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 ABXA070218Battery · dischargedEMERGENCY LIGHTS WOULD NOT TURN ON WITH THE EMERGENCY LIGHT SWITCH IN ON POSITION. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-02-4.SDR ABXA070205Bulb · inoperativeNO NOSE GEAR INDICATION IN FLIGHT. FOUND NOSE GEAR BULBS MUSHROOMED AT TIPS AND BULBS INOPERATIVE. RELAMPED AS REQUIRED. INSPECTED WIRE BUNDLE AT NOSE DOWNLOCK SWITCH, NO DISCREPANCIES NOTED.SDR ABXR070240Attach Fitting · corrodedFORWARD AND AFT SURFACE OF FIXED BRACE ATTACH LUG ON RIGHT TRUNNION WAS CORRODED. REPLACED TRUNNION ON JOB CARD 0317 AND EA 57430026.SDR ABXR070239Attach Fitting · corrodedFORWARD AND AFT SURFACE OF FIXED BRACE LUG ON LEFT TRUNNION WAS CORRODED. REPLACED TRUNNION ON JOB CARD 0317 AND EA 57430025.SDR NWAA072119604Control Panel · shortedTHE ACARS COMMUNICATIONS AND REPORTING SYSTEMS IN THE COCKPIT FAILED AND CAUSED SMOKE SHORTLY AFTER TAKEOFF. THE ELECTRIC POWER TO THE ACARS UNIT WAS DISABLED AND COM PROCEDURES WERE COMPLIED WITH. THE SMOKE DID STOP AND THE AIRCRAFT RETURNED TO A SAFE BUT OSDR NWAA071949987Line · leakingAS THE AIRCRAFT CLIMBED AFTER DEPARTING DFW, THE CREW NOTICED THE LOSS OF FLUID QUANTITY AND PRESSURE FROM THE RIGHT HYDRAULIC SYSTEM. COM PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT CONTINUED TO SCHEDULED DESTINATION. AFTER LANDING UNEVENTFULLY THE LANDISDR ABXA070159Intercostal · crackedDAMAGE TO INTERCOSTAL AT STA 351 TO 370 LONGERON 30. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-1 AND 51-30-2.SDR ABXA070157Strap · crackedMAIN ENTRY DOOR INTERIOR FRAME STRAP CRACKED JUST AFT OF DOOR UPPER HINGE POINT AT APPROXIMATELY STA 170. REMOVED AND REPLACED FRAME STRAP IAW DC9 SRM 51-30-2, 51-30-5, AND 51-30-1.SDR ABXA070156Pan · crackedMAIN ENTRY DOOR FRAME CRACKED AT FORWARD LOWER CORNER JUST FORWARD OF LOWER HINGE POINT. REMOVED AND REPLACED DOOR PAN SEGMENT IAW DC9 SRM.SDR NWAA071609606Line · disconnectedDURING CLIMB, THE FLIGHT ATTENDANT REPORTED BOTH AFT LAVATORY SMOKE DETECTORS WERE SOUNDING. A MINUTE LATER THE FLIGHT CREW SMELLED FUMES IN THE COCKPIT. NO MENTION OF COM COMPLIANCE BUT CREW DID SAY THE SMELL CLEARED SOMEWHAT AND THEN RETURNED SLIGHTLY WORSSDR NWAA071579604Vane · obstructedWHEN THE CREW SELECTED 40 DEGREES OF FLAPS DURING APPROACH FOR LANDING, THE AIRCRAFT ROLLED TO THE RIGHT UNCOMMANDED. CREW WAS ABLE TO CORRECT THE ROLL OF THE AIRCRAFT WITH FOUR UNITS OF LEFT WING DOWN AILERON. THE LANDING WAS COMPLETED WITHOUT INCIDENT ANDSDR ABXA070148Seat Track · corrodedSEAT TRACK CORRODED LOWER FLANGE AND UNDERSIDE OF TRACK AT STA 560 TO 600 LEFT BUTT LINE 12. REMOVED AND REPLACED SEAT TRACK FS 49 L - 606 LEFT BUTT LINE 1L IAW DC9 SRM 53-05.SDR NWAA071309984Line · failedTHE RIGHT HYDRAULIC SYSTEM HAD A COMPLETE LOSS OF FLUID AND PRESSURE AS THE AIRCRAFT CLIMBED THROUGH 13,000 FEET. COM PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT CONTINUED TO A NORMAL SAFE LANDING AT THE SCHEDULED DESTINATION. MAINTENANCE FOUND A HYDRAULISDR ABXA070147Angle · crackedANGLE CRACKED - PYLON AFT SPAR, AFT SIDE, LOWER STRAP, OUTBOARD END - JUST INBOARD OF AFT ENGINE MOUNT. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-5.SDR ABXA070146Floor Support · corrodedFLOOR SUPPORT CHANNEL EXFOLIATED IN 3 PLACES - FS 365 TO 380, LONGERON 28 LEFT. REPAIRED AREA IAW DC9 SRM.SDR ABXA070145Longeron · crackedLONGERON 30 CRACKED ON BOTH SIDES - FS 439 TO 446. REMOVED AND REPLACED LONGERON 30, STA 439 TO 446 IAW DC9 SRM.SDR ABXA070144Skin · cracked1.125" LFEC CRACK INDICATION BETWEEN FASTENERS AT LOWER FORWARD CORNER. FASTENERS ARE AT EDGE OF CUTOUT AND COMMON TO DOOR SEAL DEPRESSOR. REPAIRED AFT LOWER CARGO LOWER FORWARD CORNER IAW DC9 SRM.SDR ABXA070139Seat Track · corrodedSEAT TRACK SECTION BUTT LINE 0, STA 570 - 785 CORRODED AT STA 785 - 765, 737, 710 - 699, 680 - 670 AND 636 - 617. REMOVED AND REPLACED SEAT TRACK STA 160 - 784 IAW DC9 SRM 51-30-1 AND 51-10-4.SDR ABXA070143Retainer · crackedCRACK IN UPPER FORWARD CORNER OF WINDOW RETAINER JUST AFT OF STA 699 FRAME. REPAIRED AREA IAW REA D956-55634-MR.SDR ABXA070142Spar Cap · crackedLEFT HORIZONTAL STABILIZER LOWER SPAR OUTBOARD END CRACKED JUST ABOVE DRAINS, TRAVELS INBOARD UNDER HINGE. REPAIRED LEFT HORIZONTAL STABILIZER LOWER SPAR CAP IAW DC9 SRM 55-02.SDR ABXA070141Door Frame · crackedLEFT AFT OVERWING EXIT DOOR HAD CRACKED DOOR OUTER FRAME IN 3 PLACES AT SEAL SUPPORT FITTINGS. REPAIRED AREA IAW DC9 SRM.SDR ABXA070140Door Frame · crackedRIGHT FORWARD OVERWING EXIT DOOR HAD CRACKED DOOR OUTER FRAME IN 1 PLACE AT SEAL SUPPORT FITTING. REPAIRED CRACK IAW DC9 SRM.SDR ABXA070138Seat Track · corrodedFOUND SEAT TRACK RIGHT BUTT LINE 44 CORRODED AT STA 718. REMOVED AND REPLACED SEAT TRACK STA 570 TO 748 IAW DC9 SRM 51-30-1. REINSTALLED FLOOR PANELS IAW DC9 SRM 51-30-1.SDR ABXA070133Structure · crackedUPPER CARGO SUBFLOOR CRACKED AT RIGHT BUTT LINE 28, FS 180. REPAIRED SUBFLOOR RIGHT BUTT LINE 28 AT STA 180 IAW DC9 SRM 53-01.SDR ABXA070137Seat Track · corrodedFOUND SEAT TRACK AT RIGHT BUTT LINE 11 CORRODED ON BOTH SIDES OF SPLICE AT STA 493. REMOVED AND REPLACED SEAT TRACK IAW DC9 SRM 53-05.SDR ABXA070136Longeron Splice · crackedFOUND LONGERON 30 SPLICE FS 794 - 813 CRACKED. REMOVED AND REPLACED LONGERON 30 STA 794 - 813 IAW DC9 SRM 53-11-3.SDR ABXA070135Seat Track · corrodedUPPER CARGO SEAT TRACK CORRODED AT RIGHT BUTT LINE 9, FS 160. REMOVED AND REPLACED SEAT TRACK IAW DC9 SRM 51-10-3 AND 51-30-1.SDR ABXA070134Structure · crackedUPPER CARGO SUBFLOOR CRACKED AT LEFT BUTT LINE 50, FS 180. REPAIRED SUBFLOOR LEFT BUTT LINE 50 AT STA 180 IAW DC9 SRM 53-01.SDR ABXA070132Hinge Fitting · crackedAFT FLAP HINGE FITTING CRACKED AT ACTUATOR ATTACH EAR, STA 164. REMOVED AND REPLACED HINGE FITTING IAW DC9 SRM.SDR ABXA070131Rib · crackedLEFT LEADING EDGE RIB HAD CRACKED DOUBLER 2ND RIB INBOARD OF NR 11 TRACK. REPAIRED RIB IAW REA D957-55597.SDR ABXA070105Floorbeam · crackedFLOORBEAM CRACKED TO LIGHTENING HOLE APPROXIMATELY STA 175, BUTT LINE 0. REPAIRED AREA IAW REA D953-55576MR.SDR ABXA070076Unknown · odorAIRCRAFT HAS STRONG ODOR OF FUEL OR SOLVENT IN COCKPIT AND CARGO AREA. NO FUEL LEAK OR ODOR NOTED IAW DC9 MM 28-00-00.SDR ABXA070103Frame · crackedAFT RIGHT MAIN FRAME HAD CRACK AT FORWARD AND AFT FLANGES, MUST BE REPLACED PER NEA 53400102-002-30. REMOVED AND REPLACED RIGHT MAIN FRAME IAW DC9 EA 53400326-001-2. CRACK LENGTHS WERE 1" AND 1 1/4".SDR ABXA070100Attach Angle · corrodedUPPER SURFACE OF PYLON BULKHEAD TO FLOORBEAM ATTACH ANGLE AT STA 965 CORRODED FROM RIGHT BUTT LINE 55, RIGHT BUTT LINE 36. FABRICATED AND INSTALLED NEW PYLON BULKHEAD TO FLOORBEAM ATTACH ANGLE IAW DAC DWG 9912243.SDR ABXA070099Bulkhead · crackedRIGHT PYLON BULKHEAD AT STA 965 HAD CRACKED ATTACH FITTING AT RIGHT BUTT LINE 32. REMOVED AND REPLACED FITTING IAW DAC DWG 9912243.SDR ABXA070094Shear Tie · crackedSHEAR TIE CRACKED AT FS 945, BETWEEN LONGERON 15 RIGHT AND LONGERON 16 RIGHT. REMOVED AND REPLACED SHEAR TIE IAW DC9 SRM 51-30-2, 51-30-5 AND 51-30-1.SDR ABXA070102Bulkhead · crackedAFT PRESSURE BULKHEAD LOWER DOOR CORNER HAD A CRACK IN SKIN. THE REPAIR INSTALLED DID NOT MATCH ANY CONFIGURATION OF DWG J060088 IN NUMBER, PLACEMENT AND MATERIAL OF DOUBLERS. REMOVED PREVIOUS REPAIR. NO CRACKS FOUND. REPAIRED LOWER DOOR CORNER IAW SERVICESDR ABXA070096Frame · corrodedLOWER POCKETS IN MAIN FRAME IN LEFT WHEEL WELL HAD CORROSION AROUND LOWER VERTICAL ATTACH BOLTS. CLEANED, TREATED CORROSION AROUND LOWER VERTICAL ATTACH BOLT ON LEFT MAIN FRAME 718 AIW DC9 SRM.SDR ABXA070093Bulkhead · crackedAFT PRESSURE BULKHEAD LEFT UPPER DOOR CORNER HAD 2 CRACKS THAT NEEDED TO BE STOP DRILLED. REMOVED OUTSIDE DOUBLER, STOP DRILLED CRACKS IAW SRO J060088. REINSTALLED DOUBLER IAW SRO J060088 AND DC9 SRM 51-30-5. CRACK LENGTHS WERE 7/8", 3/4" AND 1".SDR ABXA070092Rib · crackedLEFT WING XRS 164, RIB FITTING CRACKED. REMOVED AND REPLACED RIB AT LEFT WING XRS 164 IAW DC9 SRM.SDR NWAA070849941Clamp · strippedAT FL340, THE CABIN TEMPERATURE BEGAN TO INCREASE. THE LEFT PACK WENT TO FULL HOT IN AUTO AND FLIGHT CREW SELECTED FULL COLD. THEN THE RIGHT PACK WENT TO FULL HOT IN AUTO AND FULL COLD WAS SELECTED IN MANUAL. CREW NOTICED THAT THE AIRCRAFT WAS LOSING CABIN SDR ABXA070068Power Supply · dischargedCOCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY POWER PACK IAW DC9 MM 33-53-00.SDR NWAA071079918Spar · crackedDURING "L" CHECK, FOUND CRACK IN LT WING TE SPAR EXISTING TEMPORARY REPAIR AT WS 267. SECTION I OF EA 99-208475 REMOVES EXISTING TEMPORARY REPAIR AND REINSTALLATION OF NEW TEMPORARY REPAIR. SECTION II OF EA REQUIRES PERMANENT REPAIR TO BE INSTALLED WITHIN 2 SDR NWAA071069941Skin · crackedDURING "H" CHECK, FOUND CRACKS IN LT FLAP NOSE SKIN AT XFS 235 AND 252. REPAIRED PER EA 99-208467.SDR NWAA070729984Panel · crackedDURING "L" CHECK, FOUND CRACK IN LT WING LEADING EDGE PANEL NR 1590 APPROXIMATELY 4 INCHES AFT OF NR 3 FLAP HINGE. REPAIRED PER EA 99-208468.SDR 0700529620Slide · inoperativeLOCAL VENDOR AT SYR ATTEMPTED TO STOW TAIL CONE RELEASE HANDLE AND INADVERTENTLY JETTISONED THE TAIL CONE. SEE LP NR 3832775. THE TAIL CONE EMERGENCY ESCAPE SLIDE DID NOT DEPLOY AND DID NOT INFLATE. NO OBVIOUS REASON FOR FAILURE OF THE SLIDE TO DEPLOY AS DESDR ABXA070043Battery · dischargedEMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00.SDR 0700439610Clamp · brokenWHILE CLIMBING PASS FL280, THE CABIN ALTITUDE BEGAN TO CLIMB UNCONTROLLABLY AT 1000 FPM. FLIGHT CREW INITIATED AN EMERGENCY DESCENT TO 8000 FEET AND RETURNED TO DEPARTURE. COM PROCEDURES WERE COMPLIED WITH, THE OUTFLOW VALVE WAS CONFIRMED CLOSED BUT THE CABISDR NWAA70089611Outflow Valve · malfunctionedDURING CLIMB AT FL 200 WITH WING ANTI-ICE ON SELECTED CABIN BEGAN TO CLIMB AND DESCEND RAPIDLY. FLIGHT DESCENDED TO FL 100. NO MENTION OF OXYGEN MASKS BEING DEPLOYED. FLIGHT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINT REPLACED CABIN PRESS CONTROLLERSDR ABXA070008Coalescer Bag · defectivePILOT REPORTED OIL ODOR FROM AIR CONDITIONING SYSTEM. REPLACED LEFT AND RIGHT WATER SEPARATOR BAGS IAW DC9 MM 21-20-02.
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