Boeing 737-376

Service difficulty reports · 195

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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.

SDR AU510001746Girt Bar · faulty(AUS) DOOR R1 ESCAPE SLIDE GIRT BAR CONTACTING DOOR FRAME.Dec 12, 2005 · Boeing 737376 · Escape SlideSDR 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.May 26, 2004 · Boeing 737376 · FastenersSDR AUS20040426Windshield · failed(AUS) FIRST OFFICER'S NR 1 WINDOW OUTER PANE SHATTERED ALONG WITH ARCING FROM THE WINDSCREEN.May 18, 2004 · Boeing 737376 · Flight Compartment WindowsSDR AUS20040423Autopilot Sys · failed(AUS) DUAL AUTOPILOT MALFUNCTION. LIMITED INFORMATION PROVIDED.May 17, 2004 · Boeing 737376 · Autopilot SystemSDR 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.May 14, 2004 · Boeing 737376 · TireSDR 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.May 13, 2004 · Boeing 737376 · Trailing Edge Flap ActuatorSDR AUS20040388Generator · failed(AUS) APU GENERATOR FAILED.May 9, 2004 · Boeing 737376 · AC Generation SystemSDR AUS20040365Oven · faulty(AUS) AFT GALLEY OVEN ELECTRICAL FAULT. INVESTIGATION FOUND FILTERBOARD CAUGHT FIRE DUE TO THE FORMATION OF DRY SOLDER JOINTS ON INDUCTOR CONTACTS.May 6, 2004 · Boeing 737376 · Buffet/GalleysSDR AUS20040330Force Limiter · faulty(AUS) AUTOPILOT WOULD NOT ENGAGE. SUSPECT FAULTY FORCE LIMITER.May 2, 2004 · Boeing 737376 · Autopilot SystemSDR AUS20040312Bolt · separated(AUS) PASSENGER SEAT SUPPORT BEAM TO AISLE SIDE LEG STRUCTURE BOLTS SEPARATED AND FOUND UNDER SEAT 12 DEF.Apr 27, 2004 · Boeing 737376 · FastenersSDR AUS20040384Indicator · faulty(AUS) FLAP POSITION INDICATOR FAULTY.Apr 26, 2004 · Boeing 737376 · Trailing Flap Position Indicating SystemSDR 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.Apr 5, 2004 · Boeing 737376 · Passenger/Crew DoorsSDR AUS20040457Limiter · faulty(AUS) AUTOPILOT TORQUE LIMITER FAULTY.Mar 30, 2004 · Boeing 737376 · Autopilot SystemSDR AUS20040192Indicator · failed(AUS) FIRST OFFICER'S AIRSPEED INDICATOR/MACHMETER FAILED.Mar 11, 2004 · Boeing 737376 · Airspeed/Mach IndicatorSDR 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 DEFMar 9, 2004 · Boeing 737376 · Passenger/Crew DoorsSDR AUS20040172Valve · failed(AUS) NR 2 ENGINE FUEL SYSTEM SPAR VALVE FAILED.Mar 7, 2004 · Boeing 737376 · Fuel Selector/Shut-Off ValveSDR AUS20040141Actuator · failed(AUS) FUEL CROSSFEED VALVE ACTUATOR FAILED.Feb 29, 2004 · Boeing 737376 · Fuel Transfer ValveSDR 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.Feb 24, 2004 · Boeing 737376 · Landing Gear Retraction/Extension SystemSDR AUS20040098Bearing · seized(AUS) ELEVATOR CONTROL CENTERING UNIT MOUNT BEARING SEIZED.Feb 10, 2004 · Boeing 737376 · Elevator Control SystemSDR AUS20040097Actuator · cracked(AUS) NR 4 GROUND SPOILER OB ACTUATOR BODY CRACKED AND LEAKING IN AREA NEXT TO RETRACT FITTING.Feb 9, 2004 · Boeing 737376 · Drag Control ActuatorSDR AUS20040080Hydraulic System · leaking(AUS) HYDRAULIC SYSTEM LEAKING.Feb 6, 2004 · Boeing 737376 · Hydraulic System, MainSDR AUS20040042Sensor · out of adjust(AUS) LEADING EDGE FLAP NR 2 EXTEND SENSOR OUT OF ADJUSTMENT.Jan 22, 2004 · Boeing 737376 · Leading Edge Slat Position Indicating SystemSDR 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.Jan 21, 2004 · Boeing 737376 · Hydraulic System, MainSDR AUS20040031Hose · burst(AUS) LT MAIN LANDING GEAR DOWNLOCK ACTUATOR HYDRAULIC HOSE BURST. LOSS OF HYDRAULIC FLUID.Jan 20, 2004 · Boeing 737376 · Hydraulic System, MainSDR AUS20040013Engine · overheated(AUS) ENGINE EXCEEDED EGT LIMITS. EGT REACHED 938 DEGREES C.Jan 5, 2004 · Boeing 737376 · Engine (Turbine/Turboprop)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.Nov 3, 2003 · Boeing 737376 · Hydraulic System, MainSDR AUS20031095Brake Assy · faulty(AUS) AUTOBRAKE SYSTEM NOT ARMING. LIMITED INFORMATION PROVIDED.Oct 27, 2003 · Boeing 737376 · Landing Gear Brake SystemSDR AUS20031076Fire Detector · inoperative(AUS) NR 1 ENGINE FIRE DETECTOR SYSTEM INOPERATIVE.Oct 24, 2003 · Boeing 737376 · Fire DetectionSDR 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.Sep 18, 2003 · Boeing 737376 · Compressor Bleed ControlSDR 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.Sep 17, 2003 · Boeing 737376 · Fire DetectionSDR AUS20030948Fire Loop · faulty(AUS) NR 1 ENGINE FIRE DETECTION SYSTEM FAULTY. NR 1 ENGINE LOOP `B` FAULTY.Sep 17, 2003 · Boeing 737376 · Fire DetectionSDR AUS20030942Warning Light · intermittent(AUS) NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATING INTERMITTENTLY.Sep 17, 2003 · Boeing 737376 · Engine Thrust ReverserSDR 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.Aug 21, 2003 · Boeing 737376 · Engine (Turbine/Turboprop)SDR AUS20030866Pump · failed(AUS) STANDBY HYDRAULIC PUMP FAILED. PUMP RUNS BUT FAILS TO PRODUCE PRESSURE. SUSPECT FAILED SHAFT.Aug 10, 2003 · Boeing 737376 · Hydraulic Pump (Electric/Engine), MainSDR 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 SPARJul 24, 2003 · Boeing 737376 · Wing 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 RECEJul 20, 2003 · Boeing 737376 · Wing, Plate/SkinSDR 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.Jul 15, 2003 · Boeing 737376 · Cabin Cooling SystemSDR 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).Jul 4, 2003 · Boeing 737376 · Cargo/Baggage DoorsSDR AUS20030674Pmc · faulty(AUS) NR 2 ENGINE LOW POWER. SUSPECT CAUSED BY FAULTY POWER MANAGEMENT CONTROL (PMC).Jul 3, 2003 · Boeing 737376 · Fuel Controlling SystemSDR 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.Jun 25, 2003 · Boeing 737376 · Fuselage Main, StructureSDR AUS20030649Sensor · faulty(AUS) RT MAIN LANDING GEAR UPLOCK SENSOR FAULTY.Jun 22, 2003 · Boeing 737376 · Landing Gear Position and WarningSDR AUS20030640Connector · faulty(AUS) RT ENGINE FIRE DETECTION SYSTEM FAULTY. SUSPECT FAULTY CONNECTOR.Jun 13, 2003 · Boeing 737376 · Fire DetectionSDR AUS20030583Sensor · faulty(AUS) MAIN LANDING GEAR AIR SENSOR S106 FAULTY.Jun 4, 2003 · Boeing 737376 · Landing Gear Position and WarningSDR AUS20030547Warning Light · illuminated(AUS) FLAP ASSYMETRY PROBLEMS. LIMITED INFORMATION PROVIDED.May 26, 2003 · Boeing 737376 · Trailing Flap Position Indicating SystemSDR 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.Apr 30, 2003 · Boeing 737376 · Fuselage Main, Attach FittingsSDR 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.Apr 28, 2003 · Boeing 737376 · Fuselage Main, StructureSDR AUS20030468Indicator · false indication(AUS) NR 1 FUEL GAUGE INDICATING FUEL LEAK. INSPECTION COULD FIND NO EVIDENCE OF LEAKS.Apr 20, 2003 · Boeing 737376 · Fuel Quantity IndicatorSDR 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 6Apr 11, 2003 · Boeing 737376 · Fuselage Main, FrameSDR AUS20030415Connector · loose(AUS) APU INOPERATIVE, LIGHT FAULTY. INVESTIGATION FOUND BACKSHELL ON CONNECTOR D4934J LOOSE.Apr 11, 2003 · Boeing 737376 · APU Indicating SystemSDR 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.Apr 8, 2003 · Boeing 737376 · Fuselage Main, Frame
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