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 9612139981Power Supplies · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLIES, OPERATIONAL CHECK NORMAL.SDR 9612129981Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.SDR 9612059910Windshear Warn · activatedWINDSHEAR WARNING ACTIVATED DURING TAKEOFF ROLL. ABORTED TAKEOFF AT 110 KNOTS AND RETURNED TO GATE. MAINTENANCE DEFERRED WINDSHEAR SYSTEM PER MEL 34-44A.SDR 9612049928Uplock Switch · malfunctionedRIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH SAME RESULTS, FLIGHT CONTINUED TO DESTINATION AT 10,000 FEET AND 250 KNOTS AIRSPEED. MAINTENANCE PERFORMED GEAR SWING AND PROBLEM COULD NOT BE DUPLICATED. REPLACEDSDR 9612599907Fitting · crackedDURING M-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR UPPER LEFT DOOR STOP FITTING. REPLACED FITTING PER SRM 51-10-2.SDR 9612149960Batteries · dischargedDURING PERIODIC CHECK, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.SDR USAAD96070Battery Pack · dishargedFORWARD AISLE EMERGENCY LIGHTS AND EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK. (X)SDR USAAD96067Switch · failedLGA/RDU - FLT 1507 - ON APPROACH, FLAPS WOULD NOT GO TO 25 DEGREES WITHOUT HORN SOUNDING. GEAR WAS DOWN. REPLACED FLAP SWITCH S1-85. ALSO, REPLACED DISCONNECT P1-227. (X)SDR 9612559965Fittings · crackedDURING M-CHECK, FOUND TWO CRACKED BEAM END FITTINGS IN THE AFT CARGO DOOR, NR 5 FORWARD END AND NR 2 AFT END. REPLACED FITTINGS.SDR USAAD96069Battery Pack · dischargedLEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK. (X)SDR USAAD96066Battery Pack · dischargedLEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK. (X)SDR ABXA9600574Bulkhead Doubler · double drilledDURING C-CHECK INSPECTION, FOUND A DOUBLE DRILLED HOLE ON THE AFT PRESSURE BULKHEAD ABOVE THE RIGHT UPPER CORNER OF THE VENTRAL DOOR. REPAIRED IAW ABX REA D953-15423-MR.SDR ABXA9600572Skin · oil canningDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN OIL CANNING BELOW THE NR 2 PYLON AT STA 996 TO 1019. REPAIRED IAW ABX REA D953-15411-MR.SDR ABXA9600564Bulkhead Doubler · crackedDURING C-CHECK INSPECTION, FOUND CRACKED AFT PRESSURE BULKHEAD STIFFENER DOUBLER BETWEEN LONGERONS 15L AND 16L. REPLACED IAW DC-9 SRM 51-30-5.SDR 9612549902Fitting · crackedDURING H-CHECK, FOUND CRACKS IN THE AFT CARGO DOOR NR 5 BEAM END FITTING, FORWARD SIDE AND IN THE HINGE SPRING BOLT DOOR FITTING. REPLACED FITTINGS.SDR 9612529905Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE FOLLOWING KEEL LONGERON END FITTINGS AT FS 600, 28L, 29L AND 28R. REPLACED END FITTINGS PER SRM 51-30-2.SDR USAAD96064Aoa Vane · failedCLT/FAY - FLT 1527 - STALL INDICATION FAILURE WARNING ILLUMINATED ON DEPARTURE. FLIGHT RETURNED TO CLT. ON APPROACH, LIGHT EXTINGUISHED. REPLACED LEFT AND RIGHT AOA VANES. (X)SDR USAA960438Angle · crackedPIT - DURING Q-4 CHECK INSPECTION, FOUND 2 INCH CRACK IN DRAG ANGLE RADIUS RT VERTICAL STABILIZER. DRAG ANGLE STA 1089. INSTALLED REPAIR ANGLE PER SRM 53-05, FIGURE 23. (X)SDR 9612519902Fitting · crackedDURING H-CHECK, FOUND CRACKS IN THE FORWARD CARGO DOOR AFT SUPPORT ANGLE FITTING AND ANGLE CLIP. REPLACED FITTING AND CLIP.SDR 9612509905Skin · corrodedDURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN INNER SURFACE FROM FS 598 TO 680, LONGERON 30 TO 27R. REPLACED SKIN PER SRM 51-30-2 AND 51-30-5.SDR 9612039915Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND CABIN CEILING EMERGENCY LIGHTS AT ROWS 14 THROUGH 19 INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.SDR 9612029905Battery Pack · dischargedDURING PERIODIC CHECK, LEFT NACELLE EMERGENCY LIGHT FAILED TEN MINUTE TEST. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR 9612009995Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.SDR 9611829944Air Distr · smokeDURING INITIAL CLIMB-OUT, FLIGHT ATTENDANT REPORTED SMOKE SMELL IN AFT CABIN. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED COCKPIT, GALLEY, LAVATORIES, AFT ACCESSORY COMPARTMENT, E/E COMPARTMENT, FORWARD ACCESSORY COMPARTMENT, ANSDR USAAD96063Windshield · crackedPIT/MKE - FLT 410 - CAPTAIN'S WINDSHIELD DEVELOPED SMALL CRACK IN LOWER LEFT CORNER AND SPREAD RAPIDLY. ARCING AND DELAMINATIONS STARTED TO FOLLOW CRACKS. DIVERTED TO LAN. REPLACED CAPTAIN'S WINDSHIELD. (X)SDR 9612789905Frame · corrodedDURING H-CHECK, FOUND CORROSION ON THE FS 218 FRAME BETWEEN LONGERONS 27L TO 27R. REPAIRED FRAME (P/N 9911520-385) PER EA 99-109117.SDR 9612499905Bulkhead Doubler · crackedDURING H-CHECK, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD -13 DOUBLER AT THE UPPER LEFT DOOR STOP SUPPORT FITTING PROPAGATING TOWARDS THE LIGHTENING HOLE. REPAIRED PER JO60088 -533, -537 AND SRM 51-30-5.SDR 9612489905Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE RIGHT KEEL FORMER TO LONGERON 29R FITTING. REPLACED FITTING PER SRM 51-30-5.SDR 9611869990Unsafe Light · illuminatedNOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SEVERAL GEAR SWINGS. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE.SDR 9611849993Uplimit Sw · malfunctionedNOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON APPROACH INTO MSP. COCKPIT OPERATING MANUAL PROCEDURES WERE PERFORMED AND AIRCRAFT LANDED WITHOUT INCIDENT. NOTE: EMERGENCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAUTION. MAINTENANCE CLEANED TERMINASDR 9611949972Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT TAIL COMPARTMENT CATWALK INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.SDR 9611929966Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.SDR 9611799905Fittings · crackedDURING H-CHECK, FOUND CRACKS ON THE LEFT KEEL FITTINGS AT FORMERS FS 617 AND 637. REPLACED FITTINGS PER SRM 51-30-2 AND 51-30-5.SDR 9611499958Seal · contaminatedDURING FLIGHT, A LOUD AIR LEAK FROM THE AFT CABIN PLUG DOOR, AIRCRAFT PRESSURIZATION WAS NORMAL. RETURNED TO DTW WITHOUT FURTHER INCIDENT. REMOVED INSULATION FROM THE PLUG HATCH SEAL.SDR 9612779905Frame · corrodedDURING H-CHECK, FOUND CORROSION ON THE FS 980 FRAME BETWEEN LONGERONS 27R TO 28R. REPAIRED FRAME (P/N 9958238-23) PER EA 99-109127.SDR 9612769905Skin · crackedDURING H-CHECK, FOUND A CRACK IN AN EXISTING FUSELAGE SKIN REPAIR AT FS 464 BETWEEN LONGERONS 22L TO 23L. REPAIRED SKIN (P/N 5911410-63) PER EA 99-109147.SDR 9612749905Frame · corrodedDURING H-CHECK, FOUND CORROSION ON THE FS 965 FRAME BETWEEN LONGERON 29L TO 30. REPAIRED FRAME (P/N 9912243-105) PER EA 99-109128.SDR 9611959979Fuse · failedDURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS AND GALLEY DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE AT GALLEY DOOR, OPERATIONAL CHECK NORMAL.SDR USAAD96062Trim Motor · failedPIT/EWR - FLT 936 - PRIMARY TRIM DOES NOT TRIM FORWARD. RETURNED TO FIELD. REPLACED PRIMARY TRIM MOTOR AND TRIM BRAKE RELAYS. (X)SDR ABXA9600567Skin · gougedDURING C-CHECK INSPECTION, FOUND GOUGE IN THE FUSELAGE SKIN AT STATION 332, LONGERON 23R. REPAIRED IAW ABX REA D953-15370-MR.SDR ABXA9600566Clip · crackedDURING C-CHECK INSPECTION, FOUND CRACKED CLIP AT CUSP WEB TO FRAME STA 996 AT LONGERON 18L. REPLACED CLIP IAW DC-9 SRM 51-10-4 AND 51-30-5.SDR ABXA9600565Bulkhead Clip · crackedDURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD STIFFENER ATTACH CLIP CRACKED AT LONGERON 14R. REPLACED IAW DC-9 SRM 51-30-5.SDR 9612739905Skin · corrodedDURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN UPPER SURFACE IN THE LEFT WHEEL WELL KEEL AREA FS 680 TO 756. REPLACED SKIN PER (P/N 5911418-111) PER EA 99-109056.SDR 9611939969Fuse · failedDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT FIRST CLASS AND GALLEY DOOR INOPERATIVE. REPLACED FUSE, OPERATIONAL CHECK NORMAL.SDR 9611919955Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR 9611479903Vent Valve · stuck openFUEL BEGAN VENTING FROM RIGHT WING AFTER TAKEOFF. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE TRANSFERRED FUEL INTO CENTER TANK AND RAN ALL SIX PUMPS WITH CROSSFEED VALVE OPEN. NO TRANSFERRING OF FUEL WAS NOTED. FOUND DEBRIS IN LEFT TANSDR USAAD96060Wire · looseCLT - ON GROUND, EMERGENCY LIGHTS ARM AND CHARGE, CIRCUIT BREAKER TRIPS. SECURED LOOSE WIRE IN FLOOR LIGHTING, ROW 20. (X)SDR ABXA9600562Bracket · crackedDURING C-CHECK INSPECTION, FOUND RIGHT FLAP BRACKETS CRACKED AT STA 353. REPLACED IAW DC-9 SRM 51-30-2.SDR ABXA9600561Bracket · crackedDURING C-CHECK INSPECTION, FOUND RIGHT FLAP BRACKETS CRACKED AT STA 353. REPLACED IAW DC-9 SRM 51-30-2.SDR 96ZZZX3046Power Supply · failedPOWER SUPPLY FOR EXIT ID FAILED DUE TO EXPOSURE TO CHEMICAL ACTION FROM HYDRAULIC FLUID. SUBMITTER STATED DEVICE IS NOT DESIGNED FOR THIS TYPE OF EXPOSURE AND NEEDS TO BE REDESIGNED FOR TAIL CONE MOUNTING.
Back to Douglas DC-9-31