Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 95UAL900147Eel Cable · inopEMERGENCY ESCAPE PATH LIGHT STRIP INOP FROM ROW 24 TO 32. REPLACED FEEDER CABLE, CHECKS OK.SDR 95UAL900130Eel Lamp · inopEMERGENCY ESCAPE PATH LIGHTING INOP AT ROW NR 16. RELAMPED. CHECKS O.K.SDR 95UAL900121Eel Lamp · failedEMERGENCY ESCAPE PATH LIGHTING INOP ROW NR 16. RELAMPED, CHECKS OK.SDR 95UAL900114Hinge · brokenRETURNED TO ORD, DUE TO LEFT OVERWING SLIDE DEPLOYED LIGHT AND OVERWING DOOR MESSAGE. A BROKEN HINGE AND IMPROPER LATCHING OF THE SERVICE DOOR AFT OF THE SLIDE COMPARTMENT ACTIVATED THE DOOR SWITCH, WHICH CAUSED THE DOOR OPEN LIGHT. REPLACED HINGE.SDR 95UAL900102Assist Bottle · rupturedDOOR ASSIST BOTTLE FOR DOOR NR 4 RT FOUND EMPTY. REPLACED DOOR ASSIST BOTTLE AND ISOLATED CAUSE AS MATERIAL DEFECT. UAL HAS A RECOVERY PLAN AND IS CORRECTING.SDR 95UAL900101Assist Bottles · dischargedDOOR ASSIST BOTTLES FOR NR 2 RT, NR 4 LT AND NR 4 RT WERE FOUND FLAT. REPLACED DOOR ASSIST BOTTLES AND ISOLATED CAUSE AS MATERIAL DEFECT. UAL HAS A RECOVERY PLAN AND IS CORRECTING.SDR 95UAL900100Compressor · stalledLEFT ENGINE COMPRESSOR STALL ON TAKEOFF OUT OF EWR AT 1,000 FT, HEARD ONE BANG. ENGINE INDICATIONS DID NOT CHANGE. DURING REMAINDER OF FLIGHT, ALL ENG OPERATIONS NORMAL. ENGINE WAS BORESCOPED AND FOUND WITHIN LIMITS, ACCOMPLISHED HIGH POWER RUN, ACCELERATIOSDR 95UAL900095Eel Connector · looseEEL LIGHT INOP AT MID LAV. FOUND EEL CONNECTOR LOOSE RESECURED.SDR 95UAL900078Slide Bottle · failedRT NR 2 SLIDE PRESSURE WILL NOT TEST IN COCKPIT. REPLACED SLIDE BOTTLE.SDR 95UAL900068Eel Inverter · failedEMERGENCY LIGHT INVERTER INOP AT OVERWING LOCATION. REPLACED INVERTER. TESTS OK.SDR 95UAL900062Eel · looseEEL LIGHT COVER LOOSE 2C TO 4C. SECURED LIGHTS AS REQUIRED.SDR 95UAL900060Smoke Detector · inoperativeLAVATORY SMOKE ALARM WON'T TURN OFF. DEBRIEF CABIN CREW FOR SPECIFIC LOCATIONS. SMOKE DETECTOR INOP IN AFT LAV, SYSTEM OP CHECKED OK. SUSPECT PASSENGER BLOCKED OFF DETECTOR.SDR 95UAL900053Reservoir · dischargedPRIOR TO DEPT, LT FWD ENTRY DOOR EMER PWR RESERVOIR PRESSURE THERMALLY DISCHARGED. INSTALLED NEW DISCHARGE KIT AND SERVICED RESERVOIR.SDR 95UAL900031Eel Lamp · failedDOOR 2 RIGHT EMERGENCY EXIT LIGHT INOP. RELAMPED. OP CHECKS OK.SDR 95UAL900018Mechanism · failedSPEED BRAKES AUTOMATICALLY DEPLOYED IN FLIGHT. A/C LOST 1500 FEET WHILE CAPTAIN STOWED SPEED BRAKES. BOTH PILOTS WERE REQUIRED TO PULL A/C FROM NOSE DOWN ATTITUDE. FOUND SPEED BRAKE LEVER RESISTANCE INCONSISTENT. THE SPEED BRAKE MECHANISM WAS FOUND TO BE BSDR 95UAL900015Smoke Detector · malfunctionedABORTED TAKEOFF AT 70 KNOTS DUE TO CARGO PIT FIRE INDICATION. NO EVIDENCE OF FIRE FOUND. REPLACED CARGO SMOKE DETECTOR, SYSTEM OP CHECKS OK.SDR 95UAL900007Eel · inoperativeLEFT FORWARD EMERGENCY OVERWING LIGHT INOP. RELAMPED, OPS CHECKS OK.SDR 95UAL900006Eel · inoperativeRIGHT FORWARD EMERGENCY OVERWING LIGHT INOP. RELAMPED, OPS CHECKS OK.SDR 95UAL900005Eel · inoperativeEMERGENCY LIGHT AT ROW 33 BULLNOSE INOP. RELAMPED, OPS CHECKS OK.SDR 95UAL757019Lock Pin · installedUNABLE TO RAISE NOSE GEAR WHEN GEAR RETRACTED. REMOVED DOWNLOCK PIN FROM NOSE LANDING GEAR.SDR 95UAL757018Engine · malfunctionedRETURN TO IAH DUE TO LOSS OF POWER ON NR 1 ENGINE. HOT GAS IMPINGING ON THE TRANSITION DUCT MOUNT BOLTS CAUSED THEM TO FAIL. THE TRANSITION DUCT BLOCKED THE GAS PATH AND CAUSED THE ENGINE TO STALL.SDR 95UAL757017Eel Strip · inoperativeAFT LT LAVATORY EEL STRIP INOPERATIVE. REPLACED EEL STRIP ASSEMBLY.SDR 95UAL757016Eel Connector · dirtyEEL INOPERATIVE ON ROWS 24ABC TO 32ABC. CLEANED AND DRIED MOISTURE FROM LAMP CONNECTION AT ROW 24. CHECKS OKAY.SDR 95UAL757015Eel Lead · failedEEL STRIP INOP SEAT 9C TO 16C. REPLACED EEL LEAD.SDR 95UAL757014Fuel Pump · oil leakDIVERTED TO DEN UNDER AMBER ALERT WITH NR 2 ENGINE SHUTDOWN DUE TO OIL QUANTITY LOSS. OIL LEAK CAUSED BY FAULTY FUEL PUMP ALLOWING OIL TO LEAK THROUGH THE WET SPLINE AREA.SDR 95UAL757013Eel · inoperativeDOOR NR 2 EXTERIOR EEL LIGHT INOP. RELAMPED OPS CHECKS OK.SDR 95UAL757012Actuator · malfunctionedLANDED UNDER AMBER ALERT DUE TO SLAT ASYMMETRY INDICATION. SLAT CORRECTED FROM FLAP ORIGINALLY REPORTED. REPLACED NR 6 SLAT ROTARY ACTUATOR.SDR 95UAL757011Fuel Return Line · cross threadedEXPERIENCED NR 2 ENGINE FIRE. SECURED ENGINE AND ACTIVATED FIRE EXTINGUISHERS. FOUND THE HPT CASE COOLING VALVE FUEL RETURN LINE CROSS THREADED AT THE 2.5 BLEED VALVE FUEL PRESSURE RETURN LINE.SDR 95UAL757010Sensor · failedLANDED UNDER AMBER ALERT, BECAUSE THE LEADING EDGE DEVICES WOULD NOT EXTEND. REPLACED THE NR 1 SLAT POSITION SENSOR. SYSTEM OP CHECKED OK.SDR 95UAL757008Engine · malfunctionedNR 1 ENGINE SHUTDOWN PRIOR TO TOP OF DESCENT. NO PRIOR THROTTLE MOVEMENT OR CHANGE IN FUEL CONFIGURATION. A/C DESCENDED TO 16,000 FEET WHERE ENGINE WAS RESTARTED, A/C CONTINUED WITHOUT FURTHER INCIDENT. THE FUEL CONTROL UNIT WAS REMOVED AND ROUTED TO HAMILSDR 95UAL757009Bearing · spalledAIRCRAFT DIVERTED AND LANDED UNDER AMBER ALERT DUE TO AN OIL FILTER BYPASS LIGHT ON. THE NR 1 BEARING FAILED. FOUND HEAVY SPALLING OF THE OUTER RACE. APPEARS TO BE AN ISOLATED INCIDENT.SDR 95UAL757007Fan Blade · bentON TAKEOFF FROM SMF, INGESTED ONE BIRD IN THE RIGHT ENGINE. DAMAGE DONE TO AT LEAST TWO BLADES. ODOR IN CABIN. INITIAL VIB 22. VIBRATION NOTED AT ALL POWER SETTINGS. PEEK VIBRATION EPR 1.05. BIRD INGESTION REQUIRED REPLACEMENT OF TWO FAN BLADE PAIRS.SDR 95ZZZX1991Eec · defectiveEEC EXHIBITS FRACTURED SOLDER JOINTS: CHAN 'A' PROCESSOR BD. LOCATION U427, PIN NR 15 (UVPROM) BD ASSY 781336-9-068, SN 89011490. CHAN 'B' PROCESSOR BD. LOCATION U427, PIN NR 14 (UVPROM) BD ASSY 781338-9-068, SN 89012339. CAUSE OF FRACTURING IS UNKNOWN ATSDR 95UAL757006Rstract Mech · malfunctionedDURING APPROACH THE FLIGHT CREW WAS UNABLE TO EXTEND FLAPS FULLY. OP CHECKED FLAPS, BITE CHECKED FLAP SLAT ELECTRONIC UNIT, AND VISUALLY INSPECTED FLAPS. NO DEFECTS FOUND.SDR 95UAL757005Eel Battery Pack · dischargedEEL LIGHTS INOP ROWS 24 TO 32. REPLACED BATTERY PACK M735.SDR 95UAL757004Engine · malfunctionRIGHT ENGINE MADE UNCOMMANDED INCREASE TO MAX POWER. SHUTDOWN ENGINE. DISASSEMBLY SHOWED SIGNS OF METAL SLIVERS ON THE LOW SIDE OF THE PRESSURE RELIEF VALVE WHICH CAUSED THE VALVE TO MALFUNCTION.SDR 95UAL757003Eel Power Cable · failedEEL INOP ROW 25C-32C. REPLACED POWER CABLE. OPS CKS OK.SDR 95UAL757002Eel Battery · dischargedEMERGENCY EXIT SIGNS IN FIRST CLASS INOP. SIGNS POWERED BY SAME BATTERY. REPLACED BATTERY, OPS CKS OK.SDR 95UAL757001Slide · damagedDURING OVERHAUL OF THE RIGHT OFF-WING SLIDE, THE WEBBING BETWEEN THE RAMP AND SLIDE PORTION OF THE UNDERSIDE DISBONDED FROM THE LOWER TRUNK TUBE. RE-ATTACHED DISBONDED WEBBING WITH ADHESIVE.
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