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 2003UALA00709Actuator · failedRIGHT MAIN GEAR DOOR FOUND FULL OPEN UPON GATE ARRIVAL. FAILED MLG DOOR RETRACT ACTUATOR. ACTUATOR WAS REPLACED.SDR 2003UALA00706Frame · damagedFRAME DAMAGED AT FUSELAGE STA.1681 AT WL210.SDR 2003UALA00690Shaft · shearedLOSS OF LEFT HYDRAULIC SYSTEM. LOST ALL HYDRAULIC FLUID ON LEFT SIDE. THE CAUSE OF THIS FAILURE WAS A SHEARED SHAFT, WHICH CAUSED THE PUMP TO SEIZE AND CRACK THE CASE. THE PUMP WAS REPLACED.SDR 2003UALA00667Battery · damagedMAIN BATTERY CHARGER STATUS MESSAGE. REPLACED MAIN BATTERY. SHOP FINDINGS: FAULT WAS CONFIRMED, ONE BAD CELL WAS FOUND IN THE BATTERY.SDR 2003UALA00643Skin · damagedCREASE & PUNCTURE EXTERNAL FUSELAGE STA 463 TO STA 440 STR 16L &17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00624Skin · damagedEXTERNAL FUSELAGE DAMAGED AT STA 620 STR 8R. INSTALLED DOUBLER REPAIR.SDR 2003UALA00631Wedge · delaminatedT/E WEDGE DELAMINATION MAJOR REPAIR ACCOMPLISHED.REPAIRED T/E WEDGE.SDR 2003UALA00609Carbon Seal · failedSMOKE AND FUMES IN FLIGHT DECK AND CABIN. ENGINE DISASSEMBLY VERIFIED A BAD NR 2&3 CARBON SEAL. WHEN THIS CARBON SEAL LEAKS, PRESSURE BUILDS UP IN THE NR 1&3 AFT COMPARTMENT. EXCESSIVE PRESSURE ALLOWS OIL TO SEEP PAST AND THOSE SEALS AND ALLOWING BURNING OIL SDR 2003UALA00600Blade · failedRIGHT ENGINE COMPRESSOR STALL, EGT OVERTEMP. OIL PRESSURE DROPPED TO ZERO. ENGINE TEARDOWN VERIFIED THAT THE HPT T1 BLADE FAILED. PRATT & WHITNEY HAS BEEN INVESTIGATING THIS FAILURE FOR ROOT CAUSE AND DETERMINED THAT THE SYMPTOMS AND PART CONDITION ARE UNIQUSDR 2003UALA00593Warning Light · illuminatedLEFT HYDRAULIC SYSTEM PRESSURE AND REVERSER EICAS ILLUMINATED. LEFT HYDRAULIC PRESSURE LINE FROM LEFT ELECTRIC HYDRAULIC PUMP FAILED. REPLACED LINE.SDR 2003UALA00601Wedge · delaminatedT/E WEDGE DELAMINATED AND SECTION HAD INFLIGHT SEPARATION. MAJOR REPAIR ACCOMPLISHED. REPLACED T/E WEDGE.SDR 2003UALA00580Skin · dentedLT EXTERNAL FUSELAGE SKIN HAS 4 EA DENTS AT STATION 600-620 AND BETWEEN STR 15-17. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00555Window · unsecureFIRST OFFICER'S WINDOW SQUEAL ON FLIGHT DECK DURING CLIMB. ATTEMPTED TO OPEN AND CLOSE DURING CLIMBOUT. DISCOVERED A LOOSE SEAL COMING OUT OF TRACK WHICH PREVENTED THE WINDOW FROM CLOSING PROPERLY. SEAL WAS REINSTALLED IN TRACK AND WINDOW OPERATED NORMALLY.SDR 2003UALA00602Wedge · delaminatedDELAMINATION AND INFLIGHT SEPARATION OF NR 6 SLAT T/E WEDGE. MAJOR REPAIR ACCOMPLISHED. REPLACED SLAT T/E WEDGE.SDR 2003UALA00548Battery Pack · inoperativeEXIT FLOOR LIGHTING INOP FROM ROWS 23-30. REPLACED BATTERY PACK.SDR 2003UALA00542Structure · failedAIRCRAFT EXPERIENCED LEADING EDGE SLAT PROBLEM. THE NR 6 SLAT TRAILING EDGE WEDGE BROKE APART. A SECTION OF THE TRAILING EDGE WEDGE SEPARATED FROM THE SLAT. THE SUSPECT CAUSE OF DAMAGE WAS CORROSION OF THE ALUMINUM HONEYCOMB IN THE TRAILING EDGE WEDGE DUE TOSDR 2003UALA00513Light · inoperativeEXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE AT DOOR 4L.SDR 2003UALA00516Skin · delaminatedNR 5 SLAT T/E WEDGE LOWER SKIN DELAMINATED. REPLACED 100 PERCENT OF UPPER & LOWER SKIN OF THE T/E WEDGE.SDR 2003UALA00502Pump · failedLOST LEFT HYD SYSTEM PRESSURE AND FLUID. LT ENGINE DRIVEN PUMP FAILED RESULTING IN A LOSS OF HYDRAULIC FLUID AND SYSTEM PRESSURE. LEFT ENGINE DRIVEN PUMP WAS REPLACED AND THE HYDRAULIC SYSTEM WAS SERVICED.SDR 2003UALA00491Lamp · inoperativeEXTERIOR EMERGENCY SLIDE LIGHT, INOPERATIVE AT DOOR 4L. RELAMPED.SDR 2003UALA00461Battery Pack · dischargedAFT CABIN EEL LIGHTS BETWEEN ROW 23 AND 31 INOPERATIVE WITH TEST SWITCH AND MASTER SWITCH IN COCKPIT. REPLACED POWER SUPPLY BATTERY PACK.SDR 2003UALA00462Lamp · burned outLEFT AFT OFF-WING EMERGENCY SLIDE LIGHT AFT OF AFT OVERWING EXIT HATCH INOPERATIVE. RELAMPED LIGHT.SDR 2003UALA00454Bearing · failedEICAS STATUS MESSAGE FWD CARGO DET AIR DISPLAYED. NR 1 LOWER CARGO SMOKE DETECTION SYSTEM BLOWER MOTOR ASSY FAILED. SHOP FINDINGS REVEALED REAR ROTOR BEARING WILL NOT ROTATE. REAR ROTOR BEARING FAILURE.SDR 2003UALA00463Lamp · burned outLEFT AFT OFF-WING EMERGENCY SLIDE LIGHT, AFT OF AFT OVERWING HATCH IS INOPERATIVE. RELAMPED LIGHT.SDR 2003UALA00399Fitting · separatedDOOR 3R GIRT BAR SHOE FITTING SEPARATED FROM GIRT BAR ASSEMBLY. REINSTALLED SHOE ASSY.SDR 2003UALA00505Wedge · delaminatedT/E WEDGE DELAMINATED, SLAT NR 5. MAJOR REPAIR ACCOMPLISHED. REMOVED, REPAIRED AND REINSTALLED T/E WEDGE.SDR 2003UALA00442Bottle · dischargedDOOR 1R ASST BOTTLE FOUND WITH NO PRESSURE. BOTTLE PRESSURE EVACUATED DUE TO RUPTURED BURST DISC ON ASSIST BOTTLE. DOOR ASSIST BOTTLE REPLACED. NO ADDITIONAL DISCREPANCIES NOTED AND NO HISTORY THAT COULD HAVE RESULTED IN EMERGENCY OPERATION OF DOOR.SDR 2003UALA00438Connector · looseEMERGENCY LIGHTS ARE INOP AT EXTERIOR AT DOOR 4L AND EEL LIGHTS, EXIT SIGN AND BULLNOSE LIGHTS BETWEEN ROWS 20-30. RELAMPED AT DOOR 4L AND RESEATED CONNECTORS ON POWER SUPPLIES.SDR 2003UALA00432Wire · brokenEEL LIGHT AFT SECTION FROM ROW 28 IS INOP. POWER FEEDER, BROKEN AT SIDE WALL. REPLACED POWER FEEDER.SDR 2003UALA00426Light · inoperativeAFT EEL STRIP FRONT OF FWD AFT LAV INOP. REPLACED EEL STRIP.SDR 2003UALA00420Skin · damagedSKIN DAMAGED AT STA 470 AT STR 23 RT. MAJOR REPAIR - FILLER AND DOUBLER INSTALLED.SDR 2003UALA00409Windshield · cracked1R COCKPIT WINDSHIELD CRACKED. FIRST OFFICERS WINDSHIELD STARTED ARCING IN LOWER CORNER AND PROGRESSED INTO THE WINDOW UNTIL THE WINDOW SHATTERED. FOD DAMAGED OUTER LAYER OF FIRST OFFICER'S NR 1 WINDSHIELD NEAR CENTER OF WINDSHIELD. THIS DAMAGE RESULTED INSDR 2003UALA00401Cable · shortedEEL LIGHTING OUT AT SEAT 23 TO 31. REPLACED TRACK FEEDER CABLE.SDR 2003UALA00396Light · inoperativeEMERGENCY SLIDE LIGHT OUTSIDE AFT CARGO DOOR INOPERATIVE. RELAMPED.SDR 2003UALA00395Shutoff Valve · failedRECEIVED LT HI-STG LIGHT AND EICAS MSG. REPLACED HI PRESSURE CONTROLLER AND HPSOV. CONTROLLER OVERPRESUURE SWITCH MALFUNCTIONED. HPSOV HAD NFF.SDR 2003UALA00380Compressor · stalledNR 2 ENGINE COMPRESSION STALL ON TAKEOFFSDR 2003UALA00379Engine · failedAIRCRAFT LOST NR 2 ENGINE AT ROTATION.SDR 2003UALA00328Frame · dentedAFT PIT STA 1480 JUST ABOVE AND BELOW STR 25L FRAME TO FLANGE DENTED MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIRSDR 2003UALA00327Frame · dentedAFT PIT STA 1400 BETWEEN STR 25L AND 26L, FRAME UPPER FLANGE DENTED IN TWO AREAS MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIRSDR 2003UALA00326Frame · dentedAFT PIT STA 1360 ABOVE STR 26L, TOP OF FRAME FLANGE IS DENTED MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIRSDR 2003UALA00325Frame · dentedAFT PIT STA 1440 BETWEEN STR 25L AND 26L UPPER FRAME FLANGE DENTED IN TWO AREAS MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR.SDR 2003UALA00324Frame · dentedAFT PIT STA 1420 BETWEEN STR 25L AND 26L, UPPER FRAME FLANGE DENTED MAJOR REPAIR ACCOMPLISHED. PERFORMED FRAME REPAIR.SDR 2003UALA00323Frame · dentedAFT PIT AT STA 1340 BETWEEN STR 25L AND 26L, TOP OF FRAME IS DENTED MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR.SDR 2003UALA00286Light · burned outRIGHT AFT EMERGENCY HATCH HANDLE LIGHT IS INOP RELAMPED.SDR 2003UALA00287Frame · puncturedAFT CABIN FUSELAGE FRAME AT BS 1360, HOLE 3.5 INCHES TO THE RIGHT OF STRINGER 1. AFT SIDE OF FRAME HAS TOOLING MARK OR MISDRILLED SURROUNDING AREA OF HOLE. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIR DONE ON AREA.SDR 2003UALA00288Light · burned outEXTERIOR EMERGENCY SLIDE LIGHT IS INOP AT DOOR 1R. RELAMPEDSDR 2003UALA00273Skin · dentedLH EXTERNAL FUSELAGE HAS JETWAY DAMAGE (DENTS) AT STA 600 TO 620 BETWEEN STR 16L AND 18L. MAJOR REPAIR ACCOMPLISHED.APPLIED DOUBLER.SDR 2003UALA00263Engine · bird ingestionA/C EXPERIENCED BIRD STRIKE IN THE NR 2 (RIGHT) ENGINE. UPDATE ROOT CAUSE DETERMINED TO BE AN 8-12 LB. CANADAN GOOSE. EWR DOES HAVE A WILDLIFE MITIGATION PROGRAM; HOWEVER, DISCUSSIONS ARE CONTINUING TO IMPROVE THEIR PROGRAM.SDR 2003UALA00264Cap · erodedCABIN STA 1640, RBL 57" FLOORBEAM TOP CAP HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. PERFORMED SINGLE FLANGE BLENDOUT REPAIR.SDR 2003UALA00260Proximity Sensor · out of rigA/C RECEIVED GEAR DISAGREE INDICATION. GEAR UP LOCK SENSORS S10069 AND S10239 WERE OUT OF RIG. THESE TWO PROXIMITY SENSORS WERE ADJUSTED PER THE AMM.
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