Mcdonnell Douglas MD 83
Service difficulty reports · 3,415
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 = 'MD83' 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 = 'MD83' 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 ASMF200508004Cooling Turbine · inoperativeDURING TRANSIT SERVICE, LT AIR CONDITIONING SYSTEM WAS DETECTED INOPERATIVE. REPORT WAS DEFERRED IAW MEL 21-1. DURING OVERNIGHT SERVICE, COOLING TURBINE WAS REPLACED IAW MM 21-51-01, TESTED CORRECT. DEFERRED REPORT WAS CLOSED.SDR ASMF200508003Control Box · inoperativeAIRCRAFT REJECTED TAKEOFF (WHEEL NOT TURNING) LIGHT TURNED ON. ANTISKID CONTROL BOX WAS REPLACED IAW MM 32-43-00, TESTED CORRECT.SDR ASMF200508001Socket · damagedDURING TRANSIT SERVICE, PERFORMED ANTISKID TEST, THE CIRCUIT BREAKER R-41 WAS ACTIVATED AND WOULD NOT RESEAT IT. ANTISKID VALVES CONNECTORS WERE DISCONNECTED AND TRANSDUCERS WERE CHECKED OF 4 MAIN WHEELS AND FAIL CONTINUE. ANTISKID CONTROL BOX WAS REPLACED ISDR ASMF200507024Gyro · failedAIRCRAFT PERFORMED A TECHNICAL LANDING AT CUL DUE TO WHEATEAR CONDITIONS AT HMO. AT CUL CAPTAIN REPORTED THAT DURING TURNS THE RADAR GOES OUT OF SERVICE, SO VERTICAL GYRO NR 2 WAS REPLACED IAW MM 34-23-00, TESTED CORRECT. AIRCRAFT WAS DISPATCHED AND CAPTAIN RESDR GTIA050217Engine · overheatedSJU - LEFT ENGINE OIL GREATER THAN 170 ON CLIMB-OUT. SHUT ENGINE DOWN PER QRH AND RETURNED TO SJU. REMOVED AND REPLACED NR 1 ENGINE IAW MM 71-00-00 AND W/C 00191. (M)SDR ASMF200507015Thermostat · failedTHE AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HERMOSILLO (HMO) DUE TO LEFT ICE PROTECT TEMP HIGHT LIGHT TURNED ON AND USTB LEGEND IN RADAR COME ON SEVERAL TIMES. THE LEFT PNEUMATIC SYSTEM THERMOSTAT AND ANTICIPATOR WERE REPLACED IAW MM 36-10-06 AND TRANSCEISDR ANCF200400053Engine · leakingRIGHT ENGINE OIL QUANTITY DECREASED SLOWLY FROM 13 QTS TO 2 QTS IN FLT ( OIL PRESS AND TEMPERATURE WERE NORMAL), ENGINE SHUTDOWN 4 MIN BEFORE LANDING AS OIL REACHED 2 QTS & OIL TEMP STARTED TO INCREASED. ENGINE INITIALLY OPERATED IN IDLE THRUST FOR ABOUT 15 MSDR 471082Turbine · failedRECEIVED SUBJECT APU WITH A BURST IMPELLER. THE OEM HAS BEEN NOTIFIED AND IS CURRENTLY UNDER INVESTIGATION FROM HONEYWELL OEM. ONCE THE INVESTIGATION IS COMPLETE AN OFFICAL REPORT WILL BE SUBMITTED TO THE CUSTOMER FROM REPAIR & OVERHAUL AND OEM ENGINEERING.SDR ASMF200507010Motor · failedDURING TRANSIT SERVICE, IN GROUND TEST THE HORIZONTAL STABILIZER MOTOR DID NOT MOVE. THE ACTUATOR AND PRIMARY MOTOR WERE REPLACED IAW MM 27-40-01, BUT FAILURE CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND ANOTHER ACTUATOR AND PRIMARY MOTOR WAS INSTALLED, THE SDR ANCF200400052Cabin Pressure · malfunctionedUNABLE TO MAINTAIN CABIN PRESSURE AT FL 330 WITH 0.78 MACH. REQUESTED FL 290 WITH SAME SET OF PWR. FLOW LIGHT REMAINED ON AND CABIN ALT CONTINUED INCREASING. NECESSARY TO SELECT ENGINE AND AIRFOIL ANTI-ICE DUE WEATHER CONDITIONS. CABIN RATE INCREASED AND NECSDR ASMF200507003Skin · dentedDURING TRANSIT CHECK CAPT REPORTED 2 HITS ON FUSELAGE. ONE BELOW 45 RT LIGHT AND OTHER IN AFT RT RVSM AREA. INSPECTION PERSONNEL SENT TO PLATFORM AND CHECK DAMAGE. DENT AT STATION 571 WITHIN LIMITS IAW SRM 53-04 CONDITION B AND DENT IN RVSM AREA WITHIN LIMITSSDR ASMF200507002Pseu · failedAIRCRAFT RETURNED TO PLATFORM DUE TO RUDDER TRAVEL UNRESTRICTED, FLAP SLAT DISAGREE AND BOTH MAIN LANDING GEAR RED LIGHTS TURNED ON. BITE TO SWC AND PSEU PERFORMED, NOT CONFIRMING FAILURE. TECHNICAL PERSONNEL SENT TO STATION AND PSEU REPLACED IAW MM 32-60-04,SDR ASMF200507001Motor · failedCAPTAIN REPORTED PRIMARY STAB TRIM STICKS OCCASIONALLY. COMPENSATION MECHANISM OF HORIZONTAL STABILIZER CHECKED IAW MM 27-40-0, BEING CORRECT. DURING TESTS, PRIMARY MOTOR OF STABILIZER FAILED. REPLACED IAW MM 27-40-01. TESTED CORRECT.SDR ASMF200506029Handset · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF FLIGHT INTERPHONE FROM CABIN TO FLIGHT DECK OF 3RD STATION INOPERATIVE. INTERPHONE WAS DISCONNECTED AND DEFERRED IAW MEL 23-8. DURING OVERNIGHT SERVICE, HANDSET NR 4 WAS REPLACED IAW MM 23-50-00, TESTED CORRESDR ASMF200506027Gyro · failedDURING LEFT ENGINE STARTING, CAPTAIN REPORTED DFGC NR 1 OUT OF SERVICE AND FLIGHT DIRECTOR SHOWED FD AND SPD MESSAGES. ENGINES WERE SHUTDOWN. DFGCS WERE INTERCHANGED AND BREAKERS WERE RESET, DISAPPEARING TRI FLIGHT DIRECTOR FLAGS. TESTS WERE PERFORMED IAW MSDR ASMF200506015Actuator · failedCAPTAIN REPORTED THAT DURING FLIGHT LIGHT AUTO SLAT FAIL CAME ON. DURING CHECK, APPLICABLE CIRCUIT BREAKERS WERE RESET AND FLAPS/SLATS WERE OPERATIONALLY TESTED TURNING ON THE OVERHEAD LIGHT IN THE SLATS PANEL LIGHTS. BITE TO BOTH STALL COMPUTERS WERE PERFORSDR ASAA0580344Skin · dentedOKC - DURING HV CHECK, AFT CARGO BAY DOOR SKIN DENTED. RECONTOURED SKIN AND INSTALLED REPAIR DOUBLER. (M)SDR ASAA0580343Skin · dentedOKC - DURING HV-CHECK, FUSELAGE SKIN DENTED. INSTALLED REPAIR DOUBLER. (M)SDR ASAA0580342Track · corrodedOKC - DURING HV CHECK, FOUND CABIN FLOOR FALSE TRACK CORRODED. REPLACED FLASE TRACK. (M)SDR ASAA0580341Track · corrodedOKC - DURING HV CHECK, CABIN FLOOR FALSE TRACK CORRODED. REPLACED FALSE TRACK. (M)SDR ASAA0580340Seat Track · corrodedOKC - DURING HV-CHECK, FOUND SEAT TRACK CORRODED. REPLACED DAMAGED SEAT TRACK SECTION. (M)SDR ASAA0580339Seat Track · gougedOKC - HV-CHECK, FOUND SEAT TRACK GOUGED. REPLACED DAMAGED SEAT TRACK SECTION. (M)SDR WX0500048Wire · inoperativeMAINTENANCE REPORTED EMERGENCY FLOOR ESCAPE LIGHTING ROW 5-8 AC/ RT INOPERATIVE. MAINTENANCE INSTALLED NEW LEAD ASSEMBLY WIRE AT FOR ROWS 5-8 AC RT. SYSTEM OPERATIONALLY CHECKS NORMAL IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE.SDR ASMF200506002Anti-Ice Valve · failedAIRCRAFT RETURNED TO PLATFORM, LT STARTER VALVE DID NOT OPEN AND ANTI-ICE BREAKER OF NOSE COWLING POPPED OUT. THE REPORT WAS DEFERRED BY MEL 80-2 AND THE ANTI ICE VALVE WAS REPLACED IAW MM 30-20-01, TESTED CORRECT. DEFERRED REPORT WAS CLOSED.SDR GTIA050184Cusp Web · corrodedAFT PIT SUBFLOOR AT LEFT CUSP CORRODED FROM STATION 1022-1041. REMOVED PANELS FOR ACCESS. REMOVED CORROSION FOUND IS OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED WEB AND DOUBLER. TREATED AND PRIMED, INSTALLED REPAIR TWO FITTINGS. RE-INSTALLED REMOVED ASDR GTIA050181Web · crackedFOUND CRACK AT WEB JUST AFT OF L1 DOOR AT LONGERON 15. CUT OUT DAMAGED SECTION OF WEB. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED REPAIRED DOUBLER AND FILLER. FABRIATED PARTS INSTALLED AT LONGERON 152 AFT L1 DOOR. (M)SDR GTIA050158Seal · leakingTAIL COMPARTMENT TEMP HIGH LIGHT CAME ON AFTER TAKEOFF, AIR RETURN BACK TO FLL AND AIRCRAFT TAIL SWAP WITH N815NK. REMOVED AND REPLACED SEALS ON LEFT AND RIGHT ACM DUCTS, SECURED TWO LOOSE CLAMPS, RAN ENGINES AT ALL PARAMETERS. OPS AND LEAK CHECKS GOOD. (M)SDR GTIA050180Floor Support · corrodedFOUND CORROSION ON FLOOR STATION 200 BL 0. REMOVED CORROSION FLOOR SUPPORT STATION 200 BL 0 MATERIAL LOSS OUT OF LIMITS. FABRICATED FLOOR SUPPORT. LOCATED AND DRILLED HOLES. TREATED AND PRIMED AND INSTALLED FLOOR SUPPORT. (M)SDR GTIA050182Cusp Web · corrodedFOUND CARGO COMPARTMENT FS 484-515 L18R CUSP WEB HAS CORROSION. REMOVED RT OUTBOARD FLOOR PANEL. CUT WEB OUT OF LIMIT 2 LOCATIONS 6 INCHES BY 8 INCHS BAND 16 INCHES BY 6 INCHES. FABRICATED REPAIR DOUBLERS AND FILLERS. TREATED AND PRIMED. INSTALLED DOUBLERSDR GTIA050183Cusp Web · corrodedFOUND FORWARD CARGO COMPARTMENT CORROSION ON CUSP WEB FS 450-475 L18L. REMOVED FLOORBOARDS AND PANELS FOR ACCESS. REMOVED CORROSION. FOUND CUSP-WEB IS OUT OF LIMITS. FABRICATED CUSP WEB 17 INCHES BY 5.5 INCHES. TREAT AND PRIMED CUSP WEB AND INSTALLED FABRSDR ASMF200505024Shutoff Valve · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE, DURING LEFT ENGINE STARTED, THE START VALVE OPEN LIGHT DID NOT TURN OFF. THE CIRCUIT BREAKERS WERE RESEATED, CROSS FEED AND CONNECTORS WERE CHECKED AND FAILURE CONTINUED. THE REPORT WAS DEFERRED IAW MEL 80-1. SDR GTIA050179Cusp Web · corrodedFOUND CORROSION -C- AT CUSP WEB LINE. REMOVED CORROSION FROM WEB/MEMBRANE. TREATED AND PRIMED CUSP WEB. CUT OUT DAMAGED AREA. FABRICATED REPAIR, DOUBLER AND FILLER. TREATED AND PRIMED REPAIR PARTS. INSTALLED REPAIR. (M)SDR ASMF200505019Generator · out of alignmentAIRCRAFT RETURNED TO PLATFORM, LT ENGINE DID NOT ACCELERATE, N2 DECREASED BELOW 50 PERCENT AND LT GENERATOR WAS FOUND OUT OF LINE. ACCELERATION CHAMBER WAS DRAINED AND LUBRICATED, LT ENGINE WAS TESTED IAW MM 73-20-03, ALL CORRECT.SDR GTIA050170Floor Support · corrodedFOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FOUND FLOOR SUPPORT TO BE OUT OF LIMITS USING CALIPERS. MATERIAL ID CHECK FOR FLOOR SUPPORT. LOCATED AND DRILL NEW FLOOR SUPPORT. TREATED AND PRIMED. TOP COAT FLOOR SUPPORT. INSTALLSDR GTIA050171Floor Support · corrodedFOUND FORWARD ENTRY AREA FLOOR SUPPORT IS CORRODED. REMOVED FLOOR SUPPORT. FOUND FLOOR SUPPORT TO BE OUT OF LIMITS USING CALIPERS. LOCATED AND DRILLED NEW FLOOR SUPPORT. TREATED AND PRIMED. TOPCOAT FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)SDR GTIA05152005Seat Track · corrodedFOUND CABIN SEAT TRACK CORRODED. REMOVED FLOOR PANELS. REMOVED DAMAGED SEAT TRACK AND FORWARD AND AFT GIRT MOUNTS. FABRICATED FORWARD AND AFT GIRT MOUNTS. LOCATED AND DRILLED NEW HOLES ON FABRICATED FORWARD AND AFT GIRT MOUNTS. LOCATED AND DRILLED NEW SEASDR ASMF200505018Engine · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT GENERATOR FREQUENCY WITH OSCILLATION. MEL 24-1 PROCEDURE WAS APPLIED. AGAIN AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT ENGINE WAS NOT ACCELERATED. ACCELERATION CHAMBER WERE DRAINED AND LUBRISDR ANCF200400050Tank · leakingDURING FLIGHT A FUEL LEAK WAS DETECTED ON LEFT MAIN FUEL TANK. ALL FUEL FLOW NORMAL AND ENGINE CONSUMPTION WAS NORMAL. PER AMM 72-00-04 P 197 ACCOM T/S FOUND FUEL PUMP DUCT CORK. ADJ IAW 73-34-01PG 201. RUN UP TEST NORMALLY IAW 72-44-0 PAG 532 , NO LEAKS FSDR ASMF200505016Interphone · malfunctionedDURING TRANSIT CHECK INTERCOMMUNICATION SYSTEM WAS DETECTED OUT SERVICE. MAINTENANCE TEST WAS PERFORMED IAW MM 23-40-00, ALL CORRECT. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF INTERCOMMUNICATION SYSTEM FAIL. MAINTENANCE PROCEDURE TEST WAS PERFORMED SDR ASMF200505015O-Ring · leakingAIRCRAFT RETURNED TO PLATFORM, LOW ACCELERATION (1.4 OF EPR) AND HIGH TEMPERATURE (600°C). DURING CHECK, THE RT ENGINE ACCELERATION CHAMBER WAS SERVICED, TESTS WERE PERFORMED TO BOTH ENGINES IAW MM 71-00-00, BEING CORRECT. DUE TO ART WAS INOPERATIVE, IT WAS DESDR GTIA050167Cusp Web · corrodedFOUND CABIN STRINGER 18L CUSP CORRODED. REMOVED RETURN-AIR GRILL ASSEMBLY. REMOVED CABIN FLOORBOARDS. REMOVED FRAME TO FLOOR FITTINGS. REMOVED CUSP MEMBRANE. FABRICATED, LOCATED AND DRILLED REPLACEMENT WEB. TREATED, PRIMED AND TOPCOATED WEB. INSTALLED CSDR GTIA050172Skin · dentedFOUND DENT AFT AIRSTAIR DOOR. REMOVED PAINT. CUT OUT DAMAGED AREA. FABRICATED ONE EACH FAIRING AND ONE REPAIR DOUBLER. PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS. TREATED AND PRIMED BARE METAL AREAS. PAINTED AFT AIR STAIR DOOR. (M)SDR GTIA050168Cusp Web · corrodedFOUND CABIN STRINGER 18R CUSP CORRODED. INSTALLED NEW SECTION OF CUSP. AND REPAIR ANGLES. INSTALLED WEB. INSTALLED REPAIR ANGLES. INSTALLED TWO AIR GRILLS. INSTALLED RIGHT OUTBOARD FLOORBOARDS. INSTALLED FRAME FITTINGS. INSTALLED WEB STATION. (M)SDR GTIA050185Cusp Web · corrodedFOUND CABIN STRINGER 18R CUSP CORRODED FS 1098-1117. REMOVED CORROSION AT CUSP WEB STATION 1098-1117. FOUND OUT OF LIMITS. REMOVED FLOOR BOARDS AND PANELS FOR ACCESS. REMOVED CUSP WEB STRINGER 18 RT STATION 1059 TO STATION 1174. FABRICATED CUSP WEB. TREASDR GTIA050166Stringer · corrodedFOUND CABIN STRINGER 18R CUSP CORRODED. REMOVED CORROSION AT STRINGER 18R CUSP MEMBRANE. CUT OUT DAMAGED SECTION OF CUSP. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED DOUBLER. INSTALLED REPAIR DOUBLER AT STRINER 18R MEMBRANE. APPLIED TOP COAT. (M)SDR GTIA050169Stiffener · crackedFOUND LEFT HORIZONTAL STABILIZER REAR SPAR STIFFENER CRACKED ON UPPER EDGE. REMOVED DAMAGED STAB REAR SPAR STIFFENER. FABRICATE STIFFENER SEAL. LOCATED AND DRILLED FABRICATED STIFFENER. TREATED AND PRIMED FABRICATED STIFFENER. TOP COATED FABRICATED STIFFESDR ASMF200505008Engine · failedDURING OVERNIGHT SERVICE AND IN ORDER TO ATTEND EPR NR 2 WITH DIFFERENCE OF 0.20 DURING CRUISE REPORT, THE RIGHT ENGINE WAS CHECKED BY LEAKS ON PT2 AND PT7 LINES AND EPRS TRANSMITTER AND FCU WERE REPLACED, BEING NOT POSSIBLE TO ADJUST THE ENGINE. IT WAS DETERSDR GTIA050173Skin · dentedFOUND DENT AT FS 278 BETWEEN LONGERONS 17L AND 18L. CHEMICALLY REMOVED PAINT. CUT OUT DAMAGED AREA. FABRICATED TWO STRAPS, 2 FINGER DOUBLER, TWO DOUBLERS, AND 1 FILLER. TREATED AND PRIMED REPAIR PARTS. INSTALLED REPAIR. PAINT DONE. (M)SDR GTIA050174Skin · dentedFOUND DENT AT STATION 1224 BETWEEN LONGERONS 25R AND 26R. REMOVED PAINT AND PRIMER. DENT FOUND TO BE OUT OF LIMITS. COLD WORKED DENT. TREATED AND PRIMED. INSTALLED DOUBLER. PAINT DONE. (M)SDR GTIA050176Skin · dentedFOUND DENT AT STATION 228.5 BETWEEN LONGERON 17R AND 18R. STRIPPED AREA. CUTOUT DAMAGED SECTION. FABRICATED -5 DOUBLER. FABRICATED -0 FINGER DOUBLER. FABRICATED -15 NEW SECTION OF SKIN. TREATED AND PRIMED -5, -9, -15 REPAIR PARTS. FABRICATED TWO -3 STRA
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