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 IXXA0100077OCable · brokenENROUTE FROM ANC TO SEA, AFTER TAKEOFF THE FLIGHT CREW NOTICED A SIGNIFICANT AIRCRAFT ROLL TO THE LEFT AND REQIURED RUDDUR INPUT. THE FLIGHT RETURNED TO ANC FOR AN UNVENTFUL LANDING. MANITHEANCE INSPECTED THE AIRCRAFT WHICH REVEALED A SEGMENT OF THE LEFT WING Dec 14, 2001 · N825BX · Doug DC871F · Flight Control SystemSDR UPS01837359Battery Pack · dischargedINSPECTION TYPE:IN EMERGENCY EXIT LIGHTS BATTERY LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01. OPS CHECKS GOOD.Dec 11, 2001 · N705UP · Doug DC871F · Emergency LightingSDR UPS01837355Windshield · crackedINSPECTION TYPE:N/A ATB- CAPT'S WINDSHIELD CRACKED. REMOVED AND REPLACED WINDSHIELD PER MM 56-10-02.Dec 6, 2001 · N700UP · Doug DC871F · Flight Compartment WindowsSDR UPS01837350Regulator · failedINSPECTION TYPE:N/A DEPARTURE-F/O'S OXY REG EMER SELECTOR FAILED. R&R F/O'S OXY REGDec 4, 2001 · N705UP · Doug DC871F · Crew Oxygen SystemSDR UPS01837349Fire Warning · false activationINSPECTION TYPE:N/A ATB-LOWER CARGO COMPT FIRE WARNING LIGHT ILLUM TEMPORARY. PERFORMED MX TEST ON CARGO COMP LOWER PIT SMOKE DETECTOR SYSTEM, NO FAULTS NOTED SYSTEM OPERATES NORMALLY IAW SECURAPLANE TECHNOLOGIES LLC AIRCRAFT MAINT MANUAL.Dec 4, 2001 · N713UP · Doug DC871F · Fire DetectionSDR UPS01837337Hinge Fitting · crackedINSPECTION TYPE:N/A PIT34 LWR AFT BELLY CARGO DOOR UPPER FWD HINGE POINT STRUCTURE CRACKED. DOOR COMES OFF TRACK AND WILL NOT CLOSE. CLOSED DOOR AND TAPED HANDLE IN STOWED POSITION. REPAIRED IAW DC8 SRM 52-2-0 LOG PAGE 780026 AND 780028.Nov 24, 2001 · N706UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS01837338Smoke Detector · faultyINSPECTION TYPE:N/A REPEAT ITEM (2) - DURING FLIGHT AMBER MX LIGHT ILLUMINATED. TECH RECOMENDS: REVIEW MX HISTORY. DURING SMOKE DETECTOR TEST MX INDICATES ON TWO OCCASIONS THAT SDU FB7739 IS FAULTED. REPLACED BATTERIES, NO HELP. REMOVE AND REPLACE SAID SDUNov 24, 2001 · N708UP · Doug DC871F · Smoke DetectionSDR UPS01837336Support · crackedINSPECTION TYPE:B LT VERT MAIN SUPPORT ANGLE ON AFT SIDE OF AFT PRESS BULKHEAD IS CRACKED IN HALF ABOUT 1 INCH FROM TOP OF BULKHEAD (AS VIEWED FROM LT ACCESS HOLE IN CANTED BULKHEAD). *S/D* LT VERT SUPPORT ANGLE P/N 57735701 1 PREVIOUSLY REPAIRED IN 4-94 IAWNov 23, 2001 · N709UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837333Engine · flamed outINSPECTION TYPE:N/A AT FL370 NR 3 ENG BEGAN TO ROLLBACK SLOWLY. NO RESPONSE TO THROTTLE. TURNED OFF PMC, NO HELP. ATTEMPTED RESTART AT FL330, NO RESTART. ATTEMPTED 2ND RESTART AT 17000 FT, NORMAL START. PERFORMED FUEL LINE NEGATIVE PRESSURE CHECK IAW MM 2Nov 23, 2001 · N709UP · Doug DC871F · Engine (Turbine/Turboprop)SDR UPS01837323Door Frame · crackedINSPECTION TYPE:IN CRACK IN COCKPIT DOOR FRAME, JUST ABOVE AND OUTBOARD OF DOOR (CLOSED) CATCH. INSTALLED DOUBLER ON DOOR FRAME AT DOOR CATCH PER DC-8 SRM 53-2-0.Nov 20, 2001 · N700UP · Doug DC871F · Fuselage Main, StructureSDR UPS01837319Battery Pack · dischargedINSPECTION TYPE:IN EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED BATTERY PACK.Nov 20, 2001 · N798UP · Doug DC871F · Emergency LightingSDR UPS01837320Battery Pack · dischargedINSPECTION TYPE:IN EMERGENCY LIGHTS WOULD NOT COME ON. REMOVED EMERGENCY BATTERY PACK. LIGHTS OPS CK OK.Nov 19, 2001 · N744UP · Doug DC871F · Emergency LightingSDR UPS01837316Door Frame · crackedINSPECTION TYPE:IN COCKPIT DOOR DAMAGED - CREW FWD ENTRY DOOR HAS A CRACK IN THE AFT DOOR FRAME NEAR LATCH. REMOVED 2 DOOR STOP FITTINGS AND FASTENERS 6 INCHES ABOVE AND BELOW DAMAGE. DYE PEN INSPECTED DAMAGED AREA. STOP DRILLED 1.125 INCH CRACK. VERIFIED Nov 17, 2001 · N700UP · Doug DC871F · Passenger/Crew DoorsSDR UPS01837317Window · leakingINSPECTION TYPE:IN LOUD SQUEAL FROM CAPTAIN`S CLEAR VIEW WINDOW TOP. CHECKED CAPTS CLEAR VIEW WINDOW SEAL FOUND NO EVIDENCE OF SEAL TORN. CLEANED WINDOW SEAL AND FRAME. PRESSURIZED AND NO NOTICE OF LOUD SQUEAL.Nov 14, 2001 · N701UP · Doug DC871F · Flight Compartment WindowsSDR UPS01837315Rib · crackedINSPECTION TYPE:N/A RT WING T/E RIB CRACKED AT FORWARD SURFACE VERTICAL CHANNEL AT XW33. THIRD OUTBOARD WAS PREVIOUSLY REPAIRED PER A/C ENGINEERING AMC HAS ASSIGNED INFORMATIONAL ITEM I226648 ASSIGNED.Nov 14, 2001 · N772UP · Doug DC871F · Wing, Rib/BulkheadSDR IXXA0100071OConnector · defectiveENROUTE FROM TOL TO BFI, ON DESCENT THE NUMBER FOUR ENGINE FIRE WARNING SHORT CIRCUIT LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND SECURED THE ENGINE. THE FLIGHT CONTINUED TO BFI FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINENov 10, 2001 · N826BX · Doug DC871F · Detection SystemSDR UPS01837269Fastener · corrodedINSPECTION TYPE:N/A SEVERAL FASTENERS CORRODED IN COMPARTMENT 60 HORZ STABILIZER ACTUATING MECHANISM AREA ITEM SUBMITTED BY FOG TEAM. REMOVED AND REPLACED FASTENERS. CLEANED CORROSION FROM MARKET BOTLS APPROX 120 EA HUCK FASTENERS EXTENDING THROUGH LIGHTENINNov 9, 2001 · N779UP · Doug DC871F · Stabilizer ActuatorSDR UPS01837268Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK VOLTAGE DEAD. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND RELAY UNIT IAW 33-50-01.Nov 9, 2001 · N744UP · Doug DC871F · Emergency LightingSDR UPS01837254Stiffener · crackedINSPECTION TYPE:B COMPARTMENT 60 AFT PRESS BULKHEAD J-BEAM 5TH FROM BOTTOM OF LT SIDE HAS CRACK AS MARKED. STOP DRILLED CRACK REF DC8-5310-15663-A14596. FABRICATED UPPER REPAIR BRACKET PER PRELIMINARY EO DC8-5310-15663-A DP 70236.Nov 5, 2001 · N779UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837185Battery Pack · dischargedINSPECTION TYPE:IN EMERGENCY LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01, OPS CHECK GOOD.Oct 26, 2001 · N700UP · Doug DC871F · Emergency LightingSDR IXXA0100066OActuator · leakingDURING DESCENT FROM DXB TO BRU, THE FLIGHT CREW NOTICED A DECLINE IN THE THE HYDRAULIC QUANTITY SYSTEM. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO BRU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND LOCATED A DEFECTIVE FLAOct 22, 2001 · N822BX · Doug DC871F · Trailing Edge Flap ActuatorSDR UPS01837256Longeron · corrodedINSPECTION TYPE:C2 STA 1690 LONG 30L IS CORRODED BEYOND LIMITS. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW SRM 53-2-2 FIG 10.Oct 18, 2001 · N718UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS01837204Fitting · corrodedINSPECTION TYPE:C2 STA 280 ST LONG 32R TO 33R CORNER T-FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3757794,AND SRM 51-1-20D.Oct 18, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837203Splice · corrodedINSPECTION TYPE:C2 STA 190 LONG 36 SPLICE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3619434,AND SRM. 51-1-20D.Oct 18, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837200Fitting · crackedINSPECTION TYPE:C2 LT HORIZONTAL STAB L/E LOWER FITTING IS CRACKED AT O/B END BETWEEN XFS 47.5 TO XFS 60. REMOVED AND REPLACED FITTING IAW DWG SE08550009, AND SRM 51-1-21, 51-1-20D.Oct 18, 2001 · N718UP · Doug DC871F · Horizontal Stabilizer StructureSDR UPS01837197Skin · crackedINSPECTION TYPE:C2 R-2 DOOR UPPER AFT CORNER HAS CRACKED SKIN, INTERNAL DOUBLER AND LONGERON 11R. TRIMMED CRACKED SKIN AND INTERNAL DOUBLER, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND STRAP IAW 8110-3 APPROVED SH SK 718-455, DC8-5330-15612-A, AND SRM 53-2Oct 18, 2001 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS01837090Sliding Window · out of adjINSPECTION TYPE:PFLT CAPTAIN SLIDING WINDOW WILL NOT OPEN. ADJUSTED PER MM 56-10-00. OPS CHECKS GOOD.Oct 18, 2001 · N715UP · Doug DC871F · Flight Compartment WindowsSDR UPS01837253Doubler · corrodedINSPECTION TYPE:C2 TAIL CONE INNER DOUBLER AT 62 ACCESS HOLE, AND LT OUTER SKIN IS CORRODED BEYOND LIMITS STA 1861-1890 APPROX. REMOVED, FABRICATED, AND REPLACED DOUBLER AND SKIN SECTION IAW DWG 5704650, AND SRM 53-1-0, 51-1-21, 51-1-20D.Oct 17, 2001 · N718UP · Doug DC871F · Aerodynamic FairingsSDR UPS01837251Web · corrodedINSPECTION TYPE:C2 RT UPPER CUSP IS CORRODED BEYOND LIMITS STA 1000-1110 LONG 21R. REMOVED, FABRICATED, AND REPLACED SECTION OF CUSP FROM STA 1080-1110 IAW SRM 53-2-5 FIG 15.Oct 17, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837250Longeron · corrodedINSPECTION TYPE:C2 LONG 35L IS CORRODED BEYOND LIMITS BETWEEN STA 1380 TO 1400. CUT OUT DAMAGED LONGERON SECTION, FABRICATED AND SPLICED IN SECTION OF LONGERON IAW SRM 53-2-2 FIG 10.Oct 17, 2001 · N718UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS01837228Fitting · crackedINSPECTION TYPE:C2 STA 1260 LONG 33R O/B AFT SIDE INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.Oct 17, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837226Fitting · crackedINSPECTION TYPE:C2 STA 1240 LONG 33R I/B INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.Oct 17, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837209Skin · corrodedINSPECTION TYPE:C2 FINGER DOUBLER AND SKIN IS CORRODED BEYOND LIMITS STA 1350 LONG 34L-35L. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5779915, CUTOUT CORRODED AREA, NDT FOR CRACKS, NO CRACKS NOTED, FABRICATED AND INSTALLED FILLER, DOUBLER, AND FINGER DOct 17, 2001 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS01837199Support · crackedINSPECTION TYPE:C2 STA 1220 LONG 27R FLOORBEAM SUPPORT IS CRACKED AT LOWER END. REMOVED AND REPLACED SUPPORT IAW DWG 9754024, AND SRM 51-1-20D, 51-1-21.Oct 17, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837198Longeron · crackedINSPECTION TYPE:C2 STA 1770 LONG 17R LONGERON AND END FITTING ARE CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-21, 51-1-20D, AND REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG S-1616757, AND SRM 51-1-20D, 51-1-21.Oct 17, 2001 · N718UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS01837196Longeron · crackedINSPECTION TYPE:C2 STA 940 LONG 24L IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED, AND INSTALLED DOUBLERS IAW SRM 53-2-0 FIG 5.Oct 17, 2001 · N718UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS01837183Rib · crackedINSPECTION TYPE:C2 LT HORIZONTAL STAB L/E LOWER RIB IS CRACKED AT XFS 116.25. REMOVED FASTENERS, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 55-2-0 FIG 2.Oct 17, 2001 · N718UP · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR UPS01837182Rib · crackedINSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E RIB IS CRACKED AT XFS 91.25. REMOVED FASTENERS, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 55-2-0 FIG 2.Oct 17, 2001 · N718UP · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR UPS01837181Web · crackedINSPECTION TYPE:C2 LOWER RUDDER MEMBRANE IS CRACKED BETWEEN ZR 54.2 AND ZR 61.156, VERTICAL MEMBRANE APPROX 12 INCHES AFT AF L/E. REMOVED, FABRICATED, AND REPLACED WEB/MEMBRANE IAW DWG 5655074, AND SRM 51-1-21.Oct 17, 2001 · N718UP · Doug DC871F · Rudder StructureSDR UPS01837255Fitting · crackedINSPECTION TYPE:C2 STA 1200 BATHTUB FITTING IS CRACKED AT LONG 34R. REMOVED AND REPLACED FITTING IAW DWG 3755841, AND SRM 51-1-20D.Oct 16, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837235Fitting · corrodedINSPECTION TYPE:C2 STA 1220 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 34R TO 35R. REMOVED AND REPLACED FITTING IAW DWG 3755843, AND SRM 53-2-0 FIG 2D.Oct 16, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837234Intercostal · crackedINSPECTION TYPE:C2 INTERCOSTAL IS CRACKED AT STA 1435 BL 0 ABOVE D-PIT DOOR. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1D.Oct 16, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837225Fitting · crackedINSPECTION TYPE:C2 STA 1152 LONG 33R BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847, AND SRM 51-1-20D, 51-1-21.Oct 16, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837223Skin · crackedINSPECTION TYPE:C2 L-1 DOOR LOWER AFT CORNER DOUBLER DOES NOT CONFORM TO SRM 53-2-0, AND SKIN IS CRACKED AT STA 55 LONG 21L AREA. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AROUND CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FOct 16, 2001 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS01837206Fitting · corrodedINSPECTION TYPE:C2 STA 1210 LONG 33R BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 5894282,AND SRM 51-1-20D.Oct 16, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837179Fitting · corrodedINSPECTION TYPE:C2 STA 70 LONG 27R END FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4611067, AND SRM 51-1-20D, 51-1-21.Oct 16, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837248Skin · crackedINSPECTION TYPE:C2 L-1 DOOR FWD UPPER CORNER DOUBLER DOES NOT CONFORM TO THE SRM AND SKIN IS CRACKED AT STA 30 LONG 10L. REMOVED EXISTING DOUBLER AND CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER IAW 8110-3 APPROct 15, 2001 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS01837227Fitting · crackedINSPECTION TYPE:C2 STA 280 LONG 33R O/B BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755827, AND SRM 51-1-20D.Oct 15, 2001 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01837222Skin · crackedINSPECTION TYPE:C2 A-PIT DOOR OPENING FWD LOWER CORNER SKIN IS GOUGED AND CRACKED AT STA 280 LONG 31R-32R APPROX. CUT OUT DAMAGED AREA, NDT FOR CRACKS AT CUTOUT, NO CRACKS NOTED, FABRICATED AND INSTALLED FILLER, DOUBLER, AND TRIPLER IAW SRM 53-2-0 FIG 20 AND SOct 15, 2001 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS01837208Doubler · corrodedINSPECTION TYPE:C2 STA 883 BL 0 UPPER SURFACE OF WHEEL WELL PRESSURE WEB HAS A FINGER DOUBLER CORRODED BEYOND LIMITS REMOVED,FABRICATED,AND REPLACED DOUBLER IAW DWG 5645332,AND SRM 51-1-21.Oct 15, 2001 · N718UP · Doug DC871F · Fuselage Main, Plate/Skin
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