Douglas DC-9-32
Service difficulty reports · 12,755
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 = 'DC932' 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 = 'DC932' 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 0602859925Line · leakingON SHORT FINAL APPROACHING CLE, THE CREW RECEIVED A FLICKERING "RUDDER CONTROL MANUAL" WARNING INDICATION WHICH WENT TO STEADY ON AFTER TOUCHDOWN. THE AIRCRAFT ALSO EXPERIENCED A COMPLETE LOSS OF HYDRAULIC FLUID AND PRESSURE IN THE RIGHT SYSTEM. COM PROCEDURSDR 0602919950Skin · crackedDURING "H" CHECK, FOUND CRACK THE RT FUSELAGE SKIN AT THE LOWER CORNER OF THE FORWARD SERVICE DOOR JAMB. REPAIRED PER EA 99-208450.SDR ABXA070001Unknown · malfunctionedAIRCRAFT LOST PRESSURIZATION AT 6500 FT IN DESCENT TO ILN, BOTH PACKS ON. CHECKED TAIL COMPARTMENT FOR LOOSE AND BLOWN DUCTS. NO DEFECTS FOUND. PERFORMED ADJ/TEST OF CABIN PRESSURE CONTROL WITH PNEUMATIC SOURCE IAW DC9 MM 21-32-00-2-0101. SYSTEM OPERATES NSDR ABXA070002Control Panel · defectiveNR 2 COM FREQUENCY SELECTOR WAS REPORTED AS INOPERATIVE BY CREW. ELECTED TO REROUTE FLIGHT 122 ICT TO ILN, OVERFLEW SGF. ON L/P 033705-049/2, NR 2 COM FREQUENCY SELECTOR OCCASIONALLY DIALED WRONG FREQUENCY. VOLUME AND SELECTOR KNOBS WHEN WIGGLED SHORTED OUTSDR 0602769620Web · crackedDURING LINE CHECK, FOUND CRACK IN RT PYLON CLOSER WEB AT THE LIGHTENING HOLE LOWER EDGE STATION YN 164. REPAIRED PER EA 96-208511.SDR 0602609920Spar · crackedDURING LINE MAINTENANCE AIRCRAFT FELL FROM JACKED POSITION RESULTING IN A DENT TO THE LEFT WING FRONT SPAR CHORD AND CRACK IN THE LOWER RADIUS OF THE FRONT SPAR STIFFENER. REPAIRED PER EA 99-207937.SDR 0602479605Rod End · bentDURING THE CLIMB TO ALTITUDE AFTER TAKEOFF, THE AILERON TRIM FELT LOCKED UP OR FROZEN AND WAS INOPERATIVE AND UNUSABLE. THE FLIGHT CREW DIVERTED THE AIRCRAFT TO DTW AND NOTED THAT THE TRIM FREED UP AS THE AIRCRAFT DESCENDED BELOW 10,000 FEET. THE LANDING AT SDR 0602449987Pump · failedDURING TAKEOFF NR 1 ENGINE FLAMED OUT. THE FLIGHT RETURNED TO GPT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE FUEL PUMP SHAFT HAD SHEARED. REMOVED AND REPLACED THE FUEL PUMP, TESTED ENGINE AND RETURNED TO SERVICE.SDR ABXA060286Coalescer Bag · odorAFTER TAKEOFF, OILY SMELL FROM AIR CONDITIONING PACK. OILY SMELL DISSIPATED AFTER REACHING 10,000 FEET. REPLACED COALESCER BAGS, FOUND NO DEFECTS. OPERATIONAL CHECK GOOD IAW DC9 MM 21-20-02.SDR ABXA060285Light · inoperativeDURING MAINTENANCE PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS WOULD NOT ILLUMINATE. RESET EMERGENCY ARM AND CHARGE 5 AMP CIRCUIT BREAKER ON OVERHEAD PANEL AND RESET EMERGENCY LIGHT CHARGING 5 AMP CIRCUIT BREAKER AT LOCATION Z32. EMERGENCY LIGHTS TEST GOOD IASDR 0602229602Skin · crackedDURING L-CHECK FOUND CRACK IN FUSELAGE SKIN AT FORWARD SERVICE DOOR JAMB. REPAIRED PER EA 96-207744.SDR ABXA060275Wire · burnedDURING FLIGHT AN ARID ODOR WAS NOTICED IN THE GLARESHIELD AREA SIMILAR TO HOT PLASTIC OR HOT ELECTRICAL INSULATION. CENTER WINDSHIELD WAS TOO HOT TO TOUCH SO CENTER WINDSHIELD ANTI-ICE CIRCUIT BREAKER WAS PULLED. ODOR CEASED AND THEN RETURNED WITH CENTER WINSDR ABXA060281Support Fitting · crackedLEFT WING INBOARD SPOILER TORQUE TUBE SUPPORT ASSEMBLY CRACKED AT XRS-236. REMOVED AND REPLACED INBOARD SPOILER SUPPORT FITTING IAW DC9 MM.SDR ABXA060274Thermal Switch · failedDURING FLIGHT, SMOKE BEGAN EMINATING FROM CENTER WINDSHIELD RIGHT SIDE. WINDSHIELD HEAT WAS SELECTED OFF AND ANTI-ICE CIRCUIT BREAKER'S WERE PULLED. SMOKING STOPPED, WINDSHIELD WAS HOT TO THE TOUCH. INSPECTED CENTER WINDSHIELD FOR DEFECTS AND OHMED OUT WINDSDR ABXA060269Switch · obstructedNO NOSE GEAR INDICATION ON GEAR, RED OR GREEN. CREW EXCHANGED BULBS. NO INDICATION AND NO LIGHTS OR TEST. RECYCLED GEAR. NO INDICATION. COULD NOT SEE MARK ON VISUAL CHECK. MIRROR WAS DIRTY OR OUT OF ALIGNMENT. TRIED TO RECYCLE GEAR AGAIN AND RECEIVED THSDR Y2PA200600021Longeron · crackedFOUND LONGERON 3L CRACKED AT STATION 157. REPAIR PENDING.SDR ABXA060268Hose · blownCLIMBING THROUGH 9000 MSL, TAIL COMP TEMP HIGH LIGHT CAME ON. AFTER COMPLETION OF EMERGENCY CHECKLIST, WAS UNABLE TO KEEP THE TEMP HIGH LIGHT OUT. AIR TURN BACK. FOUND GROUND AIR COND CHECK VALVE UPPER CONNECTOR DUCT BLOWN. REPLACED BLOWN CONNECTOR DUCTS. OPESDR Y2PA200600020Floor Support · corrodedDURING VISUAL INSPECTION PER CPCP WORK CARD 46.53305 FOUND CORROSION ON 3 FLOOR SUPPORT BRACKETS BETWEEN STATIONS 160 AND 332. REPAIRS PENDING.SDR Y2PA200600019Seat Track · corrodedDURING VISUAL INSPECTION PER CPCP WORK CARD 46.53305 FOUND RIGHT HAND CENTER SEAT TRACK STA 200-320, RIGHT HAND OUTBOARD SEAT TRACK STA 200-210, LEFT HAND CENTER SEAT TRACK STA 200-323 AND LEFT HAND OUTBOARD SEAT TRACK STA 237-272 CORRODED. REPAIR PENDING.SDR ABXA060264Skin · corrodedSURFACE CORROSION FLAP OB LEADING EDGE LOWER SURFACE. REPAIRED AREA IAW SRM 57-01.SDR ABXA060263Pitot Head · corrodedALT PITOT STATIC PORT HAD DEBRIS FALLING FROM HOLE, CORRODED. REPAIRED CORRODED AREA IAW REA B593-54745.SDR 0601999613Door Frame · crackedDURING L-CHECK FOUND CRACK IN RIGHT MAIN LANDING GEAR DOOR CUTOUT FRAME. REPAIRED PER EA 96-206883.SDR 0601939605Rod End · brokenAS THE AIRCRAFT WAS ON APPROACH FOR LANDING AT BIS THE SLAT DEPLOYMENT WAS ASYMMETRICAL AND THE AIRCRAFT EXPERIENCED AND UNCOMMANDED ROLL. CREW RETRACTED THE LEADING EDGE DEVICES AND RETURNED THE AIRCRAFT TO A NORMAL SAFE LANDING BACK AT MSP. MAINTENANCE FOUNDSDR 0601929601Flap System · malfunctionedAS THE AIRCRAFT WAS CLIMBING OUT AFTER TAKEOFF, IT ROLLED TO THE RIGHT. THE TRAILING EDGE FLAPS INDICATED THE LT FLAP WAS AT 20 DEGREES DOWN AND THE RIGHT FLAP WAS AT 0 DEGREES. A FLAP DEPLOYMENT DIFFERENTIAL WAS VISUALLY VERIFIED BY THE FLIGHT ATTENDANT, ALTHSDR Y2PA20060018Skin · crackedDURING EC INSPECTION PER AD 2002-26-10 S/B 53-277R1 FOUND A .25 INCH CRACK ON THE FORWARD PIT DOOR JAMB, UPPER FORWARD CORNER.SDR Y2PA200600017Floor Support · corrodedDURING INSPECTION OF CPCP WORK CARD FOUND CORROSION BETWEEN STA. 658-680 ON RT OB FLOOR SUPPORT. WILL UPDATE WHEN A DETERMINATION IS MADE TO IND REPAIR PROCESSURE.SDR Y2PA200600016Fitting · corrodedPERFORMING CPCP WORK CARD ON CENTER TANK -TIE-IN- FITTING BETWEEN STA 598 & 617 SHOWS SIGNS OF EXFOLIATION ON LEFT SIDE AIRCRAFT. WILL UPDATE WHEN A DETERMINATION IS MADE TO FIND REPAIR PROCEDURE.SDR 0601819922Unknown · malfunctionedAS THE AIRCRAFT WAS DESCENDING FROM FL250, CREW NOTICED RED -CABIN PRESS- LIGHT ILLUMINATED. CABIN VERTICAL AIRSPEED WAS CLIMBING IN EXCESS OF 1500 FPM BUT AN IMMEDIATE DESCENT TO 10,000 FT, SMOOTHLY PERFORMED BY F/O; ENABLED CREW TO KEEP CABIN AT NO HIGHER TSDR 0601829601Skin · crackedDURING L-CHECK FOUND CRACK AT UPPER FORWARD CORNER OF L1 DOOR CUTOUT SKIN. REPAIRED PER EA 96-206869.SDR ABXA060199Plug · unlockedON APPROACH, NO GREEN NOSE GEAR LIGHT. PUT GEAR DOWN AGAIN AND LIGHT CAME ON AFTER RECYCLE.FOUND NOSE GEAR DOWN LOCK SWITCH DEUTSCH PLUG NOT IN THE LOCKED POSITION AND DIRTY FROM GREASE. CLEANED DEUTSCH PLUG AND RECONNECTED TO THE LOCKED POSITION.SDR 0601509604Accumulator · leakingDURING INITIAL APPROACH FOR LANDING THE RIGHT HYDRAULIC SYSTEM LOST THE ENGINE DRIVEN PUMP AND ALL THE FLUID. COM PROCEDURES WERE COMPLIED WITH AND THE EMERGENCY GEAR EXTENSION WAS ACCOMPLISHED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT, STOPPED ON THE RUSDR ABXA060189Battery · dischargedON SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW 33-53-02-4-0001.SDR 0601469608Transmitter · looseON FINAL APPROACH FOR LANDING THE LEFT HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO. THE LANDING WAS ACCOMPLISHED WITHOUT FURTHER INCIDENT. MAINTENANCE LOCATED A LINE TO THE PRESSURE TRANSMITTER LOOSE AND LEAKING. THE FITTING WAS SECURED, THE SYSTEM WAS SERVICSDR 0601229603Manifold · failedDURING CLIMB, THE RIGHT ENGINE FIRE HANDLE ILLUMINATED AND THE FIRE WARNING BELL SOUNDED. THE CREW FOLLOWED THE COM AND THE WARNINGS CEASED. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE THE RIGHT ENGINE FUEL HEAT MANIFOLDSDR ABXA060183Power Supply · dischargedEMERGENCY LIGHTS WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY SUPPLY IAW DC9 MM 33-53-02. EMERGENCY LIGHTS OPS CHECKED GOOD.SDR ABXA060175Circuit Breaker · faultyUPON GEAR EXTENSION, NO THREE GEAR GREEN OR RED GEAR UNSAFE LIGHTS. FOLLOWED ABNORMALS (GEAR RECYCLE), CONTACTED MAINTENANCE CONTROL. INSTRUCTED TO PULL AND RESET LANDING GEAR WARNING CIRCUIT BREAKER. ALL INDICATIONS THEN WERE NORMAL FOR LANDING. REMOVED SDR 0600649620Slide · unwanted deployDURING MAINTENANCE ACTIVITIES AT MCO, THE TAIL CONE WAS INADVERTENTLY JETTISONED. THE TAIL CONE EMERGENCY ESCAPE SLIDE DID NOT DEPLOY AND DID NOT INFLATE. NO OBVIOUS REASON FOR FAILURE OF THE SLIDE TO DEPLOY WAS DETAILED. EVACUATION SLIDE WAS REPLACED AT MCOSDR ABXA060131Tab · corrodedRIGHT ELEVATOR LOWER SURFACE HAD SEVERAL AREAS OF BULGING AROUND FASTENERS. REMOVED AND REPLACED ELEVATOR IAW DC9 SRM.SDR 0600489918Water Separator · contaminatedAT ABOUT 500 FEET FOLLOWING DEPARTURE THE FLIGHT ATTENDANT REPORTED SMOKE AND FUMES FILLING THE AFT CABIN ACCOMPANIED BY THE AFT LAVATORY SMOKE DETECTORS IN ALARM. CREW PERFORMED COM PROCEDURES, DECLARED AN EMERGENCY, AND RETURNED TO AN UNEVENTFUL LANDING BACSDR ABXA060091Battery · dischargedEMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00-8.SDR 0600359950Coalescer Bag · dirtyTHE FLIGHT ATTENDANT AND PASSENGERS REPORTED CHEMICAL SMELL/FUMES IN THE AFT CABIN WHILE EN ROUTE. OCCUPANTS COMPLAINED ABOUT NUMBNESS IN HAND, ARMS, AND SHORTNESS OF BREATH. THE AIRCRAFT LANDED WITHOUT INCIDENT AT DTW. MAINTENANCE REPLACED BOTH OF THE COALSDR 0600169917Clamp · brokenTHE RED (CABIN PRESS) WARNING LIGHT ILLUMINATED AND THE CABIN DIFFERENTIAL INDICATED OVER 1000. THE AMBER (CABIN PRESS AUTO FAIL) LIGHT DID NOT ILLUMINATE AND THE MASKS DID NOT DEPLOY. CREW PERFORMED A RAPID DESCENT TO 9000 FEET. BOTH PACKS WERE OPERATING NORMSDR 060016917Clamp · brokenTHE RED (CABIN PRESS) WARNING LIGHT ILLUMINATED AND THE CABIN DIFFERENTIAL INDICATED OVER 1000. THE AMBER (CABIN PRESS AUTO FAIL) LIGHT DID NOT ILLUMINATE AND THE MASKS DID NOT DEPLOY. CREW PERFORMED A RAPID DESCENT TO 9000 FEET. BOTH PACKS WERE OPERATING NORMSDR 0600279941Power Supply · failedDURING ROUTINE INSPECTION, MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT ROWS 16, 18, AND 20. THE POWER SUPPLY FOR THOSE LIGHTS WAS REPLACED AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE.SDR 0600079611Controller · malfunctionedDURING CLIMB OUT AT ABOUT FL190 THE CABIN PRESSURE INDICATOR ABRUPTLY PEGGED OUT IN CABIN CLIMB DIRECTION. FLIGHT CREW QUICKLY RECOVERED PRESSURE CONTROL BUT THEN LOST IT AGAIN AT FL280. AT THAT TIME CABIN ALTITUDE INDICATION WENT FROM 1000 TO 7500 FEET. CRSDR 0600069615Boot · separatedDURING APPLICATION OF WING ANTI-ICE, ON APPROACH, CREW REPORTED A STRONG ODOR. THE FUMES WERE DESCRIBED AS (DUSTY SMOKE) AND NO IDENTIFIABLE SOURCE WAS OBVIOUS. FLIGHT CREW DONNED OXYGEN MASKS AND COMPLIED WITH COM PROCEDURES. LANDING WAS WITHOUT FURTHER INCIDSDR 0501849611Controller · failedDURING CRUISE FLIGHT AT FL340 THE AIRCRAFT SUDDENLY STARTED TO LOSE CABIN PRESSURIZATION VERY QUICKLY. THE ORANGE -CABIN PRESS AUTO FAIL- LIGHT DID NOT ILLUMINATE AND NO MENTION OF RED -CABIN PRESS- LIGHT STATUS. CREW PERFORMED A RAPID DESCENT TO 10,000 FEETSDR 0501679617Door Frame · crackedDURING L-CHECK FOUND CRACK IN AFT LOWER CORNER OF FORWARD SERVICE DOOR FRAME. REPAIRED PER EA 96-204718.SDR 0501529941Valve · leakingDURING FINAL APPROACH ENGINE NR 2 ROLLED BACK TO 30 PERCENT N2 AND WOULD NOT RESPOND TO THROTTLE INPUT. ENGINE NR 2 WAS SHUTDOWN AND FLIGHT CREW PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND A FUEL LEAK AT P&D VALVE COUPLING. MAINTENANCE REPLACED ENGINSDR ABXA050242Battery · inoperativeOVERHEAD COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW AMM 33-53-00-8.
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