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 CALA9801202Intercostal · crackedINSPECTION FOUND A 1.5 INCHCRACK IN INTERCOSTAL IN FORWARD CARGO PIT AT STA 448, LONGERON 29R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-5.SDR CALA9801201Brackets · crackedINSPECTION FOUND LT WING LEADING EDGE FRAMES HAD CRACKED BRACKETS BETWEEN STA 383 AND 370, BETWEEN STA 414 AND 426, STA 506, AND STA 551. THE CRACKS WERE .25 TO .5 INCH LONG. THE CRACKED BRACKETS WERE REMOVED AND NEW BRACKETS WERE FABRICATED AND INSTALLED IASDR CALA9801200Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT AT STA 236, STRINGER 27R. THE CRACK WAS STOP DRILLED IAW ECRA 5320-01263. AN ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.SDR VJ9800211Skin · corrodedINTERNAL SKIN UNDER AUX PUMP AT STA 560, LONGERON 29L TO 29R, CORRODED. REMOVED LONGERON END CAPS FROM 25L TO 25R. REMOVED EXISTING REPAIR, INTERNAL DOUBLERS, TRIMMED OUT CORRODED AREA AND FABRICATED REPAIR DOUBLER FROM 2024T3 .80 MATERIAL, DRILLED, DEBURREDSDR TWAA9810808Spar Cap · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON RT WING UPPER REAR SPAR CAP, AN 'EYE BROW' CRACK ABOVE BOTH THE INBD AND OTBD STUD HOLES. CRACK LENGTH WAS 0.75 INCH ABOVE THE INBD HOLE AND 0.5 INCH ABOVE THE OTBD HOLE. INSTALLED DOUBLER PER ARA 15291 AND BLUESDR TWAA9810714Splice · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON LT WING 10 INCHES OTBD OF INBD END OF NR 3 SLAT, LE OF WING SPLICE PLATE, CRACKED. REMOVED CRACKED SPLICE PLATE AND INSTALLED NEW PART, DRILLED IN, INSTALLED AD RIVETS AND TENSION HI LOCKS PER SRM 51-30-0 PG 1. SDR TWAA9810713Tie · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACKED STRINGER TIE AT FS 585, AND STR 26R. REMOVED FORMER RING AT STA 579 FROM S25L TO S25R TO GAIN ACCESS TO STRINGER TIE. REPLACED CRACKED STRINGER TIE PER SRM 51-30. (X)SDR TWAA9810710Skin · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ROUND INTERIM REPAIR AT THE RADIO ALT ANTENNA AT FS 510, L30. REMOVED PREVIOUS REPAIR. INSTALLED REPAIR DOUBLER AND FINGER DOUBLER PER DWG SRO 9530107 AND SRM 53-04, FIG 44. (M)SDR TWAA9810709Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK, A DYE CHECK SHOWED A ONE INCH CRACK IN LOWER FLANGE OF LONGERON 13R, AT FASTENER AT STA 965 FORMER FRAME. REMOVED CRACKED SECTION OF LONGERON 13R. INSTALLED NEW SECTION OF LONGERON AND INCORPORATED LONGERON SPLICE REPAISDR MWEA98761Sensor · inoperativeTHE MASTER WARNING LIGHTS AND TAIL COMPARTMENT TEMP HIGH LIGHTS ILLUMINATED APPROACHING 138 KNOTS. MAINTENANCE PERFORMED REJECTED TAKEOFF INSPECTION INSPECTED TAIL COMPARTMENT. REMOVED AND REPLACED RT TEMP HIGH SENSOR.SDR VJ9800210Frame · corrodedAFT PITDOOR FRAME, FS889, L25R-26R, SKIN CORRODED ON BACKSIDE AROUND NUTPLATES. REMOVED CORROSION FOUND BEYOND LIMITS IAW DC9 SRM 51-10-3. FABRICATED WEB DOUBLER OUT OF 7075T6, .040, AND FABRICATED REPAIR DOUBLER FROM 7075T6, .050. TRIMMED, FITTED, DRILLED,SDR 9809669610Clamps · looseTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CLAMPS AT LEFT AUGMENTATION VALVE, OPERATIONAL CHECK NORMAL.SDR VJ9800208Batteries · dischargedEMERGENCY LIGHTS AT FORWARD GALLEY, COCKPIT AND OVERWING INOP. REPLACED BATTERIES, OPS CHECKED GOOD IAW MM 33-50.SDR 9809659985Augmentation Vlv · failedLOSS OF CABIN PRESSURE OCCURRED DURING CRUISE FLIGHT AT 33,000 FEET EN ROUTE. CREW ACCOMPLISHED EMERGENCY DESCENT AND FLIGHT WAS DIVERTED TO MKE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT AUGMENTATION VALVE AND BROKEN LEFT ENGINE ANTI-ICE SDR VJ9800206Cover · looseCHECK SLIDE COVER ON GALLEY DOOR. REINSTALLED DOOR SLIDE COVER IAW MM 25-60-1 AND PERFORMED REQUIRED INSPECTIONS.SDR GTIA9800075Light · inoperativeOKC - FLT 902 - EMERGENCY FLOOR TRACK BROKE BETWEEN ROWS 11-15. REPAIRED FLOOR TRACK AND LIGHTING IAW DC-9 MM 33-51. OPERATIONAL CHECKS GOOD. (X)SDR 9809649918Sensor · brokenDURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND FLIGHT WAS DIVERTED TO ORD. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOWNLOCK PROXIMITY SENSOR BROKESDR TWAA9810715Seat Track · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TRACK NR 3, FS 937 TO FS 946. REMOVED OLD TRACK FROM STA 929 TO STA 965. INSTALLED NEW TRACK PER SRM 53-05-10C, AND SRM 51-01 PAGE 1 ITEM C. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)SDR TWAA9810615Web · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND A .50 INCH CRACK IN MEMBRANE AT LONGERON 18L, STA 234. REMOVED MEMBRANE AT L18L, FS 218 TO FS 237 PER DAC SRM 51-61 PAGE 1. FABRICATED COMPLETE PART FROM SAME MATERIAL PER DAC SRM 53-10-2, FIG 4 SHEETS 1 AND 2, ITESDR TWAA9810614Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK, ON LOWER FUSELAGE, FOUND LONGERON 25L WITH CRACK AT FASTENER AT STA 256 FORMER FRAME. INSTALLED NEW LONGERON SECTION AND TWO LONGERON REPAIR SPLICES PER SRM 53-02, FIG 18. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)SDR TWAA9810613Casting · corrodedMCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING, THE CENTER AND INBD FWD FLAP HINGE CASTING HAD BADLY PITTED MOUNT HOLES. INSTALLED NEW FLAP HINGE CASTING PER MM 57-40-01, PG 201 TO PG 205. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)SDR VJ9800209Skin · damagedREMOVED AND REPLACED TEMPORARY REPAIR WITH A PERMANENT REPAIR ON LT FUSELAGE AT FS 220. REMOVED EXISTING REPAIR, DUCTING, AND INSULATION. FABRICATED NEW REPAIR DOUBLER FROM .063 2024T3, 11 INCH BY 11.25 INCHES, AND 2 EACH FINGER DOUBLERS FROM .025 2024T3, 3 SDR TWAA9810804Splice · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON RT WING A CRACK IN WING L.E. ON SPLICE DOUBLER. LOCATED OTBD END OF NR 1 SLAT. INSTALLED SPLICE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)SDR TWAA9810716Support · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR PANEL SUPPORT HAT SECTION WITH APPROXIMATELY 1.5 INCH CRACK AT STA 237, RBL 2 INCHES. REPAIRED PER SRM 51-01, PAGE 1, ITEM C, TWA STD PRACTICES, AND SRM 51-30-2, SRM 51-01 PAGE 4 FIG 1. ACFT TT: 77,783 HOURSSDR TWAA9810610Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND A CRACK IN AFT FASTENER RIB, 18 IN OUTBOARD OF NR 5 SLAT CENTER TRACK RIB IN LE OF LEFT WING. REPLACED RIB PER SRM 51-01, PAGE 1 ITEM C. REPLACED HI-LOKS PER SRM 51-30-5. REPLACED RIVETS PER SRM 51-30-5. (M)SDR TWAA9810201Connector · failedSTL - AFTER REPLACEMENT OF THE AUXILIARY HYDRAULIC PUMP, DURING CHECK-OUT, A FIRE IGNITED AT THE PUMP. FIRE WAS QUICKLY EXTINGUISHED WITH GROUND FIRE BOTTLE. PASSENGERS WERE DEPLANED THROUGH JETWAY. FOUND SHORT IN AUXILIARY PUMP HARNESS CONNECTOR. REPLACEDSDR MWEA98758Seat Track · wornFOUND CAPTAINS AFT OUTBOARD SEAT TRACK WORN BEYOND LIMITS. MTC FABRICATED AND INSTALLED SEAT TRACK.SDR MWEA98757Angle · crackedFOUND CRACK ON VENTRAL DOOR JAMB CUTOUT THRESHOLD SUPPORT ANGLE. MTC FABRICATED AND INSTALLED REPAIR DOUBLER.SDR MWEA98756Intercostal · crackedFOUND CRACKED INTERCOSTAL ON LEFT WHEEL WELL STATION 718 AFT SIDE. MTC FABRICATED AND INSTALLED DOUBLERS.SDR MWEA98755Channel · crackedFOUND CRACK ON RIGHT PYLON 2 CHANNEL FORWARD OF AFT ENGINE MOUNT. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS.SDR CALA9801160Frame · crackedINSPECTION FOUND A 2.5 CRACK IN FORWARD PIT FRAME AT STA 484 BETWEEN STRINGER 26L AND 27L. THE CRACKED AREA OF FRAME WAS CUT OUT IAW ECRA 5320-01263. A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.SDR TWAA9810717Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND IN CABIN DYE CHECK SHOWING 2 EACH CACKS IN LOWER FLANGE OF LONGERON 16R, AT STA 965 FORMER FRAME. REMOVED CRACKED SECTION OF L16R AND FITTED AND INSTALLED NEW SECTION OF LONGERON PER SRM 53-02, FIG 18. ACFT T: 77,SDR TWAA9810611Skin · crackedMCI - DURING OP16 MAINTENANCE CHECK, EDDY CURRENT INDICATED .125 INCH LONG CRACK RUNNING AFT FROM UNDER RIVET RBL 13 IN, STATION 699, TOP FUSELAGE SKIN. ACCOMP HFEC PER SRM 51-00-2 FOR CRACK CONTAINMENT. NO CRACK INDICATED. REPAIRED PER DAC REWORK DRAWING SSDR CALA9801153Jamb · corrodedINSPECTION FOUND INNER AFT CARGO DOOR PAN CUTOUT CORRODED. THE DOOR PAN AND THRESHOLD TRIM WERE REMOVED IAW SRM 51-30-2. THE THRESHOLD WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. A THRESHOLD WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-5. SDR CALA9801152Web · crackedINSPECTION FOUND A CRACK IN CABIN INTERIOR WEB AT STA 756, RBL 53. THE WEB WAS REMOVED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 4.SDR CALA9801151Door · gougedINSPECTION FOUND RT WING LEADING EDGE SLAT DOOR GOUGED AT XOS 240. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5730-01568.SDR VJ9800207Light · inoperativeEMERGENCY EXIT LIGHT AT GALLEY DOOR INOP. REPLACED LIGHT, OPS CHECKED GOOD.SDR VJ9800200Cable · detachedDURING PREFLIGHT, FOUND THE FWD LOADING DOOR CHUTE CABLE DETACHED. REINSTALLED L-1 DOOR SLIDE IAW MM 25-62-0.SDR VJ9800199Power Supply · inoperativeEMERGENCY EXIT LIGHTS INOP AT OVERHEAD SEATS 18 TO 22. REPLACED THE FWD POWER SUPPLY AND BATTERIES ALONG WITH THREE LIGHT BULBS.SDR CALA9801143Beam · crackedINSPECTION FOUND A 2 INCH CRACK IN FORWARD END OF NR 6 BEAM OF FORWARD SERVICE DOOR. THE BEAM WAS REPAIRED IAW EA 5240-01192.SDR CALA9801142Beam · crackedINSPECTION FOUND A .25 INCH CRACK AT FORWARD END OF BEAM NR 1 FASTENER LOCATION AND A .5 INCH CRACK AT FORWARD END OF BEAM NR 5 FASTENER LOCATION OF FORWARD CARGO COMPARTMENT DOOR OUTER PAN. THE CRACKS WERE STOP DRILLED. REPAIRS WERE FABRICATED AND INSTALLEDSDR CALA9801141Fitting · crackedINSPECTION FOUND A 1 INCH CRACK IN OUTER PAN RADIUS OF FORWARD CARGO COMPARTMENT DOOR LOWER FORWARD STOP FITTING. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 2-03, FIGURE 8.SDR CALA9801140Skin · corrodedINSPECTION FOUND RT WING PANEL NR 1246 CORRODED AND DELAMINATED. THE OUTER SKIN WAS REMOVED AND HONEYCOMB WAS CLEANED. NEW SKIN AND HONEYCOMB WERE FABRICATED AND INSTALLED IAW SRM 51-31-1, FIGURE 1 AND 51-70-2.SDR VJ9800196Battery · dischargedOVERHEAD EMERGENCY LIGHTS INOP IN AFT CABIN. REPLACED BATTERIES IN POWER SUPPLY; OPS CHECKED GOOD IAW MM 33-42.SDR TWAA9810612Longeron · crackedMCI - DURING OP16 MAINTENANCE CHECK, FOUND FWD ENTRY DOOR AREA LONGERON CRACKED AT STATION 200, L2L. REMOVED CRACKED LONGERON. INSTALLED NEW LONGERON PER SRM 51-06, PAGE 1, ITEM C, AND INSTALLED FASTENERS PER SRM 51-30-05. (M)SDR MWEA98754Girt Bar · bindingTHE MAIN CABIN DOOR GIRT BAR IS HARD TO ARM AND DISARM. MTC REMOVED PAINT BUILD-UP FROM THE NEW LATCHES.SDR MWEA98752Cover · detachedTHE LANYARD ON THE GALLEY DOOR SLIDE COVER DETACHED FROM THE ANCHOR POINT. MTC REINSTALLED GALLEY SLIDE COVER AND LANYARD.SDR MWEA98749Light · inoperativeFOUND FORWARD ENTRANCE EMERGENCY LIGHT INOP. MTC REMOVED AND REPLACED FORWARD ENTRANCE EMERGENCY LIGHT ASSEMBLY.SDR CALA9801139Wedge · crackedINSPECTION FOUND A .5 INCH CRACK IN RUDDER TRAILING EDGE WEDGE. THE AREA WAS REPAIRED IAW SRM 55-03 AND 51-70-2.SDR CALA9801138Fairing · crackedINSPECTION FOUND A 2.5 INCH CRACK IN LT FLAP INBOARD FLAP TRACK FAIRING TRAILING EDGE. THE FAIRING WEB AND ANGLE WERE REMOVED. A NEW WEB AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.
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