Boeing 737-800

Service difficulty reports · 843

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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 = '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.

SDR AU510002182Metering Valve · faulty(AUS) NR 2 ENGINE HYDROMECHANICAL UNIT (HMU) FUEL METERING VALVE FAULTY. (CASA NR 510002182)Dec 12, 2005 · Boeing 737800* · Fuel Control/Turbine EnginesSDR AU510002164Motor · failedSTABILIZER TRIM MOTOR FAILED. CIRCUIT BREAKER TRIPPED.Dec 12, 2005 · Boeing 737800* · Stabilizer ActuatorSDR AU510002157Window · crackedCOCKPIT NR 4 (EYEBROW) WINDOW INNER PANE SHATTERED.Dec 12, 2005 · Boeing 737800* · Flight Compartment WindowsSDR AU510002103Transceiver · failedWEATHER RADAR TRANSCEIVER FAILED.Dec 12, 2005 · Boeing 737800* · Weather Radar SystemSDR AU510002075Heat Exchanger · cracked(AUS) LT AND RT AIR CONDITIONING PACK SECONDARY HEAT EXCHANGERS CRACKED.Dec 12, 2005 · Boeing 737800* · Cabin Cooling SystemSDR AU510002054Transmitter · failed(AUS) WEATHER RADAR TRANSMITTER/RECEIVER FAILED. (CASA NR 510002054)Dec 12, 2005 · Boeing 737800* · Weather Radar SystemSDR AU510002052Display · failedWEATHER RADAR PEDESTAL FAILED.Dec 12, 2005 · Boeing 737800* · Weather Radar SystemSDR AU510002051Proximity Sensor · faultyNR 6 LEADING EDGE SLAT POSITION PROXIMITY SENSOR FAULTY.Dec 12, 2005 · Boeing 737800* · Leading Edge Slat Position Indicating SystemSDR 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 FDec 12, 2005 · Boeing 737800* · Wing, Center BoxSDR 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.Dec 12, 2005 · Boeing 737800* · Nose/Tail Landing GearSDR AU510002008Windshield · failedCAPTAIN`S NR 2 WINDSHIELD OUTER PANE SHATTERED.Dec 12, 2005 · Boeing 737800* · Flight Compartment WindowsSDR 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 ODec 12, 2005 · Boeing 737800* · Hydraulic Power System WiringSDR 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.Dec 12, 2005 · Boeing 737800* · Extinguishing SystemSDR AU510001813Control Panel · failed(AUS) ATC TRANSPONDER CONTROL PANEL FAILED. (CASA NR 510001813)Dec 12, 2005 · Boeing 737800* · ATC Transponder SystemSDR 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)Dec 12, 2005 · Boeing 737800* · Interphone/Passenger Announcement (PA) SystemSDR AU510001743Hose · leakingLT AIR CONDITIONING PACK AIRCYCLE MACHINE SENSE LINE LEAKING. HOSE APPEARS TOO LONG CAUSING TO TIGHT A CURVE RAD.Dec 12, 2005 · Boeing 737800* · Cabin Cooling SystemSDR AU510001688Relay · faultyCENTER FUEL TANK RT BOOST PUMP CONTROL RELAY R55 FAILED.Dec 12, 2005 · Boeing 737800* · Fuel Boost PumpSDR 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.Dec 12, 2005 · Boeing 737800* · Drag Control SystemSDR 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)Dec 12, 2005 · Boeing 737800* · APU Core EngineSDR AU510001525Hmu · faultyNR 1 ENGINE HYDROMECHANICAL UNIT (HMU) FAULTY. INVESTIGATION FOUND THE DEFECT WAS CAUSED BY FAILURE OF THE FMV RESOLVER BODY ASSEMBLY.Dec 12, 2005 · Boeing 737800* · Fuel Controlling SystemSDR 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 PUMDec 12, 2005 · Boeing 737800* · Fuel System WiringSDR AU510001500Seal · leakingFOUND CABIN WINDOW 15A INNER AND OUTER PANES TOUCHING AND FULL OF WATER. INVESTIGATION FOUND SEAL LEAKING.Dec 12, 2005 · Boeing 737800* · Passenger Compartment WindowsSDR AU510001499Pump · cavitatesCENTER FUEL TANK PUMPS CAVITATES.Dec 12, 2005 · Boeing 737800* · Fuel Boost PumpSDR AU510001484Hydraulic System · low pressure(AUS) HYDRAULIC B-SYSTEM LOW PRESSURE. INVESTIGATION CONTINUING. (CASA# 510001484)Dec 12, 2005 · Boeing 737800* · Hydraulic System, MainSDR 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:Dec 12, 2005 · Boeing 737800* · Turbine Engine Compressor SectionSDR 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)Dec 12, 2005 · Boeing 737800* · Turbine SectionSDR AU510001467Actuator · failed(AUS) AUTOPILOT STABILISER TRIM ACTUATOR MOTOR FAILED. (CASA# 510001467)Dec 6, 2005 · Boeing 737800* · Autopilot SystemSDR 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 SLIGHTDec 6, 2005 · Boeing 737800* · Pneumatic Distribution SystemSDR SCNA05011Lens · wornDURING CONFORMITY INSPECTION DISCOVERED ROW 15DEF AFT EMERGENCY EXIT LENS ILLEGIBLE. REMOVED AND REPLACED LENS AS REQUIRED, CHECKED GOOD.Nov 17, 2005 · Boeing 737800* · Emergency LightingSDR 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.Nov 16, 2005 · Boeing 737800* · Turbine Engine Oil SystemSDR AU510002125Clamp · fractured(AUS) APU BLEED AIR DUCT FRACTURED. BLEED AIR SUPPLY DUCT SEPARATED IN HORIZONTAL STABILISER COMPARTMENT. (CASA# 510002125)Nov 11, 2005 · Boeing 737800* · Pneumatic Distribution SystemSDR 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.Nov 11, 2005 · Boeing 737800* · Buffet/GalleysSDR 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. (SW152006063Oct 26, 2005 · N977RY · Boeing 737800* · Hydraulic Power System WiringSDR 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.Oct 22, 2005 · N381DA · Boeing 737800* · Fuselage Main, Plate/SkinSDR DL738050645Battery Pack · inoperativeFOUND F/C EMERGENCY LIGHTS DO NOT ILLUMINATE. T/S SYSTEM AND REPLACED BATTERY PACK M1674, OPS CHECK GOOD.Oct 22, 2005 · N383DN · Boeing 737800* · Emergency LightingSDR AU510001838Hose · leaking(AUS) RT ENGINE DRIVEN HYDRAULIC PUMP TO PYLON QUICK DISCONNECT PRESSURE HOSE LEAKING.Sep 9, 2005 · Boeing 737800* · Hydraulic System, MainSDR 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)Sep 6, 2005 · Boeing 737800* · Humidity Control SystemSDR 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.Aug 10, 2005 · Boeing 737800* · Hydraulic Power System WiringSDR AU510001689Seal · failedAPU BLEED VALVE AND DUCTS CONTAMINATED WITH OIL. INVESTIGATION FOUND THE APU LOAD COMPRESSOR SEAL FAILED.Aug 8, 2005 · Boeing 737800* · APU Core EngineSDR AU510002222Heat Exchanger · crackedRT AIR CONDITIONING PACK HEAT EXCHANGER CRACKED AND LEAKING.Jul 12, 2005 · Boeing 737800* · Cabin Cooling SystemSDR AU510001573Switch · faultyCENTER FUEL TANK RT BOOST PUMP RUNNING WHEN SWITCH `OFF`. SUSPECT FUEL PANEL CONTROL SWITCH.Jul 7, 2005 · Boeing 737800* · Fuel Boost PumpSDR 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 BLOJul 7, 2005 · Boeing 737800* · Navigation System WiringSDR AU510002101Odor · detectedELECTRICAL BURNING ODOR IN CABIN IN AREA OF ROW 18. EXTENSIVE INVESTIGATION COULD FIND NO CAUSE FOR THE ODOR.Jun 11, 2005 · Boeing 737800* · Air Distribution SystemSDR AU510001840Controller · faultyNR 2 CABIN PRESSURE CONTROLLER FAULTY.Jun 8, 2005 · Boeing 737800* · Cabin Pressure ControllerSDR AU510001720Window · failedNR 4 RT FLIGHT COMPARTMENT WINDOW INNER PANE SHATTERED. WINDOW HEAT SYSTEM WAS FOUND TO BE SERVICEABLE.Jun 8, 2005 · Boeing 737800* · Flight Compartment WindowsSDR 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.Jun 7, 2005 · Boeing 737800* · Passenger/Crew DoorsSDR 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 340-001-8May 7, 2005 · Boeing 737800* · Turbine Engine Compressor SectionSDR AU510001786Coupler · failed(AUS) NR 1 HF SYSTEM ANTENNA COUPLER FAILED. (CASA NR 510001786)Mar 7, 2005 · Boeing 737800* · HF Communications SystemSDR 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 SWIFeb 23, 2005 · Boeing 737800* · Pressure Regulator/Outflow ValveSDR 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 VALFeb 23, 2005 · Boeing 737800* · Cabin Pressure Control System
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