHED EMERGENCY LANDING.Apr 18, 1999 · N807DH · Doug DC873F · Instrument PanelSDR UPS99829504Fitting · crackedINSPECTION TYPE:C3, MAIN CABIN SUPPORT FITTING AT FS 55, RBL 48, FWD OTBD IS CRACKED. REMOVED AND REPLACED FITTING EAW SRM 51-1-20D AND 51-1-21.Apr 17, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829335Valve · inoperativeINSPECTION TYPE:N/A, AFTER LANDING LEFT BRAKE DID NOT APPEAR TO BE APPLYING BRAKE PRESSURE. FOUND LEFT FORK ON HYD PWR BRAKE BROKEN. REMOVED AND REPLACED VALVE PER 32-42-02. LEAK CHECKS, PRESSURE CHECKS AND DECAY CHECKS GOOD PER MM REFERENCED ABOVE. (P/N 3Apr 17, 1999 · N801UP · Doug DC873F · Landing Gear Brake System
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