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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR WX0500003Outflow Valve · obstructedDURING FLT AT APPROX 25,000 FT, HAD IND`S OF INCREASED RATE OF CLIMB THAT EXCEEDED 1000 FPM. ATTEMPTED TO ADJUST RATE OF CLIMB WITH CONTROL KNOB. REPEATED ATTEMPTS DID NOT SLOW RATE, AFTER LEVEL OFF AT 35,000 FT CABIN PRESS CONTROLLER CONTINUED TO INDICATE CSDR WX0500004Pseu · failedCUN - CREW REPORTED SLATS ANNUNCIATOR WARNING DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE. MAINTENANCE PERFORMED AUTO TEST ON PSEU, TEST SHOWED INTERNAL FAULTS 580, 620 AND 840. DISAGREE LIGHT STAYED ILLUMINATED AFTER RERACK OF PSEU AND RESET OF BREAKER SDR CA050103002Start Valve · malfunctioned(CAN) NR 1 ENGINE, THE LT START VALVEOPEN LIGHT CAME ON IN CLIMB. THE AIRCRAFT LEVELED OFF, WHEN THE POWER REDUCED, THE LIGHT WENT OUT. WHEN CLIMB POWER INITIATED AGAIN, THE LIGHT CAME BACK ON. THE AIRCRAFT CAME BACK TO PLACE OF DEPARTURE. THE AIRCRAFT WAS RELSDR WX0500001Proximity Switch · dirtyLAS - ON FINAL APPROACH WITH GEAR AND FLAPS DOWN, HAD GEAR UNSAFE LIGHT AND HORN LEFT MAIN. WENT AROUND AND CYCLED GEAR WITH NO FURTHER INDICATIONS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND MASKING TAPE AND DEBRIS ON LEFT MAIN GEAR DOWN LOCK PROXSDR AALA20050001Battery Pack · dischargedRDU - OVERHEAD EMERGENCY LIGHTS AT ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20050003Cylinder · brokenPHX - EN ROUTE PHX TO ORD LEFT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED PHX AND LANDED WITHOUT INCIDENT. FOUND LEFT GEAR BUNGEE CYLINDER ROD END BROKEN. REMOVED AND REPLACED LEFT GEAR CYLINDER. ACCOMPLISHED GEAR SWING AND LUBE. SYSTEM GROUND CHSDR AALA20050002Battery · dischargedAUS - CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 31 INOPERATIVE. REPLACED BATTERIES FOR CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR WX0400069Windshield · crackedLAS - AIR TURN BACK DUE TO CAPTAIN’S WINDSHIELD CRACKED ON CLIMB-OUT PASSING 9000 FEET. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAIN’S WINDSHIELD AND INSTALLED ANTI-ICE/ANTI-FOG TERMINAL BLOCKS IAW AMM 56-10-02. AIRCRAFT RETURNSDR ASAA0480628Lanyard · disconnectedSEA - PREFLIGHT CHECK, AFT SERVICE L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)SDR CA050104004Line · contaminated(CAN) AIRCRAFT REJECTED TAKE OFF AT LESS THEN 40 KNOTS, DUE TO NR 2 ENGINE EPR DID NOT RESPOND TO THROTTLE MOVEMENT. MAINTENANCE FOUND WATER IN EPR LINE. MAINTENANCE BLEW AIR AND CLEANEDTHE EPR LINES PT7, PT2 IAW AMM 77-1 1-03, 77-11-04. ENGINE RUN CARRIED OUSDR CA050104003Indicator · inoperative(CAN) AIRCRAFT REJECTED TAKE OFF AT 65 KNOTS, DUE TO NR 2 ENGINE EPR GAUGE BEING INOPERATIVE. MAINTENANCE REMOVED EPR LINES AND FOUND WATER INU PIPE OF PT7. THE WATER WAS BLOWN OUT AND DRIED. ENGINE RUN CARRIED OUT, SYSTEM FOUND SERVICEABLE.SDR ASAA0480627Power Supply · dischargedDURING LINE CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M)SDR ASAA0580394Light · looseSEA - PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTING DID NOT ILLUMINATE DURING SYSTEM TEST. RESECURED LOOSE CONNECTOR AT L2-550. LIGHTS THEN OPERATED PROPERLY. (M)SDR ASAA0480626Skin · dentedOKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. RECONTOURED DOOR SKIN AND INSTALLED DOUBLER. (M)SDR ASAA0480625Door Frame · crackedOKC - HV-CHECK, FORWARD ENTRY DOOR JAMB WEB CRACKED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER. (M)SDR ASAA0480624Skin · dentedOKC - HV-CHECK, FUSELAGE DENTED BETWEEN LONGERON 16R AND 17R. RECONTOURED DENT AND INSTALLED DOUBLER. (M)SDR ASAA0480623Skin · gougedOKC - HV-CHECK, FUSELAGE GOUGED ON LEFT SIDE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER. (M)SDR GTIA040874Control Box · faultyDTW - BRAKES FAILED ON TAXI OUT TO RUNWAY 25R, ANTI-SKID TEST SHOWED 3 ANTI-SKID FAIL. FOUND ANTI-SKID CONTROL BOX AT FAULT, REPLACED ANTI-SKID CONTROL UNIT. OPS CHECK NORMAL. (M)SDR ASAA0480622Lanyard · disconnectedSEA - PREFLIGHT CHECK, FORWARD PASSENGER L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)SDR AALA20041249Battery Pack · dischargedDFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 9, 10 AND 11 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 9, 10 AND 11. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20041256Landing Gear · malfunctionedORD - EN ROUTE PSP AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT COMPLETELY. RED NOSE GEAR LIGHT REMAINED ON AND GREEN NOSE GEAR WENT OUT. RETURNED ORD AND LANDED WITHOUT INCIDENT. JACKED AIRCRAFT PER MM 7-12-00-2, PERFORMED INSPECTION OF NOSE GEAR. NO FAULTS SDR WX0400068Steering Sys · malfunctionedFNL TO LAS - CREW CONTACTED MAINTENANCE CONTROL TO REPORT AIRCRAFT NOSE WHEELS DROVE OFF TAXIWAY INTO DIRT AT FNL. MAINTENANCE POSITIONED AIRCRAFT BACK ONTO TAXIWAY AND INSPECTED NOSE LANDING GEAR IAW 05-51-03 A-CHECK. NO DAMAGE NOTED, OKAY FOR CONTINUED SERSDR AALA20041240Warning Light · illuminatedORD - INFLIGHT T1335/22 NOSE GEAR RED LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. ACCOMPLISHED FULL SERVICE ON NOSE LANDING GEAR STRUT AND GEAR SWING. SYSTEM GSDR CA041223001Compressor · damaged(CAN) A LOUD BANG HEARD ON ROTATION FROM NR 2 ENGINE. POWER WAS REDUCED TO IDLE AND AIRCRAFT LANDED BACK. ENGINE FAN BLADES FOUND DAMAGED. ENGINE REPLACED. THE CAUSE HAS NOT BEEN IDENTIFIED. AWAITING FOR SHOP REPORT.SDR GTIA040869Pump · inoperativeFLT 478 - DURING TEST ON RIGHT AFT BOOST PUMP B-TEST IS INOPERATIVE, AIRCRAFT SWAP. REMOVED AND REPLACED AFT FUEL TANK B-BOOST PUMP. OPS CHECK GOOD. (M)SDR GTIA040868Packing · leakingDTW - FLT 503 - DURING PREFLIGHT, FOUND HYDRAULIC FLUID ON RT MLG, AIRCRAFT SWAP. RE-PACKED RT MAIN GEAR STRUT, LEAK CHECK GOOD. (M)SDR WX0400066Controller · malfunctionedMSN TO LAS - DURING CLIMBOUT AT 9000 FT CREW REPORTED FLOW LIGHT ILLUMINATED. CABIN CLIMBED 500 FT PER MINUTE WHILE LEVEL. COULD NOT MAINTAIN CABIN IN AUTO. CREW COMPLETED FLOW LIGHT ILLUMINATED CHECKLIST. AIRCRAFT RETURNED TO MSN AND LANDED WITHOUT INCIDESDR WX0400067Regulator Valve · malfunctionedLAS TO OKC - DURING CLIMBOUT CREW REPORTED, UNABLE TO CONTROL TEMP IN AUTO OR MANUAL BOTH PACKS. OVERHEAT TRIPPED OFF RIGHT PACK. BOTH VALVES SHOW FULL COLD, CABIN SUPPLY TEMP 60 DEGREES CELSIUS. HP BLEED OFF, NO CHANGE. AIRCRAFT RETURNED TO LAS AND LANDESDR WX0400064Bulb · inoperativeLAS - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS AT ROW 8 AND ROWS 23 THROUGH 32 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULBS IAW 33-51-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR ASAA0480615Longeron · corrodedOKC - HV-CHECK, LONGERON 29L IS CORRODED. APPLIED SEALANT PER EA 5310-02430. (M)SDR ASAA0480614Longeron · corrodedOKC - HV-CHECK, FOUND LONGERON 30 IS CORRODED. REMOVED DAMAGED SECTION. INSTALLED U-CHANNEL AND FILLER. (M)SDR ASAA0480612Access Panel · chafedOKC - HV-CHECK, LEFT WING FUEL PANEL 1303 CHAFED AND PITTED. REPLACED PANEL. (M)SDR ASAA0480616Door Frame · gougedOKC - HV-CHECK, TWO MOUNTING HOLES GOUGED AT BOTTOM FRAME OF LEFT OVERWING EXIT. INSTALLED DOUBLER PER EA 53-20-01679. (M)SDR ASAA0480607Vane · wornOKC - HV-CHECK, RIGHT WING FLAP OUTBOARD VANE INBOARD T/E IS WORN. REMOVED WORN AREA. INSTALLED FILLER AND REPAIR DOUBLER. (M)SDR ASAA0480605Joint · damagedOKC - DURING HV-CHECK, LT WING FLAP FLEX JOINT UPPER BAR 6TH HOLE FROM T/E DAMAGED. REPAIRED WITH WASHER PER EA 5750-02019. (M)SDR ASAA0480621Skin · crackedOKC - HV-CHECK, AFT CARGO DOOR FORWARD AND AFT LATCH CUTOUTS ARE BENT AND CRACKED. RECONTOURED ARE STOP DRILLED CRACKS. INSTALLED REPAIR ANGLES. (M)SDR ASAA0480613Longeron · corrodedOKC - HV-CHECK, LONGERON 29R SPLICE IS CORRODED IN AFT CARGO COMPARTMENT AREA. REPLACED DAMAGED CORRODED SECTION OF LONGERON. (M)SDR ASAA0480620Skin · dentedOKC - HV-CHECK, FUSELAGE UNDERSIDE DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER EA 5330-01875. (M)SDR ASAA0480611Spacer · corrodedOKC - HV-CHECK, AFT CARGO BAY DOOR JAMB BEAM SPACER IS CORRODED. REPLACED SPACER. (M)SDR ASAA0480618Skin · dentedHV-CHECK, FUSELAGE SKIN DENTED AT R1 DOOR CUTOUT. REPAIRED DENT PER EA 5330-01864. (M)SDR ASAA0480610Access Panel · gougedOKC - HV-CHECK, RIGHT WING STRUCTURE UNDER FUEL PANEL 1436 RUB STRIP IS GOUGED. REPLACED DAMAGED SECTION PR EA 5720-01258. (M)SDR ASAA0480619Skin · dentedHV CHECK, FORWARD CARGO BAY DOOR DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER. (M)SDR ASAA0480609Skin · gougedOKC - HV-CHECK, RIGHT WING INNER LOWER SKIN GOUGED JUST FORWARD OF DRAIN HOLE. REPLACED DAMAGED SECTION PER EA 5720-01259 AND -10702. (M)SDR ASAA0480606Vane · chafedOKC - HV-CHECK, RIGHT WING OUTBOARD FLAP INBOARD VANE PREVIOUS L/E REPAIR IS CHAFED. REPLACED DAMAGED REPAIR DOUBLER. (M)SDR ASAA0480617Frame · gougedOKC - HV-CHECK, MOUNTING HOLES GOUGED AT BOTTOM FRAME OF RIGHT OVERWING EXIT. INSTALLED DOUBLER PER EA 5320-01680. (M)SDR ASAA0480608Bracket · corrodedOKC - HV-CHECK, LEFT WING INBOARD FLAP TRACK MOUNTING BRACKET BOLT HOLES ARE PITTED. REAMED HOLES AND INSERTED BUSHINGS PER EA 5750-01160. (M)SDR CA041217005Transmitter · malfunctioned(CAN) DURING CRUISE, LT ENGINE EPR DROPPED TO 1.35 FOLLOWED BY AUTO THROTTLE DISCONNECT AND AIRCRAFT DECELERATION. EPR LINE INSPECTED, NO FAULTS FOUND. ENGINE RUN-UP CARRIED OUT AS PER AMM AND ENGINE PARAMETERS FOUND WITHIN LIMIT. THE PRESSURE TRANSMITTER WSDR 2005F00007Lanyard · misroutedDTW - FOUND R1 DOOR SLIDE PULL HANDLE, INSPECT PULL HANDLE ROUTING. INSPECTED AND CORRECTED PULL LANYARD ON R1 DOOR SLIDE. NO OTHER DEFECTS NOTED. (M)SDR ASAA0480600Floor Panel · crackedOKC - HV-CHECK, CABIN FLOOR PANEL, FLOORBOARD, CRACKED. REPAIRED DAMAGED AREA WITH FIBERGLASS. (M)SDR ASAA0480599Floor Panel · delaminatedOKC - HV-CHECK, CABIN FLOOR PANEL, FLOORBOARD DELAMINATED. REPLACED PANEL. (M)
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