Boeing 737-376
Service difficulty reports · 195
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 = '737376' 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 = '737376' 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 AU510001746Girt Bar · faulty(AUS) DOOR R1 ESCAPE SLIDE GIRT BAR CONTACTING DOOR FRAME.SDR AUS20040494Bolt · sheared(AUS) RT MAIN LANDING GEAR OB STABILIZING FITTING OB LOWER ATTACHMENT BOLT SHEARED ALONG THE SHANK IN AN AREA COINCIDING WITH THE WING REAR SPAR.SDR AUS20040426Windshield · failed(AUS) FIRST OFFICER'S NR 1 WINDOW OUTER PANE SHATTERED ALONG WITH ARCING FROM THE WINDSCREEN.SDR AUS20040423Autopilot Sys · failed(AUS) DUAL AUTOPILOT MALFUNCTION. LIMITED INFORMATION PROVIDED.SDR AUS20040422Tire · damaged(AUS) RT NOSE LANDING GEAR TIRE DAMAGED BY DEBRIS ON RUNWAY. TIRE SHREDDED AND CAUSED DAMAGE TO FORWARD LOWER FUSELAGE SKIN. FOD WAS IDENTIFIED AS THRUST REVERSER BLOCKER DOOR PARTS.SDR AUS20040415Drive Shaft · worn(AUS) NR 4 TRAILING EDGE FLAP TRANSMISSION UNIVERSAL DRIVESHAFT WORN AXIALLY BEYOND LIMITS. END FLOAT WAS APPROXIMATELY 0.406MM(0.016IN) AT OUTPUT END.SDR AUS20040388Generator · failed(AUS) APU GENERATOR FAILED.SDR AUS20040365Oven · faulty(AUS) AFT GALLEY OVEN ELECTRICAL FAULT. INVESTIGATION FOUND FILTERBOARD CAUGHT FIRE DUE TO THE FORMATION OF DRY SOLDER JOINTS ON INDUCTOR CONTACTS.SDR AUS20040330Force Limiter · faulty(AUS) AUTOPILOT WOULD NOT ENGAGE. SUSPECT FAULTY FORCE LIMITER.SDR AUS20040312Bolt · separated(AUS) PASSENGER SEAT SUPPORT BEAM TO AISLE SIDE LEG STRUCTURE BOLTS SEPARATED AND FOUND UNDER SEAT 12 DEF.SDR AUS20040384Indicator · faulty(AUS) FLAP POSITION INDICATOR FAULTY.SDR AUS20040260Stop · faulty(AUS) FOLLOWING LOUD CRACKING NOISES IN FLIGHT AN INSPECTION OF THE DOOR AND DOOR CUTOUT AREA WAS CARRIED OUT. I NVESTIGATION FOUND THE DOOR STOPS HEAVILY WORN AND DRY.SDR AUS20040457Limiter · faulty(AUS) AUTOPILOT TORQUE LIMITER FAULTY.SDR AUS20040192Indicator · failed(AUS) FIRST OFFICER'S AIRSPEED INDICATOR/MACHMETER FAILED.SDR AUS20040182Pin · separated(AUS) L2 OUTER DOOR HANDLE MOVED TO VERTICAL POSITION AFTER DEPARTURE. DURING INVESTIGATION, THE WHOLE HANDLE AND SHAFT ASSEMBLY CAME AWAY FROM THE DOOR. A LOOSE CASTELLATED NUT AND SHIMS WERE FOUND IN THE HOUSING ASSEMBLY. FURTHER INVESTIGATION FOUND A DEFSDR AUS20040172Valve · failed(AUS) NR 2 ENGINE FUEL SYSTEM SPAR VALVE FAILED.SDR AUS20040141Actuator · failed(AUS) FUEL CROSSFEED VALVE ACTUATOR FAILED.SDR AUS20040123Hose · leaking(AUS) RT MAIN LANDING GEAR ACTUATOR UP LINE LEAKING DUE TO CHAFING ON B SYSTEM LOW PRESSURE RETURN LINE. ENGINE DRIVEN PUMP FAILED AND RETURN FILTERS CONTAMINATED.SDR AUS20040098Bearing · seized(AUS) ELEVATOR CONTROL CENTERING UNIT MOUNT BEARING SEIZED.SDR AUS20040097Actuator · cracked(AUS) NR 4 GROUND SPOILER OB ACTUATOR BODY CRACKED AND LEAKING IN AREA NEXT TO RETRACT FITTING.SDR AUS20040080Hydraulic System · leaking(AUS) HYDRAULIC SYSTEM LEAKING.SDR AUS20040042Sensor · out of adjust(AUS) LEADING EDGE FLAP NR 2 EXTEND SENSOR OUT OF ADJUSTMENT.SDR AUS20040198Hydraulic System · contaminated(AUS) HYDRAULIC SYSTEM A FAULTY. ENGINEERING INVESTIGATION SUSPECTS AIR IN HYDRAULIC SYSTEM. LT MAIN LANDING GEAR HYDRAULIC HOSE HAD BEEN REPLACED ON THE PREVIOUS DAY.SDR AUS20040031Hose · burst(AUS) LT MAIN LANDING GEAR DOWNLOCK ACTUATOR HYDRAULIC HOSE BURST. LOSS OF HYDRAULIC FLUID.SDR AUS20040013Engine · overheated(AUS) ENGINE EXCEEDED EGT LIMITS. EGT REACHED 938 DEGREES C.SDR AUS20031125Pipe · chafed(AUS) NOSE LANDING GEAR UP HYDRAULIC PIPE CHAFED AND LEAKING. LOSS OF HYDRAULIC FLUID. SPRAY OF HYDRAULIC FLUID CONTAMINATED E1-3 AVIONICS RACK CONNECTORS D4115P AND D4067P.SDR AUS20031095Brake Assy · faulty(AUS) AUTOBRAKE SYSTEM NOT ARMING. LIMITED INFORMATION PROVIDED.SDR AUS20031076Fire Detector · inoperative(AUS) NR 1 ENGINE FIRE DETECTOR SYSTEM INOPERATIVE.SDR AUS20030996Actuator · binding(AUS) NR 1 ENGINE VARIABLE BLADE VALVE ACTUATORS AT THE 4 O'CLOCK AND 5 O'CLOCK POSITIONS BINDING AND INTERNAL HEXAGONAL DRIVES WORN.SDR AUS20030950Fire Loop · faulty(AUS) NR 1 ENGINE FIRE DETECTION SYSTEM FAULTY. INVESTIGATION FOUND A HIGH RESISTANCE (2000OHMS) SENSOR IN LOOP B'. MEL APPLIED BUT DEFECT OCCURRED DURING NEXT TAKEOFF AND ON SUBSEQUENT FAULT FINDING GROUND RUN. SEE MDR 03/0948 FOR RELATED INCIDENT.SDR AUS20030948Fire Loop · faulty(AUS) NR 1 ENGINE FIRE DETECTION SYSTEM FAULTY. NR 1 ENGINE LOOP `B` FAULTY.SDR AUS20030942Warning Light · intermittent(AUS) NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATING INTERMITTENTLY.SDR AUS20030858Engine · malfunctioned(AUS) NR 1 ENGINE MOMENTARILY LOST POWER. POWER LOSS NOTED ON ENGINE GAUGES AND AIRCRAFT YAWED. NO REOCCURRENCE DURING FLIGHT. VIBRATION NOTICEABLE AT FLIGHT IDLE.SDR AUS20030866Pump · failed(AUS) STANDBY HYDRAULIC PUMP FAILED. PUMP RUNS BUT FAILS TO PRODUCE PRESSURE. SUSPECT FAILED SHAFT.SDR AUS20030829Spar · corroded(AUS) RT WING VENT BOX CORRODED. NR 10 STIFFENER AFT FACE CORRODED IN AN AREA LOCATED BETWEEN WS563 & WS 578 OVER AN AREA APPROX 381MM BY 63.5MM. RT WING UPPER SKIN INNER SURFACE CORRODED BETWEEN WS 557 & 583 IN AN AREA BETWEEN STIFFENER NR 11 & WING REAR SPARSDR AUS20030761Access Panel · leaking(AUS) FUEL LEAKING FROM WING AND RUNNING OVER UPPER SURFACE OF INBOARD FLAPS. INVESTIGATION FOUND THE FUEL LEAKING FROM THE FUEL TANK PANEL ACCESS DOOR AT LOWER WING SKIN CUTOUT NR 7404R LOCATED BETWEEN WBL 157 AND WBL 183.4. THE FUEL TANK CUTOUT HAD BEEN RECESDR AUS20030714Odor · detected(AUS) FUMES WITH SLIGHT SULPHUR ODOR REPORTED BY CABIN CREW AROUND REAR GALLEY AND REAR CABIN VENTS. DURING INVESTIGATION AND GROUND RUNNING THE EQUIPMENT COOLING EXHAUST FAN FAILED AND THE CIRCUIT BREAKER POPPED.SDR AUS20030727Structure · cracked(AUS) AFT CARGO DOOR OUTER TEE STRUCTURE CRACKED IN AFT LOWER CORNER. CRACK WAS LOCATED BETWEEN TWO FASTENERS. CRACK LENGTH APPROXIMATELY 19.05MM (0.75IN).SDR AUS20030674Pmc · faulty(AUS) NR 2 ENGINE LOW POWER. SUSPECT CAUSED BY FAULTY POWER MANAGEMENT CONTROL (PMC).SDR AUS20030707Door Frame · cracked(AUS) DOOR FRAME CRACKED. FORWARD CORNER HAS CRACK INDICATIONS IN FIVEHOLES. AFT CORNER HAS CRACK INDICATION IN ONE HOLE. FOUND DURINGEDDY CURRENT INSPECTION IAW QANTAS ENGINEERING INSTRUCTION733-53-14R4, BOEING SB:737-53-1116 AND CASA AD/B737/24.SDR AUS20030649Sensor · faulty(AUS) RT MAIN LANDING GEAR UPLOCK SENSOR FAULTY.SDR AUS20030640Connector · faulty(AUS) RT ENGINE FIRE DETECTION SYSTEM FAULTY. SUSPECT FAULTY CONNECTOR.SDR AUS20030583Sensor · faulty(AUS) MAIN LANDING GEAR AIR SENSOR S106 FAULTY.SDR AUS20030547Warning Light · illuminated(AUS) FLAP ASSYMETRY PROBLEMS. LIMITED INFORMATION PROVIDED.SDR AUS20030545Attach Fitting · cracked(AUS) FUSELAGE FRAME CLEATS CRACKED. SMALL CRACK IN CLEAT AT UPPER AFT FASTENER HOLE IN BS707 STRINGER 10L. FOUND DURING EDDY CURRENT INSPECTION.SDR AUS20030652Bear Strap · cracked(AUS) FORWARD GALLEY DOOR CRACKED. SEVEN CRACKS FOUND ON FORWARD UPPER CORNER (BEAR STRAP AND INTERNAL DOUBLER) AND ONE CRACK FOUND ON THE AFT UPPER CORNER (BEAR STRAP DOUBLER). FOUND DURING EDDY CURRENT INSPECTION IAW ENGINEERING INSTRUCTION 737-53-14R4.SDR AUS20030468Indicator · false indication(AUS) NR 1 FUEL GAUGE INDICATING FUEL LEAK. INSPECTION COULD FIND NO EVIDENCE OF LEAKS.SDR AUS20030559Frame · cracked(AUS) FUSELAGE FRAME BS 400 CRACKED. CRACK LENGTH 10.16MM (0.4IN). FUSELAGE FRAME BS440 CRACKED. CRACK LENGTH 12.7MM (0.5IN). FRAMES CRACKED AT FLANGE BEND RADIUS BETWEEN S-13R AND S-14R. FOUNDDURING EDDY CURRENT INSPECTION IAW EI 733-53-11 , BOEING NTM PART 6SDR AUS20030415Connector · loose(AUS) APU INOPERATIVE, LIGHT FAULTY. INVESTIGATION FOUND BACKSHELL ON CONNECTOR D4934J LOOSE.SDR AUS20030544Frame · cracked(AUS) FUSELAGE FRAMES CRACKED AT PSU ATTACHMENT POINTS. A TOTAL OF ELEVEN FRAMES CRACKED ON LT SIDE AND SEVEN FRAMES ON THE RT SIDE. FOUND DURING EDDY CURRENT INSPECTION IAW EI 737-53-61R1.
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