Boeing 737-322
Service difficulty reports · 4,751
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 = '737322' 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 = '737322' 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 2005UALA00286Crease Beam · corrodedAFT CABIN CREASE BEAM RBL 57, WL 208.1 CORRODED IN NUMEROUS LOCATIONS FROM STA 947.5 TO STA 990. REPLACED CREASE BEAM.SDR 2005UALA00276Pressure Panel · crackedLEFT STA 664 PRESSURE DECK WEB IS CRACKED AT APPROXIMATELY LBL 30 JUST FWD OF OUTBOARD AILERON TOWER SHAFT. MAJOR REPAIR ACCOMPLISHED. CUT OUT CRACK, FABRICATED AND INSTALLED A DOUBLER REPAIR.SDR 2005UALA00275Skin · gougedFWD CARGO DOOR CUTOUT FWD EDGE IS GOUGED AT STR 24R. MAJOR REPAIR ACCOMPLISHED. BLENDED DAMAGE AND INSTALLED DOUBLER REPAIR.SDR 2005UALA00274Skin · wornUPPER FUSELAGE SKIN WORN AT STA 868 AT LBL 5 INCHES FROM DORSAL FIN SEAL WEAR. REPAIR STRAPS, FILLERS AND WEAR STRIP INSTALLED EXTERNAL SKIN AT DORSEL FIN SEAL AREA.SDR 2005UALA00273Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 787 STRINGER 21 RIGHT. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED STRINGER CLIP.SDR 2005UALA00272Frame · crackedSTA 616 FRAME IS CRACKED BELOW STR 17L. MAJOR REPAIR ACCOMPLISHED. TRIMMED DAMAGE AND INSTALLED REPAIR ANGLE.SDR 2005UALA00270Floorbeam · corrodedAFT CABIN FLOORBEAM T-CAP HAS CORROSION AT STA 967 LBL 17 TO RBL 12. REPLACED TEE CAP.SDR 2005UALA00269Floorbeam · corrodedCABIN FLOORBEAM UPPER SURFACE LIGHT CORROSION AT STA 312 AT RBL 8 WL 208. REPLACED TEE CHORD.SDR 2005UALA00268Floorbeam · corrodedAFT CABIN FLOORBEAM STA 986 RBL 16 TO RBL 28 WL 208 IS CORRODED. REPAIR ANGLE AND FLOOR BEAM T-CAP REPLACED.SDR 2005UALA00263Light · damagedFORWARD GALLEY EEL LIGHT INOP. REPLACED FWD GALLEY EEL LIGHT STRIP.SDR 2005UALA00264Wire · damagedFLOOR EEL LIGHTS ARE INOP FROM SEAT 15ABC TO 21ABC. *S/D* REPLACED EEL CABLE AND EEL LIGHT.SDR 2005UALA00257Overheat Loop · malfunctionedRETURNED TO ORD DUE TO NR 2 ENGINE OVERHEATED AND SHUTDOWN. CREW REPORTED NR 2 ENGINE OVERHEAT INDICATION AT CLIMB. CREW SHUT DOWN NR 2 ENGINE PER QRC. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM. FOUND NR 2 ENGINE CORE DETECTOR M1122, LOOPSSDR 2005UALA00246Frame · damagedUPPER FRAME LT SIDE STA 178 HAS LOW EDGE DISTANCE. FABRICATED AND INSTALLED A REPAIR CHORD SPLICE ANGLE, PICKING UP AN ADDITIONAL FASTENER LOCATION.SDR 2005UALA00244Generator · failedRETURNED TO FIELD DUE TO A LOST NR 1 ENGINE GENERATOR. FOUND THE CSD OVERSERVICED, AND THE DELTA P INDICATOR POPPED. METAL SHAVINGS WERE FOUND IN THE FILTER BOWL, SO CSD OIL SYSTEM WAS FLUSHED AND SERVICED. BOTH THE CSD AND GENERATOR WERE REPLACED.SDR 2005UALA00236Skin · dentedFOUND DENT IN HORIZONTAL STAB RT SIDE ABOUT 2 FEET IN FROM TIP. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR.SDR 2005UALA00235Skin · dentedDENT WITH SHARP BOTTOM ON RT SIDE OF FUSELAGE 36 INCHES BEHIND DOOR 1R AND 30 INCHES BELOW WINDOWS. DENT IS 1 INCH X 1 INCH WITH A 0.25 INCH CREASE, 0.65 INCH DEEP. CUT AND REMOVED DAMAGED, AND INSTALLED DOUBLER AND FILLER REPAIR.SDR 2005UALA00200Bear Strap · damagedAFT CARGO DOOR AFT LOWER CORNER BEAR STRAP DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR.SDR 2005UALA00192Seal · tornUNABLE TO PRESSURIZE THE AIRCRAFT. DOOR 1L LEAKING. SEAL TORN BY LOWER HINGE AREA. REPLACED LOWER HINGE SEAL. REPLACED L1 DOOR SNUBBER. ADJUSTED DOOR STOPS.SDR 2005UALA00186Sill · corrodedAFT PIT SIL BEAM UPPER STRAP HAS CORROSION FROM STA 847-787. REPLACED STRAP.SDR 2005UALA00184Pressure Panel · crackedSTA 664 PRESSURE DECK IS CRACKED AT APPROXIMATELY LBL 30. ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2005UALA00183Floorbeam · corrodedCORROSION ON FWD LT CABIN FLOORBEAM AT STA 294.5 LBL 37-53. ACCOMPLISHED. BLENDED OUT DAMAGE AND INSTALLED ANGLE/STRAP REPAIR.SDR 2005UALA00158Connector · disconnectedEEL STRIP AT AFT GALLEY INOPERATIVE. FOUND POWER SOCKET DISCONNECTED. CONNECTED SOCKET.SDR 2005UALA00136Relay · failedAFTER TAKEOFF GEAR HANDLE WOULD NOT GO UP AND TAKEOFF WARNING HORN SOUNDING. REPLACED R276 RELAY AND ADJUSTED SAFETY SENSOR TARGET. PERFORMED EXTENSION AND RETRACTION CHECK OF THE LANDING GEAR. OPERATIONS CHECK GOOD.SDR 2005UALA00128Frame · crackedFWD CARGO DOOR CUTOUT FRAME CRACKED AT FWD LOWER STOP. MANUFACTURED AND INSTALLED REPAIR ANGLE DOUBLER.SDR 2005UALA00113Relief Valve · out of adjustFLIGHT DIVERTED TO CMH DUE TO LOSS OF CABIN PRESSURE. THE INBOARD SAFETY RELIEF VALVE FAILED OPERATIONAL TEST AND WAS REPLACED. THE CABIN PRESSURE CONTROLLER WAS ALSO REPLACED PRECAUTIONARY.SDR 2005UALA00114Skin · dentedRT HORIZ LEADING EDGE DENT APPROX 7 FT FROM INBOARD EDGE. DENT IS APPROX 5 INCHES IN LENGTH, 1.5 INCH WIDE AND .125 IN DEPTH. REPAIR ACCOMPLISHED. INTERIM DOUBLER REPAIR REPLACED WITH PERMANENT FLUSH REPAIR.SDR 2005UALA00107Skin · dentedVERTICAL STAB LEADING EDGE IS DENTED AT L/E STA 104. REMOVED DENT DAMAGE AND INSTALLED DOUBLER REPAIR.SDR 2005UALA00106Floorbeam · corrodedCABIN FLOORBEAM HAS CORROSION REMOVAL BEYOND LIMITS AT STA 967 LBL 18. INSTALLED STRAP REPAIR.SDR 2005UALA00104Unknown · unknownRETURNED TO SFO DUE TO PRESSURIZATION PROBLEM. FOUND EXCESSIVE LEAK AROUND E&E COMPARTMENT DOOR. REPLACED E&E COMPARTMENT DOOR SEAL.SDR 2005UALA00103Controller · failedAT 32,000 FEET CABIN, FLIGHT MADE EMERGENCY DESCENT FROM 32,000 TO 15,000 DUE TO CABIN PRESSURE PROBLEM. CABIN PRESSURE CONTROLLER FAILED. REPLACED CONTROLLER.SDR 2005UALA00090Light · inoperativeAFT CABIN EEL LIGHTS INOP FROM ROWS 15 TO AFT GALLEY. REPLACED EEL CABLE AND MISSING END CAP.SDR 2006UALA00125Rivet · crackedCRACKED RIVETS. REPLACED RIVETS REF SRM 51-40-02 & 53-00-01.SDR 2005UALA00084Indicator · malfunctionedABORTED TAKEOFF DUE TO F/O AIR SPEED INDICATOR. REPLACED FIRST OFFICERS AIR SPEED INDICATOR.SDR 2005UALA00078Skin · dentedSTA 341-359 HAS 3 DENTS ABOVE STR 21R. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR.SDR 2005UALA00077Skin · dentedLT FUSE SKIN IS DENTED AT STA 897 BETWEEN STR 24L AND 25L. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. CUT-OUT DAMAGE AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLER.SDR 2005UALA00076Pressure Panel · crackedSTA 664 PRESSURE DECK HAS 2 CRACKS AT LBL 30. CUT-OUT WEB AND INSTALLED SPLICE REPAIR.SDR 2005UALA00057Keelbeam · crackedKEEL BEAM LOWER CHORD BS 685-695 IS CRACKED. TRIMMED OUT CRACKED LOWER CHORD. INSTALLED REPAIR ANGLE AND STRIP.SDR 2005UALA00056Floorbeam · corrodedSTA 947 FLOORBEAM HAS MATERIAL LOSS FROM CORROSION AT LBL 4. REMOVED CORROSION INTALLED REPAIR STRAP.SDR 2005UALA00055Frame · crackedSTA 616 FRAME INNER CHORD IS CRACKED FROM BOTTOM FASTENER BELOW STR 17 LT. CUT-OUT DAMAGE AND INSTALLED ANGLE DOUBLER.SDR A6WA200440204Keelbeam · crackedKEEL BEAM LOWER CHORD BS 685-695 IS CRACKED. TRIMMED OUT CRACKED LOWER CHORD. INSTALLED REPAIR ANGLE AND STRIP.SDR MAMA040915Door · leakingAIRCRAFT RETURNED WITH CABIN PRESSURE PROBLEM.SDR 2005UALA00025Seal · leakingAIRCRAFT RETURNED WITH CABIN PRESSURE PROBLEM. SEAL REPLACED AND RIGGED THE FORWARD CARGO DOOR.SDR 2006UALA00010Light · inoperativeEEL FLOOR LIGHTING IN FIRST CLASS IS INOP.SDR 2005UALA00026Sensing Element · damagedCREW REPORT NR 1 ENG -A- OVERHEAT LIGHT ILLUMINATED. *S/D* CREW REPORTED NR 1 ENGINE -A- LOOP OVERHEAT LIGHT ILLUMINATED. SHUTDOWN ENGINE AND DISCHARGED BOTH FIRE EXTINGUISHER BOTTLES. OVERHEAT DETECTION LOOP -B- WAS INOPERATIVE AND DEFERRED, ELIMINATING RSDR 2005UALA01298Warning System · activatedABORTED TAKEOFF AT 100 KNOTS DUE TO WINDSHEAR WARNING INDICATION. REPLACED EMERGENCY LIGHT ON SEAT 42R.SDR 2005UALA00008Warning System · activatedABORTED TAKEOFF AT 100 KNOTS DUE TO WINDSHEAR WARNING INDICATION. OPS CHECK OF WEATHER RADAR TRANSCEIVER PERFORMED, AND NO FAULT FOUND.SDR 2004UALA01256Skin · dentedVERTICAL FIN L/E SKIN HAS A DENT AT LES 132. DENT IS 1.55 BY 0.046 INCH DEEP. DENT IS A ZONE 3 DENT. INSTALLED FLUSH REPAIR.SDR 2004UALA01251Windshield · crackedDIVERTED DUE TO FIRST OFFICER'S WINDSHIELD CRACKED. WINDOW HEATING ELEMENT ARCED. REPLACED WINDOW.SDR 2004UALA01249Smoke · detectedFLIGHT ATTENDANT SAW SMOKE COMING FROM AFT GALLEY TRASH COMPACTOR AREA. LINE MAINTENANCE ACCOMPLISHED A DETAILED INSPECTION AND OPERATIONAL CHECK ON THE SUSPECT TRASH COMPACTOR. NO EVIDENCE OF SMOKE WAS FOUND ON THE DETAILED INSPECTION, AND A SUBSEQUENT OPERASDR 2004UALA01244Switch · malfunctionedGEAR WOULD NOT RETRACT AFTER TAKEOFF. FLIGHT DIVERTED. A FAILED S106 LANDING GEAR SAFETY SWITCH CAUSED THE AIRCRAFT TO REMAIN IN THE GROUND MODE, RESULTING IN THE GEAR FAILING TO RETRACT. THE S106 LANDING GEAR SAFETY SWITCH WAS REPLACED AND THE LANDING GEAR
Back to Boeing 737-322