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 UPS01836813Frame · crackedINSPECTION TYPE:C2,3 STA 17 FRAME IS CRACKED AT LONG 16L-17L. REPAIRED FRAME IAW SRM 53-2-0 FIG 23.Aug 9, 2001 · N866UP · Doug DC873F · Fuselage Main, FrameSDR UPS01836790Fitting · crackedINSPECTION TYPE:C2,3 RT WHEEL WELL LONG 24R SUPPORT FITTING IS CRACKED AT STA 920. REMOVED AND REPLACED FITTING IAW DWG 5753113, AND SRM 51-1-20D, 53-2-0 FIG 8.Aug 9, 2001 · N866UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836703Skin · crackedINSPECTION TYPE:C2,3 STA 1600 AT LONG 20L-21L FUSELAGE SKIN AT FWD LOWER CORNER. REPAIRED SKIN IAW SRM 53-2-0 FIG 18.Aug 9, 2001 · N866UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01836650Doubler · corrodedINSPECTION TYPE:C2,3 COCKPIT SUBFLOOR FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STA -25 TO -8 LBL 69. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5612298, AND SRM 51-1-21.Aug 9, 2001 · N866UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836646Rib · crackedINSPECTION TYPE:C2,3 RT HORIZONTAL STAB L/E UPPER RIB IS CRACKED AT XFS 88. REPAIRED RIB IAW SRM 55-2-0 FIG 2.Aug 9, 2001 · N866UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR DHL2001804527Seat Track · brokenCOCKPIT F/E FWD & AFT SEAT TRACKS BROKEN. REMOVED BROKEN SEAT TRACKS IAW SRM 51-8-0 PAR 1. INSTALLED NEW SEAT TRACKS IAW SRM 51-8-0.Aug 9, 2001 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001804523Angle · crackedEXTERIOR WEB .5 INCH CRACK AT STA 812 LBL 55. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-1-21 PG 1.Aug 9, 2001 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836561Skin · crackedINSPECTION TYPE:IN 2 ADJACENT CRACKS AND DISTORTION IN PIT 31 DOOR LOWER EDGE NR 1 PIT DOOR HAS 2 CRACKS IN LOWER SKIN APPROX 14 INCHES FROM TRAILING EDGE. TRIMMED OUT DAMAGED SKIN ENCOMPASSING BOTH CRACKS AND INSTALLED NEW FASTENER, PER EO DC8-5230-14302.Aug 9, 2001 · N868UP · Doug DC873F · Cargo/Baggage DoorsSDR RRXA010060Gyro · failedCAPT'S VG FAILURE AFTER TAKEOFF. R&R CAPT'S VG IAW DC8 MM 34-25-0. OPS CHECKS GOOD.REMOVED & REPLACED CAPTS. ADI SYSTEM CHECKS GOOD IAW DC-8 MM 34-25-0 NO DEFECTS NOTEDAug 9, 2001 · N961R · Doug DC873F · Attitude Gyro and Indicating SystemSDR UPS01836712Rib · crackedINSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 335.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Aug 8, 2001 · N866UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01836704Rib · crackedINSPECTION TYPE:C2,3 LEFT WING L/E RIB IS CRACKED AT XFS 224. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Aug 8, 2001 · N866UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01836702Angle · crackedINSPECTION TYPE:C2,3 LEFT WING L/E VERTICAL ATTACH ANGLE IS CRACKED AT XS 250. REMOVED,FABRICATED,AND REPLACED ANGLE IAW DWG 9753293,AND SRM 51-3-0,51-1-20D.Aug 8, 2001 · N866UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS01836701Skin · crackedINSPECTION TYPE:C2,3 LEFT WING L/E SKIN IS CRACKED AT XW 485. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H.Aug 8, 2001 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836696Longeron · crackedINSPECTION TYPE:C1,3 STA 1770 LONG 17R IS CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG S1616757, AND SRM 53-2-0 FIG 2.Aug 8, 2001 · N809UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS01836691Fitting · crackedINSPECTION TYPE:C1,3 STA 1770 LONG 17R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-20D.Aug 8, 2001 · N809UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA11459Wedge · dentedDURING A MAINTENANCE VISIT FOUND LT WING O/B FLAP I/B TRAILING EDGE WEDGE DENTED AND HOLE, STA XRS 351 TO 380. REMOVED WEDGE, FABRICATED AND INSTALLED IAW SRM 51-1-21,51-1-21D AND DWG 56429704Aug 8, 2001 · N873SJ · Doug DC873F · Wing, Control SurfacesSDR UPS01836654Doubler · crackedINSPECTION TYPE:C2,3 LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XW 257. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21, 51-1-20D.Aug 8, 2001 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836651Panel · corrodedINSPECTION TYPE:C2,3 LEFT WING OUTBOARD AILERON INBD WEIGHTED PANEL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED WEIGHTED PANEL IAW DWG 5764617, AND SRM 57-1-0, 51-3-0.Aug 8, 2001 · N866UP · Doug DC873F · AileronsSDR UPS01836649Doubler · corrodedINSPECTION TYPE:C2,3 RIGHT WING L/E INTERNAL DOUBLER IS CORRODED BEYOND LIMITS AT XFS 366.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21.Aug 8, 2001 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836647Rib · crackedINSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 304. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Aug 8, 2001 · N866UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01836644Angle · crackedINSPECTION TYPE:C2,3 LEFT WING L/E IB SLOT VANE IB ATTACH ANGLE IS CRACKED AT XILD .7095. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5770138, AND SRM 51-1-21, 51-1-20D.Aug 8, 2001 · N866UP · Doug DC873F · Leading Edge DevicesSDR UPS01836642Rib · crackedINSPECTION TYPE:C2,3 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 835.75, XFS 853.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Aug 8, 2001 · N866UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01836641Rib · crackedINSPECTION TYPE:C1,3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 722.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Aug 8, 2001 · N866UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01836623Fitting · crackedINSPECTION TYPE:C1,3 STA 1770 LONG 17L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-20D, AND 51-1-21.Aug 8, 2001 · N809UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836619Longeron · crackedINSPECTION TYPE:C1,3 STA 1770 LONG 17L IS CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 5649327, AND SRM 51-1-20D, 51-1-21.Aug 8, 2001 · N809UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2001804522Support · crackedWING TO FUSELAGE FAIRING SUPPORT CRACKED 1 IN AT STA 640 BETWEEN L-21 ANDL-22L.REMOVED AND REPLACED CRACKED SUPPORT PER SRM 51-3-0 PG 1.Aug 8, 2001 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001804521Skin · crackedLT WING UPPER SKIN SURFACE SHOWS A 1 INCH CRACK AT STA XLS 421 STL. CUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 57-2-1.Aug 8, 2001 · N804DH · Doug DC873F · Wing, Plate/SkinSDR UPS01836791Skin · crackedINSPECTION TYPE:C2,3 FUSELAGE SKIN CRACKED STA 25 LONG 10L FWD UPPER CORNER L-1 DOOR. REPAIRED SKIN IAW SRM 53-2-1 FIG 15.Aug 7, 2001 · N866UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01836742Floorbeam · corrodedINSPECTION TYPE:C1,3 STA 798 FLOORBEAM IS CORRODED BEYOND LIMITS AT LBL 60. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 809-212.Aug 7, 2001 · N809UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS01836706Skin · damagedINSPECTION TYPE:C2,3 LEFT IB SLOT VANE HAS SCREWS PULLING THRU SKIN AT XILD 7095. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H.Aug 7, 2001 · N866UP · Doug DC873F · Wing, Plate/SkinSDR RRXA11458Angle · corrodedDURING A MAINTENANCE VISIT FOUND A/C BAY R/H SIDE FRAME HAS EXFOLIATION BETWEEN L26 AND L25 STA 35. *** CORRECTIVE ACTION *** REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE PER REF DHSK 873-216-15 AND SRM 51-1-20D.Aug 7, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11457Bushing · corrodedDURING A MAINTENANCE VISIT FOUND R/H WOKING BLKD OF CONSTANT SECTION OF HORIZ HAS HEAVY CORROSION. *** CORRECTIVE ACTION *** REMOVED CORROSION PER SRM 51-1-8, FABRICATED AND INSTALLED REPAIR BUSHING PER REF DHSK 873-297 AND CHAPTER 12 AND 13 .Aug 7, 2001 · N873SJ · Doug DC873F · Horizontal Stabilizer StructureSDR RRXA11456Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CABIN SEAT TRACK IS CORRODED AT FS 760 RBL48. *** CORRECTIUVE ACTION *** SEAT TRACK FOUND OUT OF LIMITS PER DC8 SRM 53-2-3 FIG 12. REMOVED DAMAGED SECTION OF SEAT TRACK PER DC8 SRM 51-30-. FABRICATED SEAT TRACK AND SPLINE ANAug 7, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11455Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CABIN SEAT TRACK HAS CORROSION AT STA FS 610 AT RBL 48. REPAIRED SEAT TRACK IAW DC8 SRM 53-23 FIG 8A.Aug 7, 2001 · N873SJ · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA11454Skin · crackedDURING A MAINTENANCE VISIT FOUND RT WING L/E SKIN CRACKED AT STA XFS300. REPAIRED SKIN IAW 8110-3 APPROVED DHSK 873-883Aug 7, 2001 · N873SJ · Doug DC873F · Wing, Plate/SkinSDR UPS01836648Skin · crackedINSPECTION TYPE:C2,3 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 316.5 AND HAS A ELONGATED HOLE AT XFS 329. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 866-235.Aug 7, 2001 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836640Skin · crackedINSPECTION TYPE:C2,3 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 666.25. REPAIRED SKIN IAW SRM 57-2-1 FIG 38.Aug 7, 2001 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836621Fitting · crackedINSPECTION TYPE:C1,3 STA 822 FLOORBEAM ATTACH FITTING IS CRACKED AT LBL 24. REMOVED AND REPLACED FITTING IAW DWG 3755222, AND SRM 51-3-0.Aug 7, 2001 · N809UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836774Doubler · crackedINSPECTION TYPE:C1,3 LT WING FUEL PANEL 505F INTERNAL DOUBLER IS CRACKED AT XRS 12 AT STRINGER 5-6 AREA ON WING. REPAIRED DOUBLER IAW SRM 57-2-1 FIG 36.Aug 6, 2001 · N809UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836773Splice · crackedINSPECTION TYPE:C1,3 STA 680-700 LONG 1 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG4750521, AND SRM 51-1-21, 51-1-20D.Aug 6, 2001 · N809UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836731Fitting · crackedINSPECTION TYPE:C1,3 STA 680 WING BOX TO FRAME SUPPORT FITTING IS CRACKED BELOW LONG 21L. REMOVED AND REPLACED FITTING IAW DWG 3642974, AND SRM 51-1-20D, 51-3-0.Aug 6, 2001 · N809UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836722Pan · corrodedINSPECTION TYPE:C1,3 RT WING IB SLOT PAN HAS INTERGRANULAR CORROSION AT XS 250. REMOVED AND REPLACED PAN IAW DWG 5769859, AND SRM 51-1-21, 51-3-0.Aug 6, 2001 · N809UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836698Longeron · crackedINSPECTION TYPE:C1,3 STA 1260-1280 LONG 34R IS CRACKED. REPAIRED LONGERON IAW 8110-3 APPROVED DH SK 809-819.Aug 6, 2001 · N809UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS01836697Longeron · crackedINSPECTION TYPE:C1,3 STA 1260-1280 LONG 35R IS CRACKED. REPAIRED LONGERON IAW 8110-3 APPROVED DH SK 809-818.Aug 6, 2001 · N809UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS01836695Frame · crackedINSPECTION TYPE:C1,3 STA 35 FRAME IS CRACKED AT LONG 24R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.Aug 6, 2001 · N809UP · Doug DC873F · Fuselage Main, FrameSDR RRXA11453Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND AFT PIT AT FS1140 BETWEEN LONGERON 35R AND 36 HAS SHEER TIE BLOWN OUT WITH CORROSION. *** CORRECTIVE ACTION *** CUT OUT DAMAGED SECTION OF SHEAR TIE IAW DC8 SRM 53-2-0 FIG 2A. FABRICATED REPLACEMENT SHEAR TIE AND SPLICE AND IAug 6, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11452Link · corrodedDURING A MAINTENANCE VISIT FOUND LH FLAP #3 ACTUATOR COMP LINKS (XW340) CORRODED ON SIDE FACE. *** CORRECTIVE ACTION *** REMOVED CORROSION ON #3 FLAP ACTUATER LH PER SRM 27-28-7 TEMP REV 27-38. WITHIN LIMITS CAD PLATED PER DC8 OHM 2-13Aug 6, 2001 · N873SJ · Doug DC873F · Trailing Edge Flap Control SystemSDR RRXA11451Doubler · corrodedDURING A MAINTENANCE VISIT FOUND AFT ACCY COMPT HEAVY CORROSION ON INTERNAL SKIN DOUBLER, AREA PREVIOUSLY BLENDED. FS 1620 - 1640 L32R - L33R. *** CORRECTIVE ACTION *** REMOVED DAMAGED INTERNAL DOUBLER, FABRICATED AND INSTALLED PER DHSK 873-024.Aug 6, 2001 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11450Doubler · corrodedDURING A MAINTENANCE VISIT FOUND AF ACCY COMPT HEAVY CORROSION ON INTERNAL SKIN DOUBLER BETWEEN FS 1620 AND 1640 L32L L33L *** CORRECTIVE ACTION *** BLENDED AREA FOUND TO BE OUT OF LINITS IAW DC8 SRM 51-1-8 AND 53-2-0 FIG 1. REMOVED DAMAGED AREA OF INTERNAL Aug 6, 2001 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01836639Fitting · crackedINSPECTION TYPE:C1,3 STA 660-680 LONG 11L END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 5750540, AND SRM 51-1-20D.Aug 6, 2001 · N809UP · Doug DC873F · Fuselage Miscellaneous Structure
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