Douglas DC-9-31
Service difficulty reports · 7,433
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 = 'DC931' 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 = 'DC931' 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 9608209996Battery · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERY IN BATTERY PACK. OPERATIONAL CHECK NORMAL.SDR 9608079954Fitting · crackedDURING H-CHECK, FOUND A CRACK AND CORROSION IN THE RIGHT MAIN LANDING GEAR WHEEL WELL KEEL, LONGERON 29R AFT END FITTING. REPLACED FITTING PER SRM 51-30-5.SDR ABXA9600523Tr Link · crackedDURING COMPLIANCE OF AD'S 75-14-06, 90-18-03 SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND RIGHT THRUST REVERSER OUTBOARD UPPER DRIVER LINK HAD A CRACK INDICATION. REPLACED RIGHT THRUST REVERSER OUTBOARD UPPER DRIVER LINK IAW DC-9 MM 78-31-5. LINK FOUND TO BE CRSDR 9609539968Door Jamb · corrodedDURING H-CHECK, FOUND CORROSION IN THE FORWARD CARGO DOOR LOWER JAMB PAN. REPAIRED PAN (P/N 5912494) PER EA 99-109426.SDR 9608069968Fitting · corrodedDURING M-CHECK, FOUND CORROSION ON THE LONGERON 23L FITTING AT FS 996. REPLACED FITTING (P/N 3914654-1D).SDR ABXA9600463Skin · damagedDURING C-CHECK INSPECTION, A TEMPORARY REPAIR WAS REMOVED FROM THE MAIN ENTRY DOOR OUTER SKIN FOR INSTALLATION OF A PERMANENT REPAIR. FUSELAGE SKIN WAS REPAIRED IAW ABX REA D952-14946-MR.SDR 9608389954Splice · corrodedDURING H-CHECK, FOUND CORROSION ON THE LONGERON 30 SPLICE AT FS 560. REPLACED SPLICE (P/N 5920319-504) PER EA 99-109493.SDR 9607929915Turbine · failedNR 2 ENGINE EXPERIENCED A CONTAINED TURBINE FAILURE AFTER DEPARTING. AIRCRAFT RETURNED TO BIL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE WITH A SERVICEABLE UNIT.SDR USAA960367Skin · crackedPIT - DURING SCHEDULED PRODUCTION CONTROL ITEM, FOUND A 2 INCH CRACK RIGHT SIDE SKIN LONGERON 14R-15R AT STATION 965. INSTALLED TITANIUM DOUBLER PER USAIR EA NR 32460. (M)SDR 9607809933Wire · brokenDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BROKEN WIRING AT ROW 1, OPERATIONAL CHECK NORMAL.SDR GTIA96NK153Wire · brokenLEFT GEAR GREEN LIGHT CAME ON AND OFF IN FLIGHT. UPON GEAR EXTENSION THE GEAR UNSAFE LIGHT CAME ON. GEAR VISUALLY CHECKED DOWN AND LOCKED. REPAIRED BAD GROUND CONNECTION AT STUD NR 551, REPAIRED BAD CONNECTION TO TERM NR 5 (53-65). REPAIRED BROKEN WIRE AT SDR 9607779979Connectors · crossedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN AND ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. FOUND CONNECTORS CROSSED IN GALLEY OVERHEAD PANEL. CORRECTED WIRING, OPERATIONAL CHECK NORMAL.SDR 9607589994Cable · brokenAFTER TAKEOFF, A LOUD BANG WAS HEARD FROM NOSE LANDING GEAR WHEELWELL AREA. FLIGHT RETURNED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT NOSE GEAR DOOR STOP CABLE BROKEN. DEFERRED CABLE PER MEL 32-7. AIRCRAFT RETURNED TO SERVICE.SDR 9607799952Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR 9607769954Fitting · crackedDURING H-CHECK, FOUND CRACKS IN THE FORWARD CARGO DOOR UPPER AFT AND LOWER AFT DOOR STOP FITTINGS. REPLACED FITTINGS.SDR 96ZZZM799Power Supply · inoperativeDURING A PREFLIGHT CHECK OF THE EMERGENCY EGRESS LIGHTS, THEY REMAINED ILLUMINATE. REMOVED AND REPLACED EGRESS POWER SUPPLY, MFG P/N 5322-2. OPERATIONAL CHECK NORMAL.SDR 9608349954Frame · corrodedDURING H-CHECK, FOUND CORROSION ON THE FUSELAGE FRAME STRAPS AT FS 484 AND 522 BETWEEN LONGERONS 29L AND 29R. REPAIRED STRAPS (P/N RW2800206-8) PER EA 99-109471 AND 99-109475.SDR 9607789937Wire · brokenDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 3 AND 5 INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE AT ROW 3 AND LOOSE CONNECTOR AT ROW 5. REPAIRED WIRE AND RESECURED CONNECTOR, OPERATIONAL CHECK NORMAL.SDR 9607759954Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE LONGERON 25R END FITTING AT FS 579 TO 598. REPLACED FITTING PER SRM 51-10-2.SDR 9607749954Fitting · crackedDURING H-CHECK, FOUND CRACKS ON THE LONGERON 26, 29R AND 30 END FITTINGS AT APPROXIMATELY FS 586. REPLACED ALL FITTINGS PER SRM 51-30-2.SDR 9607409943Evac Slide · low pressureDURING LINE MAINTENANCE INSPECTION, FOUND GALLEY DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE.SDR USAAD96037Tire · wornSTRONG BURNING RUBBER SMELL AFTER TAKEOFF (OUT OF ATL). DECLARED EMERGENCY INBOUND TO CLT. LANDED UNEVENTFULLY. INSPECTED BOTH ENGINE INTAKES, GROUND RAN PACKS. NO SMELLS PRESENT. FOUND BOTH NOSE TIRES WORN. REMOVED AND REPLACED BOTH NOSE TIRES. (M)SDR USAAD96034Engine · failedBWI FL 349 - CLIMBING THROUGH 9000 FEET OUT OF BWI, LEFT ENGINE FAILED. CREW HEARD LOUD BANG (SIMILAR TO A COMPRESSOR) STALL AND ENGINE RPM BEGAN TO DECREASE. CREW SHUT DOWN ENGINE. FLIGHT RETURNED TO BWI AND LANDED WITH NO FURTHER INCIDENT. SET 8 MINUTES.SDR 96ZZZX2792Spar · crackedRADIOGRAPHIC INSPECTION REVEALED CRACK IN LEFT ELEVATOR FRONT SPAR UPPER FLANGE, EMANATING FROM RIVET HOLE IN FORWARD DIRECTION AND TERMINATING AT EDGE OF FLANGE APPROXIMATELY .300 INCH IN LENGTH. REPAIRED AREA IAW DC-9 SRM 55-02, PAGE 31. BALANCED ELEVATOR SDR 9607519954Longeron · crackedDURING H-CHECK, FOUND A CRACK IN THE LONGERON 25R END FITTING AT FS 585. REPLACED FITTING PER SRM 51-30-2.SDR 9607399909Duct Clamp · looseLOSS OF CABIN PRESSURIZATION OCCURRED AT 35,000 FEET, AN EMERGENCY DESCENT WAS MADE TO 10,000 FEET AND FLIGHT DIVERTED TO MCO. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LOOSE DUCT CLAMP AND BOOT DISCONNECTED AT WATER SEPARATOR. TIGHTENED CLAMPSDR GTIA96NK154Actuator · failedON CLIMB-OUT, AT 8,000 FEET, PRIMARY LONGITUDINAL TRIM FAILED, NEITHER YOKE SWITCHES NOR THE SUITCASE SWITCHES WORKED. USED AUTOPILOT WITH ALTERNATE TRIM TO RETURN TO TPA. REMOVED PRIMARY LONGITUDINAL TRIM MOTOR. OPS CHECKED GOOD. (M)SDR GTIA96NK152Controller · failedCABIN PRESSURIZATION FAILURE DESCENDING THROUGH 27,000 FEET. DECLARED EMERGENCY, MASKS DROPPED. DIVERTED TO TPA. REPLACED CABIN PRESSURE CONTROLLER. GROUND RUN PERFORMED, SYSTEM CHECKS SATISFACTORY. (M)SDR GTIA96NK151Anticipator · malfunctionedCABIN PRESSURIZATION FAILURE. DESCENDING THROUGH 27,000 FEET. DECLARED EMERGENCY, MASKS DROPPED. DIVERTED TO TPA. REPLACED LEFT AUG VALVE ANTICIPATOR. GROUND RUN PERFORMED, SYSTEM CHECKS SATISFACTORY. (M)SDR GTIA96NK150Thermostat · malfunctionedCABIN PRESSURIZATION FAILURE DESENDING THROUGH 27000 FEET. DECLARED EMERGENCY, MASKS DROPPED. DIVERTED TO TPA. REPLACED LEFT AUG VALVE THERMOSTAT. GROUND RUN PERFORMED. SYTSEM CHECKS SATISFACTORY. (M)SDR ABXA9600423Power Supply · inoperativeEMERGENCY LIGHTS INTERMITTENTLY STAY ON WITH POWER OFF. REPLACED EMERGENCY LIGHT POWER SUPPLY.SDR USAA960346Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN FASTENER HOLES LONGERON 24L STATION 160 AND 200. REPLACED SECTION OF LONGERON BY SPLICING PER SRM 53-02 FIG 2. (M)SDR USAA960345Pan · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .5 INCH CRACK IN FORWARD LEFT OVERWING EMERGENCY EXIT IN DOOR PAN BOTTOM FORWARD NR 5 STOP. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03 AND SRM 52-05 FIG 51. (M)SDR USAA960344Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK AT FASTENER HOLES STATION 160 LONGERON 25L. SPLICED IN NEW SECTION OF LONGERON STATION 150 TO 190 PER SRM 53-02 FIG 2. (M)SDR USAA960343Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN LONGERON 12R AT ATTACH FASTENERS STATION 965. REPLACED SECTION OF LONGERON BY SPLICING PER USAIR TYPICAL REPAIR 53-10-17. (M)SDR USAA960342Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN LONGERON 4L AT STATION 180. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M)SDR USAA960341Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACKS AT FASTENER HOLES LONGERON 23L STATION 180 AND STATION 200. SPLICED IN SECTION OF LONGERON FROM STATION 160 TO STATION 230 PER SRM 53-02 FIG 2. (M)SDR USAA960340Belt Frame · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND A .25 INCH CRACK AT FASTENER STA 180, BELT FRAME LONGERON 23L. INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-03, FIGURE 4. (X)SDR USAA960339Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND 1 INCH CRACK IN LONGERON 17L, AT STATION 945. SPLICED IN LONGERON SECTION PER USAIR TYPICAL REPAIR 53-10-17. (M)SDR USAA960338Cusp Membrane · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND TWO 2 INCH CRACKS IN CUSP MEMBRANE STATION 617 RIGHT SIDE. REPLACED SECTION OF CUSP MEMBRANE FROM STATION 598 TO 637 PER SRM 53-05 FIG 97. (M)SDR USAA960337Skin · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND 1.5 INCH CRACK UPPER LEADING EDGE SURFACE HORIZONTAL STABILIZER LEFT SIDE APPROXIMATELY 6 FEET OUTBOARD OF VERT STAB. INSTALLED DOUBLER REPAIR .071 2024TS ALU PER SRM 55-03 FIG 3 AND SRM 55-01 FIG 2. (M)SDR 9607259903Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR UPPER AFT BEAM END FITTING. REPLACED FITTING.SDR 9607169956Wire · chafedDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 7 AND 12 INOPERATIVE. FOUND CHAFED WIRES INSIDE SIDEWALL AT ROW 12. REPAIRED WIRES AND OPERATIONAL CHECK NORMAL.SDR 96ZZZX2791Filler · corrodedLEFT WING TEE CAP OUTBOARD HORIZONTAL LEG CORRODED. REMOVED CORROSION, INSTALLED REPAIRS IAW DC-9 SB 37-98 PER DRAWINGS NR 5932267 AND NR 593226 AND DC-9 SRM'S 51-10-3, 51-30-5, AND DC-9 MM 20-30-0. REF: NR 060N1-0001 AND NR 060F1-0002.SDR 96ZZZX2790Clips · corrodedLEFT WING TEE CAP OUTBOARD HORIZONTAL LEG CORRODED. REMOVED CORROSION, INSTALLED REPAIRS IAW DC-9 SB 57-98 PER DRAWINGS NR 5932267 AND NR 593226 AND DC-9 SRM'S 51-10-3, 51-30-5, AND DC-9 MM 20-30-0. REF: NR 060N1-0001 AND NR 060F1-0002.SDR 9607029996Vent Valves · openFUEL BEGAN VENTING FROM THE RIGHT WING AFTER TAKEOFF. THE LEFT FUEL QUANTITY DROPPED 800 LBS BELOW RIGHT SIDE. BOTH FUEL QUANTITIES WERE BELOW 8,800 LBS. FLIGHT RETURNED TO YUL AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET CLIMB VENT VALVES.SDR USAAD96033ABolts · missingYOW - FL 1171 - UPON GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT FAILED TO EXTINGUISH. NOISE FROM THAT AREA INDICATED THAT THE DOORS WERE NOT CLOSED. FLIGHT RETURNED TO YOW AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND TWO BOLTS MISSING FROM THE NOSDR 9607019960Evac Slide · low pressureDURING PERIODIC CHECK, FOUND TAILCONE EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE.SDR USAAD96032Line · crimpedPIT - FL 441 - AFTER TAKEOFF FROM PIT AND REACHING 6000 FEET, CREW COULD NOT PRESSURIZE THE AIRCRAFT. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A CRIMPED SENSE LINE TO THE PRESSURE CONTROLLER. LINE WAS REPLACED AND REPOSISDR 9607149903Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE LONGERON 30 SPLICE FITTING AT FS 570. REPLACED SPLICE PER SRM 51-30-2.
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