Boeing 737-476
Service difficulty reports · 223
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 = '737476' 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 = '737476' 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 EE4Y2019100409925Floorbeam · crackedUPPER FUSELAGE MAIN CARGO CABIN BS 727B, RBL 45.57 AFT END OF LONGITUDINAL FLOOR BEAM UPPER CHORD OUTBOARD FLANGE WITH CRACK. THE DAMAGE AREA WAS REPAIRED PER SERVICE BULLETIN PEMCO 737-57-0002.SDR EE4Y2019100409923Skin · crackedLOWER FUSELAGE SKIN DAMAGED AT BS 500B+5, BETWEEN STRINGERS 22L AND 23L. THE DAMAGED AREA WAS REPAIRED IAW INSTRUCTIONS ON EO PD37-53-3026.SDR AU510002193Stringer · crackedFUSELAGE STRINGER SPLICE CRACKED. CRACK LENGTH APPROXIMATELY 5MM (0.200IN). UPON REMOVAL OF THE SPLICE THERE WAS EVIDENCE OF MULTI-SITE CRACKING ON OUTBOARD SURFACE OF SPLICE (TWO HOLES). FOUND DURING EDDY CURRENT INSPECTION OF FUSELAGE UPPER LOBE FASTENER HSDR AU510002185Valve · stickingNR 2 ENGINE SPAR VALVE FAULTY.SDR AU510002153Iru · failedLT INERTIAL REFERENCE UNIT (IRU) FAILED.SDR AU510002152Spring · failedELEVATOR FEEL SPRING BROKEN.SDR AU510002105Actuator · faultyLT MAIN LANDING GEAR ACTUATOR FAULTY. LT MAIN LANDING GEAR NOT FULLY RETRACTED.SDR AU510002104Tire · debondedNR 3 MAIN WHEEL TIRE TREAD DEBONDED.SDR AU510002060Shroud · failed(AUS) LT ENGINE FAILED TO START. INVESTIGATION FOUND ENGINE SEIZED AND A SMALL AMOUNT OF DEBRIS IN THE TAILPIPE. BOROSCOPE INSPECTION FOUND DAMAGE TO HIGH PRESSURE TURBINE (HPT). INVESTIGATION FOUND THE HPT SHOUD HAD FAILED AND LODGED BETWEEN THE HPT BLADESSDR AU510002047Adapter · faultyRT INERTIAL REFERENCE SYSTEM (IRS) FAILED. CAUSED BY FAULTY RT DIGITAL ANALOGUE ADAPTER (DAA).SDR AU510002038Door · misrepairedPAPER AND LINEN WASTE RECEPTACLE DOORS IN TOILETS NOT SEALING. INVESTIGATION FOUND LAV A (FWD) TO BE LATCHING SECURELY BUT NOT SEALING. INVESTIGATION REVEALED EXTRA STRIKER PLATE BONDED OVER EXISTING STRIKER PLATE CAUSING DOOR TO SIT OUT FURTHER THAN REQUIRESDR AU510002014Iru · failedNR 1 INERTIAL REFERENCE UNIT (IRU) FAILED.SDR AU510001933Pump · failedHYDRAULIC SYSTEM `B` HYDRAULIC PUMP FAILED.SDR AU510001921Cabin Pressure · faulty(AUS) AIRCRAFT PRESSURISED ON LANDING. NUMEROUS COMPONENTS CHANGED. INVESTIGATION CONTINUING. (CASA NR 510001921)SDR AU510001913Transmitter · faulty(AUS) LT FLAP POSITION TRANSMITTER FAULTY. (CASA NR 510001913)SDR AU510001907Indicator · faulty(AUS) TRAILING EDGE FLAP ASSYMETRY. FLAPS RECYCLED AND OPERATED NORMALLY. INVESTIGATION CONTINUING. (CASA NR 510001907)SDR AU510001772Turbine Blades · damaged(AUS) NR 1 ENGINE MAKING (POPPING) SOUNDS. SOUNDS INCREASED WHEN THRUST LEVER INCREASED AND DECREASED WHEN THRUST LEVER RETARDED. BORESCOPE INSPECTION FOUND HPC BLADES DAMAGED BEYOND LIMITS. INVESTIGATION CONTINUING. (CASA NR 510001772)SDR AU510001687Outflow Valve · failedPRESSURIZATION SYSTEM AFT OUTFLOW VALVE FAILED TO OPEN. INVESTIGATION FOUND A DEFECTIVE AC MOTOR AND AC POTENTIOMETER.SDR AU510001672Bearing · failedLT WING OUTBOARD KRUGER FLAP NOSE LINK EYE END SHEARED.SDR AU510001638Flap System · sticking(AUS) LT FLAP STOPPED. FLAP ASSYMETRY. INVESTIGATION CONTINUING. (CASA NR 510001638)SDR AU510001606Pump · faultyNR 2 ENGINE HAS A HISTORY OF STARTING DIFFICULTIES AND FLUCTUATING PARAMETERS. INVESTIGATION FOUND FUEL PUMP HAD NO FLOW AT LOW SPEED AND WAS WELL BELOW LIMIT OF FLOW AT HIGHER SPEED. THE PUMP GEARS WERE FOUND SCORED. THIS CAUSED DAMAGE TO THE BEARINGS AND THSDR AU510001524Gcu · failedNR 1 GENERATOR CONTROL UNIT (GCU) FAILED.SDR AU510001496Sensor · faultyNR 3 LEADING EDGE FLAP RETRACTION SENSOR FAULTY.SDR AU510002148Panel · misinstalledVERTICAL STABILIZER RT LOWER PANEL INCORRECTLY FITTED BETWEEN FORWARD AND AFT ATTACHMENT POINTS.SDR AU510001728Slide · no testDOOR 1R ESCAPE SLIDE FAILED TO DEPLOY NORMALLY DURING TEST. SLIDE CONTACTED EDGE OF DOOR DURING OPENING CAUSING IT TO TWIST SIDEWAYS.SDR AU510001727Window · damagedCAPTAIN`S NR 1 WINDOW CRACKED DUE TO ARCING.SDR AU510002184Door Frame · crackedFORWARD CARGO DOOR CUTOUT AFT FRAME WEB CRACKED. CRACK LENGTH APPROXIMATELY 17.78MM (0.700IN). FOUND DURING EDDY CURRENT INSPECTION IAW AD/737/242 AND BOEING SB 737-53A1228.SDR AU510002177Frame · crackedFUSELAGE FRAMES (21OFF) CRACKED AT PASSENGER SERVICE UNIT (PSU) ATTACHMENT POINTS. FOUND DURING EDDY CURRENT INSPECTION IAW EI 737-53-68R3 AND NDT TECHNIQUES E-13 AND E-18.SDR AU510001468Actuator · failed(AUS) STABILISER ELECTRIC TRIM ACTUATOR FAILED. CAUSED BY WORN AND STICKING CLUTCH. (OTHER CAUSE: STICKING CLUTCH PLATES ) (CASA# 510001468)SDR AU510001457Servo · failed(AUS) AUTOPILOT STABILISER TRIM SERVO FAILED. WORKSHOP INVESTIGATION FOUND ROTOR GEAR STRIPPED AND ROTOR BEARING JOURNAL WORN. (OTHER CAUSE: AGE ) (CASA# 510001457)SDR AU510001584Wire · burned(AUS) WIRE LOCATED ON THE BACK OF PLUG D4001P LOCATED BEHIND THE E I RACK BURNED DUE TO CONTACT WITH TRAY DISCONNECT BRACKET. (OTHER CAUSE: MATERIAL ) (CASA NR 510001584)SDR AU510002009Symbol Generator · failedCAPTAIN`S SYMBOL GENERATOR FAILED.SDR AU510001934Frame · crackedFUSELAGE FRAMES CONTAINED 28 CRACKS AT PASSENGER SERVICE UNIT (PSU) ATTACHMENT POINTS. FOUND DURING EDDY CURRENT INSPECTION IAW EI 737-53-68R3 AND B737 NTM PT6 51-00-00 FIG 4 AND FIG 16.SDR AU510001571Slide · faultyDOOR L1 ESCAPE SLIDE PRESSURE OUTSIDE OF OPERATING RANGE.SDR AU510001552Coupler · faultyNR 2 HF SYSTEM FAILED. NEW TRANSMITTER FITTED BUT PROBLEM REMAINED. SUSPECT FAULTY COUPLER.SDR AU510001547Actuator · failedAUTOPILOT STABILIZER TRIM ACTUATOR FAILED DUE TO STRIPPED ROTOR GEAR AND WORN ROTOR BEARING JOURNAL.SDR AUS20040500Oven · faulty(AUS) FORWARD GALLEY OVEN FAILED. FIRE EXTINGUISHED DISCHARGED INTO OVEN.SDR AUS20040493Window · cracked(AUS) CAPTAIN'S NR 2 SLIDING WINDOW OUTER PANE CRACKED IN UPPER FORWARD CORNER.SDR AUS20040487Bearing · faulty(AUS) FIRST OFFICER'S CONTROL WHEEL BEARING NOTCHY.SDR AUS20040479Light · faulty(AUS) RT MAIN LANDING GEAR DOWN LIGHT FAILED TO ILLUMINATE ON GEAR SELECTION. INVESTIGATION FOUND A FAULTY LOCK MECHANISM IN THE LAMP LENS CAP.SDR AUS20040427Panel · faulty(AUS) LANDING GEAR POSITION PANEL FAULTY.SDR AUS20040394Spar · cracked(AUS) HORIZONTAL STABILIZER REAR SPAR SUSPECT CRACKED. EDDY CURRENT INSPECTION CONFIRMED THE FOLLOWING CRACKS. STABILIZER REAR SPAR RT FORWARD FACE OF TOP WEB ASSEMBLY. CRACK INDICATION CONFIRMED. CRACK LENGTH 10.16MM (0.400IN)OUT OF FASTENER HOLE. HORIZOSDR AUS20040367Slide · failed(AUS) DOOR 2L ESCAPE SLIDE LIGHTS FAILED TO ILLUMINATE FOLLOWING SLIDED EMPLOYMENT. SUSPECT FLAT BATTERY.SDR AUS20040387Control Column · binding(AUS) FIRST OFFICER'S CONTROL COLUMN ELL FITTING CHAFING ON TRANSFER MECHANISM FORK. TRANSFER MECHANISM WAS FOUND TO HAVE A PRESERVICE BULLETIN FORK FITTED INSTEAD OF A POST SERVICE BULLETIN FORK.SDR AUS20040290Spindle · fractured(AUS) RT OB MID FLAP CARRIAGE SPINDLE SUSPECT CRACKED. FOUND DURING ULTRASONIC INSPECTION IAW EI 737-57-72R2.SDR AUS20040456Indicator · faulty(AUS) FLAP POSITION INDICATOR FAULTY.SDR AUS20040283Flap · faulty(AUS) AIRCRAFT HAD AN ASSYMETRIC FLAP INDICATION DURING SELECTION. THE AIRCRAFT HAS HAD A TOTAL OF FOUR SIMILAR OCCURRENCES DURING A TWO WEEK PERIOD. INVESTIGATION IS CONTINUING.SDR AUS20040230Valve · sticking(AUS) NR 1 ENGINE FUEL SHUTOFF VALVE STICKING.SDR AUS20040199Panel · faulty(AUS) AUTOPILOT MODE CONTROL PANEL FAULTY.SDR AUS20040184Frame · cracked(AUS) FUSELAGE FRAME LOCATED AT BS 663.75 STRINGER 3R-3L CRACKED AT S1AND S2R FASTENER HOLES. FOUND DURING EDDY CURRENT INSPECTION.
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