Boeing DC-9-83

Service difficulty reports · 16,530

Newest first. General aviation reporting is voluntary.

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 ASAA0580425Skin · dentedOKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. COLD-WORKED DENTED AREA. INSTALLED INTERNAL REPAIR DOUBLER. (M)Dec 19, 2005 · N947AS · Doug DC983 · Fuselage Main, Plate/SkinSDR GTIA050274Seat Track · corrodedSTA 1136, LT IB SEAT TRACK TANG DIMENSION BELOW 0.90. REMOVED DAMAGED AREA DRILLED NEW TRACK, TREATED, PRIMED AND INSTALLED SPLICE. (K)Dec 13, 2005 · N802NK · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0580542Floor Panel · corrodedC-CHECK, CABIN FLOOR PANEL HAS CORRODED INSTERTS AND IS DELAMINATED AROUND INSTERS. REPLACED FLOOR PANEL. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0580557Vane · dentedC-CHECK, LT WING NR 1 FLAP VANE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (K)Dec 12, 2005 · N973AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0580556Vane · puncturedC-CHECK, LT WING NR 1 FLAP VANE IS PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (K)Dec 12, 2005 · N973AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0580555Vane · gougedC-CHECK, LT WING OB FLAP IB VANE IS GOUGED. BLENDED GOUGE. INSTALLED REPAIR DOUBLER. (K)Dec 12, 2005 · N973AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0580554Skin · dentedC-CHECK, FUSELAGE SKIN DENTED. COLD WORKED TO ORIGINAL CONTOUR. INSTALLED REPAIR DOUBLER. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0580553Skin · dentedC-CHECK, FUSELAGE SKIN DENTED. COLD-WORKED TO ORIGINAL CONTOUR. INSTALLED REPAIR DOUBLER. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0580552Web · crackedC-CHECK, CABIN FLOOR WEB CRACKED. REMOVED DAMAGED WEB SECTION. INSTALLED REPAIR DOUBLER. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0580551Track · corrodedC-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0580550Track · corrodedC-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0580549Track · corrodedC-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0580548Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0580547Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0580546Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0580545Floor Panel · corrodedC-CHECK, CABIN FLOOR PANEL HAS CORRODED INSERTS AND IS DELAMINATED AROUND INSERTS. REPLACED FLOOR PANEL. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0580544Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0580543Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0850542Floor Panel · corrodedC-CHECK, CABIN FLOOR PANEL HAS CORRODED INSERTS AND DELAMINATED AROUND INSERTS. REPLACED FLOOR PANEL. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0580541Web · corrodedC-CHECK, L-1 DOOR JAMB LOWER SILL WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. INSTALLED REPAIR DOUBLER. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0580540Web · corrodedC-CHECK, CABIN FLOOR WEB CORRODED. REPLACED WEB. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0580539Intercostal · crackedC-CHECK, INTERCOSTAL CRACKED AT RADIUS. REPLACED INTERCOSTAL. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0580538Frame · puncturedC-CHECK, FUSELAGE FRAME WEB PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0580537Fitting · corrodedC-CHECK, R-1 DOOR FLOOR MOUNTED GIRT BAR FITTING CORRODED. REPLACED CORRODED FITTING. (K)Dec 12, 2005 · N973AS · Doug DC983 · Emergency EquipmentSDR GTIA050286Bleed Valve · malfunctionedLT ENGINE N2 DROPS BELOW 45 PERCENT WHEN LOAD APPLIED. REPLACED A/C WITH 832NK ON LINE. REMOVED NR1 ENGINE FUEL CONTROL. OPS AND LEAK CHECK GOOD. REMOVED AND REPLACED START BLEED CONTROL VALVE, PERFORMED IDLE CHECK, ENGINE ACCELERATION CHECK. OPS CHECK GOODec 10, 2005 · N834NK · Doug DC983 · Fuel Controlling SystemSDR GTIA050285Unknown · unknownON RUNWAY CLEARED FOR TAKEOFF THE LT ENGINE WOULD NOT RESPOND TO THROTTLE ADVANCE THE LT ENGINE REMAINED AT IDLE POWER THEN SLOWLY WOUND DOWN TO 44 PERCENT N2, AIRCRAFT TAIL SWAP WITH 803NK. INSPECTED THROTTLE LINKAGE AT FUEL CONTROL. NO DEFECTS NOTED. INSPDec 10, 2005 · N832NK · Doug DC983 · Fuel Controlling SystemSDR AALA20050811Valve · inoperativeSTL - WHEEL NOT TURNING LIGHT ON AT APPROXIMATELY 130 KNOTS DURING TAKEOFF. EXTINGUISHED AFTER LIFT OFF. NOTED BURNED RUBBER SMELL IN COCKPIT AND CABIN THAT DISSIPATED QUICKLY. ALL BRAKE TEMPS BELOW 50 DEGREES. REPLACED LEFT HAND INBOARD AND OUTBOARD ANTI-Dec 10, 2005 · N9616G · Doug DC983 · Brake Anti-Skid SectionSDR AALA20050809Tire · failedSFO - NUMBER ONE MAIN TIRE BLOWN ON LANDING. ANTI SKID AND WHEEL NOT TURNING LIGHTS CAME ON. REPLACED NUMBER ONE AND NUMBER TWO WHEEL ASSEMBLY AND TIRES. REPLACED WHEEL SPEED TRANSDUCER. NO OTHER DAMAGE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.Dec 9, 2005 · N9616G · Doug DC983 · TireSDR ASMF200512008Bungee Cylinder · leakingDURING TRANSIT CHECK, TECHNICAL PERSONNEL DETECTED A HYDRAULIC LIQUID LEAK IN THE RT MAIN LANDING GEAR. BUNGEE CYLINDER WAS REPLACED IAW MM 32-32-02, TESTED CORRECT.Dec 8, 2005 · N583MD · Doug DC983 · Landing Gear Retraction/Extension SystemSDR AALA20050798Connector · inoperativeSFO - EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED CONNECTOR UNDER SEAT 3F FOR EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.Dec 8, 2005 · N434AA · Doug DC983 · Light System WiringSDR GTIA050284Ahrs · malfunctionedAHARS NR2 CIRCUIT BREAKER POPPED, PFD AND ND OUT. AIRCRAFT TAIL SWAP WITH 808NK. REMOVED AND REPLACED NR2 AHRU. OPS CHECK GOOD. (K)Dec 7, 2005 · N835NK · Doug DC983 · Directional Gyro and Indicating SystemSDR AALA20050806Strut · inoperativeORD - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF, HAD RED NOSE GEAR LIGHT ON WITH HANDLE UP. GEAR EXTENDED OK. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. FOUND NOSE STRUT NEEDED SERVICE. SERVICED NOSE STRUT. SYSTEM GROUND Dec 7, 2005 · N9622A · Doug DC983 · Main Landing Gear Strut/Axle/TruckSDR AALA20050805Pad · inoperativeORD - DURING APPROACH EXTENDED LANDING GEAR AND GEAR DOOR OPEN REMAINED ILLUMINATED. TOWER ADVISED GEAR DOORS MAIN WRE OPEN. WENT AROUND AND ACCOMPLISHED GEAR DOOR OPEN LIGHT QRH, NO HELP. REPLACED BOTH MAIN LANDING GEAR DOOR PADS. SYSTEM GROUND CHECKED NODec 5, 2005 · N9629H · Doug DC983 · Landing Gear DoorsSDR GTIA050283Landing Gear · vibrationAC SHIMMY VERY EXTREME ON LANDING ROLL OUT WHEN BRAKING BETWEEN 60-65 KTS, AC TAIL SWAP WITH 832NK. BLED ALL 4 BRAKES, CHECKED TORQUE VALUES OF ALL 4 MAIN TIRE AXLE NUTS. ALL CHECKED GOOD. NOTE: NR2 BRAKE AFT BLEEDER EMITTING AIR BUBBLES, PURGED AIR FROM SYNov 30, 2005 · N814NK · Doug DC983 · Nose/Tail Landing GearSDR AALA20050782Battery Pack · inoperativeLGA - EMERGENCY LIGHTS FROM FORWARD TO AFT INOPERATIVE. REPLACED BATTERY PACK IN AFT CARGO FOR EMERGENCY LIGHTS FROM FORWARD POSITION TO AFT. SYSTEM GROUND CHECKED NORMAL OPERATION.Nov 27, 2005 · N9677W · Doug DC983 · Emergency LightingSDR AALA20050834Actuator · corrodedTUL - LEFT HAND MAIN LANDING GEAR SUPPORT FITTING ASSEMBLY RETRACT ACTUATOR FITTING BORE HAS CORROSION IN LARGE BORE. AREA IS 1.75 INCHES BY 2.2515 INCHES. FINAL MEASUREMENT IS 2.253 INCHES IN 1.75 INCH BUSHING AREA. LOCAL BLEND WHERE BUSHING DOES NOT CONTANov 23, 2005 · N968TW · Doug DC983 · Landing Gear ActuatorSDR AALA20050831Bushing · corrodedTUL - MAIN LANDING GEAR SUPPORT BEAM RIGHT HAND RETRACT BUSHING INBOARD BUSHING OUTBOARD FACE HAS MINOR CORROSION. AREA IS 2.13 INCHES BY 2.13 INCHES WITH A DEPTH OF .025. ORIGINAL THICKNESS 1.235 INCHES. FINAL THICKNESS 1.210 INCHES. RIGHT HAND MAIN LANDINov 22, 2005 · N968TW · Doug DC983 · Fuselage, Landing Gear Attach FittingsSDR AALA20050832Actuator · corrodedTUL - RIGHT HAND MAIN LANDING GEAR SUPPORT FITTING ASSEMBLY RETRACT ACTUATOR FITTING BORE HAS CORROSION. AREA IS 1.75 INCHES BY 2.2515 INCHES. RIGHT HAND MAIN LANDING GEAR SUPPORT FITTING ASSEMBLY RETRACT ACTUATOR FITTING BORE REWORKED IN ACCORDANCE WITH ESONov 22, 2005 · N968TW · Doug DC983 · Landing Gear ActuatorSDR AALA20050833Bushing · corrodedTUL - LEFT HAND MAIN LANDING GEAR SUPPORT BEAM RETRACT BUSHING AREA INBOARD BUSHING OUTBOARD FACE HAS MINOR CORROSION. AREA IS 2.13 INCHES BY 2.13 INCHES. ORIGINAL THICKNESS .033 AND FINAL MEASUREMENT IS 1.202 REMAINING THICKNESS. LEFT HAND MAIN LANDING GEANov 22, 2005 · N968TW · Doug DC983 · Landing Gear Retraction/Extension SystemSDR ANCF200400062Engine · malfunctionedDURING TAKEOFF AND AFTER TAKEOFF THRUST WAS APPLIED, RT ENGINE ACCELERATION WAS VERY SLOW AND STOPPED AT 1.7 EPR. ACCELERATION TO 2 EPR WAS REACHED MOVING RT POWER LEVER MANUALLY. WHEN RT ENGINE REACHED 2 EPR N1 INDICATION STARTED FLASHING AND INDICATION WAS 1Nov 22, 2005 · N593AN · Doug DC983 · Engine (Turbine/Turboprop)SDR GTIA050282Doubler · corrodedFWD SERVICE DOOR HAS CORROSION ON FLOOR WEB BETWEEN STA 1460 TO 218. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DOUBLER AND FABRICATED NEW ONE, TREATED PRIMED AND INSTALLED REPAIR DOUBLER. (K)Nov 21, 2005 · N802NK · Doug DC983 · Fuselage Miscellaneous StructureSDR GTIA050275Seat Track · corrodedRT OB SEAT TRACK FS 493 BOTTOM OF TRACK OUT OF LIMITS, CORROSION. REMOVED CORRODED SEAT TRACK SECTION, DRILLED NEW SEAT TRACK, FABRICATED SPLICE AND PLATE, TREATED, PRIMED AND INSTALLED REPAIR. (K)Nov 21, 2005 · N802NK · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA050281Diaphragm · corrodedFWD GALLEY AFT CORNER IB HAS A 6 INCH HOLE CORRODED THROUGH SUBFLOOR WEB. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED DIAPHRAGM AND FABRICATED NEW DIAPHRAGM, TREATED PRIMED AND INSTALLED. (K)Nov 19, 2005 · N802NK · Doug DC983 · Fuselage Miscellaneous StructureSDR GTIA050280Floor Support · corrodedFLOOR SUPPORT LBL 5, STA 195-200 HAS CORROSION ALONG LENGTH. REMOVED CORROSION AND FOUND ADDITIONAL CORROSION ON UNDERSIDE OF FLOOR SUPPORT TO BE OUT OF LIMITS, FABRICATED NEW SUPPORT, TREATED PRIMED AND INSTALLED NEW SUPPORT. (K)Nov 19, 2005 · N802NK · Doug DC983 · Fuselage Miscellaneous StructureSDR GTIA050279Floor Support · corrodedFORE AND AFT FLOOR SUPPORTS AT STA 170-195 ON OB LT SEAT TRACK HAS SPOTS OF CORROSION ALONG LENGTH. REMOVED CORROSION ON SUPPORTS FOUND TO BE OUT OF LIMITS, FABRICATED NEW FLOOR SUPPORT ANGLE, TREATED PRIMED AND INSTALLED SUPPORT. (K)Nov 19, 2005 · N802NK · Doug DC983 · Fuselage Miscellaneous StructureSDR GTIA050278Floor Support · corrodedFLOOR SUPPORT AT STA 198 BETWEEN LT SEAT TRACKS IS CORRODED. REMOVED FLOOR SUPPORT, FABRICATED NEW SUPPORT TREATED AND PRIMED, INSTALLED REPAIR. (K)Nov 19, 2005 · N802NK · Doug DC983 · Fuselage Miscellaneous StructureSDR GTIA050273Seat Track · corrodedSTA 1136, SEAT TRACK HAS CORROSION. FABRICATED, TREATED AND INSTALLED SECTION OF SEAT TRACK AT STA 1136. (K)Nov 19, 2005 · N802NK · Doug DC983 · Fuselage Main, Floor BeamSDR AALA20050765Connector · brokenSFO - EMERGENCY LIGHT EXIT SIGN AT FORWARD GALLEY DOOR INOPERATIVE. FOUND WIRE BROKEN AT SIGN CONNECTOR. REPINNED CONNECTOR FOR EMERGENCY LIGHT EXIT SIGN AT FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.Nov 19, 2005 · N589AA · Doug DC983 · Emergency LightingSDR AALA20050761Engine · failedINFLIGHT, SHORTLY AFTER LEVEL OFF AT FL320, RIGHT ENGINE FAILED. RIGHT HAND ENGINE OIL QUANTITY AND PRESSURE WERE NORMAL. EXHAUST GAS TEMPERATURE REACHED 800 DEGREES BEFORE SHUTDOWN. NO FIRE INDICATION OCCURRED. LANDED ORD WITHOUT INCIDENT. REPLACED NUMBENov 18, 2005 · N963TW · Doug DC983 · Engine (Turbine/Turboprop)SDR GTIA050277Angle · crackedANGLE IS CRCKED IN LT MLG WHEEL WELL FWD DOOR JAMB STRUCTURE STA 946. REMOVED CRACKED ANGLE, FORMED NEW ANGLE, TREATED PRIMED AND INSTALLED REPAIR. (K)Nov 16, 2005 · N802NK · Doug DC983 · Main Landing Gear Strut/Axle/Truck
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