Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  ORDER BY difficulty_date DESC"

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SDR UPS02838856Intercostal · crackedINSPECTION TYPE:C2 STA 90 INTERCOSTAL IS CRACKED AT LONG 33R. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5750726, AND SRM 51-1-20D.Jun 21, 2002 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838855Intercostal · crackedINSPECTION TYPE:C2 STA 90 INTERCOSTAL IS CRACKED AT LONG 33L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5750726 AND SRM 51-1-21, 51-1-20D.Jun 21, 2002 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838781Frame · crackedINSPECTION TYPE:C2 STA 1400 FRAME IS CRACKED BELOW LONG 34R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, AND FILLER IAW DC8-5310-11728-A, AND DWG DC8-53A-011.Jun 21, 2002 · N730UP · Doug DC871F · Fuselage Main, FrameSDR UPS02838715Longeron · crackedINSPECTION TYPE:C2 STATION 940 LONGERON 24L IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-2-2 FIG 5.Jun 21, 2002 · N730UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02838857Longeron · crackedINSPECTION TYPE:C2 STA 1660 LONG 11R IS CRACKED. STOP DRILLED CRACK NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED REPAIR STRAP ALONG WITH SKIN DOUBLER AND TRIPLER AND FILLER.Jun 20, 2002 · N730UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02838734Skin · crackedINSPECTION TYPE:C2 REMOVE EXISTING REPAIR DOUBLER ON L-1 DOOR LOWER FWD TO AFT CORNER TO EVALUATE DAMAGE, INTERNAL DOUBLER CRACKED AT LONG 21L, AND SKIN DAMAGED STA 31-70 BETWEEN LONG 21L TO 14L. REMOVED EXISTING REPAIR, CUTOUT DAMAGE AREAS AND SKIN SEGMENT BJun 20, 2002 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838732Skin · crackedINSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 360.25. STOP-DRILLED CRACK, NDT VERIFIED STOPDRILLS TERMINATES CRACK. INSTALLED CONICAL WASHERS, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-7767-A AND SRM 51-1-26.Jun 20, 2002 · N730UP · Doug DC871F · Wing, Plate/SkinSDR UPS02838733Skin · crackedINSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON R-1 DOOR UPPER FWD CORNER AND REP AIR PER DC8 SRM 53-2-0 FIG 14, SKIN IS CRACKED STA 160 LONG 10R. REMOVED STEEL DOUBLER, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED DOUBLER,TRIPLER, Jun 19, 2002 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838794Skin · crackedINSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON L1 DOOR UPPER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 15 AT STA 25 LONG 10L AREA. REMOVED EXISTING REPAIR, CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FJun 18, 2002 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838782Skin · crackedINSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLERS ON L2 DOOR LOWER FWD CORNER AND REPAIR IAW SRM 53-2-0 FIG 18, STA 1620 LONG 21L SKIN IS CRACKED. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIJun 18, 2002 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838714Skin · damagedINSPECTION TYPE:C2, REMOVE STEEL DOUBLER ON L-1 DOOR UPPER AFT CORNER AND REPAIR IAW SRM 53-2-0 FIG 15. REMOVED EXISTING DOUBLER, NDT VERIFIED NO CRACKS AT EXISTING CUTOUT, FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG 15.Jun 18, 2002 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838713Skin · crackedINSPECTION TYPE:C2 REMOVE STAINLESS DOUBLER ON THE R2 DOOR UPPER AFT CORNER AND REPAIR FUSELAGE SKIN CRACKED AT STA 1660 LONG 10R AT UPPER CORNER. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AND INSTALLED REPAIR DJun 18, 2002 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838712Skin · crackedINSPECTION TYPE:C2, NR 1 PYLON OUTBOARD SIDE SKIN IS CRACKED AT YN 343. NDT VERIFIED CRACK TERMINATES AT END OF PART. FABRICATED AND INSTALLED DOUBLER IAW DC8 70 SERIES SRM 54-2-0 FIG 6.Jun 18, 2002 · N730UP · Doug DC871F · Nacelle/Pylon, Plate/SkinSDR UPS02838576Support · crackedINSPECTION TYPE:B CK FWD PRESSURE BULKHEAD SUPPORT FRAME CRACK. FORMED DOUBLER IAW 53-2-0 FIG 1B. FABRICATED DOUBLERS PER SRM 53-2-0 FIG 1B. INSTALLED DOUBLER PER 53-2-0.Jun 7, 2002 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838559Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY DISCHARGED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. CHECKS OK.Jun 5, 2002 · N755UP · Doug DC871F · Emergency LightingSDR UPS02838600Stringer · corrodedINSPECTION TYPE:C1 STA 1700 STRINGER 34L HAS CORROSION. BLENDED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED NEW REPAIR AND STRAPS IAW DC8 SRM 53-4-1 & 53-2-2. INSTALLED NEW PARTS IAW DC8 SRM 53-2-2 FIG 8.Jun 3, 2002 · N700UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02838631Web · crackedINSPECTION TYPE:C1 L1 DOOR FWD CENTER TORQUE BOX WEB CRACKED. REMOVED DAMAGED WEB. FABRICATED NEW WEB IAW DWG 5597646. INSTALLED WEB IAW DC8 SRM 51-3-0Jun 1, 2002 · N700UP · Doug DC871F · Passenger/Crew DoorsSDR UPS02838535Floor Support · corrodedINSPECTION TYPE:C1, CABIN FLOOR SUPPORT BRACKET HAS EXFOLIATED CORROSION AT STA 1754, BL 0. REMOVED CORRODED FITTING BRACKET IAW DC8 SRM 51-3-0, BRACKET WAS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, INSTALLED FITTING SUPPORT BRACKET IAW DC8 SRM 51-3-1, 51May 29, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838563Intercostal · corrodedINSPECTION TYPE:C1 MAIN CABIN INTERCOSTAL AT STA 67, RBL 44 IS CORRODED. TRIMMED OUT CORROSION AREA IAW DC8 SRM 53-2-0, FABRICATED REPAIR FILLER AND DOUBLER IAW DC8 SRM 53-2-0, INSTALLED REPAIR FILLER AND DOUBLER IAW DC8 SRM 53-2-0 AND DC8 SRM 51-1-20.May 27, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838599Floor Support · corrodedINSPECTION TYPE:C1 MAIN CABIN UNDER FLOOR AT STA 67 RBL 40 BULGING. BLENDED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED AND INSTALLED T EXTRUSION IAW TIMCO REO G08633, ALODINED AND PRIMED IAW DC8 SRM 51-1-8.May 26, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838470Battery Pack · dischargedINSPECTION TYPE:N/A LIGHT BULBS VERY DIM WHEN EMERGENCY LIGHT SWITCH SELECTED TO ARM. SUSPECT LOW BATTERY. REMOVED AND REPLACED EMERGENCY BATTERY PACK MM 33-50-01, OPS CHECK NORMAL.May 26, 2002 · N701UP · Doug DC871F · Emergency LightingSDR UPS02838541Fitting · crackedINSPECTION TYPE:C1, STRINGER END FITTING CRACK STRINGER 51 2 MAIN. REMOVED AND REPLACED STRINGER END FITTING IAW DC8 SRM 51-1-20D.May 20, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838542Shear Tie · crackedINSPECTION TYPE:C1 INSIDE DOOR 60-VERT STAB CENTER SPAR CANTED BULKHEAD SHEAR TIE IS CRACKED BETWEEN L9L & L10L. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0 & 51-1-20D.May 17, 2002 · N700UP · Doug DC871F · Fuselage Main, StructureSDR UPS02838543Floorbeam · crackedINSPECTION TYPE:C1 PROBLEM WITH FLOORBEAM CRACK UNDER FLANGE FS 1746 BL 2L. FABBED REPAIR PARTS IAW DC8 SRM 53-2-0. INSTALLED REPAIR PARTS IAW DC8 SRM 536-2-0 AND 51-2-20D.May 16, 2002 · N700UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS02838538Floor Support · corrodedINSPECTION TYPE:C1 FLOOR SUPPORT ANGLE CORRODED AT FS 1723 BL19R. REMOVED CORRODED SUPPORT ANGLE AT STA 1723 BL19R IAW DC8 SRM 51-3-0, SUPPORT ANGLE 5755032-26, DETERMINED TO BE CORRODED OUT OF LIMITS IAW DC8 SRM 53-2-0. INSTALLED NEW PART IAW DC8 SRM 51-1-May 16, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838632Fitting · damagedINSPECTION TYPE:C1 C-PIT TORQUE BOX WEB AND FITTING HAVE ELONGATED HOLES. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-24 FABBED & INSTALLED DOUBLER IAW SRM 53-2-0.May 15, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838588Floorbeam · corrodedINSPECTION TYPE:C1 MAIN CABIN TOP MLG PRESSURE WEB AREA FLOORBEAM IS CRACKED AND CORRODED ON FWD & AFT LEG AT STA 900 LBL 44. REMOVED MVD CORROSION FROM FLOORBEAM, OUT OF LIMITS. FABBED REPAIR PARTS IAW R EO G08638 MPI OF REPAIR PARTS IAW ASTM E1444. NO CRAMay 15, 2002 · N700UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS02838586Support Fitting · crackedINSPECTION TYPE:C1 RT WING FLAP HINGE SUPPORT FITTING AT XF 339-7332 HAS A CRACK INDICATION WITH NDT OUTBOARD. FABBED BLOCKS IAW DC8 DWG 5894377. LOCATED, DRILLED AND DEBURRED 3751728-502 FITTING & BASE FITTING IAW DC8 DWG 5894377. INSTALLED 5751 186-508, 3May 15, 2002 · N700UP · Doug DC871F · Trailing Edge FlapsSDR UPS02838584Angle · crackedINSPECTION TYPE:C1 C-PIT FRAME REINFORCEMENT ANGLE HAS SEVERAL CRACKS & AN IMPROPER REPAIR STA 1150, L32R. REMOVED ATTACH ANGLE IAW DC8 SRM 51-1-21D, FABRICATED REPLACEMENT PARTS IAW DC8 SRM 51-1-20D, INSTALLED IAW DC8 SRM 51-1-20D.May 15, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838565Floorbeam · corrodedINSPECTION TYPE:C1 AFT PIT FLOORBEAM CORRODED AT STA 1440 UPPER FWD FLANGE AT RBL 60. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0. FOUND AFT FLANGE CORRODED REMOVED AFT FLANGE OF FLOORBEAM IAW TRSM 95T0345001 STD 6310-001. FABBEDMay 15, 2002 · N700UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS02838540Skin · crackedINSPECTION TYPE:C1 L-2 DOOR CUTOUT LOWER FWD CORNER SHOWS CRACK INDICATION ON FIRST FASTENER HOLE ABOVE DOOR PAN. FABRICATED DOULBERS IAW DC8 SRM 53-2-0 FIG 18. INSTALLED DOUBLERS IAW DC8 SRM 51-1-8 & 51-3-0.May 15, 2002 · N700UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838536Fitting · crackedINSPECTION TYPE:C1 RT WING FLAP HINGE SUPPORT FITTING AT XF 339-7332 HAS A CRACK INDICATION WITH NDT OUTBOARD. FABBED BLOCK IAW DC8 DWG 5894377. INSTALLED FITTING IAW DC8 DWG 5751174 & 5894377.May 15, 2002 · N700UP · Doug DC871F · Trailing Edge FlapsSDR UPS02838531Floorbeam · crackedINSPECTION TYPE:C1 AFT PIT - STA 1060 CABIN FLOORBEAM UPPER AFT FLANGE IS CRACKED HORIZONTALLY ACROSS AFT EDGE AT RBL 60. CUTOUT CRACKED AREA IAW REO G08643. FABRICATED REPAIR ANGLE IAW REO G08643. INSTALLED REPAIR ANGLE AND FLOOR PANEL IAW DC8 SRM 51-1-20DMay 15, 2002 · N700UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS02838528Door Frame · crackedINSPECTION TYPE:C1 R-1 DOOR CUTOUT UPPER FWD CORNER SHOWS CRACK INDICATION ON THE FIRST FASTENER HOLE IN THE FIRST ROW OF RIVETS. REPAIRED DOOR CORNER IAW DC8 SRM 53-2-0 FIG 14.May 15, 2002 · N700UP · Doug DC871F · Fuselage Main, StructureSDR UPS02838526Attach Angle · gougedINSPECTION TYPE:C1 MAIN CABIN AT STA 832 RBL 38 AFT SIDE OF INTERCOSTAL ATTACH ANGLE GOUGED. REMOVED AND REPLACED DAMAGED ANGLE IAW DC8 SRM 51-1-20D & DAC DWG 5773 275.May 15, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838523Angle · corrodedINSPECTION TYPE:C1 COCKPIT VERT WEB I/B SIDE AT FS 6 RBL 14. BLENDED CORROSION ON WEB IAW DC8 SRM 51-1-8, WITHIN LIMITS DC8 SRM 53-2-0. REMOVED L-ANGLE IAW DC8 SRM 51-1-21 OUT OF LIMITS IAW DC8 SRM 53-2-0, AND INSTALLED L-ANGLE IAW DC8 SRM 51-1-8 AND 51-1-21May 15, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838570Shear Tie · crackedINSPECTION TYPE:C1 CTR FUSE SHEAR TIE CRACKED ON TOP OF FRAME STA 680 BL 0. REMOVED BRACKET DRILLED UP AND INSTALLED NEW BRACKET IAW DC8 SRM 51-1-8 AND DAC DWG 615535.May 14, 2002 · N700UP · Doug DC871F · Fuselage Main, StructureSDR UPS02838566Fitting · corrodedINSPECTION TYPE:C1 LT MLG W/W STA 891 FITTING OVER LONG 24 CORRODED. REMOVED FITTING, DRILLED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D & 51-3-2.May 13, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838525Frame · bentINSPECTION TYPE:C1 MAIN CABIN AT STA 240 BETWEEN STR 19R & STR 20R FRAME IS BENT AND IMPROPERLY REPAIRED. REMOVED OLD REPAIR. FABRICATED AND INSTALLED FRAME REPAIR IAW DC8 SRM 53-2-0 FIG 2A.May 13, 2002 · N700UP · Doug DC871F · Fuselage Main, FrameSDR UPS02838524Frame · crackedINSPECTION TYPE:C1 STA 220 STR 20R FRAME CRACKED. REMOVED DAMAGE FRAME SECTION AND REPAIRED PER DC8 SRM 53-2-0 FIG 2 AND 51-1-8.May 13, 2002 · N700UP · Doug DC871F · Fuselage Main, FrameSDR UPS02838405Intercostal · crackedINSPECTION TYPE:C1 MAIN CABIN AT STA 345 STR 17R INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL. REMOVED DAMAGE INTERCOSTAL AND GUSSET, FABBED NEW INTERCOSTAL AND GUSSET, INSTALLED INTERCOSTAL AND GUSSET IAW TPS 1003 DC8 SRM.May 13, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838630Fitting · crackedINSPECTION TYPE:C1 ABOVE RT CUSP AT STA 1170-1180 C PIT TORQUE BOX FITTING IS CRACKED. REMOVED AND REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D.May 12, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838603Longeron · crackedINSPECTION TYPE:C1 A-PIT L35R HAS 1 INCH LONG CRACK AT STA 343. FABBED AND INSTALLED NEW SECTION OF LONGERON AND U-CHANNEL IAW TIM CO REO G068621 AND DC8 SRM 53-2-2 FIG 10 AND 51-1-20.May 12, 2002 · N700UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02838534Fitting · crackedINSPECTION TYPE:C1, RT MLG W/W TRAPEZOID TO WING LOWER OUTBOARD FITTINGS CRACKED. REMOVED FITTINGS, DRILLED UP AND INSTALLED NEW FITTINGS IAW DAC DWGS 5656229, 3641117 AND 3656004. REINSTALLED STIFFENER AND ACCESS PNLS IAW DC8 M/M 51-1-20D AND 51-3-0.May 12, 2002 · N700UP · Doug DC871F · Wing, Landing Gear Attach FittingsSDR UPS02838533Frame · corrodedINSPECTION TYPE:C1, A-PIT DOOR TORQUE BOX FRAME HAS EXFOLIATION CORROSION AT STA 280 L 32-33R INSIDE LIGHTNING HOLE. REMOVED CORROSION FROM FRAME IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FRAME REPAIRED IAW TIMCO REO G08626.May 12, 2002 · N700UP · Doug DC871F · Fuselage Main, FrameSDR UPS02838532Longeron · crackedINSPECTION TYPE:C1, RT MLG W/W LONG 2R CRACKED BY UPLOCK MOUNT. FABRICATED REPAIR PARTS IAW DC8 SRM 53-2-2 TR 53-123. INSTALLED REPAIR IAW DC8 SRM 53-2-2 TR 53-123 AND DC8 SRM 51-1-20D.May 12, 2002 · N700UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02838529Shear Tie · corrodedINSPECTION TYPE:C1 A-PIT TORQUE BOX WEB HAS BROKEN SHEAR TIE AT STA 280 L33R. FABRICATED WEB IAW DAC DWG 5753892. FABRICATED SPLICE DOUBLER IAW DC8 SRM 53-2-0. INSTALLED WEB AND SPLICE IAW DC8 SRM 51-1-20D AND 51-1-21.May 12, 2002 · N700UP · Doug DC871F · Fuselage Main, StructureSDR UPS02838406Splice · crackedINSPECTION TYPE:C1 A-PIT L-31-L STA 380-400 SPLICE IS CRACKED 4 INCHES LONG. REMOVED CRACKED FITTING SPLICE IAW DC8 SRM 51-1-20D, LOCATED DRILLED AND DEBURRED NEW FITTING, INSTALLED AT LONG 31L, STA 390 IAW DC8 SRM 51-1-20D.May 12, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838404Attach Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN RT SIDE STA 759 L13R ATTACH FITTING CRACKED. REMOVED DAMAGED PART AND INSTALLED NEW PART IAW DC-8 SRM 51-1-20D.May 12, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838633Attach Fitting · crackedINSPECTION TYPE:C-1 MAIN CABIN LT SIDE STA 780 L14L FRAME TO LONGERON ATTACH FITTING IS CRACKED. REMOVED FITTING & INSTALLED NEW FITTING IAW DC8 SRM 51-3-0.May 11, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous Structure
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