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"

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SDR UPS05845405Rib · crackedCRACK IN RIB AT LT INBD GROUND SPOILER INBD MOUNT FITTING (MARKED). STOP DRILLED CRACK REF SRM 57-02-00 1199249 9/12/05. ACCOMPLISHED HFEC OF AREA NO DEFECTS NOTED. REPAIRED RIB AS PER DC8-SRM 57-02-00-51-1-20 SEE LOG PAGE 418971 M-3 FOR FITTING ASSY-END.Sep 12, 2005 · N810UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845553Fitting · corrodedINSPECTION TYPE:C3 CORROSION ON BACK UP FITTING AT STA 320 BETWEEN L33R-L34R. REMOVED BACK UP FITTING AND INSTALLED REPLACEMENT FITTING AND CLIPS IAW SRM 51-1-20D AND 51-3-0.Sep 11, 2005 · N874UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845517Fitting · corrodedINSPECTION TYPE:C3 DEEP CORROSION PIT OR DRILL START IN BATHTUB FITTING TA STA 315 BETWEEN L33R AND L34R. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-1-20D, 51-3-0 AND 51- 1-21.Sep 11, 2005 · N874UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845516Intercostal · corrodedINSPECTION TYPE:C3 HEAVY CORROSION ON INTERCOSTAL AT STA 1079 L35L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW 51-1-20D AND DWG 9758 507.Sep 11, 2005 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05845389Slide · misinstalledUNABLE TO READ PRESSURE ON EMERGENCY SLIDE ON ENTRY DOOR, NEED TO BE REPACKED. REMOVED AND REPLACED COVER.Sep 11, 2005 · N810UP · Doug DC873F · Escape SlideSDR UPS05845515Fitting · crackedINSPECTION TYPE:C3 INSIDE 60 HOLE, LONGERON END FITTING CRACKED 2" LONG AT STA 1766 L10R. REMOVED AND REPLACED END FITTING IAW SRM 51-3-0, 51-1-21 AND 51-1-20D.Sep 10, 2005 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05845490Fitting · crackedRT WING FUEL TANK NR 4 ALTERNATE STA XW 408 LWR STR NR 58 END FITTING CRACKED 2" LONG. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-1-20D.Sep 10, 2005 · N874UP · Doug DC873F · Wing, Attach FittingsSDR UPS05845489Fitting · crackedLT WING XW 408 STRINGER NR 58 UNDER THE BOOST PUMP FITTING CRACKED. REMOVED AND REPLACED BOOST PUMP FITTING IAW SRM51-1-20D AND 51-1-21.Sep 10, 2005 · N874UP · Doug DC873F · Wing, Attach FittingsSDR UPS05845488Fitting · crackedLT WING XW 408 STRINGER NR 59 UNDER THE BOOST PUMP FITTING CRACKED. REMOVED AND REPLACED BOOST PUMP FITTING IAW SRM 51-1-20D AND 51-1-21.Sep 10, 2005 · N874UP · Doug DC873F · Wing, Attach FittingsSDR DHL2005806535Skin · corrodedLWR FUSELAGE EXTERIOR SKIN CORRODED, BS 1265.000 L-36 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, DWG U80-R28 REV. IR DATED 08-08-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG.Sep 9, 2005 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05845550Tee Fitting · corrodedC3 TEE CHORD CRACKED STA 860 RBL 40 UPPER AFT END OF CENTER TANK LOOKING FROM INSIDE MAIN CABIN. AFTER FURTHER EVALUATION CRACK FOUND TO BE CAUSED BY INTERGRANULAR CORROSION, CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-5 FIG 12 AND DWGSep 9, 2005 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845549Fitting · crackedLEFT FWD LOWER TRAP FITTING IS CRACKED. REMOVED AND REPLACED TRAP FITTING IAW DC-8 SRM 51-3-0 AND 51-2-20D.Sep 9, 2005 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845514Skin · crackedINSPECTION TYPE: C3, CRACK ON FUSEAGE SKIN STA 1746 L15R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-02-01, 53-05-03, 51-1-26, 51-1-20D AND 51-1-21.Sep 9, 2005 · N874UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05845377Battery Pack · failedINSPECTION TYPE:N/A DURING ROUTINE MX, EMERGENCY LIGHTING WOULD NOT TEST. REMOVED AND REPLACED BATTERY PACK ASSY IAW AMM 33-50-01-2, EMERGENCY LIGHTING OPS CHECKS NORMAL.Sep 9, 2005 · N808UP · Doug DC873F · Emergency LightingSDR UPS05845428Doubler · corrodedINSPECTION TYPE:C3 MAIN CABIN CENTER WING BOX STA 960 TO 980 RBL 65 FINGER DOUBLER HAS CORROSION. REMOVED FINGER DOUBLER, REMOVED CORROSION FROM DOUBLER AND SUBFLOOR FOUND DOUBLER OUT OF LIMITS. FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 51-1-21, 53-02-Sep 8, 2005 · N874UP · Doug DC873F · Wing, Center BoxSDR UPS05845417Cusp Web · crackedINSPECTION TYPE:C3, MAIN DECK STA 1535 WEB AT CUSP AREA IS CRACKED APPROX .5 INCH. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 23 AND DWG 9753254.Sep 8, 2005 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05845548Door Frame · corrodedINSPECTION TYPE:C3 "B" PIT DOOR TORQUE JAMB FROM FS 520-560 HAS CORROSION AROUND NUT PLATES. REMOVED CORROSION AROUND NUT PLATES AND FOUND IN LIMITS. FOUND CORROSION ON FRAME AT FS 540 L36. CORROSION FOUND OUT OF LIMITS, CUT OUT DAMAGE, FABRICATED, AND INSTSep 7, 2005 · N801UP · Doug DC873F · Fuselage Main, StructureSDR UPS05845594Fitting · crackedINSPECTION TYPE:C3 STA 3 LT FLAP TRACK ATTACH POINT IS CRACKED. REMOVED AND REPLACED STA 3 LT FLAP TRACK ATTACH POINT FITTING IAW DC-8 SRM 51-3-0, 51-1-21, AND 51-1-20D.Sep 6, 2005 · N801UP · Doug DC873F · Trailing Edge FlapsSDR DHL2005806537Longeron · crackedAFT CARGO COMPT L-36 CRACKED 7 INCHES BETWEEN STA 1270 & 1280. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, CUT OUT CRACKED LONGERON SEGMENT, PERFORMED NDT INSP OF WORK AREA IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK NEITHER CORROSION FOUND. FABRICATED NEW Sep 6, 2005 · N806DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2005806536Longeron · crackedAFT CARGO COMPT L-34R CRACKED 7.5 INCH BETWEEN STA 1260 & 1280. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, CUT OUT CRACKED LONGERON SEGMENT, PERFORMED NDT INSPECTION OF WORK AREA. NO CRACK NEITHER CORROSION FOUND. FABRICATED NEW LONGERON SEGMENT. PERFORMESep 6, 2005 · N806DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2005806538Longeron · crackedAFT CARGO COMPT L-34L CRACKED 1.5 INCH BETWEEN STA 1260 & STA 1280. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, CUT OUT CRACKED LONGERON SEGMENT, PERFORMED NDT INSP OF WORK AREA, NO CRACK NEITHER CORROSION FOUND. FABRICATED NEW LONGERON SEGMENT. PERFORMED NDSep 6, 2005 · N806DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2005806532Fitting · corrodedITEM REF NR 041339: AFT CARGO COMPT. SPLICE FITTING CORRODED (STA 1260.000-1280.000, L-36) MAJOR REPAIR, PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED CORROSION FROM SPLICE FITTING (STA 1260.000-1280.000 L-36) IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMSep 4, 2005 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2005806534Fitting · crackedITEM REF NR 040974: FWD CARGO COMPARTMENT, FLOORBEAM FITTING CRACKED 0.250 IN, STA 280.000 BL 0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALASep 4, 2005 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845529Rib · crackedC3 - RT WING LE UPPER RIB CRACKED AT XS 484.895. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA. REPAIR ANGLES IAW SRM 57-2-0 FIG 2, 53-3-3 FIG 5.Sep 4, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845528Rib · crackedC3 - RT WING LE UPPER RIB IS CRACKED AT XFS 347.750. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA. REPAIR ANGLES IAW SRM 57-2-0 FIG 2 AND 57-3-3 FIG 5.Sep 4, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845486Rib · crackedRT WING LE LOWER RIB IS CRACKED AT XFR 791.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2, 51-1-21 AND 51-1-20D.Sep 4, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845424Rib · chafedINSPECTION TYPE:C3, RT WING L/E LOWER RIB IS CHAFED AT XFS 422.750. BLEND OUT OF LIMITS. FABRICATED AND INSTALLED 2 EA ANGLE REPAIRS IAW SRM 57-2-0 FIG 6, 57-3-3 FIG 5 AND 51-1-20D.Sep 4, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845416Stiffener · crackedINSPECTION TYPE: C3, RIGHT WING L/E, OUTBOARD STUB WING L/E STIFFENER CRACKED 1 INCH LONG AT XW 463.000 NR 4 PYLON UPPER. REMOVED CRACKED STIFFENER, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW 51-3-0, 51-1-21A, AND DWG 5769891.Sep 4, 2005 · N874UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS05845513Rib · crackedINSPECTION TYPE:C3 LT WING LE LOWER RIB IS CRACKED AT XFS 622.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-3-0 FIG 1 AND 51-1-21.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845512Rib · crackedINSPECTION TYPE:C3 LT WING LE LOWER RIB PREVIOUS REPAIR IS CRACKED AT XFS 360.250. REMOVED REPAIR ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE.IAW SRM 5 1-1-20D,57-3-3 FIG 5,57-2-0 FIG 2 AND 51-1-15.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845511Rib · crackedINSPECTION TYPE:C3 LT WING LE LOWER RIB PREVIOUS REPAIR IS CRACKED AT XFS 385.250. REMOVED REPAIR ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51 -1-20D, 57-3-3 FIG 5, 57-2-0 FIG 2 AND 51-1-15.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845505Fitting · crackedINSPECTION TYPE:C3 C PIT STA 1180 LONG 35R BATH TUB FITTING IS CRACKED. REMOVED AND REPLACED BATH TUB FITTING IAW DC-8 SRM 53-2-0 FIG 2D.Sep 3, 2005 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845487Rib · crackedLEFT WING LE LOWER RIB IS CRACKED AT XFS 616.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-3-0 FIG 2.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845451Skin · corrodedLEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 785.000. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-8,51-1-21 AND EO DC8-5720-7767-A.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845449Doubler · crackedINSPECTION TYPE:C3 LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 335.250. REMOVED INTERNAL DOUBLER. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-3-0, 51-1-20D AND 51-1-21.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845448Rib · crackedINSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 816.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845447Rib · crackedINSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 822.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0, 51-1-21 AND 2-51-1-20D.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845446Rib · crackedINSPECTION TYPE:C3 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 772.500. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, 51-1-20D AND 51-1-21.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845445Rib · crackedINSPECTION TYPE:C3 RIGHT OUTER WING OUTBOURD EXTENDED LEADING EDGE UPPER RIB CRACKED AT XFS 722. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2, 51-1-21 AND 51-1-20D.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845444Rib · crackedINSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 846. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845443Rib · crackedINSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 835.000. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845427Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 297.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-02-00 FIG 2 AND 51-01-20D.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845422Rib · crackedINSPECTION TYPE:C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 778.750. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845418Skin · crackedINSPECTION TYPE: C3, LEFT WING L/E UPPER SKIN HAS A DAMAGED FASTENER HOLE AT XFS 347.750. FABRICATED AND INSTALLED DOUBLER IAW 57-03-03 FIG 005 PG 1,EO DC8-572 0-7767-A AND SRM 51-1-21.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845415Rib · crackedINSPECTION TYPE:C2, LT WING L/E LOWER RIB IS CRACKED AT XFS 653.750. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, 5 1-1-20D AND 51-1-21.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845413Rib · crackedINSPECTION TYPE: C3, LT WING L/E LOWER RIB IS CRACKED AT XFS 660.000. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-2-0, 51-1-20D AND 51-1-21.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845411Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XS 461.372. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 21.1.20D, 57-02-00 FIG 2, 57-03-03 FIG 5.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845410Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 803.750. STOP DRILLED, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-1-21, 51-1-20D AND 57-2-0.Sep 3, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR DHL2005806531Skin · corrodedLT OB AILERON UPPER PLATING INTERNAL SKIN CORRODED (STA XA 724.000-756.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG. 4 PG. 9, DACO DWG NR 5763133. REMOVED CORROSION ON INTERNAL SKIN OF LT OB AIL UPPER PLATING IAW SRM 51-1-8 PG. 17-18. FOUND OUTSep 2, 2005 · N806DH · Doug DC873F · AileronsSDR DHL2005806523Fitting · crackedFWD CARGO COMPT ZEE FITTING CRACKED 0.500 IN STA 300.000 L-27L. REMOVED CRACKED ZEE FITTING IAW SRM 53-1-0 PG. 1, SRM 51-1-20D. FABRICATED 2EA REPAIR ANGLES IAW SRM 53-2-0 FIG 2D SHEET 1,2, SRM 51-1-4 PG. 1 (FORMING). CUT NEW ZEE FITTING IN HALF USING TRIM DISep 2, 2005 · N806DH · Doug DC873F · Fuselage Main, Attach Fittings
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