Boeing 737-322
Service difficulty reports · 4,751
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 = '737322' 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 = '737322' 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 96UAL900295Power Supply · inoperativeBULLNOSE EMERGENCY LIGHTS INOP ROWS 7DEF AND 9ABC. FOUND BATTERY CHARGER AND BATTERY POWER SUPPLY DEFECTIVE. REPLACED BATTERY CHARGER M1135 AND BATTERY POWER SUPPLY.SDR 96UAL900281Light Socket · inoperativeEMERGENCY LIGHT ON THE OUTSIDE OF DOOR TWO LEFT INOPERABLE. REPLACED SOCKET ASSEMBLY. CHECKS O.K.SDR 96UAL900262T/O Warning · soundedDURING TAKEOFF WARNING HORN SOUNDED, RETURNED TO BLOCKS. *S/D* MAINTENANCE PERFORMED OPERATIONAL CHECK OF TAKEOFF WARNING SYSTEM WITH NO FAULTS FOUND.SDR 96UAL900260Throttle Control · malfunctionedAFTER LEVEL OFF AT CRUISE ALTITUDE, NR 1 THROTTLE WOULD NOT RETARD BELOW 93 PERCENT N1 WITH AUTOTHROTTLES ON OR OFF. RETURNED TO DEN AND SHUTDOWN NR 1 ENGINE PRIOR TO LANDING IN DEN.SDR 96UAL900255Retract Mech · malfunctionedDURING FLAP EXTENSION FELT SLIGHT ROLL, THERE WAS NO INDICATION OF FLAP EXTENSION EITHER VISUALLY OR INDICATION. SEVERAL SECONDS LATER THE FLAPS STARTED DOWN AND AN ASYMMETRY CONDITION DEVELOPED AT 15 DEGREES.SDR 96UAL900245Aoa Sensor · inoperativeSTICK SHAKER OCCURRED ON ROTATION, RETURNED TO LAX FOR NORMAL LANDING. *S/D* REPLACED ANGLE OF ATTACK SENSOR, SYSTEM CHECKS OK.SDR 96UAL900244Feeder Wire · failedEMERGENCY ESCAPE LIGHT STRIP BETWEEN ROWS 10 AND 16 INOP. REPLACED EMERGENCY ESCAPE LIGHT STRIP POWER FEEDER AND OPERATION NORMAL.SDR 96UAL900242Strip Light · inoperativeAFT GALLEY EMERGENCY ESCAPE LIGHT STRIP INOP. REPLACED FAULTY LIGHT STRIP AND OPERATION NORMAL.SDR 96UAL900241Fmc · malfunctionedFMC FAILS DURING TAKEOFF AT APPROXIMATELY 80 TO 100 KTS. FLAGS ARE DISPLAYED AND AUTO THROTTLES DISENGAGE. *S/D* NAVIGATION DATA BASE WAS RELOADED AND NO FURTHER PROBLEMS WERE FOUND.SDR 96UAL900233Reflector · inoperativeEMERGENCY EXIT LIGHT INOP AT DOOR TWO RIGHT HAND. REPLACED REFLECTOR ASSEMBLY, CHECKS OK.SDR 96UAL900224Light · inoperativeROW 3 EMERGENCY LIGHT INOP. RELAMPED, OPERATION CHECKS NORMAL.SDR 96UAL900223Controller · inoperativeAIRCRAFT DIVERTED TO LAX DUE TO LOSS OF CABIN PRESSURIZATION. *S/D* REPLACED CABIN PRESSURE CONTROLLER, CHECKS OK.SDR 96UAL900205Light Strip · inoperativeEMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 11 AFT. REPLACED AFT CHARGER AND LIGHT STRIP IN GALLEY. CHECKS O.K.SDR 96UAL900202Outflow Valve · leakingON CLIMBOUT, HAD LOUD FLUTTERING TYPE NOISE IN FORWARD AREA OF FUSELAGE. *S/D* REPLACED FLOW CONTROL VALVE, CHECKS OK.SDR 96UAL900182Accessory Unit · failedNR 4 LEADING EDGE FLAP WOULD NOT RETRACT. SUPPLEMENTAL DATA UPDATE: REPLACED FLAP/SLAT POSITION SWITCH ACCESSORY UNIT. SYSTEM CHECKED GOOD. FAILURE OF THE ACCESSORY UNIT COULD NOT BE VERIFIED BY THE HOME SHOP.SDR 96UAL900177Battery · dischargedEMERGENCY ESCAPE PATH LIGHTING INOP AT ROWS ONE AND TWO. REPLACED BATTERY PACK, CHECKS OK.SDR 96UAL900176Lamp · failedEMERGENCY EXIT SLIDE LIGHT INOP. CLEANED SOCKET AND REPLACED LAMP. CHECKS O.K.SDR 96UAL900172Door Handle · not securedUNABLE TO CONTROL CABIN PRESSURE IN ANY MODE. AFT PIT DOOR RELEASE HANDLE UNDER PIT DOOR SEAL. SECURED HANDLE, PRESSURIZED AIRCRAFT, CHECKS NORMAL.SDR 96UAL901011Bearing · crackedRUDDER PCU WAS REMOVED FROM AIRCRAFT TO ACCOMPLISH AD94-01-07. THE SUMMING LEVER BEARING WAS FOUND CRACKED AT THE INNER RACE. DURING SHOP OVERHAUL OF THE PCU THE PRIMARY SUMMING LEVER WAS REPLACED. AN ALTERNATE CONFIGURATION BOLT WAS USED IN PLACE OF THE BOSDR 96UAL900165Battery Pack · dischargedNR TWO LEFT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. CHECKS O.K.SDR 96UAL900149Csd · failedNUMBER TWO GENERATOR TRIPPED OFF LINE ON TAKEOFF AND UNABLE TO RESET. REPLACED NUMBER TWO ENGINE CONSTANT SPEED DRIVE AND GENERATOR. RAN ENGINE, CHECKS OK. SHOP FINDINGS SHOWED THE CONSTANT SPEED DRIVE GOVERNOR TRIM HEAD AND BUSHING WAS LOOSE WHICH WOULD CASDR 96UAL900140Strip · inoperativeAFT CABIN EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED POWER STRIP, CHECKS OK.SDR 96UAL900135Disk · crackedDURING SHOP VISIT, FLUORESCENT PENETRATE INSPECTION OF THE FAN DISK, TWO DOVETAIL CRACKS WERE FOUND. ONE CRACK WAS FOUND AT THE BOTTOM OF THE DOVETAIL SLOT NR 6 RIGHT PRESSURE FACE. THE SECOND CRACK WAS FOUND AT THE BOTTOM OF THE DOVETAIL SLOT NR 22 LEFT PRESDR 96UAL900101Actuator · failedWHEN AUTOPILOT 'B' SELECTED, THE STABILIZER OUT OF TRIM LIGHT DISPLAYED. AIRCRAFT STARTED DESCENT AND WOULD NOT HOLD ALTITUDE, THE AIRCRAFT CLIMBED SEVERAL TIMES. AFTER DISCONNECTING AUTOPILOT, COULD NOT TRIM FWD USING YOKE SWITCH OR MANUALLY TRIM FWD PAST 4SDR 96UAL900080Connector · looseEMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 12 TO ROW 18. RESEATED CONNECTOR ON POWER CABLE, CHECKS OK.SDR 96UAL900079Brake Plate · chippedCREW REPORTS THAT THE HORIZONTAL STABILIZER TRIM IS JAMMED AND CANNOT BE TRIMMED MANUALLY OR ELECTRONICALLY. JACKSCREW ASSEMBLY WAS JAMMED, ASSEMBLY WAS REMOVED FROM AIRCRAFT AND ROUTED TO THE SHOP. DURING DISASSEMBLY A BRAKE PLATE WAS FOUND CHIPPED. CHIP SSDR 96UAL900078Adc · inoperativeON TAKEOFF, CAPTAIN'S AIRSPEED INDICATOR AND BOTH FLIGHT MANAGEMENT COMPUTERS INOP. NUMBER ONE AIR DATA COMPUTER SHOWED BARO REFERENCE NUMBER TWO, OUT OF LIMIT IN FAULT MEMORY. REPLACED NUMBER ONE AIR DATA COMPUTER, CHECKS OK.SDR 96UAL900067Circuit Breaker · defectiveLOST CAPTAIN'S AND FIRST OFFICER'S INSTRUMENTS. RESTORED POWER TO FIRST OFFICER'S INSTRUMENTS BUT NEVER REGAINED CAPTAIN'S INSTRUMENTS. THE NUMBER ONE ELECTRICAL BUS CIRCUIT BREAKER AND THE NUMBER TWO GENERATOR BREAKER AUXILIARY CONTACTS WERE FOUND DEFECTIVESDR 96UAL900055Battery · inoperativeEMERGENCY LIGHTS INOP AT ROWS 1, 10 TO 16, 18 AND DOOR 2 LEFT. REPLACED BATTERY PACK AND CHECKS OK.SDR 96UAL900037Mec · malfunctionedNUMBER ONE ENGINE SURGED DURING CLIMB, N1 WENT FROM A TARGET OF 92 PERCENT TO 94.3 PERCENT. ALSO, HAD A 1,000 POUND INCREASE IN FUEL FLOW, THROTTLE WAS RETARDED AND ENGINE SURGED TWO MORE TIMES BEFORE IT STABILIZED. ENGINE SURGING WAS CAUSED BY AN INTERMITTESDR 96UAL900024Engine · failedNUMBER TWO ENGINE WENT TO 935 DEGREES, ABORTED TAKEOFF AT 90 KNOTS. THE ENGINE EXPERIENCED AN EXHAUST GAS TEMPERATURE EXCEEDENCE, DUE TO NORMAL ENGINE PERFORMANCE DETERIORATION. ENGINE WAS REMOVED AND SENT TO THE SHOP FOR REPAIR. HIGH PRESSURE TURBINE HARDWSDR 96UAL900023Compressor · bird strikeNUMBER ONE ENGINE FAILED DURING ROTATION. HEAVY FIRST STAGE FAN DAMAGE. A BIRD STRIKE WAS THE CAUSE OF THE ENGINE FAILURE. ENGINE WAS REMOVED AND SENT TO THE SHOP FOR REPAIR.SDR 96UAL900013Panel · damagedPRESSURIZATION AUTO FAIL LIGHT CAME ON, WAS UNABLE TO CONTROL PRESSURIZATION IN STANDBY OR MANUAL MODE. CABIN WAS CLIMBING AT AN UNCONTROLLABLE RATE. REPLACED MAIN OUTFLOW VALVE AND PRESSURIZATION SELECTOR PANEL. FOUND PIN PUSHED IN ON PANEL, TESTED PRESSURSDR 95UAL900371Seal · leakingNOTICED A STEADY LOSS OF 'B' SYSTEM HYDRAULIC QUANTITY AFTER REACHING CRUISE. TRIED TO ISOLATE SYSTEMS AND WHEN TURNING OFF THE 'B' SYSTEM SPOILER SWITCH QUANTITY STABILIZED AT 39 PERCENT. REPLACED THE SEAL PLATE BETWEEN THE TRAILING EDGE FLAP CONTROL VALVE SDR 95UAL900352Controller · malfunctionedDURING CRUISE AT 330 FEET, HEARD A THUMP, FELT PRESSURE ON EARS AND THE CABIN WAS DESCENDING AT 900 FEET PER MINUTE. SWITCHED TO STANDBY MODE AND WORKED NORMALLY. ON DESCENT THROUGH LANDING ALTITUDE, CONTINUED TO DESCEND AT 500 FEET PER MINUTE. THE CABIN PRSDR 95UAL900331Strip · inoperativeEMERGENCY ESCAPE PATH LIGHTING INOP AT ROW 13. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP. CHECKS O.K.SDR 95UAL900326Eel · inoperativeFORWARD GALLEY EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED LIGHT ASSEMBLY. CHECKS O.K.SDR 95UAL900320Bulb · failedEMERGENCY OVERWING EXIT LIGHTS INOP ON BOTH THE LEFT AND RIGHT SIDES. REPLACED BULBS. CHECKS O.K.SDR 95UAL900299Battery Pack · inoperativeEMERGENCY EXIT LIGHTS INOP IN AFT GALLEY AND DOOR TWO RIGHT. REPLACED BATTERY PACK. CHECKS O.K.SDR 95UAL900296Eel Strip · inoperativeEMERGENCY ESCAPE PATH LIGHTING INOP AT ROWS 19 AND 20. RERPLACED LIGHT STRIP. CHECKS O.K.SDR 95UAL900289Eel · looseEMERGENCY ESCAPE PATH LIGHTING INOP AT ROW TWO. SECURED LOOSE LIGHT STRIP, CHECKS OK.SDR 95UAL900279Position Ind · malfunctionedON APPROACH AT ORD, FLAPS DID NOT INDICATE PAST 10 DEGREES WHEN 25 DEGREES SELECTED. INITIATED GO AROUND, SELECTED FLAPS 15 DEGREES. AFTER A FEW SECONDS, FLAPS INDICATED 15 DEGREES. DIVERTED TO IND. FLAPS OPERATED NORMALLY INTO IND. LIGHT RIME ICE ENCOUNTSDR 95UAL900278Eel Power Cable · failedEMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 12 TO 15. REPLACED POWER CABLE, CHECKS OK.SDR 95UAL900275Seal · leakingPRESSURE LEAK AT DOOR ONE LEFT AT LOWER FORWARD CORNER. REPAIRED LOWER FORWARD DOOR HINGE SEAL, CHECKS OK.SDR 95UAL900267Overheat Control · inoperativeCREW REPORTS RIGHT WING BODY OVERHEAT LIGHT FLICKERED DURING FLIGHT. TURNED OFF BLEED AND CLOSED ISOLATION VALVE, NO HELP. DIVERTED TO IAD. REPLACED THE OVERHEAT CONTROL UNIT. CHECKS O.K.SDR 95UAL900265Lever Assy · wornAILERON AUTOPILOT ACTUATOR LEVER ASSEMBLY WAS FOUND WITH SHEAR FASTENERS SHEARED. ONE FASTENER MAINTAINED CONNECTION BETWEEN THE POWER CONTROL UNIT AND THE LEVER ASSEMBLY. THE PLAY IN THE ASSEMBLY ELONGATED THE HOLES OF THE LEVER ATTACH HOLES AND CAUSED DRIFSDR 95UAL900259Ac Module · inopAIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE AFTER TAKEOFF. AIR CONDITIONING RELAY MODULE OPERATIONALLY CHECKS PACKS OK. AFTER ARRIVING AT GATE, FOUND NO PACK OPERATION. REPLACED THE AIR CONDITIONING ACCESSORY MODULE, CHECKS OK.SDR 95UAL900258Eel · inoperativeONE LIGHT STRIP OF EMERGENCY ESCAPE PATH LIGHTING ROW NR 21 INOP. REPLACED LIGHT, CHECKS OK.SDR 95UAL900235Battery Pack · dischargedEMERGENCY ESCAPE PATH LIGHTING INOP AT ROW FOUR. REPLACED BATTERY PACK. CHECKS O.K.SDR 95UAL900234Control Syst · bindingON TAKEOFF, RUDDER TRIM WAS ADDED WITH NO RESPONSE ON CONTROLS. SEVERAL MINUTES LATER, RUDDER PEDALS KICKED BACK TO RIGHT AND TRIM WAS ADDED INSTANTLY. SYSTEM SEEMS TO BIND. ALSO, BINDS WHEN PUTTING IN LEFT TRIM.
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