Boeing 757-222

Service difficulty reports · 15,539

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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.

SDR 2005UALA00327O-Ring · leakingLOW PRESSURE ON CYLINDER. O-RING LEAK AT FILLER VALVE FITTING. REPLACED O-RING.Apr 8, 2005 · N587UA · Boeing 757222 · Escape SlideSDR 2005UALA00326Aspirator · leakingASPIRATOR FLAPPER VALVE LEAKS. LEAKAGE OF ASPIRATOR FLAPPER VALVE. ASPIRATOR WAS REPLACED.Apr 8, 2005 · N537UA · Boeing 757222 · Escape SlideSDR 2005UALA00322Engine · shutdownRETURNED TO FIELD DUE TO NR 2 ENGINE SHUTDOWN. THE ENGINE EXPERIENCED A SURGE IN THE HPC AND WAS SHUTDOWN. THE ENGINE SURGE WAS CAUSED BY A DISRUPTION IN AIRFLOW THROUGH THE HPC THAT WAS CAUSED BY DAMAGE TO THE COMPRESSOR AIRFOILS. THE AIRFOIL DAMAGE WAS CAUSApr 8, 2005 · N580UA · Boeing 757222 · Engine (Turbine/Turboprop)SDR 2005UALA00365Floor Support · corrodedAFT PIT FLOOR THRESHOLD SUPPORT UPPER AND LOWER SURFACE CORRODED AT STA 1380 TO 1440 RBL 20. DAMAGE CAUSED BY CORROSION IN DOOR CUTOUT AREA AT THE AFT PIT THRESHOLD SUPPORT. PART WAS REPLACED.Apr 7, 2005 · N585UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2005UALA00314Skin · damagedLT FUSELAGE STATION 440 TO 475, STRINGER 16L TO 17L. DAMAGE CAUSED BY CONTACT WITH GROUND EQUIPMENT. DAMAGE SKIN WAS CUTOUT AND DOUBLER REPAIR INSTALLED.Apr 7, 2005 · N594UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00312Skin · gougedFUSELAGE SKIN ON LT SIDE BETWEEN STA 598 AND 604 AT STR 17L IS GOUGED. DAMAGE CAUSED BY CONTACT WITH GROUND EQUIPMENT. DAMAGE WAS CUTOUT AND DOUBLER WAS INSTALLED.Apr 7, 2005 · N594UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00311Skin · damagedFUSELAGE SKIN ON LT SIDE BETWEEN STA 418 AND 435 AT STR 17L IS DAMAGED. DAMAGE CAUSED FROM CONTACT WITH GROUND EQUIPMENT. DAMAGE WAS CUTOUT AND A REPAIR DOUBLER INSTALLED.Apr 7, 2005 · N594UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00309Skin · dentedDENT WAS FOUND AT BS 1708 STR 17R APPROX 2 INCHES LONG. DENT DAMAGE ON FUSELAGE SKIN CAUSED BY IMPACT. DAMAGE TO THE SKIN WAS CUTOUT AND A DOUBLER, TRIPLER, AND FILLER REPAIR STACKUP WAS INSTALLED.Apr 7, 2005 · N584UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00307Stringer · corrodedSTRINGER 22L CORRODED AT STA 700 TO 720. DAMAGE CAUSED BY CORROSION. MAJOR REPAIR ACCOMPLISHED. STRINGER DAMAGE WAS TRIMMED OUT AND A DOUBLER REPAIR WAS INSTALLED.Apr 7, 2005 · N584UA · Boeing 757222 · Fuselage Main, Longeron/StringerSDR 2005UALA00313Warning System · activatedCREW ABORTED TAKEOFF AT APPROXIMATELY 105 KNOTS NECESSARY TO LOCK OUT LEFT HIGH STAGE VALVE. PRIMARY CAUSE OF FAILURE WAS PRESSURE REGULATOR. REPLACED HIGH STAGE PILOT.Apr 7, 2005 · N573UA · Boeing 757222 · Pneumatic Indicating SystemSDR 2005UALA00298Skin · dentedFUSELAGE SKIN DENTED OVER FRAME AT STA 560 BETWEEN STRINGERS 16L AND 17L. DENT IS .070 INCH DEEP. DENT WAS CUTOUT AND THE FUSELAGE SKIN REPAIRED USING A DOUBLER.Apr 6, 2005 · N594UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00310Floorbeam · corrodedAFT CABIN FLOORBEAM IS CORRODED AROUND FASTENERS AT APPROXIMATELY BS 1661 RBL 58. DAMAGE CAUSED BY FLOORBEAM CORROSION IN WET AREAS OF THE CABIN. NEW T-CAP WAS FABRICATED AND INSTALLED TO REPLACE THE DAMAGED PORTION OF THE FLOORBEAM.Apr 5, 2005 · N585UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00308Frame · dentedAFT PIT STA 1580 AT STR 26L FRAME DENTED. FRAME DENT DAMAGE WAS TRIMMED AND A DOUBLER REPAIR WAS INSTALLED.Apr 5, 2005 · N584UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00296Sensor · failedUPON DESCENT, CREW RETRACTED FLAPS AND RECEIVED A FLAP TRAILING EDGE SYS INDICATION. A FAILED FLAP POSITION SENSOR INITIATED A FAILURE PROTECTION SHUTDOWN OF TE FLAP SYSTEM BY THE FLAP SLAT ELECTRONICS UNIT (FSEU NR 1 AND 2), WHICH IN TURN ILLUMINATED TE MASTEApr 4, 2005 · N581UA · Boeing 757222 · Trailing Flap Position Indicating SystemSDR 2005UALA00293Aspirator · crushedFOUND LOWER TUBE ASPIRATOR CRUSHED. SLIDE WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. DAMAGED ASPIRATOR WAS OBSERVED DURING SHOP MAINTENANCE. THE EXACT CAUSE OF THE DAMAGE TO THE ASPIRATOR COULD NOT BE DETERMINED.Apr 4, 2005 · N537UA · Boeing 757222 · Escape SlideSDR 2005UALA00278Skin · delaminatedSLAT NR 6 TRAILING EDGE WEDGE DEPARTED THE AIRCRAFT. LEADING EDGE PANELS DAMAGED AFT OF THE NR 6 SLAT. DELAMINATION OF SLAT'S TRAILING WEDGE (INDUSTRY PROBLEM). WEDGE DAMAGED LEADING EDGE PANELS PRIOR TO DEPARTURE. NEW NR 6 LEADING EDGE SLAT INSTALLED. LEApr 2, 2005 · N524UA · Boeing 757222 · Leading Edge DevicesSDR 2005UALA00368Barrel · damagedDAMAGED ASPIRATOR BARREL. THE EXACT CAUSE OF DAMAGE TO THE ASPIRATOR COULD NOT BE DETERMINED, INVESTIGATION HAS ATTRIBUTED THE CAUSE TO ACCIDENTAL DAMAGE DURING THE LAST PACKING PROCESS.Apr 1, 2005 · N531UA · Boeing 757222 · Escape SlideSDR 2005UALA00367O-Ring · leakingLOW SLIDE PRESSURE. PRESSURE LOSS WAS DUE TO LEAKAGE AT RESERVOIR TO VALVE O-RING. O-RING WAS REPLACED.Mar 31, 2005 · N576UA · Boeing 757222 · Escape SlideSDR 2005UALA00271Floorbeam · corrodedCABIN FLOORBEAM CAP AT FS 365 RBL 33 CORRODED AT EXISTING REPAIR. DAMAGE TO THE FLOOR BEAM CAUSED BY TYPICAL CORROSION. REMOVED THE EXISTING REPAIR AND FABRICATED NEW T-CAP SPLICED INTO EXISTING TEE CAP.Mar 31, 2005 · N585UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00258Wire · damagedLANDED UNDER AMBER ALERT DUE TO NR 2 ENGINE OIL FILTER BYPASS LIGHT. DETECTED A BROKEN SHIELD WIRE AT OIL FILTER SWITCH CONNECTOR. RETURNED TO ORD DUE TO NR 2 ENGINE OVERHEATED AND SHUTDOWN. SUPPLEMENTAL DATA UPDATE CREW REPORTED NR 2 ENGINE OVERHEAT INDICAMar 23, 2005 · N537UA · Boeing 757222 · Overheat DetectionSDR 2005UALA00284O-Ring · leakingLOW BOTTLE PRESSURE. RESERVOIR/VALVE ASSEMBLY PRESSURE GAGE O-RING LEAKING. REPLACED O-RING.Mar 15, 2005 · N583UA · Boeing 757222 · Escape SlideSDR 2005UALA00250Frame · gougedAFT PIT FUSELAGE FRAME GOUGED IN 6 PLACES BS 1520 STR 22R TO 25R. DAMAGE TO FRAMES IN AFT PIT DUE TO NORMAL CARGO LOADING. DAMAGE WAS REMOVED AND REPAIR ANGLE FABRICATED TO REPAIR FRAME.Mar 15, 2005 · N583UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00249Tear Strap · corrodedTEAR STRAP AT STA 1400 BETWEEN STR 27L AND 28L IS CORRODED. DAMAGE CAUSED BY TYPICAL CORROSION. TEAR STRAP REPAIR AND EXTERNAL DOUBLER WAS INSTALLED.Mar 15, 2005 · N583UA · Boeing 757222 · Fuselage Main, StructureSDR 2005UALA00248Skin · dentedEXTERNAL FUSELAGE SKIN IS DENTED AT 5 AREAS AT FUSELAGE STA 600 TO 625 BETWEEN STR 15LT AND 17LT.Mar 15, 2005 · N583UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00247Shear Tie · corrodedCORROSION FOUND AT BS 1400 FRAME FROM STR 27L TO 28L AT SHEAR TIE. DAMAGE CAUSED BY TYPICAL CORROSION. SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS FABRICATED AND INSTALLED.Mar 15, 2005 · N583UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00239Frame · dentedAFT PIT STA 1540, STR 27R, FRAME INBD FLANGE IS DENTED. FABRICATED AND INSTALLED NEW PRODUCTION SPLICE ANGLE EXTENDED TO ACCOMODATE REPAIR TO THE DAMAGED FRAME.Mar 14, 2005 · N583UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00238Frame · dentedAFT PIT STA 1440, STR 26L FRAME INBD FLANGE DENTED. FABRICATED AND INSTALLED NEW PRODUCTION SPLICE ANGLE EXTENDED TO ACCOMODATE REPAIR TO THE DAMAGED FRAME.Mar 14, 2005 · N583UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00242Wire · chafedFOUND WIRES FROM K114 RELAY CHAFING ON CURRENT SENSING TRANSFORMER BRACKET. FOUND HARNESS ARCING AND SMOLDERING. P-34 ELECTRICAL POWER PANEL, WIRE W1134-0024-8 FROM RELAY K114 TERMINAL C1, WAS FOUND CHAFFED AND ARCING ON THE SUPPORT BRACKET OF CURRENT TRANSFMar 14, 2005 · N506UA · Boeing 757222 · Electrical Power System WiringSDR 2005UALA00240Frame · corrodedCORROSION FOUND AT BS 1480 FRAME BETWEEN STR 27L TO 28L, ON INBD FLANGE. DAMAGE CAUSED BY CORROSION. REPAIRED FRAME USING A NESTED J-ANGLE REPAIR DOUBLER.Mar 14, 2005 · N583UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00241Warning Light · malfunctionedDOOR 3L SLIDE LIGHT WOULD NOT GO OFF WITH DOOR DISARMED. ALTHOUGH UNABLE TO DUPLICATE INCIDENT, IT IS SPECULATED CONDITION WAS CAUSED BY DIRT OR DEBRIS ON PROXIMITY SENSORS WHICH AFFECTS THE INDUCTANCE NECESSARY FOR SYSTEM OPERATION.Mar 13, 2005 · N553UA · Boeing 757222 · Escape SlideSDR 2005UALA00283O-Ring · leakingLOW BOTTLE PRESSURE. RESERVOIR/VALVE ASSEMBLY SHAFT O-RING LEAKING. REPLACED SHAFT O-RING AND BACK-UP O-RING.Mar 11, 2005 · N553UA · Boeing 757222 · Escape SlideSDR 2005UALA00234Frame · corrodedDOOR 4L AFT FRAME CORROSION AT STA 1681 BOTTOM OF STR 17L. DAMAGE CAUSED BY TYPICAL FLOOR STRUCTURE CORROSION. DAMAGE WAS REMOVED AND REPAIR ANGLES WERE FABRICATED AND INSTALLED.Mar 10, 2005 · N582UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00233Shear Web · corrodedSHEAR WEB STA 1700 CORRODED FROM RBL 8 TO RBL 38. DAMAGE CAUSED BY TYPICAL AFT PRESSURE DECK WEB CORROSION. CORROSION WAS REMOVED AND THE WEB WAS REPAIRED USING DOUBLERS.Mar 10, 2005 · N582UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00232Skin · damagedSTA 620 BETWEEN STR 16L AND 17L HAS HOLE DAMAGE. HOLE DAMAGE CAUSED DURING INSTALLATION OF AN EXTERNAL FUSELAGE SKIN REPAIR. SHEAR TIE WAS REMOVED, A REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED.Mar 10, 2005 · N582UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00231Shear Tie · damagedSHEAR TIES AT STA 580 BETWEEN STRINGERS 15L-16L, 16L-17L, AND 17L TO 18L HAVE HOLE DAMAGE. HOLE DAMAGE CAUSED DURING INSTALLATION OF EXTERNAL FUSELAGE SKIN REPAIR. SHEAR TIES WERE REMOVED, NEW SHEAR TIES WERE FABRICATED AND INSTALLED.Mar 10, 2005 · N582UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00230Skin · damagedEXTERNAL FUSELAGE SKIN HAS MULTIPLE REPAIRS BS 550 TO BS 630 STR 14L-19L. ORIGINAL DAMAGE CAUSED BY JETWAY IMPACT. MULTIPLE TIME-LIMITED REPAIRS WERE REMOVED AND A PARTIAL SKIN REPLACEMENT WAS ACCOMPLISHED. CONSTANT THICKNESS SKIN SECTION WAS SPLICED IN USINMar 10, 2005 · N582UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00228Shear Tie · corrodedAFT PIT STA 1280, STR 28L TO 29L FRAME SHEAR TIE IS CORRODED. DAMAGE CAUSED BY TYPICAL AFT PIT CORROSION. FABRICATED AND INSTALLED NEW SHEAR TIE.Mar 9, 2005 · N582UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00227Splice · corrodedAFT PIT STA 1620, STRINGER 29L, LONGERON SPLICE HAS CORROSION BEYOND LIMITS. DAMAGE CAUSED BY CORROSION. REMOVED CORRODED STRINGER SPLICE AND INSTALLED NEW STRINGER SPLICE.Mar 9, 2005 · N582UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2005UALA00226Frame · dentedAFT PIT STA 1440, STR 26L FRAME INBOARD FLANGE IS DENTED. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES.Mar 9, 2005 · N582UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00225Frame · dentedAFT PIT STA 1480 AT STR 26L, FRAME IS DENTED ON INBOARD FLANGE. FRAME FLANGE WAS REPAIRED BY EXTENDING THE EXISTING SPLICE ANGLE TO REPAIR THE DAMAGED FLANGE.Mar 9, 2005 · N582UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00224Frame · dentedAFT PIT STA 1460 AT STR 26L FRAME IS DENTED ON INBOARD FLANGE. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES.Mar 9, 2005 · N582UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00223Frame · dentedAFT PIT STA 1580 FRAME DENTED ON INBOARD FLANGE AT STR 26R. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES.Mar 9, 2005 · N582UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00222Frame · dentedAFT PIT FRAME IS DENTED 3 EA PLACES ON INBOARD FLANGE AT BS 1420, BETWEEN STR 23L AND 26L. FRAME FLANGE WAS REPAIRED BY EXTENDING THE EXISTING SPLICE ANGLE TO REPAIR THE DAMAGED FLANGE.Mar 9, 2005 · N582UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00221Frame · dentedAFT PIT AT STA 1540, APPROX AT STR 26R FRAME IS DENTED ON THE INBOARD FLANGE. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES.Mar 9, 2005 · N582UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00216Crease Beam · corrodedRIGHT CREASE BEAM WEB CORRODED BETWEEN BS 1380 AND 1400 RT SIDE. DAMAGE CAUSED BY CORROSION TYPICAL FOUND ON CREASE BEAMS. CREASE BEAM WEB REPLACEMENT WAS FABRICATED AND INSTALLED.Mar 7, 2005 · N582UA · Boeing 757222 · Fuselage Main, StructureSDR 2005UALA00215Shear Web · corrodedSHEAR WEB AT STA 1680, RBL 74 IS CORRODED. REPAIR DOUBLERS WERE INSTALLED TO REPAIR THE AFT PRESSURE DECK WEB.Mar 7, 2005 · N582UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2005UALA00214Floorbeam · corrodedBS 365 FLOORBEAM CORRODED BEYOND LIMITS BETWEEN RBL 59 TO BL 0. TEE CAP WAS TRIMMED AND REPAIR ANGLES AND STRAPS WERE USED TO SPLICE IN NEW SECTION OF TEE CAP.Mar 7, 2005 · N582UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00211Shear Tie · corrodedAFT PIT STA 1620, RBL 2 SHEAR TIE HAS CORROSION. REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED.Mar 4, 2005 · N582UA · Boeing 757222 · Fuselage Main, StructureSDR 2005UALA00209Shear Tie · corrodedPIT SHEAR TIE HAS CORROSION, STA 1600, LBL 9. REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED.Mar 3, 2005 · N582UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00208O-Ring · leakingESCAPE SLIDE BOTTLE HAS LOW PRESSURE. FILLER VALVE O-RING WAS LEAKING. FILLER VALVE O-RING WAS REPLACED.Mar 3, 2005 · N595UA · Boeing 757222 · Escape Slide
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