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 2004UALA01232Gcu · malfunctionedDIVERTED TO TWF (TWIN FALLS, ID) DUE TO LEFT GENERATOR BUSS FAILURE. AIRCRAFT EXPERIENCED ELECTRICAL FAILURE WHILE CLIMBING. NR 1 GEN OFF BUS LIGHT WITH ASSOCIATED "BUSS OFF" LIGHT ILLUMINATED. TRANSFER BUS LIGHT DID NOT ILLUMINATE BUT HAD BOTH LT TANK FUELSDR 2004UALA01231Fan · failedLANDED UNDER AMBER ALERT DUE TO REPORTED SMOKE IN CABIN. FOUND EQUIPMENT COOLING NORMAL FAN FAILED. REPLACED NORMAL FAN.SDR 2004UALA01216Light · inoperativeAFT EMERGENCY FLOOR EEL LIGHTS INOP FROM MID TO AFT OF AIRCRAFT. REPLACED EEL LIGHTS MID TO AFT GALLEY.SDR 2004UALA01214Light · looseEMERGENCY EXIT FLOOR LIGHTS AT ROW 12 HAVE BEEN PULLED UP. REPLACED DAMAGED EEL STRIP.SDR 2004UALA01203Slide · deployedDURING SERVICING, CATERERS REPORTED THAT THE DOOR 1R WAS OPEN AND HAD THE SLIDE PARTIALLY DEPLOYED. THE DOOR WAS NOT DISARMED. CAUSE IS UNKNOWN. A SLIDE COMPARTMENT (CLAMSHELL) LATCH WAS FOUND OPENED DURING INSPECTION. WHETHER THE LATCH WAS OPENED WHILE ISDR 2004UALA01202Transmitter · malfunctionedRETURNED TO GATE AFTER 90 KNOT ABORTED TAKEOFF DUE TO OIL PRESSURE INDICATION. ENG 2 OIL PRESSURE WENT TO ZERO. REPLACED NR 2 OIL PRESSURE INDICATOR, OIL TEMPERATURE INDICATOR AND OIL PRESSURE TRANSMITTER. RAN ENGINE AND OPS CHECKED OK. THEN ON DEC 15, OILSDR 2004UALA01184Warning Light · activatedFLIGHT RETURNED TO DEN DUE TO B-SYSTEM HYDRAULIC PRESSURE LIGHT. PROBLEM COULD NOT BE REPEATED ON GROUND. OPS CHECKED OK. NO UNITS REPLACED.SDR 2004UALA01173Overheat Loop · failedDIVERTED TO SLC DUE TO WING BODY OVERHEAT INDICATION. DISCREPANCY FOUND TO BE NR 2 ENGINE, STRUT CAVITY OVERHEAT DETECTOR ELEMENT FAULT. REPLACED OVERHEAT DETECTOR SENSING ELEMENT OF NR 2 ENGINE STRUT CAVITY .SDR 2004UALA01164Proximity Sensor · malfunctionedRETURNED TO DEN, DUE TO A GEAR IN TRANSIT LIGHT PROBLEM. INDICATION WAS CAUSED BY FAULTY GEAR DOWN LOCK PROXIMITY SWITCH. REPLACED GEAR DOWN LOCK SWITCH. PERFORMED OPERATIONAL AND FUNCTIONAL CHECK OF THE SYSTEM. GEAR OPEARTION AND INDICATION FOUND NORMAL.SDR 2004UALA01149Overheat Loop · failedDIVERTED TO PIT DUE TO WING BODY OVERHEAT INDICATION. DISCREPANCY FOUND TO BE NR 2 ENGINE, STRUT CAVITY OVERHEAT DETECTOR ELEMENT FAULT. REPLACED OVERHEAT DETECTOR SENSING ELEMENT OF NR 2 ENGINE STRUT CAVITY .SDR 2004UALA01172Cylinder · damagedSQUIB FIRED A HOLE STRAIGHT THROUGH THE CYLINDER. FIRE EXTINGUISHER BOTTLE AND CARTRIDGE WERE SUBJECTED TO AN ABNORMALLY HIGH AMBIENT TEMP, NOT CONSISTENT WITH THE DESIGN PARAMETERS OF BOTH UNITS, AND THEY FUNCTIONED AS EXPECTED. THE ELEVATED AMBIENT TEMPERATUSDR 2004UALA01138Light · inoperativeLAST 6 ROWS OF EMERGENCY FLOOR LIGHTING INOP. REPLACED POWER STRIP FOR AFT SET OF FLOOR LIGHTS. CHECKS GOOD.SDR 2004UALA01128Wire · failedEEL LIGHTS INOPERATIVE FROM SEATS 17 TO AFT GALLEY. REPLACED FLOOR FEEDER CABLE FOR EEL LTS FROM ROW 17 BACK.SDR 2004UALA01112Skin · crackedFWD GALLEY DOOR EXT SKIN IS CRACKED AT THE LWR HINGE CUTOUT. TRIMMED OUT DAMAGE AND INSTALL REPAIR DOUBLER.SDR 2004UALA01121Bear Strap · damagedAFT CARGO DOOR BEAR STRAP REPAIR NEEDS TO BE REPLACED AT BS 847 STR. 23R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR 2004UALA01120Bear Strap · damagedREPAIR AT AFT CARGO DOOR BEAR STRAP BS 807 ABOVE STR 25 RT AT CARGO DOOR OPENING IS INSUFFICIENT. FABRICATED EXTERNAL DOUBLER,TRIPLER AND FILLER AND INSTALLED,SDR 2004UALA01133Slide · dislodgedDOOR 1L SLIDE HAS SLID DOWN FROM ITS MOUNT. UNIT WAS INSPECTED AND FOUND TO BE OK. SLIDE WAS REINSTALLED.SDR 2004UALA01126Wire · failedEMERGENCY EEL LIGHTS ROWS 15ABC TO 21ABC ARE INOPERATIVE. REPLACED LOWER FEEDER WIRE.SDR 2004UALA01041Overheat Loop · malfunctionedDIVERTED TO COS DUE TO WING BODY OVERHEAT INDICATION. EXPERIENCED RIGHT WING BODY OVERHEAT WARNING IN FLIGHT WITH ENGINE SUPPLYING AIR. ISOLATED TO RIGHT WING LEADING EDGE OVERHEAT DETECTOR LOOP M1204. REPLACED OVERHEAT DETECTOR LOOP M1204. SYSTEM OPERATIOSDR 2004UALA01038Duct · failedSKIN, STRINGER AND FRAME HEAT DAMAGE FROM FS 516.5 TO 540. STR 26 TO 28. SUPPLEMENTAL DATA UPDATE - MIX MUFF DUCT OF DUCT ASSEMBLY LOCATED IN MIX CHAMBER AIR DISTRIBUTION BAY AT APPROXIMATE STA 540, BL 0 BLOWN CAUSING HOT AIR TO ESCAPE AND DAMAGE THE STRUCTURSDR 2004UALA01022Frame · crackedFRAME WEB IS CRACKED AT STA 194 AT LBL 16 AND WL 208. FABRICATED AND REPLACED SHEAR WEB.SDR 2004UALA01021Computer · malfunctionedABORTED TAKE OFF AT 80 KNOTS, DUE TO A WINDSHEAR ALERT. EGPWS COMPUTER WAS REPLACED. SUBSEQUENT SHOP TESTING SHOWED NO FAULTS FOUND, AND NO RECORD OF WINDSHEAR WARNING BEING GIVEN.SDR 2004UALA01011Stringer · dentedSTRINGER 13L HAS 2 DENTS AT BS 1025 AND 1030. REMOVED DAMAGED SECTION OF THE STRINGER AND FABRICATED AND INSTALLED STRINGER AND SKIN DOUBLER.SDR 2004UALA01016Sign · malfunctionedEMERGENCY EXIT SIGNS INOP AT LT OVERWING EXIT HATCH, FWD OF LT OVERWING EXIT HATCH AND MID AISLE CEILING AT ROW 10. REPLACED BATTERY PACK FOR ITEM M1134.SDR 2004UALA01013Frame · crackedFUSELAGE FRAME CRACKED AT BS 188 WL 208.1 LT SIDE. INSTALLED REPAIR ANGLE.SDR 2004UALA01012Skin · puncturedNR 1 ENG INLET COWL OUTER SURFACE PUNCTURED-DELAMINATED AT THE 2 O`CLOCK POSITION APPROXIMATELY 30 INCHES FROM FWD END. DAMAGE WAS FOUND ON INLET COWL WAS PERMANENTLY REPAIRED.SDR 2004UALA01014Duct · leakingFUSELAGE SKIN LOCATED DIRECTLY BELOW DUCT ASSY SHOWS SIGNS OF PEELED PAINT DUE TO MIX CHAMBER DUCT ASSY HOT AIR LEAK. MIX MUFF DUCT OF DUCT ASSEMBLY LOCATED IN MIX CHAMBER AIR DISTRIBUTION BAY AT APPROXIMATE STA 540, BL 0 BLOWN CAUSING HOT AIR TO ESCAPE AND DSDR 2004UALA00988Pressure Panel · crackedSTA 664 PRESSURE WEB IS CRACKED AT LBL 31 JUST FWD OF AIL TOWER SHAFT. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.SDR 2004UALA00980Skin · damagedSKIN AT STA 360-380 AND STR 16L-17L IS DAMAGED. INSTALLED DOUBLER AND TRIPLER REPAIR.SDR 2004UALA00981Pin · wornRT MLG TRUNNION PIN HAS CHROME WORN OFF END. REPLACED TRUNNION PIN.SDR 2004UALA00973Light · inoperativeAFT EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK IN CEILING CENTER LEFT SIDE NEAR DOOR 2L.SDR 2004UALA00979Control Cable · misroutedAILERON CONTROL CABLE FRAYED. CABLE GUIDE DAMAGED ON AILERON BUSS DRUM. DAMAGED DUE TO MISROUTING OF CABLE. SUSPECT CABLE WAS MISROUTED DURING HEAVY MAINTENANCE VISIT. BOTH ITEMS REPLACED.SDR 2004UALA00963Squat Switch · malfunctionedDUE TO LOSS OF CABIN PRESSURE, AIRCRAFT DESCENDED TO A LOWER ALTITUDE CAUSING ADDITONAL FUEL BURN. FLIGHT DIVERT- TO BNA FOR ADDITIONAL FUEL. SUSPECTED GND SENSING SQUAT SW M990 FAILED. REPLACED M990 AS PRECAUTION AND ADJUSTED MLG SAFETY SENSOR.SDR 2004UALA00961Indicator · malfunctionedDIVERTED TO MCI DUE TO HIGH ENGINE GAS TEMPERATURE READING IN NR 1 ENGINE. REVIEWED CHRONIC EGT INDICATION HISTORY, ACCOMPLISHED CONTINUITY CHECK FROM EGT CIRCUIT BREAKER TO D442 CONNECTOR AND HAND-OVER-HAND INSPECTION OF WIRING BETWEEN CIRCUIT BREAKER AND INSDR 2004UALA00933Light · inoperativeEMERGENCY LIGHTS AT REAR OF AIRCRAFT INOP EEL STRIP. REPLACED AFT EEL STRIP.SDR 2004UALA00931Light · inoperativeEMERGENCY EXIT LIGHT AT DOOR 1L AND 2R INOP. REPLACED LAMP.SDR 2004UALA00929Beam · crackedTWO CRACKS WERE DISCOVERED AT THE FWD END OF THE LWR BEAM OF THE AFT CARGO DOOR. ONE CRACK AT A FASTENER HOLE IN THE VERTICAL FLANGE OF THE OUTBOARD TEE CHORD AND THE OTHER AT THE FASTENER HOLE IN THE WEB. THE TEE CHORD CRACK IS 0.375 INCH LONG AND WEB CRACKSDR 2004UALA00889Planetary Gear · wornDIVERTED UNDER AMBER ALERT WITH NR 2 ENGINE MOVED TO IDLE DUE TO NR 2 GENERATOR PROBLEM. REPLACED CSD AND CSD OIL COOLER. SHOP FOUND A WORN PLANETARY GEAR USED FOR INTERNAL CSD LUBRICATION.SDR 2004UALA00854Slide · dislodgedDOOR 1 LEFT SLIDE PACK FELL OUT. GIRT BAR DISENGAGED FROM GIRT BAR RETAINERS (CLIPS USED FOR STOWING GIRT BAR WHEN SLIDE IS DISARMED) ON SLIDE COMPARTMENT COVER AND FELL INTO BRACKETS (FLOOR FITTINGS THAT KEEP SLIDE ATTACHED TO AIRCRAFT DURING DEPLOYMENT), RSDR 2004UALA00842Warning Light · illuminatedABORTED TAKEOFF AT 105 KTS AND RETURNED TO GATE DUE TO A FORWARD ENTRY DOOR WARNING. *S/D* DOOR OPERATION NORMAL. SECURED DOOR LIGHT SENSOR TARGET.SDR 2004UALA00835Mec · malfunctionedRETURNED TO ORD WITH NR 2 ENGINE SURGE. REPLACED MAIN ENGINE CONTROL (MEC) AND ENGINE RAN NORMAL. RIGGED THE VSV AND VVB AND TRIMMED.SDR COOSDR040038Skin · delaminatedLT WING, OB AFT FLAP LOWER AND UPPER SKIN DELAMINATED AT WBL 240.SDR 2004UALA00807Control Panel · malfunctionedCARGO FIRE LIGHT FLICKERING ON CARGO SUPPRESSION PANEL. CREW REPORTED THAT CARGO FIRE LIGHT FLICKERING ON CARGO SUPPRESSION PANEL WITH NO OTHER INDICATION OR FAULTS. REMOVED AND REPLACED FIRE DETECTION AND SUPPRESSION CONTROL PANEL. SYSTEM CHECKED NORMAL.SDR 2004UALA00794Proximity Sensor · malfunctionedLANDED DCA UNDER AMBER ALERT DUE TO LEADING EDGE SLAT PROBLEM. *S/D* AMBER INTRANSIT LIGHT ON NR 2 SLAT, OVERHEAD ANNUNCIATOR PANEL STAYS AMBER WITH SLAT DOWN AND LOCKED. SLAT INTRANSIT LIGHT ON FWD INSTRUMENT PANEL ALSO STAYS ON. RAN FLAPS THROUGH FULL CYSDR 2004UALA00786Smoke · detectedACRID SMOKE IN THE CABIN. CHECKED ALL CABIN LIGHTS AND ALL GALLEY EQUIPMENT, RAN BOTH PACKS, RECIRC FAN AND ENG BLEEDS, CHILLERS AND OVENS. VISUAL CHECK FOR HYD AND OIL LEAKS. PERFORMED A VERIFICATION FLIGHT. ALL SYSTEM FOUND NORMAL. SMOKE ODOR COULD NOT SDR 2004UALA00787Fire Detector · malfunctionedAT GATE APU FIRE HANDLE LIGHT ON AND BELL, PULLED HANDLE AND DISCHARGED BOTTLE. INSPECTED THE APU COMPARTMENT AND NO EVIDENCE OF FIRE DAMAGE OR OVERHEAT CONDITION WERE NOTED. RESET APU FIRE HANDLE AND ACCOMPLISHED APU FIRE TEST. SYSTEM TESTED NORMAL. REPLACESDR 2004UALA00785Fire Detector · malfunctionedON TAXI OUT, RECEIVED AN APU FIRE WARNING. MAINTENANCE INSPECTED APU COMPARTMENT AND NO EVIDENCE OF FIRE DAMAGE OR OVERHEAT CONDITION WERE NOTED. INSPECTED APU OVERHEAT DETECTION SYSTEM AND FOUND APU TAILPIPE OVERHEAT DETECTOR LOOP M717 SHORTED TO GROUND. RESDR COOSDR040037Skin · delaminatedLT WING, OB FORE FLAP LOWER AND UPPER SKIN DELAMINATED AT WBL 300 AND AT WBL 210.SDR 2004UALA00781Elevator · malfunctionedRETURNED TO DEN WITH ELEVATOR PROBLEM. NO FAULT HAS BEEN IDENTIFIED WITHIN THE ELEVATOR SYSTEM. THE FOLLOWING ACTIONS WERE TAKEN IN THE COURSE OF TROUBLESHOOTING:1. PITOT LEAK CHECK OF ELEVATOR FEEL SYSTEM. ACCOMPLISHED WITH NO LEAKS FOUND. 2. HORIZONTAL STSDR COOSDR040036Beam · crackedMAIN CARGO, BS 685, LBL 45.5, WL 203.1, STUD BEAM CRACKED.
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