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 2004UALA00132Wire Harness · damagedEQUIPMENT CTR LIGHT, DRAIN MAST HTR GND, SEAT BELT SIGNS, RT FWD ENTRY AND ATTENDANT LIGHTS, FUEL VALVE QTY CTL LIGHT, SIDEWALL LIGHT, RT SIDEWALL LIGHT, CONT SIDEWALL LIGHT, ENTRY GALLEY LIGHTS, RT CEILING LIGHT AND CTL CEILING CIRCUIT BREAKERS FOUND POPPED. SDR 2004UALA00139Actuator · failedON FLAP RETRACTION THE L/E FLAP DISAGREE EICAS MESSAGE ILLUMINATED. EXCESSIVE TORQUE FORCES IN THE LE SLAT DRIVE SYSTEM INITIATED A LE SLAT DISAGREE FAULT WHICH WAS DETECTED BY THE FLAP/SLAT ELECTRONIC UNIT (FSEU) LE SLAT MOVEMENT IS AUTOMATICALLY INHIBITED SDR 2004UALA00124Skin · damagedFUSELAGE SKIN IS DAMAGED AT BS 1440 AND SKIN LAP 20L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2004UALA00126Skin · dentedSKIN DENT STATION 1718 AND STRINGER 14L LAP JOINT. MAJOR REPAIR. INSTALLED DOUBLER REPAIR.SDR 2004UALA00125Skin · dentedSMALL SKIN DENT BELOW AND FWD OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2004UALA00127Skin · dentedSKIN DENTS STA 600-640, AND STRINGER 14L-19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER TRIPLER REPAIR.SDR 2005UALA00159Engine · fluctuatesDIVERTED TO HNL DUE TO NR 2 ENGINE POWER FLUCTUATION. AS A PRECAUTIONARY MEASURE BOROSCOPED ENGINE TO CHECK COMPRESSOR HEALTH, RECHECKED CHIP DETECTORS AND OIL FILTER. ALSO REPLACED 10TH STAGE CHECK VALVE.SDR 2004UALA00150Skin · dentedFUSELAGE DENT NEXT TO DOUBLER AT FWD LOWER CORNER OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REMOVED & REPAIRED.SDR 2004UALA00104Stringer · damagedSTRINGER 16L HAS DAMAGE AT STA 617. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE REPAIR.SDR 2004UALA00101Skin · lightning strikeLIGHTNING STRIKE ON EXTERIOR FUSE SKIN APPROX 2.5 INCH FWD OF BS 560 STR 2R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2004UALA00092Lamp · inoperativeDOOR 1R EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECK OK.SDR 2004UALA00729Bottle · dischargedLOW BOTTLE PRESSURE. CAUSE NOT FOUND. BOTTLE TOPPED OFF AND CHECKED FOR LEAKS. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS. THERE WAS NO FAULT FOUND.SDR 2005UALA00099Skin · dentedLT EXT FUSELAGE SKIN AT BS 620 AND STR 16L IS DENTED. INSTALLED PARTIAL SKIN REPLACEMENT USING DOUBLERS AND TRIPLERS.SDR 2005UALA00088Light · deterioratedEMERGENCY EQUIPMENT LIGHT (EEL) STRIPS DETERIORATED THROUGHOUT THE CABIN. REPLACED EEL LIGHT STRIPS.SDR 2004UALA00056Skin · dentedFUSELAGE BS 600L, STRINGER 14L-19L SKIN DENTED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN SPLICE REPAIR.SDR 2004UALA00048Proximity Sensor · malfunctionedGEAR DISAGREE EICAS MESSAGE WITH THE GEAR HANDLE IN THE UP POSITION. AMBER CAUTION LIGHT ILLUMINATED. THE CAUSE WAS A GEAR POSITION PROXIMITY SENSOR. MAINTENANCE JACKED THE AIRCRAFT AND CLEANED MULTIPLE PROXIMITY SENSOR TARGETS.SDR 2004UALA00045Skin · dentedTHERE ARE TWO SMOOTH DENTS FWD OF DOOR 2L ON AN EXISTING PATCH. EACH DENT IS APPROX 2 INCHES WIDE BY .125 INCHES DEEP. MAJOR REPAIR ACCOMPLISHED. REPLACED EXISTING DOUBLER WITH DOUBLER-TRIPLER.SDR 2004UALA00041Skin · dentedEXTERNAL FUSELAGE STA 600-620 HAS 3 DENTS OUT OF LIMITS BETWEEN STR 16L-17L. MAJOR REPAIR ACCOMPLISHED. REPLACED EXISTING REPAIRED SKIN SPLICE.SDR 2004UALA00040Shear Tie · crackedBS 620 AT STR 18L-19L, SHEAR TIE CRACKED ON BOTH ENDS. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE.SDR 2005UALA00061Frame · dentedAFT PIT STA 1500 FRAME DENTED AT STR 25 LT ON FRAME INBD FLANGE. REPAIRED FRAME WITH NESTED J-ANGLE.SDR 2005UALA00060Frame · dentedAFT PIT STA 1440 FRAME DENTED STR 26 LT AT INBD FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR.SDR 2005UALA00059Frame · dentedAFT PIT STA 1460 FRAME DENTED STR 26 LT ON INNER FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR.SDR 2005UALA00067Window Frame · crackedRT CABIN WINDOW FRAME NR 4 IS CRACKED DUE LIGHTNING STRIKE. INSTALLED NEW WINDOW FRAME.SDR 2005UALA00066Frame · crackedRT CABIN WINDOW FRAME NR 6 IS CRACKED DUE LIGHTNING STRIKE. INSTALLED NEW WINDOW FRAME.SDR 2004UALA00390Indicator · faultyABORTED TAKEOFF AT 100KTS DUE TO A CAPT AIRSPEED INDICATOR PROBLEM. THE CAPTAIN'S AIRSPEED INDICATOR WAS REPLACED.SDR 2004UALA00033Skin · gougedLEFT WING INBOARD TRAILING EDGE AFT FLAP IS GOUGED. MAJOR REPAIR ACCOMPLISHED. REPAIRED AFT FLAP PER SRM 57-53-01 AND TIMCO REO (EVA) G-09637.SDR 2004UALA00029Skin · dentedDENT ON LEFT SIDE OF FUSELAGE, MEASURES .125 INCH DEEP BY 3 INCH WIDE, LOCATED AT BS 610 BETWEEN STR 15L-16L JUST BELOW WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2004UALA00025Sill · corrodedCORROSION FOUND ALONG AFT PIT LOWER DOOR SILL, ADJACENT STRINGER 26R, BS 1380-1440. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW STRAP REPAIR.SDR 2004UALA00028Light · burnedON ENGINE SHUTDOWN, ELECTRICAL ODOR IN COCKPIT. FOUND PARKING BRAKE ANNUNCIATOR BASE AND LENS ASSEMBLY FAILED. REPLACED LIGHT ASSEMBLY AND BASE L413.SDR 2004UALA00389Warning System · activatedRETURNED TO THE FIELD WITH A SLAT DISAGREE MESSAGE. EXCESSIVE TORQUE LOAD IN SLAT DRIVE SYSTEM. ACCOMPLISHED SLAT LUBE AND PERFORMED BITE OF ALL THREE FSEU'S. FOUND NO CURRENT FAULTS. PREVIOUS FLIGHT FAULTS INDICATE LE SLAT DISAGREE WITH NO FAULTED UNIT. FOUNDSDR 2005UALA00022Floorbeam · corrodedCABIN FLOORBEAM T-CAP CORRODED ON PREVIOUS REPAIR DOUBLER AT BS 1640, RBL 48-56.SDR 2005UALA00021Frame · dentedFWD PIT FUSELAGE FRAME PRODUCTION SPLICE HAS A DENT ON INNER FLANGE AT STA 580 ABOVE STR 26L.SDR 2005UALA00020Floorbeam · corrodedCABIN FLOORBEAM AT STA 324 RBL 40 IS CORRODED BEYOND LIMITS.SDR 2005UALA00019Floorbeam · corrodedFLOORBEAM HAS AREAS OF CORROSION FROM BL 0 TO RBL 60 AT BS 365.SDR 2005UALA00018Attach Angle · corrodedATTACH ANGLE FOR BS 940 FRAME BELOW LEFT FWD OVERWING DOOR CUTOUT CORRODED BETWEEN STR 16L.SDR 2005UALA00017Shear Web · corrodedCABIN AFT FLOOR SHEAR WEB HAS UPPER SURFACE CORROSION IN AREAS FROM BS 1680-1720 FROM LBL 62 TO RBL 56.SDR 2005UALA00011Frame · dentedAFT CARGO PIT STA 1480 BETWEEN STR 25L AND 27L FRAME DENTED.SDR 2004UALA00001Actuator · jammedAFTER TAKEOFF WITH FLAP HANDLE SELECTED TO UP HAD A LE EDGE SLAT DISAGREE MESSAGE AND LIGHT. FOUND JAMMED NR 3 LEADING EDGE (LE) SLAT ROTARY ACTUATOR. JAMMING WAS ATTRIBUTED TO EXCESSIVE TORQUE LOADING IN THE LE SLAT DRIVE TORQUE TUBE SYSTEM. NR 3 ROTARY ACTSDR 2004UALA00037Skin · damagedREMOVED SKIN SPLICE DOUBLER AND UPPER LAP TRIPLER AT LEFT SIDE FUSELAGE STA BS 593 IN ANTICIPATION OF SKIN SECTION REPLACEMENT. MAJOR REPAIR ACCOMPLISHED. REINSTALLED SKIN SPLICE DOUBLER AND UPPER LAP TRIPLER.SDR 2005UALA00009Frame · dentedAFT PIT FRAME UPPER FLANGE DENTED AT BS 1460 STR 25L.SDR 2005UALA00007Frame · dentedAFT PIT FRAME UPPER FLANGE DENTED AT BS 1400 STR 26L.SDR 2005UALA00006Frame · dentedFRAME AT STA 1500 AND STR 26L-25L IS DENTED.SDR 2005UALA00005Frame · dentedFRAME AT STA 1520 AND STR 26L AND 25L IS DENTED.SDR 2005UALA00004Frame · damagedAFT PIT STA 1560 STR 25L FRAME IS DAMAGED.SDR 2005UALA00003Floorbeam · corrodedCABIN FLOORBEAM CAP AT STA 324 CORRODED FROM RBL 30 TO RBL 63.SDR 2005UALA00002Frame · dentedAFT CARGO PIT FRAME UPPER FLANGE DENTED AT BS 1420 STR 27L.SDR 2004UALA00724Valve · dischargedLOW BOTTLE PRESSURE. PRESSURE RELIEF VALVE DEFECTIVE. PRESSURE GAUGE WAS REPLACED WHICH INCLUDED REPLACEMENT OF PRESSURE RELIEF VALVE. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS.SDR 2003UALA00990Connector · contaminatedRIGHT ENG PRI CONT AND AUTO THROTTLE EICAS STATUS MESSAGE. AFTER TROUBLESHOOTING THE ENTIRE WIRING SYSTEM, A SMALL WIRE-LIKE FILAMENT WAS FOUND CROSSED BETWEEN TWO PINS INSIDE AN EEC CONNTECTOR. UPON CLEANING THE CONNECTOR AND RE-POSITIONING THE PINS, TESTS SDR 2003UALA00982Idg · inoperativeABORTED TAKEOFF DUE TO LT IDG LIGHT. LEFT INTEGRATED DRIVE GENERATOR (IDG) FAILED. REPLACED THE LEFT IDG. NORMAL WEAR, REPLACED THE PUMP AND MOTOR ASSEMBLY.SDR 2004UALA00721O-Ring · failedLOW BOTTLE PRESSURE. BOTTLE TO VALVE O-RING WAS DETERIORATED. REPLACED CYLINDER ASSY. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS.
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