Boeing 737-800
Service difficulty reports · 843
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 = '737800' 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 = '737800' 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 AU510002182Metering Valve · faulty(AUS) NR 2 ENGINE HYDROMECHANICAL UNIT (HMU) FUEL METERING VALVE FAULTY. (CASA NR 510002182)SDR AU510002164Motor · failedSTABILIZER TRIM MOTOR FAILED. CIRCUIT BREAKER TRIPPED.SDR AU510002157Window · crackedCOCKPIT NR 4 (EYEBROW) WINDOW INNER PANE SHATTERED.SDR AU510002103Transceiver · failedWEATHER RADAR TRANSCEIVER FAILED.SDR AU510002075Heat Exchanger · cracked(AUS) LT AND RT AIR CONDITIONING PACK SECONDARY HEAT EXCHANGERS CRACKED.SDR AU510002054Transmitter · failed(AUS) WEATHER RADAR TRANSMITTER/RECEIVER FAILED. (CASA NR 510002054)SDR AU510002052Display · failedWEATHER RADAR PEDESTAL FAILED.SDR AU510002051Proximity Sensor · faultyNR 6 LEADING EDGE SLAT POSITION PROXIMITY SENSOR FAULTY.SDR AU510002045Vapor Barrier · out of limitsWING CENTER SECTION FUEL VAPOR BARRIER UNDER LIMITS IN THE FOLLOWING SIX AREAS ON THE TRIANGLE POCKET-FRONT SPAR/SIDE OF BODY, TP3-R THICKNESS 1.7 2. TP3-L 2.2, TP6-L 5.9 4. TP9-L 2.0 SHEAR FITTING, FRONT SPAR CORNER WITH TOP PANEL 5. SF4-R 6.3 6. SF5-R 5.8 FSDR AU510002023Landing Gear · malfunctionedAFTER TAKEOFF, NOSE LANDING GEAR EXTENDED WHEN LANDING GEAR LEVER WAS SELECTED TO `OFF`. NLG WAS NOT OVERSPED. INVESTIGATION COULD FIND NO FAULTS WITH THE EXTENSION/RETRACTION SYSTEM.SDR AU510002008Windshield · failedCAPTAIN`S NR 2 WINDSHIELD OUTER PANE SHATTERED.SDR AU510001826Connector · brokenLOSS OF SYSTEM `A` HYDRAULIC PRESSURE AND QUANTITY. INVESTIGATION FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP CONNECTOR DP1204 HARD PLASTIC INSERT BROKEN. METAL CONTAMINATION OF HYDRAULIC FILTER. BURNING SMELL DURING TAKEOFF SUSPECTED TO BE HYDRAULIC PUMP OSDR AU510001815Circuit Breaker · trippedAPU FIRE EXTINGUISHING SYSTEM CIRCUIT BREAKER PULLED AND RED COLLARED. CIRCUIT BREAKER RESET AND SYSTEM TESTED SERVICEABLE. SUSPECT CIRCUIT BREAKER PULLED WHEN MEL APPLIED AND NOT RESET WHEN MEL CLEARED.SDR AU510001813Control Panel · failed(AUS) ATC TRANSPONDER CONTROL PANEL FAILED. (CASA NR 510001813)SDR AU510001793Audio Panel · faulty(AUS) SMOKE AND FUMES IN IN COCKPIT. INVESTIGATION FOUND CAPTAIN`S INTERPHONE SYSTEM AUDIO SELECTOR PANEL FAULTY WITH THE MIC SELECTOR SWITCH STUCK AND THE LED NOT WORKING. SUSPECT CAUSED BY FLUID SPILLAGE CAUSING CORROSION. (CASA NR 510001793)SDR AU510001743Hose · leakingLT AIR CONDITIONING PACK AIRCYCLE MACHINE SENSE LINE LEAKING. HOSE APPEARS TOO LONG CAUSING TO TIGHT A CURVE RAD.SDR AU510001688Relay · faultyCENTER FUEL TANK RT BOOST PUMP CONTROL RELAY R55 FAILED.SDR AU510001661Cable · brokenGROUND SPOILER INTERLOCK CABLE BROKEN. INVESTIGATION FOUND VERY STIFF BEARING OPERATION DUE TO MOISTURE INGRESS INTO THE BEARING LINER LEAD TO FATIGUE AND ULTIMATELY FAILURE OF THE CABLE RODEND.SDR AU510001627Seal · leaking(AUS) APU LEAKING OIL INTO AIR DUCTING. STRONG OIL SMELL IN COCKPIT. INVESTIGATION FOUND THE APU LOAD COMPRESSOR SEAL FAILED AND LEAKING. SEE ATTACHMENT FOR INVESTIGATION DETAILS. (OTHER CAUSE: LOAD COMP SEAL LEAKAGE ) (CASA NR 510001627)SDR AU510001525Hmu · faultyNR 1 ENGINE HYDROMECHANICAL UNIT (HMU) FAULTY. INVESTIGATION FOUND THE DEFECT WAS CAUSED BY FAILURE OF THE FMV RESOLVER BODY ASSEMBLY.SDR AU510001501Wire · damagedNR 2 AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED AND CIRCUIT BREAKER TRIPPED. INVESTIGATION FOUND FUEL PUMP WIRING BADLY BURNT AT EARTH PIG TAIL FERRULE. IT APPEARS THAT WHEN THE WIRING HARNESS WAS MANUFACTURED, ONE OR ALL THREE PHASE POWER WIRES TO THE PUMSDR AU510001500Seal · leakingFOUND CABIN WINDOW 15A INNER AND OUTER PANES TOUCHING AND FULL OF WATER. INVESTIGATION FOUND SEAL LEAKING.SDR AU510001499Pump · cavitatesCENTER FUEL TANK PUMPS CAVITATES.SDR AU510001484Hydraulic System · low pressure(AUS) HYDRAULIC B-SYSTEM LOW PRESSURE. INVESTIGATION CONTINUING. (CASA# 510001484)SDR AU510001475Pin · loose(AUS) DURING FAN LUBE INSPECTION OF THE FAN HUB FOUR (4) FORWARD BOOSTER SPOOL PINS WERE FOUND TO BE VISIBLY LOOSE. AFTER A TORQUE CHECK OF THE REMAINDER, A FURTHER FIVE (5) PINS WERE FOUND TO BE LOOSE. TOTAL NUMBER OF UNDERTORQUED PINS NINE (9). (OTHER CAUSE:SDR AU510001465O-Ring · deteriorated(AUS) ENGINE TURBINE REAR FRAME OIL COVER GASKET PNO 340-179-401-0 AND O-RING SEAL PNO 649-393-271-0 DETERIORATED AND LEAKING. SEE ATTACHMENT FOR INVESTIGATION DETAILS. (CASA# 510001465)SDR AU510001467Actuator · failed(AUS) AUTOPILOT STABILISER TRIM ACTUATOR MOTOR FAILED. (CASA# 510001467)SDR AU510001446Ring · dislodged(AUS) NR 1 ENGINE BLEED AIR SYSTEM HIGH STAGE VALVE GATE SEALING RING DISLODGED, PREVENTING VALVE FROM FULLY CLOSING. INVESTIGATION FOUND THE HIGH STAGE VALVE BUTTERFLY PLATE SEALING RING CLIP FAILED ALLOWING THE SEALING RING TO JAM THE THE VALVE IN THE SLIGHTSDR SCNA05011Lens · wornDURING CONFORMITY INSPECTION DISCOVERED ROW 15DEF AFT EMERGENCY EXIT LENS ILLEGIBLE. REMOVED AND REPLACED LENS AS REQUIRED, CHECKED GOOD.SDR 2005F00109Cover · misinstalledON CLIMB OUT HAD LOW OIL QUANITY INDICATION ON ROLL OUT. QUANITY DROPPED TO ZERO OIL PRESSURE AND TEMPERATURE OKAY. FOUND THE HANDCRANKING DRIVE COVER NOT INSTALLED. RESERVICED ENGINE AND PERFORMED IDLE RUNS FOR 15 MIN. WITH NO DEFFECTS NOTED.SDR AU510002125Clamp · fractured(AUS) APU BLEED AIR DUCT FRACTURED. BLEED AIR SUPPLY DUCT SEPARATED IN HORIZONTAL STABILISER COMPARTMENT. (CASA# 510002125)SDR AU510002118Oven · failedSPARKS AND ELECTRICAL FUMES EMANATING FROM REAR GALLEY AREA. INSPECTION COULD FIND NO FAULTS BUT THE OVEN WAS REPLACED AS A PRECAUTION. INVESTIGATION CONTINUING.SDR 2005FA0001479Wire · crossedDURING TROUBLESHOOTING FOLLOWING PTU TEST FIRE, THE PTU CONTROL VALUE AS FOUND FAILED IN CLOSED POSITION WITH 28 VDC ON PIN: 2 OF VALVE CONNECTOR. AN INVESTIGATION REVEALED WIRES WERE CROSSED AT MFG. WIRING REMADE IAW WDM2911 AND NEW VALVE FIT. (SW152006063SDR DL738050649Skin · puncturedTHE FUSELAGE SKIN WAS STRUCK BY GROUND EQUIPMENT BETWEEN FS 365 & 382, JUST ABOVE STRINGER 24R. THE DAMAGE TO THE SKIN WAS REMOVED WITH A 20 X 6 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 451256-14, REV A.SDR DL738050645Battery Pack · inoperativeFOUND F/C EMERGENCY LIGHTS DO NOT ILLUMINATE. T/S SYSTEM AND REPLACED BATTERY PACK M1674, OPS CHECK GOOD.SDR AU510001838Hose · leaking(AUS) RT ENGINE DRIVEN HYDRAULIC PUMP TO PYLON QUICK DISCONNECT PRESSURE HOSE LEAKING.SDR AU510001436Water Separator · cracked(AUS) AIR CONDITIONING SYSTEM FORWARD WATER SEPARATOR CRACKED ALONG INBOARD WELDED SEAM. CRACK LENGTH APPROXIMATELY 50.8MM (2IN).(OTHER CAUSE: CRACKED ALONG THE WELDED SEAM ) (CASA# 510001436)SDR AU510002039Connector · damagedHYDRAULIC PUMP CONNECTOR AND MATING RECEPTACLE CONTAMINATED WITH HYDRAULIC FLUID AND BADLY BURNT. ONE OF THE CONNECTOR SOCKETS WAS WELDED ONTO THE PUMP CONNECTOR PINS.SDR AU510001689Seal · failedAPU BLEED VALVE AND DUCTS CONTAMINATED WITH OIL. INVESTIGATION FOUND THE APU LOAD COMPRESSOR SEAL FAILED.SDR AU510002222Heat Exchanger · crackedRT AIR CONDITIONING PACK HEAT EXCHANGER CRACKED AND LEAKING.SDR AU510001573Switch · faultyCENTER FUEL TANK RT BOOST PUMP RUNNING WHEN SWITCH `OFF`. SUSPECT FUEL PANEL CONTROL SWITCH.SDR AU510001567Wire · separated(AUS) WEATHER RADAR SYSTEM WIRES PN W6491-0016-20 AND PN W6491-0065-24 FOUND PULLED OUT OF TERMINAL BLOCK GD383. SUSPECT WIRES DISTURBED DURING AIRCRAFT MODIFICATION. SEE ATTACHMENT FOR INVESTIGATION DETAILS.(OTHER CAUSE: WIRES FOUND PULLED OUT OF TERMINAL BLOSDR AU510002101Odor · detectedELECTRICAL BURNING ODOR IN CABIN IN AREA OF ROW 18. EXTENSIVE INVESTIGATION COULD FIND NO CAUSE FOR THE ODOR.SDR AU510001840Controller · faultyNR 2 CABIN PRESSURE CONTROLLER FAULTY.SDR AU510001720Window · failedNR 4 RT FLIGHT COMPARTMENT WINDOW INNER PANE SHATTERED. WINDOW HEAT SYSTEM WAS FOUND TO BE SERVICEABLE.SDR AU510001557Bolt · dislodgedDOOR L1 UPPER GATE STUCK IN LOCKED POSITION DUE TO LOWER ROD ASSEMBLY BOLT DISLODGED IN THE TORQUE BOX ASSEMBLY. SUSPECT BOLT INSUFFICIENTLY TORQUED.SDR AU510001558Compressor Wheel · wrong partNR 2 ENGINE FAN BLADE PLATFORMS NR 1 AND NR 4 LOCATED OPPOSITE NR 13 AND NR 16 FAN BLADES WERE NOT CHANGED WHEN NR 13 AND NR 16 FAN BLADE PLATFORMS WERE CHANGED AS DIRECTED BY SB CFM56-7B-0353. NR 13 AND NR 16 FAN BLADE PLATFORMS WERE CHANGED TO P/N 340-001-8SDR AU510001786Coupler · failed(AUS) NR 1 HF SYSTEM ANTENNA COUPLER FAILED. (CASA NR 510001786)SDR RYNA200500007Outflow Valve · malfunctionedDURING CRUISE AT FL350, THE AUTO PRESSURE FAIL LIGHT ILLUMINATED. SWITCHED THE PRESSURE MODE CONTROL TO ALTN AND THE LIGHTS REMAINED ON AND DIFFERENTIAL PRESSURE BEGAN TO RISE. WHEN THE DIFFERENTIAL PRESSURE REACHED 8.7 PSI, THE PRESSURE MODE CONTROL WAS SWISDR RYNA200500009Line · leakingDURING CRUISE FLT AT FL350, AUTO PRESSURE FAIL LIGHT ILLUMINATED. SWITCHED PRESSURE MODE CONTROL TO ALTN & LIGHTS REMAINED ON & DIFF PRESSURE BEGAN TO RISE. DIFF PRESSURE REACHED 8.7 PSI, PRESSURE MODE CONTROL SWITCHED TO MANUAL & SLIGHTLY OPENED OUTFLOW VAL
Back to Boeing 737-800