Boeing DC-9-83

Service difficulty reports · 16,530

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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 = 'DC983'
  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 GTIA200600073Hydraulic System · contaminatedRIGHT HYDRAULIC SYSTEM LOST PRESSURE AT TOP OF DESCENT. GEAR DOORS WOULD NOT CLOSE. MX FOUND AIR IN RIGHT HYDRAULIC SYSTEM. BLED AIR FROM SYSTEM AND NO HYDRAULIC FLUID REQUIRED.Jul 29, 2006 · N815NK · Doug DC983 · Hydraulic System, MainSDR FX7A200600006Fcu · leakingAFTER ENGINE STARTING AND DURING TAXI A STRONG ODOR OF FUEL IN THE AIRCRAFT CABIN WAS DETECTED FOR THESE REASON THE AIRCRAFT RETURNED TO THE BLOCK. LOG PAGE 38680 - MIA LINE MTX INSPECTED THE AIRCRAFT AND FOUND THAT THERE WAS FUEL LEAKING OUT OF THE APU FUELJul 27, 2006 · N836NK · Doug DC983 · APU Engine Fuel and ControlSDR ASAA0680807Skin · gougedRIGHT OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR AT INBOARD LEADING EDGE. REMOVED EXISTING REPAIR DOUBLER. INSTALLED SKIN FILLER AND EXTERNAL DOUBLER PER SRM 57 03.Jul 25, 2006 · N958AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0680806Skin · gougedLEFT OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR AT INBOARD LEADING EDGE. REMOVED EXISTING REPAIR DOUBLER. INSTALLED SKIN FILLER AND EXTERNAL DOUBLER PER SRM 57 03.Jul 25, 2006 · N958AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0680805Shear Tie · corrodedFOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 4 51 10 3 AND 51 30 5.Jul 25, 2006 · N958AS · Doug DC983 · Fuselage Internal Mounting StructureSDR ASMF200607016Unknown · unknownAIRCRAFT RETURNED TO PLATFORM DUE TO AFTER RT ENGINE STARTING SPEED AND F/D FLAGS WERE SHOWN IN ADI AND FLIGHT GUIDANCE COMPUTER WITHOUT INDICATION IN FMA NR 2. AC POWER SWITCH WAS RESET CORRECTING THE FAILURE, TESTED CORRECT IAW MM 24-20-00.Jul 22, 2006 · N583MD · Doug DC983 · Standard Practices/StructuresSDR ASAA0680790Rib · gougedTHE RT NR 4 SLAT O B FITTING (RIB ASSY) IS GOUGED OUT OF LIMITS. REMOVED DAMAGED RIB ASSY LOCATED DRILLED AND INSTALLED A REPLACEMENT RIB ASSY IAW MD 80 SRM 51 10 4 AND 51 30 8Jul 20, 2006 · N958AS · Doug DC983 · Leading Edge DevicesSDR ASAA0680789Skin · misdrilledFUSELAGE SKIN HAS MECHANICAL DAMAGE. (MISDRILLS DUE TO PREVIOUSLY ACCOMPLISHED STOP DRILLS ON THE R H ENGINE PYLON UPPER AFT FAIRING SUPPORT ANGLE) CUT OUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED A FILLER EXTERNAL DOUBLER AND TWO TAPERED SHIMS IAW AARJul 20, 2006 · N958AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0680788Shear Tie · corrodedSHEAR TIE CORRODED OUT OF LIMITS AT FS 1211 BETWEEN LONGERONS 29R AND 30. REMOVED DAMAGED SHEAR TIE FABRICATED AND INSTALLED A REPLACEMENT SHEAR TIE IAW MD 80 SRM 51 10 4 51 40 3 AND 51 30 5.Jul 20, 2006 · N958AS · Doug DC983 · Fuselage Internal Mounting StructureSDR AALA20060462Battery Pack · inoperativeLGA - OVERHEAD EMERGENCY LIGHTS AT ROWS 29 TO 32 AND COCKPIT INOPERATIVE. REPLACED BATTERY PACKS AT OVERHEAD ACROSS FROM FIRST CLASS LAVATORY AND B5107 FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 29 TO 32 AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 16, 2006 · N983TW · Doug DC983 · Emergency LightingSDR AALA20060463Pin · inoperativeSTL - TAIL CONE JETTISON SYSTEM INSPECTION AND OPERATIONAL CHECK FAILED FIRST DROP FROM AFT PASSENGER DOOR. ADJUSTED AND LUBRICATED PUSH PIN. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 16, 2006 · N599AA · Doug DC983 · Aerodynamic FairingsSDR ANCF200600025Unknown · multiple failAT FL 330, WITH AIRFOIL AND ENG ANTI-ICE ON, R ICE PROT TEMP LOW ANNUNCIATION CAME ON WITH 22 PSI WITH RT CABIN TEMP IN AUTO MODE AFTER 10 MIN R PACK WAS TRIPPED AND PRESS DROPPED TO 0, ABNORM PROCEDURE PERFORMED, WITH UNSATISFACTORY RESULT WITH R PACK TRIPPEJul 13, 2006 · N836RA · Doug DC983 · Air Conditioning SystemSDR ASAA0680759Lanyard · wornINADVERTENTLY DEPLOYED TAIL CONE WHICH SHOULD HAVE ALSO CAUSED AFT EMERGENCY SLIDE TO DEPLOY. LANYARD VELCRO AND SNAP PULLED LOOSE FROM THE SLIDE COVER BUT THE SLIDE DID NOT DEPLOY. RETRIGGER SLIDE ASSEMBLY WITH NEW LANYARD. ENGINEERING INVESTIGATION HAS BEJul 11, 2006 · N961AS · Doug DC983 · Escape SlideSDR ASAA0680753Channel · corrodedCABIN FLOOR PANEL HAT CHANNEL CORRODED AT HOLE. REPLACED HAT CHANNEL PER DAC DRAWING 9957921.Jul 10, 2006 · N972AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0680752Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05.Jul 10, 2006 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680751Skin · damagedAFT CARGO BAY DOOR CREASED JUST BELOW HANDLE. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER FILLER AND SHIMS PER ASA EA 5230 01321.Jul 10, 2006 · N972AS · Doug DC983 · Cargo/Baggage DoorsSDR AALA20060447Battery Pack · inoperativeORD - EMERGENCY LIGHTS AT FORWARD AND AFT GALLEY AND LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD AND AFT GALLEY AND LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 8, 2006 · N9402W · Doug DC983 · Emergency LightingSDR ASAA0680750Skin · corrodedFUSELAGE SKIN INTERNAL DOUBLER IS CORRODED. REMOVED DAMAGED AREA. INSTALLED INTERNAL FILLER AND AN EXTERNAL DOUBLER PER EA 5330 02114.Jul 7, 2006 · N950AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0680749Skin · corrodedFUSELAGE SKIN INTERNAL DOUBLER CORRODED. REMOVED DAMAGED AREA OF DOUBLER. INSTALLED FILLER AND AN EXTERNAL DOUBLER PER EA 5330 02113.Jul 7, 2006 · N950AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0680748Skin · corrodedFUSELAGE SKIN CORRODED. TREATED AND PRIMED CORRODED AREA. INSTALLED REPAIR DOUBLER PER SRM 53-04.Jul 7, 2006 · N950AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0680747Skin · dentedRIGHTHAND NR 1 SLAT LEADING EDGE DENTED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER PER SRM 57-09.Jul 7, 2006 · N950AS · Doug DC983 · Leading Edge DevicesSDR ASAA0680746Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. BOND REPAIRED DAMAGED AREA PER SRM 51-70-3.Jul 7, 2006 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680745Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. BOND REPAIRED DAMAGED AREA PER SRM 51-70-3.Jul 7, 2006 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680744Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. BOND REPAIRED DAMAGED AREA PER SRM 51-70-3.Jul 7, 2006 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680743Floor Panel · chafedCABIN FLOOR PANEL CHAFED. REPLACED FLOOR PANEL PER SRM 51-30-2.Jul 7, 2006 · N972AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0680742Floorbeam · corrodedCABIN FLOORBEAM CORRODED. REPLACED SUPPORT PER SRM 51-30-2.Jul 7, 2006 · N972AS · Doug DC983 · Fuselage Main, Floor BeamSDR ASAA0680740Fitting · corrodedGALLEY MOUNT FITTING CORRODED. REPLACED FITTING PER SRM 51-10-4 AND 51-30-5.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Main, Attach FittingsSDR ASAA0680739Insert · pulledCABIN FLOOR PANEL INSERTS PULLED. REPLACED FLOOR PANEL PER SRM 53-05.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680738Support · corrodedR1 DOOR GIRT BAR SUPPORT CORRODED. REPLACED SUPPORT PER SRM 51-10-4.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Main, Attach FittingsSDR ASAA0680737Insert · pulledCABIN FLOOR PANEL HAS PULLED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680736Web · corrodedR1 DOOR AREA WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. INSTALLED FILLER AND DOUBLER PER SRM 51-70-04.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0680735Seat Track · corrodedSEAT TRACK CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR SECTION PER SRM 53-05.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0680734Seat Track · corrodedCABIN SEAT TRACK CORRODED. REPLACED DAMAGED SECTION. INSTALLED REPAIR DOUBLER PER SRM 53 05.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0680733Angle · corrodedCABIN FLOOR PANEL Z-ANGLE SUPPORT CORRODED. REPLACED Z-ANGLE SUPPORT PER SRM 51-30-2.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0680732Dummy Rail · corrodedFALSE TRACK CORRODED. REPLACED FALSE TRACK PER SRM 51-30-1.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0680731Floor Panel · corrodedCABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680730Floor Panel · corrodedCABIN FLOOR PANEL CORRODED. REPLACED FLOOR PANEL PER SRM 53-05.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680729Floor Panel · corrodedCABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680728Floor Panel · damagedCABIN FLOOR PANEL CREASED. REPLACED FLOOR PANEL PER SRM 53-05.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680727Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680726Vane · gougedRT WING OUTBOARD FLAP INBOARD VANE GOUGED ON LEADING EDGE. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2.Jul 6, 2006 · N972AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0680725Cusp Web · corrodedCUSP WEB CORRODED. REMOVED CORROSION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-01 AND 51-70-4.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0680724Skin · dentedFUSELAGE DENTED. RECONTOURED SKIN. INSTALLED DOUBLER PER SRM 53-04.Jul 6, 2006 · N972AS · Doug DC983 · Fuselage Main, Plate/SkinSDR AALA20060445Compressor · stalledRIGHT ENGINE HAD COMPRESSOR STALLS UPON TAKEOFF AT MAXIMUM POWER. STALLS CLEARED AT OR NEAR IDLE THRUST. REPLACED RIGHT ENGINE ON 07 JUL 2006. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 4, 2006 · N591AA · Doug DC983 · Turbine Engine Compressor SectionSDR AALA20060426Blade · failedMCI - INFLIGHT STL TO SEA. CLIMBING THROUGH FLIGHT LEVEL 280 HEARD LOUD BANG FROM RIGHT HAND ENGINE ACCOMPANIED BY THRUST LOSS. RIGHT HAND ENGINE N1 LESS THAN LEFT HAND ENGINE N1. RIGHT HAND ENGINE SHUT DOWN AND LANDED MCI OVERWEIGHT WITHOUT INCIDENT. RIGHJun 30, 2006 · N435AA · Doug DC983 · Engine (Turbine/Turboprop)SDR AALA20060421Oven · dirtyDFW - INFLIGHT FLIGHT ATTENDANT REPORTED SMOKE COMING FROM FORWARD GALLEY OVEN. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION. PLACARDED FIRST CLASS OVEN AND PULLED AND COLLARED CIRCUIT BREAKER. CLEANED HEATING Jun 28, 2006 · N9626F · Doug DC983 · Buffet/GalleysSDR AALA20060416Pump · inoperativeORD - INFLIGHT CENTER FUEL TANK CIRCUIT BREAKER POPPED. REPLACED AFT CENTER FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.Jun 27, 2006 · N597AA · Doug DC983 · Engine Fuel PumpSDR ASMF200606015Cowling · damagedDURING TRANSIT CHECK, A LOSE OF MATERIAL IN THE LT ENGINE NOISE SUPPRESSOR WAS DETECTED. AN INSPECTION WAS PERFORMED AND DAMAGE WAS OUT OF LIMITS, THEREFORE, THE AIRCRAFT WAS SENT TO THE HANGAR AND THE LT ENGINE NOSE COWLING WAS REPLACED IAW MM 71-10-01, TESTEJun 25, 2006 · N583MD · Doug DC983 · Engine (Turbine/Turboprop)SDR AALA20060411Trim Motor · inoperativeDTW - INFLIGHT AFTER LOC CAP DISCONNECTED AUTOPILOT REALIZED HAD RUNAWAY TRIM. RAN PROCEDURE IN QRH FOR RUNAWAY STABILIZER. PULLED CBS D9-10-11 LOST ALL TRIM, HAD NO ALTERNATE TRIM. DECLARED EMERGENCY DID GO AROUND AND CONFIGURED W .5 NOSE DOWN TRIM. AUTO Jun 24, 2006 · N589AA · Doug DC983 · Stabilizer Position IndicatingSDR AALA20060400Fire Detector · inoperativeLAS - INFLIGHT LAX ORD NUMBER TWO ENGINE FIRE WARNING LOOP-B WHILE LOOP-A ON PLACARD. AIRCRAFT DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. NO OTHER INDICATIONS OF FIRE. NO FIRE WAS CONFIRMED UPON LANDING. REPLACED LOWER FIRE DETECTION UNIT ON RIGHT HAND EJun 20, 2006 · N984TW · Doug DC983 · Fire Detection
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