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 2000UALA00775Skin · dentedFUSELAGE DENT AT FS 760 AND STR 15. DAMAGE MEASURES 3 INCHES LONG, 1.75 INCHES WIDE AND .187 INCHES DEEP. SUPPLEMENTAL DATA UPDATE SKIN, CHANNEL, AND STRINGER WERE REPAIRED PER STRUCTURAL REPAIR MANUAL.SDR 2000UALA00693Housing · looseAPU SHUTDOWN INFLIGHT. SUPPLEMENTAL DATA UPDATE FOUND DRIVEN COMPRESSOR ON APU SCROLL HOUSING P/N 3826140-5, WITH BOLT INSERTS LOOSE AND THREADS DAMAGED. THE BACKSHROUD BOLTS P/N MS9489-27 WERE TORQUED TO SPECIFIC VALUES, BUT STAT-O-SEALS WERE NOT CRUSHED. OSDR 2000UALA00678Line · rupturedAT 8 MIN AFTER TAKEOFF THE LEFT HYDRAULIC QUANTITY EICAS MSG FOLLOWED BY LEFT HYD RSR AND LEFT HYD PRESS LIGHTS CAME ON. SUPPLEMENTAL DATA UPDATE REPLACED LEFT MLG DOWNLOCK ACTUATOR PRESSURE LINE.SDR 2000UALA00677Idg · overservicedDIVERTED TO LAS. RIGHT GENERATOR FAILED, COULD NOT RESET. SUPPLEMENTAL DATA UPDATE REPLACED IDG. REPAIR SHOP FOUND IDG OVER SERVICED.SDR 2000UALA00671Heater · overheatedELECTRICAL ODOR IN FORWARD CABIN DUE TO WATER HEATER OVERHEATING.SDR 2000UALA00658Bearing · failedLEFT OIL FILTER EICAS MESSAGE. SHUTDOWN LEFT ENGINE. *S/D* FOUND FAILED BUMPER BEARING DUE TO ONE ROLLER ROTATING 90 DEG IN THE CAGE. THIS CAUSED THE ROLLER TO SKID AND THE BEARING TO FAIL.SDR 2000UALA00653Line · looseAPU SHUTDOWN AT FL290. *S/D* FOUND LINE AT OIL PUMP OUTLET FITTING LOOSE JUST ABOVE OIL CAP. SECURED LINE. CLEANED AREA AND RAN APU. APU SERIAL NUMBER 61889, TOTAL TIME 434, TOTAL CYCLES 481.SDR 2000UALA00652Apu · lack of lubeAPU SHUTDOWN. ATTEMPTED RESTART, SHUTDOWN AFTER 1 MINUTE. *S/D* FOUND OIL SERVICE CAP FALSE LATCHED AND NO OIL IN SIGHT GAUGE. SERVICED APU OIL TO FULL AND RAN APU FOR AN HOUR. OP CHECKED NORMAL. APU SERIAL NUMBER 61889, TOTAL TIME 433, TOTAL CYCLES 480.SDR 2000UALA00595Valve · failedNOSE GEAR GREEN DOWN LIGHT FAILED ON APPROACH. *S/D* REPLACED NOSE DOOR SEQUENCE VALVE.SDR 2000UALA00577Bottle · dischargedRT OVERWING BOTTLE PRESS INDICATION INOP DURING TEST NR 2 OF SQUIB TEST PANEL ON P-61. *S/D* INSTALLED NEW BOTTLE.SDR 2000UALA00576Structure · vibrationVIBRATION IN CABIN LASTING 50 SECONDS, 300 KNOTS INDICATED AIRSPEED AND CENTER AUTOPILOT ENGAGED.SDR 2000UALA00539Bypass Valve · leakingLEFT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. GEAR AND FLAP WERE EXTENDED BY ALTERNATE METHOD. *S/D* REPLACED SLAT BYPASS VALVE IAW AMM 27-81-09. OPERATIONAL CHECK GOOD.SDR 2000UALA00538Cdu · failedFIRST OFFICER CONTROL DISPLAY UNIT CDU FAILED PRIOR TO CLASS II AIRSPACE. *S/D* REPLACED FIRST OFFICERS CDU PER AMM, CHECKS OK.SDR 2000UALA00523Control Box · failedSPOILER EICAS MESSAGE AND LIGHT ON OVERHEAD PANEL ILLUMINATED. *S/D* REPLACED ELECTRICAL CONNECTOR AT NR 2 LEFT SPOILER AND REPLACED NR 1 RIGHT SPOILER CONTROL MODULE SYSTEM. CKS NORMAL.SDR 2000UALA00526Pump · failedRIGHT AFT BOOST PUMP LOW PRESS LIGHT ON, EICAS MESSAGE RIGHT AFT FUEL PUMP DISPLAYED. *S/D* REPLACED RIGHT AFT BOOST.SDR 2000UALA00521Hose · rupturedSHORTLY AFTER DEPARTURE, THE LEFT HYDRAULIC QTY DROPPED TO .13 AS THE LEFT HYDRAULIC PUMP WAS SHUT OFF, THE HYD QTY DROPPED TO .01. *S/D* FOUND LT MLG SIDE BRACE LOCK ACTUATOR FLEXIBLE HOSE RUPTURED. REPLACED LEFT MLG DOWNLOCK ACTUATOR HOSE. BLED AND LEAK SDR 2000UALA00563O-Ring · failedCREW ABORTED TAKEOFF AT 135 KNOTS DUE TO LEFT ENGINE FIRE WARNING. *S/D* ONE FUEL TRANSFER TUBE B-NUT FOUND LOOSE. THE NUT AND O-RING WERE REINSTALLED, SEATED BY HAND AND THEN RETORQUED. THE SYSTEM WAS PRESSURIZED AND RUN AT IDLE POWER, WITH NO LEAKS NOTESDR 2000UALA00513Circuit Board · defectiveAT APPROX 130 KT, MASTER WARNING AND CONFIG LIGHTS ILLUMINATED ACCOMPANIED BY FLAPS EICAS MESSAGE. T/O WAS ABORTED. *S/D* SHOP TESTED THE SUBJECT T/O CONFIG WARNING CARD AND FOUND AN INTERMITTENT FAILURE. REPLACED T/O CONFIG WARNING MODULE M620.SDR 2000UALA00510Unknown · odorELECTRICAL SMOKE ODOR NOTED IN THE COCKPIT. ODOR WAS FOUND EMANATING FROM F/OS POSITION. SUSPECT F/OS FMC CDU DUE IT RESYNCHING SEVERAL TIMES. PERFORMED CHECK OF LIGHTS AND BALLASTS AND PERFORMED PAC TEST. NO SMELL DETECTED. LOOKED AT VENT OF LEFT AND RIGSDR 2000UALA00511Pump · failedAFTER TAKEOFF NOTICED CENTER HYDRAULIC QUANTITY DECREASING. SECURED CENTER HYDRAULIC PUMPS AT .72 QUANTITY. *S/D* REPLACED NR 2 CENTER AC MOTOR PUMP.SDR 2000UALA00449Transmitter · failedRT HYDRAULIC QUANTITY ZERO AND NO PRESSURE. *S/D* THIS WAS AN INDICATION PROBLEM. REPLACED QUANTITY TRANSMITTER.SDR 2000UALA00447Fire Warning · false indicationWHEEL WELL FIRE INDICATION ILLUMINATED. *S/D* REPLACED DEFECTIVE DUCT LEAK AND WHEEL WELL FIRE CONTROL CARD. VENDOR REPORTED PART RECEIVED (P/N 3500838 38) WAS VERY DUSTY WITH FASTENERS FOUND LOOSE ON RELAY BOARD SIDE; CODE 84 IN MEMORY.SDR 2000UALA00436Skin · crackedFIVE FEET FORWARD OF DOOR 2 LEFT HAS A 14 INCH DENT WITH A 9 INCH CRACK IN SKIN. *S/D* REPAIRED PER SRM 53-00-01 FIGURE 204.SDR 2000UALA00448Access Door · damagedTAIL CONE AND AUXILIARY POWER UNIT DOOR ON LEFT SIDE, AFT OF HORIZONTAL STABILIZER, IS DAMAGED. *S/D* MAJOR REPAIR ACCOMPLISHED WHERE THE FOLLOWING PARTS WERE REPLACED: APU DOOR SUPPORT LONGERON (148N8201-1), APU COMPARTMENT FRAME (148N1604-1), APU COMPARTMSDR 2000UALA00441Battery · dischargedELECTRONIC INDICATION AND CREW ALERT SYSTEM MESSAGE, MAIN BATTERY CHARGER DISPLAYED AND BATTERY DISCHARGER LIGHT EXTINGUISHED. *S/D* REPLACED BATTERY CHARGER AND MAIN BATTERY. SHOP FINDINGS REPORTS BATTERY DISCHARGED.SDR 2000UALA00427Generator · failedLOSS OF AUXILIARY POWER UNIT GENERATOR. *S/D* LINE MAINTENANCE PERFORMED AN OIL SERVICE TO THE AUXILIARY POWER UNIT FOLLOWED BY AN OPERATIONAL CHECK WHICH WAS SATISFACTORY.SDR 2000UALA00417Light · inoperativeDOOR 1 RIGHT SLIDE LIGHT INOPERATIVE.SDR 2000UALA00410Eec · failedRIGHT HAND ENGINE EXPERIENCED POWER FLUCTUATIONS. *S/D* REMOVED FUEL CONTROL UNIT, P/N 779100-5, REMOVAL CAUSE NOT CONFIRMED ON TEST STAND. REMOVED ELECTRONIC ENGINE CONTROL, (P/N 783600-14-071), OEM REPLACED FAILED PRESSURE TRANSDUCER.SDR 2000UALA00413Slide · deployedAFT GALLEY DOOR SLIDE WAS INADVERTENTLY DEPLOYED. *S/D* SLIDE INADVERTENTLY BLOWN BY CONTRACT CLEANERS.SDR 2000UALA00411Duct · looseOVERHEAD AIR CONDITIONING DUCT BLOCKED. *S/D* AIRCRAFT WAS FOUND WITH 5 SECTIONS OF OVERHEAD DUCT PULLED AWAY FROM CEILING SUPPORTS. 2 SECTIONS FROM MONITOR NR 2 TO ROW 10 HAD SUPPORT BRACKET FAILURES. THREE ADDITIONAL DUCT SECTIONS FAILED BETWEEN ROWS 15 SDR 2000UALA00412Controller · surgesNUMBER 1 ENGINE SURGED FROM 1.10 TO 1.22 ENGINE PRESSURE RATIO. *S/D* REPLACED HIGH STAGE CONTROLLER.SDR 2000UALA00401Light · inoperativeAFT MAIN ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. *S/D* RELAMPED ACCORDINGLY. OPERATIONAL CHECK SATISFACTORY.SDR 2000UALA00388Sensor · failedFLIGHT DECK TEMPERATURE UNCONTROLLABLE. *S/D* REPLACED THE RIGHT MIX MANIFOLD AND PACK TEMPERATURE SENSORS WITH NEW SENSORS. ALSO, REPAIRED BROKEN GROUNDING JUMPER AT THE RIGHT PACK TEMPERATURE SENSOR.SDR 2000UALA00387Flight Dir · malfunctionedAUTOPILOT AND BOTH FLIGHT DIRECTORS REFUSED TO TRACK AND ARE UNRELIABLE. *S/D* ACCOMPLISHED CAT III CHECK REF MM 22-10-00, AND ILS OP CK. NO PARTS WERE REPLACED AND NO FURTHER DISCREPANCIES HAVE BEEN REPORTED.SDR 2000UALA00385Light · inoperativeEMERGENCY SLIDE LIGHT AT DOOR 2 RIGHT IS INOPERATIVE. *S/D* SLIDE LIGHT WAS RELAMPED.SDR 2000UALA00384Connector · failedLEFT HAND ELECTRIC HYDRAULIC PUMP FAILED. *S/D* CONNECTOR PIN WAS FOUND BURNED FROM ARCING. REPLACED PUMP AND AC CONNECTOR.SDR 2000UALA00383Carbon Seal · failedBURNING OIL SMELL IN COCKPIT AND CABIN. UPON ENGINE DISASSEMBLY, FOUND ENGINE OIL IN THE LOW PRESSURE COMPRESSOR SHAFT. PRESSURE CHECK OF THE NR 1 MAINLINE BEARING CARBON SEAL CONFIRMED THAT THE CARBON SEAL HAD FAILED.SDR 2000UALA00382Line · leakingLOW HYDRAULIC SYSTEM PRESSURE DISPLAYED ON ENGINE INDICATION AND CREW ALERTING SYSTEM. *S/D* RETURN LINE ON RIGHT MAIN LANDING GEAR DOWNLOCK LEAKING. REPLACED LINE 3.SDR 2000UALA00459Strap · missingNUMBER 3 MAIN ENTRY DOOR SLIDE MISSING D-RING AND STRAP. *S/D* FOUND D-RING BEHIND SHROUD, ATTACHED TO SIDE OF DOOR.SDR 2000UALA00360Antenna · defectiveCOPILOTS VARIABLE OMNI RANGE WILL NOT TEST. *S/D* THE VOR ANTENNA WAS FOUND DEFECTIVE. THE VOR ANTENNA WAS REPLACED.SDR 2000UALA00544Structure · damagedOVER ROTATION ON LANDING CAUSED TAIL STRIKE. *S/D* AIRCRAFT HAD A PREVIOUS TAIL STRIKE PRIOR TO THIS EVENT. THE EXISTING REPAIR WAS ABRADED AWAY BY CONTACT WITH RUNWAY. NO FURTHER DAMAGE WAS DONE TO AIRCRAFT STRUCTURE. REMOVED EXISTING REPAIR, AND RESTORESDR 2000UALA00340Thrust Link · shearedNR 2 ENG FWD MOUNT LEFT HAND THRUST LINK HAS FOUR SHEARED, AND FOUR MISSING ATTACH BOLTS AT THE FWD ATTACH POINT TO THE U FLANGE AT THE BACK OF THE INTERMEDIATE CASE. *S/D* THE BOLTS DID NOT SHEAR, THEY FAILED DUE TO STRESS FRACTURES CAUSED BY VIBRATORY STRSDR 2000UALA00336Slide · damagedDOOR 1 SLIDE/RAFT DEVELOPED SEAM BLISTERS IN BOTH THE SLIDE/RAFT INFLATABLE DOOR SILL PILLOWS DURING SHOP OVERHAUL. THE CAUSE OF THE SEAM BLISTERS IS UNKNOWN. UNIT IS BEING SENT TO THE VENDOR FOR EVALUATION AND REPAIR.SDR 2000UALA00335Slide · leakingDOOR 1 SLIDE FAILED AIR RETENTION TEST WHILE IN THE HOME SHOP FOR OVERHAUL. THE FAILURE OF THE SLIDE TO PASS THE AIR RETENTION TEST WAS CAUSED BY POROSITY IN THE INFLATABLE MATERIAL. THE SLIDE IS BEING SCRAPPED.SDR 2000UALA00285Diode · failedRETURNED TO DEN AND LANDED UNDER AN AMBER ALERT DUE TO AN ELECTRICAL PROBLEM. *S/D* THE LEFT (NR 1) INTEGRATED DRIVE GENERATOR WAS REPLACED. THE IDG HAD AN INTERNAL DIODE FAILURE. C901 GEN CIRCUIT BREAKER WAS REPLACED. THE CIRCUIT BREAKER HAD BURNED AND PSDR 2000UALA00274Hose · rupturedLANDED IN DEN UNDER AMBER ALERT DUE TO HYDRAULIC SYSTEM FAILURE. *S/D* AIRCRAFT EXPERIENCED A COMPLETE LEFT SYSTEM HYDRAULIC LOSS WHEN THE RT MLG PRESSURE HOSE FOR THE UPLOCK ACTUATOR RUPTURED. REPLACED HOSE.SDR 2000UALA00272Unknown · odorRETURNED TO MSP DUE TO ELECTRICAL ODOR IN THE CABIN. *S/D* ODOR REPORTED TO COME FROM MID GALLEY. LINE MAINTENANCE RAN UTILITY BUSSES WITH LOAD FROM MID GALLEY. REMOVED COFFEEMAKER, HOT PLATE AND GALLEY CONT PNL. CHECKED ALL VISIBLE WIRES AND CONNECTIONS SDR 2000UALA00271Axle · fracturedTHE RT MLG WHEEL TRUCK AFT AXEL WAS FOUND BROKEN. *S/D* NR 7 AXLE WAS FOUND COMPLETELY FRACTURED APPROX 18 INCHES FROM AXLE END. CAUSE IS DUE TO STRESS CORROSION CRACKING. THERE MAYBE A POSSIBLE CHROME PLATING ADHESION ISSUE RELEVANT TO OTHER AXLES THAT HASDR 2000UALA00238Sensor · contaminatedAIRCRAFT DIVERTED TO LAX DUE TO THE INABILITY TO START THE APU. *S/D* DUE TO THE CHRONIC NATURE OF REPEATED NO ALTITUDE STARTS, THE APU WAS REPLACED MAY 14, 2000. APU SHOP ACCOMPLISHED A PRELIMINARY BASE CHECK. THE ORIFICE FOR THE COMPRESSOR INLET PRESSURESDR 2000UALA00237Engine · fluctuatesAIRCRAFT DIVERTED TO HNL, DUE TO NR 2 ENGINE POWER FLUCTUATIONS.
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