Douglas DC-8-71F

Service difficulty reports · 8,938

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Query with SQL
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"

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 UPS02837617Fitting · crackedINSPECTION TYPE:C2 AFT PIT CORROSION FS 1060 ON L35L AT FRAME INTERSECT, LONGERON SPLICE FITTING FOUND TO BE CRACKED.Jan 29, 2002 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXAO200003OUplock · lack of lubeEN ROUTE FROM MCI TO TOL, THE LANDING GEAR NOT LATCHED LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE LANDING BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPEJan 29, 2002 · N826BX · Doug DC871F · Landing Gear Retraction/Extension SystemSDR IXXA0200019SFitting · gougedDURING ROUTINE C-CHECK INSPECTION A GOUGE WAS DETECTED ON THE FLAP SUPPORT FITTING INBOARD INNER EDGE, STATION 405. BLENDED OUT DAMAGED AREA IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 57-DC8-1839.Jan 28, 2002 · N823BX · Doug DC871F · Wing StructureSDR UPS02837616Pan · crackedINSPECTION TYPE:C2 C PIT DOOR FRAME CRACKED AT UPPER AFT CORNER NEAR GRAB HANDLE. INSTALLED NEW DOOR PAN IAW DC8 SRM 51-1-21, 51-3-0, 51-1-20D, 51-1-21A.Jan 28, 2002 · N752UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS02837614Floorbeam · crackedINSPECTION TYPE:C2 AFT ACCY COMPT STA 1660 FLOORBEAM WEB IS CRACKED I/B OF PREVIOUS REPAIR AT RBL 37.Jan 27, 2002 · N752UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS02837615Doubler · crackedINSPECTION TYPE:C2 REMOVED STEEL DOUBLER FROM L1 DOOR JAMB EXTERIOR UPPER FWD CORNER. REPAIRED AREA IAW REO G08505 AND UPS EO DC8-5330-15976-A.Jan 26, 2002 · N752UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837452Angle · crackedINSPECTION TYPE:C2 STA 798 LBL 49 FLOORBEAM WEB ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW DWG 3643112 AND SRM 51-1-20D.Jan 22, 2002 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837426Skin · crackedINSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1350 LONG 34R. CUT OUT CRACK, NDT VERIFIED NO CRACK AT CUT OUT AREA. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-1 FIG 7.Jan 18, 2002 · N702UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200002OTransmitter · defectiveWHILE ENROUTE FROM JFK TO BDL, THE FLIGHT CREW NOTICED THAT THE MAIN HYDRAULIC QUANTITY SYSTEM WAS DECLINING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO BDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND TRACED THE PROBLEJan 17, 2002 · N824BX · Doug DC871F · Hydraulic Quantity IndicatorSDR IXXA0200001OTransmitter · defectiveWHILE ENROUTE FROM JFK TO BDL, THE FLIGHT CREW NOTICED THAT THE MAIN HYDRAULIC QUANTITY SYSTEM WAS DECLINING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO BDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND TRACED THE PROBLEJan 17, 2002 · N824BX · Doug DC871F · Hydraulic Quantity IndicatorSDR UPS02837411Cdu · malfunctionedINSPECTION TYPE:N/A DIVERSION TO PIT LOWER FWD CARGO SMOKE WARNING IN FLIGHT. NOTE: MX STATED SYSTEM TESTED OK ON GROUND. MX SMELLED CHEMICAL WHEN OPENING CARGO DOOR. HAZMAT TEAM ON SITE. PERFORMED TEST OF EACH FIRE DET PER MM 26-18-00 SYSTEM. COMPLETE BJan 16, 2002 · N744UP · Doug DC871F · Smoke DetectionSDR UPS02837422Warning System · malfunctionedINSPECTION TYPE:N/A DURING FAULT ON NR 4 BUSS POWER FAIL LANDING GEAR FAULT ON EXTENSION THE GEAR HAD UNSAFE INDICATION ON ALL THREE GEARS AND GEAR WARNING HORN. PERFORMED LANDING GEAR CONTROL SYSTEM CHECK PER MM 32-31-00, NO FAULTS NOTED. SYSTEM CHECKS GOODJan 16, 2002 · N744UP · Doug DC871F · Landing Gear Position and WarningSDR IXXA0200016SDoor · gougedDURING ROUTINE C-CHECK INSPECTION, A GOUGE WAS DETECTED ON THE C-1 DOOR CUTOUT, AFT SECTION BY THE LIGHT SWITCH, STATION 340. BLENDED OUT DAMAGED AREA. FABRICATED AND INSTALLED NEW REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERINJan 10, 2002 · N823BX · Doug DC871F · DoorsSDR UPS02837435Skin · crackedINSPECTION TYPE:C2 STA 1470 AT LONG 34R SKIN IS CRACKED. CUT OUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUT OUT. FABRICATED REPAIR AND INSTALLED IAW SRM 53-2-1 FIG 7.Jan 10, 2002 · N702UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200006SWing · crackedDURING ROUTINE C-CHECK INSPECTION A CRACK WAS DETECTED ON THE RIGHT WING CENTER LEADING EDGE FORWARD SIDE AT STATION WS485. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER EDJan 7, 2002 · N823BX · Doug DC871F · Leading Edge DevicesSDR UPS02837437Floorbeam · corrodedINSPECTION TYPE:C2 STA -80 FLOORBEAM AND PRESSURE WEB ARE CORRODED BEYOND LIMITS AT LBL 47-59 APPROX. FABRICATED AND INSTALLED WEB AND FINGER DOUBLERS IAW SRO 8530026, FABRICATED AND INSTALLED FLOORBEAM SPLICE REPAIR IAW 8110-3 DH SK 702-953.Jan 5, 2002 · N702UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS03840035Intercostal · crackedINSPECTION TYPE: C2, STA 950 INTERCOSTAL IS CRACKED BETWEEN MAIN LANDING GEAR DOORS AT RBL 4. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5616306, AND SRM 51-1-20D.Jan 3, 2002 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837392Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS BATTERY INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01. OPS CHECKS GOOD.Jan 3, 2002 · N752UP · Doug DC871F · Emergency LightingSDR UPS02837391Battery Pack · dischargedINSPECTION TYPE:IN EMERGENCY LIGHTS WILL NOT TEST ON PREFLIGHT CHECK. REMOVED, REPLACED BATTERY PACK AND RELAY UNIT PER DC8 MM 33-50-01. OPS CHECK GOOD.Jan 3, 2002 · N705UP · Doug DC871F · Emergency LightingSDR UPS02837433Splice · crackedINSPECTION TYPE:C2 STA 200-220 LONG 31L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED FITTING IAW 8110-3 APPROVED DH SK 702-811.Jan 2, 2002 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837487Shear Tie · crackedINSPECTION TYPE:C2 STA 1860 LONG 3R CLIP/SHEAR TIE IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 53-2-0 FIG 1B.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Main, StructureSDR UPS02837486Fitting · crackedINSPECTION TYPE:C2 BATHTUB FITTING IS CRACKED AT STA 1230 BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843, AND SRM 53-2-0 FIG 2D.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837455Longeron · crackedINSPECTION TYPE:C2 STA 1770 LONG 17R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 5649327 AND SRM 51-1-20D, 51-3-0, 51-1-21.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837454Fitting · crackedINSPECTION TYPE:C2 FLOORBEAM ATTACH FITTING IS CRACKED AT STA, 742 LBL 24. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837453Fitting · corrodedINSPECTION TYPE:C2 BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STA 1230 BETWEEN LONG 36 TO 35L. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837451Fitting · crackedINSPECTION TYPE:C2 STA 1240 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D, 51-3-0.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837438Web · crackedINSPECTION TYPE:C2 RUDDER NR 2 HINGE CUT OUT LOWER WEB IS CRACKED AT ZR 161 APPROX. REMOVED, FABRICATED AND REPLACED WEB IAW DWG 5656229 AND SRM 51-1-21.Dec 30, 2001 · N702UP · Doug DC871F · Rudder StructureSDR UPS02837436Fitting · corrodedINSPECTION TYPE:C2 STA 1230 BETWEEN LONG 27L-28L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755842 AND SRM 53-2-0 FIG 2D.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837434Longeron · crackedINSPECTION TYPE:C2 STA 1260-1280 LONG 34R IS CRACKED. REMOVED LONGERON, FABRICATED LONGERON REPAIR AND SPLICES AND INSTALLED IAW 8110-3 APPROVED DH SK 702-586.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837432Splice · crackedINSPECTION TYPE:C2 STA 1040-1060 LONG 35R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837431Fitting · crackedINSPECTION TYPE:C2 STA 987 LONG 23L END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3753306 AND SRM 51-1-20D.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837430Fitting · crackedINSPECTION TYPE:C2 STATION 1180 LONG 34R-35R BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755843, AND SRM 51-1-20D.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837429Fitting · crackedINSPECTION TYPE:C2 STATION 1200 LONG 34R-35R BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 53-2-0 FIG 2D.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837427Splice · crackedINSPECTION TYPE:C2 STA 1040-1060 LONG 35L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750545, AND SRM 51-1-20D.Dec 30, 2001 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837387Shear Tie · crackedINSPECTION TYPE:IN AFT PRESS BULKHEAD CANTED WEB 2 SHEAR TIES CRACKED RT SIDE BETWEEN L10 & L11 45 ANGLE BRACKET ATTACHED TO CONTROL BULKHEAD CRACKED AS MARKED. REMOVED EXISTING FASTENER FOR REPAIR. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER.Dec 30, 2001 · N705UP · Doug DC871F · Fuselage Main, StructureSDR UPS02837508Longeron · corrodedINSPECTION TYPE:C2 STA 1395 - 1447 LONG 34R IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LONGERON SEGMENT IAW DWG 3646937 AND SRM 53-1-0, 51-1-20D, 51-1-21.Dec 29, 2001 · N702UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837483Longeron · crackedINSPECTION TYPE:C2 LONG 24L IS CRACKED PAST STOP DRILL STA 857-879. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-2 FIG 5.Dec 29, 2001 · N702UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837488Frame · crackedINSPECTION TYPE:C2 LT WHEEL FWD BULKHEAD LOWER WING CHORD STA 857 AT XCW 0 CRACK. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR ANGLES AND FILLERS IAW 8110-3 APPROVED DH SK 702-461.Dec 28, 2001 · N702UP · Doug DC871F · Fuselage Main, FrameSDR UPS02837485Skin · crackedINSPECTION TYPE:C2 R-2 DOOR UPPER AFT CORNER FUSELAGE SKIN IS CRACKED AT STA 1660 LONG 11R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0 FIG 16.Dec 28, 2001 · N702UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837480Skin · crackedINSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT L-2 DOOR LOWER FWD CORNER STA 1620 AT LONG 20L. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0 FIG 18.Dec 28, 2001 · N702UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837396Skin · corrodedINSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 347.5 AND XFS 366.5. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38.Dec 28, 2001 · N702UP · Doug DC871F · Wing, Plate/SkinSDR UPS02837428Angle · crackedINSPECTION TYPE:C2 STATION 1766 AT LONG 2L FUSELAGE TO VERTICAL STAB ANGLE IS CRACKED AND CORRODED. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-5 FIG 16A.Dec 27, 2001 · N702UP · Doug DC871F · Fuselage, Stabilizer Attach FittingsSDR UPS02837397Pressure Panel · crackedINSPECTION TYPE:C2 STATION 683 BULKHEAD IS CRACKED AT RBL 5 AND RBL 12 AT WEB AT LOWER WING SPAR. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUT OUT. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW SRM 53-2-5 FIG 13.Dec 27, 2001 · N702UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS02837489Frame · corrodedINSPECTION TYPE:C2 STA 70 FRAME IS CORRODED BEYOND LIMITS AT LONG 35R TO 36. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-5 FIG 8C.Dec 26, 2001 · N702UP · Doug DC871F · Fuselage Main, FrameSDR UPS02837395Frame · crackedINSPECTION TYPE:C2 STA 55 FRAME IS CRACKED AT ROD ATTACH POINT LONG 23R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FRAME AND SEGMENT IAW SRM 53-2-0 FIG 2.Dec 26, 2001 · N702UP · Doug DC871F · Fuselage Main, FrameSDR UPS01837381Longeron · corrodedINSPECTION TYPE:N/A CORROSION AT LONGERON 34.Dec 22, 2001 · N772UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS01837380Bulkhead · crackedINSPECTION TYPE:N/A FWD FRAME PRESS BULKHEAD LONGERON 35 CRACKED.Dec 22, 2001 · N772UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS01837373Battery Pack · dischargedINSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY, OPS CHECKED NORMAL.Dec 19, 2001 · N750UP · Doug DC871F · Emergency LightingSDR UPS01837369Engine · flamed outINSPECTION TYPE:N/A EXPERIENCED IN FLIGHT FLAME-OUT NR 2 ENG DURING CRUISE. FLAME-OUT OCCURRED APPROX 1 MINUTE AFTER NR 2 X-FEED LEVER PLACED DOWN/OPEN. ALL MAIN BOOST PUMPS ON 1, 3 AND 4 FILL VALVES OPEN. NR 2 TANK 1000 LBS HEAVIER THAN 1, 3 + 4. PERFORMEDec 18, 2001 · N701UP · Doug DC871F · Engine (Turbine/Turboprop)SDR UPS01837372Battery Pack · dischargedINSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK, OPS OK.Dec 18, 2001 · N798UP · Doug DC871F · Emergency Lighting
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