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 UPS05845280Fitting · crackedLONGERON END FITTING CRACKED AT FS 857.125 L10L. REMOVED AND REPLACED LONG END FITTING AT FS 857.125 L10L IAW SRM 51-1-8,51-1-20, 51-3-01 AND 53-3-0.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845279Fitting · crackedLONGERON END FITTING CRACKED AT FS 867.125 L5L. REMOVED AND REPLACED LONGERON END FITTING AT FS 857.125 L5L IAW SRM 51-1-20D, 51-1-21 AND 51-3-0.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845277Fitting · crackedCRACK ON SPLICE FITTING ON LONG 1L STA 680. REMOVED CRACKED FITTING AND LONGERON SPLICE IAW SRM 51-1-20D, INSTALLED FITTING, SPLICE AND STRAPS IAW SRM 51-1-21,51-1-20D AND 51-01-23 FIG 48.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845276Fitting · crackedMAIN CABIN CENTER SUBFLOOR STA 923 L22L "T" FITTING AROUND FASTNERS AREA HAS HEAVY CORROSION. REMOVED CORROSION FROM "T" FITTING AND VISUALLY FOUND CRACK IAW SRM 51-1-8. REMOVED AND REPLACED "T" FITTING IAW SRM 51-3-2 AND DWG 3649114.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845274Fitting · crackedFS 834.500 L18R FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FRAME FITTING AT STA 834.500 L18R IAW SRM 51-1-20 D, SRM 51-3-2.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845258Angle · crackedCENTER WING BOX SUB FLOOR "L" ANGLE CRACKED AT FS 798 LBL 48. REMOVED AND REPLACED "L" ANGLE AT FS 798 LBL 48 IAW SRM 51-3-2 AND SRM 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845253Fitting · crackedFRAME TO INTERCOSTAL ATTACH FITTING CRACKED AT FS 781 LONG 18R AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG 3750025 AND SRM 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845237Finger Doubler · corrodedMAIN CABIN CENTER SUB FLOOR AT STA 925 LBL 65, FINGER DOUBLER AREA HEAVY CORRODED. REMOVED, FAB`D FINGER DOUBLER AND REPAIRED IAW DWG 5645332 AND SRM 53-0 7-01-0 FIG 010.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05845233Fitting · crackedFRAME TO INTERCOSTAL ATTACH FITTING CRACKED AT F/S 857.125 L19L. REMOVED AND REPLACED ATTACH FITTING IAW SRM 51-1-21D AND 51-3-2.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845232Fitting · crackedFRAME TO INTERCOSTAL ATTACHED FITTING CRACKED AT F/S 834.500 L18L. REMOVED AND REPLACED INTERCOSTAL ATTACH FITTING IAW SRM 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845226Fitting · crackedLONGERON END FITTING CRACKED AT FS 857.125 L1 FWD SIDE. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845221Fitting · crackedLONGERON END FITTING CRACKED FS 907 L8R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845220Fitting · crackedFITTING CRACKED FS 822 L20L. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845203Finger Doubler · corrodedINSPECTION TYPE:C1 MAIN CABIN SUB FLOOR FINGER DOUBLER CORRODED AND SHEAR HEAD FASTENER A T STA 960 TO 980 RBL 65. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER IAW DWG 5645332 AND DC-8 SRM 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05845202Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING CRACKED (2 INCHES) STA 680 L2R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D,51-1-21,AND 51-1-23 .Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA0500092OMec · out of adjustDURING DESCENT FROM MPDC TO KTOL FLIGHT LEVEL 38.0, NR 4 ENGINE FLAMED OUT WHEN THROTTLE WAS RESTARTED. ALL ENGINE PARAMETERS WERE NORMAL CREW ACCOMPLISHED FLAME OUT IN FLIGHT START. WHEN A IGNITER WAS USED FOR IN-FLIGHT START ENGINE STARTED NORMALLY NO OTHAug 11, 2005 · N823BX · Doug DC871F · Fuel Controlling SystemSDR UPS05845452Pressure Panel · corrodedPOPPED RIVET, PILLOWED SKIN, LT W/W CEILING, STA 940 OB ABOVE L24L. REMOVED CORROSION AND FOUND OUT OF LIMITS AT STA 940 L24L IAW SRM 51-1-8, FABRICATED AND INSTALLED FILLER, SPLICE DOUBLER FINGER DOUBLER AND TAPERED FILLER AT STA 940 L24L IAW SAA SK 750-8463Aug 10, 2005 · N750UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS05845367Skin · crackedINSPECTION TYPE:C1 RIGHT WING UPPER SKIN .25 INCH CRACK AT STA XCW 69 REAR SPAR AREA. CUT OUT CRACKED SECTION OF RIGHT WING AT XCW 69, NDT VERIFIED CRACK TERMINATION IAW HFEC INSP PER NDTSPM 06-10-01.001. FABRICATED -4 FILLER, -6 FILLER AND -8 DOUBLER IAW SRAug 10, 2005 · N750UP · Doug DC871F · Wing, Plate/SkinSDR UPS05845204Rib · crackedINSPECTION TYPE: C1, RT WING L/E LWR RIB CRACKED AT XFS 806. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0, 51-1-20D, AND 51-1-21.Aug 10, 2005 · N750UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS05845238Skin · corrodedSEVERE CORROSION BETWEEN OUTER SKIN AND FRAME LOWER SURFACE AT SKIN SEAM IN FRONT OF THE LEFT SIDE FUEL DUMP MANIFOLD. REMOVED EXISTING DOUBLER, REMOVED DAMAGE, FAB`D FILLER AND DOUBLER AND INSTALLED IAW SRM 57-02-00-0, DWG 5649654.Aug 9, 2005 · N750UP · Doug DC871F · Wing, Plate/SkinSDR UPS05845234Skin · crackedFUSELAGE EXTERIOR SKIN CRACKED 1/2 INCH LONG AT STA 1746 L15L. REMOVED DAMAGED AREA FAB`D FILLER, DOUBLER AND FINGER DOUBLER AND INSTALLED IAW SRM 53-2-1 AND 53-2-1 FIG 7.Aug 8, 2005 · N750UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500083OWire Harness · defectiveDURING TAKEOFF FROM KTOL BOTH EGT INDICATIONS ON NR 2 ENG BECAME ERRATIC. INFLT-ANALOG WENT OFF SCALE HIGH AND DIGITAL SHOWS 1000 INTERMITTENTLY. THE CREW RETURNED THE AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED EGT HARNESS, RAN ENGINJul 26, 2005 · N828BX · Doug DC871F · Engine Indicating System WiringSDR UPS05844958Battery · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. R&R BATTERY AND RELAY UNIT W/REF TO MM 33-50-01-2. OPS CHECK GOOD.Jul 24, 2005 · N715UP · Doug DC871F · Emergency LightingSDR IXXA0500082OWire Harness · defectiveDURING TAKEOFF FROM KTOL TO KATL AFTER V1 NR 2 EGT STARTED TO FLUX FROM 860 TO MAX EGT 1000 (DIGITAL AND POINTER) CONTINUED TO FLUX ON CLIMB-OUT. ALL OTHER ENGINE INDICATIONS WERE NORMAL. THE CREW ELECTED TO OVERFLY INTERIM STOP ATL AND FLY DIRECT TO KMCO. Jul 22, 2005 · N828BX · Doug DC871F · Engine Indicating System WiringSDR UPS05844986Battery Pack · inoperativeDURING LIGHT CK EMERGENCY EXIT LIGHT BY FWD ENTRY DOOR DID NOT COME ON. PEANUT LIGHT UNDER FRONT INSTRUMENTS DO NOT COME ON AS WELL. REPLACED BATTERY PACK/ RELAY UNIT IAW MM SEC 33-50-01. OPS CHK GOOD.Jul 20, 2005 · N718UP · Doug DC871F · Emergency LightingSDR UPS05844933Hydraulic System · leakingATB - HYDRAULIC FLUID LOSS, EMERGENCY DECLARED. FOUND LEFT MAIN GEAR DOWNLOCK BUNGEE CYLINDER PRESSURE LINE LEAKING/ DAMAGED. R/R LINE PER MM 30-12-2. SVCD HYD SYSTEM PER MM 12-30-01-3 LEAK CK O.K.Jul 20, 2005 · N702UP · Doug DC871F · Hydraulic System, MainSDR IXXA05SMN158SVane · improperDURING ROUTINE C CHECK INSPECTION, RT WING. OB VANE SLOT HAS INTERIM REPAIR XOLDO 67.000. PERFORMED MAJOR REPAIR, REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21 PAGE 1. REMOVED THE DAMAGED AREA IAW DWG NR ED 4022, PERFORMED NDT INSPECTION. IAW NDT SPM PART 06Jul 6, 2005 · N822BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA05SMN157SSkin · crackedDURING ROUTINE C CHECK INSPECTION, LT WING. STUB WING UPPER SURFACE STA XS 250.000 XS 240.000 HAS TWO CRACKS OF .5 INCH. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 38, TR NR 57-85, EO SEMAN NR 2005983 DATE 06-18-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1.Jul 6, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN156SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RT WING IB L/E UPPER PART EXTERNAL SKIN CORRODED XS 250.089. PERFORMED MAJOR REPAIR IAW SRM, TR NR 57-85, EO SEMAN NR 2005984 DATE 06-18-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM. REMOVED CORROSION IAW SRM. FOUND Jul 6, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN155SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, MID ACCESSORY COMPARTMENT L-31R CORRODED, STA 665.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG. 11, EO SEMAN NR 20051003 DATE 06-27-05. REMOVED FASTENERS IAW SRM 51-1-20D PAGE 21. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-Jul 6, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN154SFrame · crackedDURING ROUTINE C-CHECK INSPECTION, FWD ACCES COMPT. FRAME CRACKED 2” STA 55.000 L-24R. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-0 FIG. 2 SHEET 5, TR 53-125 DATE 08-31-01, DC-8 SRM 53-2-0 FIG. 2 (SHEET 6) EO SEMAN NR 20051015 DATE 06-29-05. REPAIRED PER SJul 6, 2005 · N822BX · Doug DC871F · Fuselage Main, FrameSDR IXXA05SMN147SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, LT WING INTERIOR ANGLE DEFORMED, STA XFS -17.500 TO XFS -11.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05259 DATE 06-24-05, SEMAN DWG ED 4016 DATE 06-20-05, EO SEMAN NR 2005948 DATE 06-24-05.Jun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN145SGate · improperDURING ROUTINE C CHECK INSPECTION, EXTERNAL FUSELAGE. FREON SYSTEM EXHAUST GATE NON STANDARD REPAIR FS 55.000 L-29L. PERFORMED MAJOR REPAIR IAW SRM, EO SEMAN NR 2005946 DATE 06-21-05. REMOVED EXISTING REPAIR DOUBLER IAW SRM. FABRICATED REPAIR DOUBLER (ALCLADJun 30, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN153SSkin Panel · improperDURING ROUTINE C-CHECK INSPECTION, RH. INBD. FLAP.- FWD UPPER PLATING HAS INTERIN REPAIR, XF 134.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN 20051009 DATE 06-28-05. REMOVED PLATING WITH INTERIM REPAIR IAW DC-8 SRMJun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN152SSkin · improperDURING ROUTINE C CHECK INSPECTION, FWD.- PASSENGER DOOR UPPER PART HAS INTERIN REPAIR. PERFORMED MAJOR REPAIR IAW DC-8 SRM 52-2-0 FIG. 4, EO SEMAN NR 20051011 DATE 06-28-05. REMOVED INTERIM REPAIR IAW DC-8 SRM 51-1-21 PAGE 1. PERFORMED DETAILED VISUAL INSPECTJun 30, 2005 · N822BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA05SMN151SSkin Panel · corrodedDURING ROUTINE C CHECK INSPECTION, LT WING. SLANT PANEL UPPER PART CORRODED, XFS 38.750 - XFS 70.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 37, EO NR 20051004 DATE 06-16-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 21. SMOOTHED AND PEJun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN150SSkin · dentedDURING C CHECK INSPECTION, LT IB FLAP UPPER PART WITH SEVERAL DENTS XW 2.000 - XW 20.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG. 1, EO NR 20051013 DATE 06-29-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-3-0PAGE 1. REMOVED PLATING SEGMENT (DAMAGED)Jun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN149SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LH INBD FLAP UPPER PART DENTED, XW 131.000 PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN Nº 20051010 DATE 06-28-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED NEW PLJun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN146SAngle · deformedDURING ROUTINE C CHECK INSPECTION, LT WING INTERIOR ANGLE DEFORMED, STA XFS -17.500 TO XFS -11.000. PERFORMED MAJOR REPAIR, EO MFG NR 2005948 DATE 06-24-05. REMOVED FASTENERS IAW SRM. REMOVED DAMAGED AREA IAW DWG NR ED 4016, PERFORMED NDT INSPECTION. IAW NDT.Jun 30, 2005 · N822BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA05SMN144SSkin · improperDURING ROUTINE C CHECK INSPECTION, RT WING. CTR L/E SKIN FWD PART HAS NON STANDARD REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-3-1 FIG. 5 SHEET 1, EO SEMAN NR 2005910 DATE 06-18-05. REMOVED DAMAGED PLATING WITH INTERIM REPAIR IAW SRM 51-1-21 Jun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN143SPan · crackedDURING ROUTINE C CHECK INSPECTION, RT WING. CTR L/E ZEE PAN CRACKED 2 INCHES, XFS 520.168. REMOVED AND REPLACED ZEE PAN ON RT WING CTR. L/E XFS 520.168 IAW SRM 51-1-21, SRM 51-1-20 PAGE 9, 21.Jun 30, 2005 · N822BX · Doug DC871F · Wing Main, Frame StructureSDR IXXA05SMN142SVane · misrepairedDURING ROUTINE C CHECK INSPECTION, LT WING SLOT VANE NON STANDARD REPAIR, STA XOLDI 6.235. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21 PAGE 1. REMOVED DAMAGED AREA IAW SEMAN DWG ED 4003, PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED Jun 30, 2005 · N822BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA05SMN141SSkin · deformedDURING ROUTINE C CHECK INSPECTION, LT WING INBD L/E UPPER SURFACE DEFORMED, STA XFS -11.250 TO XFS -23.750. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 05259, SEMAN DWG ED 4016, EO SEMAN 2005948.Jun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN140SSkin · brokenDURING ROUTINE C CHECK INSPECTION, LT WING IB L/E UPPER SURFACE BROKEN, STA XFS 51.250 - 57.500. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 25, EO SEMAN NR 2005908 DATE 06-15-05. REMOVED DAMAGED AREA IAW SRM 57-2-1 FIG. 21. PERFORMED NDT INSPECTION IAW NDT SJun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN139SDoubler · corrodedDURING ROUTINE C CHECK INSPECTION, FUSELAGE EXTERIOR INTERNAL DOUBLER CORRODED , STA 35.000 - 70.000 BETWEEN L - 28 TO L 31. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1, SRM 53-3-1 FIG. 1, EO SEMAN NR 2005877 DATE 06-22-05. REMOVED CORROSION IAW SRJun 30, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN138SSkin · improperDURING ROUTINE C CHECK INSP, RT OB FLAP FWD UPPER PLATING NON STANDARD REPAIR AT STA XF 415.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4 TR NR 57-94, EO SEMAN NR 2005914 DATE 06-18-05. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PAGE 1. FJun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN137SSkin · wornDURING ROUTINE C CHECK INSPECTION, RT OTBD FLAP FWD UPPER PLATING WORN, STA XF 226.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05258 DATE 06-24-05, SEMAN DWG ED 4005 DATE 06-20-05, EO SEMAN 2005913 DATE 06-24-05. REMOVED FASTENERS IAW DC-8 SRJun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN136SSkin · damagedDURING ROUTINE C CHECK INSPECTION, RT OB FLAP FWD UPPER PLATING NON STANDARD REPAIRS (03 EA) AND WEAR DAMAGES BETWEEN STA XF 197.000 - XF 213.000PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4 TR NR 57-94, EO SEMAN NR 2005912 DATE 06-18-05. REMJun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN135SSkin · improperDURING ROUTINE C CHECK INSPECTION, RT IB FLAP LOWER UPPER PLATING NON STANDARD REPAIRS (02 EA) STA XF 45.000 - XF 87.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG. 1, EO NR 2005947. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. REMOVED DAMAGED AREA IAW SRM Jun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN134SSkin Panel · improperDURING ROUTINE C CHECK INSPECTION, RT IB FLAP FWD UPPER PLATING NON STANDARD REPAIRS (02 EA ) STA XW 84.00 -XW 91.00. PERFORMED MAJOR REPAIR IAW NR 05258 DATE 06-24-05, DWG ED 4004, EO NR 2005911 DATE 06-24-05. REMOVED FASTENERS IAW SRM. REMOVED PLATIJun 29, 2005 · N822BX · Doug DC871F · Wing, Plate/Skin
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