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 2005UALA00451Iru · failedFLIGHT DIVERTED DUE TO RIGHT IRU FAILURE, VISIBILITY RESTRICTIONS AND LOW CEILINGS. CENTER IRU FAULT LIGHT ON, IRU FAIL. REPLACED THE CENTER IRU AND OPS CHECK PER AMM.May 15, 2005 · N541UA · Boeing 757222 · Inertial Guidance SystemSDR 2005UALA00447Slide · tornTORN INFLATABLE SEAM IN DOG LEG. BEYOND SCOPE OF CMM. SEAM AT DOGLEG DISBONDED DURING AIR RETENTION TEST. DISBOND WAS BEYOND CMM REPAIR LIMITS. UNIT WAS RETURNED TO OEM FOR REPAIR AND INFLATABLE WAS REPLACED.May 10, 2005 · N527UA · Boeing 757222 · Escape SlideSDR 2005UALA00436Unknown · malfunctionedLANDED UNDER AMBER ALERT DUE TO A FUEL TRANSFER PROBLEM. UNEXPLAINABLE FUEL TRANSFER FROM RIGHT MAIN TANK TO CENTER TANK. MAINTENANCE ACCOMPLISHED INTERNAL LEAK CHECK OF SYSTEM BY PRESSURIZING FUEL FEED AND FUELING MANIFOLDS USING AIRCRAFT BOOST PUMPS. AFTERMay 9, 2005 · N587UA · Boeing 757222 · Fuel Transfer ValveSDR 2005UALA00434Odor · detectedDIVERTED TO ORD UNDER AMBER ALERT DUE TO AN ELECTRICAL SMELL IN THE FLIGHT DECK. REPLACED FAN.May 9, 2005 · N529UA · Boeing 757222 · Air Distribution SystemSDR 2005UALA00437Unknown · unknownRETURNED TO FIELD DUE TO A LOUD BANG IN THE CAPTAIN'S CONTROL COLUMN. THE SUBJECT DISCREPANCY WAS DUE TO A BROKEN SPRING RETAINER ON THE ELEVATOR TENSION REGULAR WHICH ALLOWED THE SUBJECT TENSION STRING TO BECOME DETACHED. THE SUBJECT TENSION REGULATOR WAS May 8, 2005 · N548UA · Boeing 757222 · Control Column SectionSDR 2005UALA00424Threshold · corrodedAFT PIT STA 1420 RBL 26, CARGO DOOR THRESHOLD T-CAP REPAIR FILLER CORRODED AT THRESHOLD FORMING HORN. INSTALLED NEW T CAP AND REPLACED FILLER.May 7, 2005 · N586UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2005UALA00423Frame · dentedAFT PIT FRAME DENTED STA 1560, STR 26R. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.May 6, 2005 · N586UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00422Door Frame · corrodedDOOR R4 FWD FRAME AT STA 1645 IS CORRODED. REPAIR CONSISTED OF REMOVING CORROSION AND INSTALLING 0.032 REPAIR DOUBLER AS OUTLINED IN REPAIR DOCUMENT.May 6, 2005 · N586UA · Boeing 757222 · Service DoorsSDR 2005UALA00421Frame · dentedAFT PIT FRAME DENTED STA 1480, STR 25L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.May 6, 2005 · N586UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00420Frame · dentedAFT PIT FRAME DENTED STA 1540, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.May 6, 2005 · N586UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00419Frame · dentedAFT PIT FRAME DENTED STA 1460, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.May 6, 2005 · N586UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00418Frame · dentedAFT PIT FRAME DENTED STA 1560, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.May 6, 2005 · N586UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00417Frame · dentedAFT PIT FRAME DENTED STA 1440, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.May 6, 2005 · N586UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00416Frame · dentedFWD PIT FRAME DENTED STA 600, STR 24L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.May 6, 2005 · N586UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00415Stringer · corrodedAFT PIT LWR BILDGE, BETWEEN STA 1440-1460, STRINGER 29L IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED SECTION OF CORRODED STRINGER AND SPLICED IN NEW STRINGER SECTION.May 6, 2005 · N586UA · Boeing 757222 · Fuselage Main, Longeron/StringerSDR 2005UALA00414Frame · dentedAFT PIT FRAME DENTED STA 1420 BETWEEN STR 25 & 26 LEFT. DAMAGE WAS CUTOUT OF FRAME AND REPAIR ANGLES INSTALLED.May 6, 2005 · N586UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00401Floorbeam · corrodedFLOORBEAM AT STA 1640, RBL 60 IS CORRODED. FLOORBEAM WAS BLENDED TO REMOVE CORROSION AND REPAIR STRAP INSTALLED ON THE FLOOR BEAM UPPER CAP.May 2, 2005 · N586UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00400Floorbeam · corrodedFLOORBEAM AT STA 324, RBL CORRODED. FLOORBEAM TEE WAS TRIMMED TO REMOVE CORROSION AND REPAIR ANGLES AND STRAPS WERE SPLICED TO REPAIR THE FLOORBEAM UPPER CAP.May 2, 2005 · N586UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00399Shear Tie · corrodedCIRCUMFERENTIAL FRAME SHEAR TIE CORRODED AT STA 1480 + 3 INCHES LEFT OF STR 30. FABRICATED AND INSTALLED NEW SHEAR TIE.May 2, 2005 · N586UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00398Shear Tie · corrodedCIRCUMFERENTIAL FRAME SHEAR TIE CORRODED AT STA 1460, BETWEEN STR 27L AND 28L. FABRICATED AND INSTALLED A NEW SHEAR TIE.May 2, 2005 · N586UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00391Gauge · defectiveDOOR 2R LOW SLIDE PRESSURE. PRESSURE GAUGE WAS FALLING APART. NO FAULT FOUND. INSPECTION OF PRESSURE VESSEL/VALVE ASSEMBLY REVEALED NO DISCREPANCIES. UNIT WAS OVERHAULED AND RETURNED TO SERVICE.Apr 26, 2005 · N572UA · Boeing 757222 · Escape SlideSDR 2005UALA00387Floorbeam · corrodedAFT CABIN FLOORBEAM UPPER CAP IS CORRODED AT STA 1661 RBL 60. CORROSION WAS REMOVED AND A STRAP REPAIR WAS INSTALLED.Apr 24, 2005 · N586UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00385Reservoir · lowFILL ON LOW SIDE OF GREEN BAND WITHIN MANUAL TOLERANCE. SLIDE WAS REMOVED FROM AIRCRAFT DUE TO LOW INFLATION CYLINDER PRESSURE. WHEN RECEIVED AT COMPONENT SHOP, PRESSURE INDICATOR NEEDLE WAS REPORTED TO STILL BE WITHIN THE GREEN 'GO' BAND. RESERVOIR PRESSUREApr 20, 2005 · N568UA · Boeing 757222 · Escape SlideSDR 2005UALA00374Sensor · failedCOCKPIT TEMPERATURE RISING & UNCONTROLLABLE. CAUSE ATTRIBUTED TO A MIX MANIFOLD SENSOR. REPLACED SENSOR.Apr 19, 2005 · N526UA · Boeing 757222 · Cabin Temperature SensorSDR 2005UALA00359Floorbeam · corrodedCABIN FLOORBEAM CAP CORRODED AT BS 324, RBL 60-64 UPPER SURFACE. FLOORBEAM WAS REPAIRED USING REPAIR ANGLES AND STRAP.Apr 17, 2005 · N585UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00358Skin · dentedEXTERNAL FUSELAGE SKIN AT BS 758, STRINGER 16L IS DENTED. REPAIR DOUBLER AND TRIPLER WERE INSTALLED.Apr 17, 2005 · N585UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00362Transceiver · malfunctionedRETURNED TO LAX DUE TO LOSS OF HF RADIOS. MAINTENANCE OPERATED SYSTEM ON GROUND AND COULD NOT DUPLICATE THE PROBLEM. THE HF SYSTEM FOR LEFT AND RIGHT SIDE OPERATED NORMALLY ON GROUND. AIRCRAFT HAS FLOWN WITHOUT HF PROBLEMS SINCE 4/19/2005. MAINTENANCE DID REApr 16, 2005 · N545UA · Boeing 757222 · Communications SystemSDR 2005UALA00357Frame · dentedDENT ON FRAME STA 1580, JUST ABOVE STR 23L, AFT PIT. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.Apr 16, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00356Frame · dentedFWD PIT FRAME STA 600 ABOVE STR 25L IS DENTED ON UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.Apr 16, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00355Frame · dentedFRAME AT STA 1460 ABOVE STR 25L IS DENTED. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.Apr 16, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00354Frame · dentedFWD PIT RIGHT SIDE STA 660 FRAME HAS DENT BETWEEN STR 25R AND 26R, UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.Apr 16, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00353Frame · dentedFWD PIT LEFT SIDE STA 660 FRAME HAS DENT ABOVE STR 25L UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.Apr 16, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00352Frame · dentedFRAME AT STA 1440 ABOVE STR 25L DENTED. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.Apr 16, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00351Shear Web · corrodedAFT CABIN SHEAR WEB IS CORRODED AT STA 1681 TO 1720 AROUND DRAIN ATTACH FASTENER HOLES RBL 48. CORROSION WAS REMOVED AND A DOUBLER REPAIR INSTALLED.Apr 16, 2005 · N585UA · Boeing 757222 · Fuselage Main, StructureSDR 2005UALA00350Frame · dentedFWD PIT STA 540 LEFT SIDE, FRAME HAS DENT ABOVE STR 25L UPPER FLANGE INTO RADIUS. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.Apr 16, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00349Frame · dentedAFT PIT STA 1540 RIGHT SIDE FRAME HAS DENT ABOVE STR 26R, UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.Apr 16, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00348Frame · dentedAFT PIT STA 1480, FRAME HAS DENT ABOVE STR 26L, UPPER FLANGE. DENT DAMAGE WAS TRIMMED OUT AND A DOUBLER ANGLE REPAIR WAS INSTALLED.Apr 15, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00347Frame · dentedAFT PIT HAS DENTED FRAME, STA 1520, ABOVE STR 25L, DENT IS IN UPPER FWD RADIUS OF UPPER FLANGE. DENT DAMAGE IN FRAME WAS TRIMMED OUT. REPAIR ANGLE WAS INSTALLED.Apr 15, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00346Frame · dentedFRAME DENTED STA 1340, ABOVE STR 25R. DAMAGE TO THE FRAME WAS TRIMMED OUT AND A J-ANGLE DOUBLER REPAIR WAS INSTALLED.Apr 15, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00345Frame · dentedFWD PIT LEFT SIDE STA 640 FRAME HAS A DENT ABOVE STR 25L - 26L, UPPER FLANGE. FRAME DENT WAS ROUTED OUT AND DAMAGE REMOVED. INSTALLED ANGLE DOUBLER.Apr 15, 2005 · N585UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00360Seal · leakingDIVERTED TO ORD DUE TO THE LOSS OF APU OIL QUANTITY. OIL LEAK CONFIRMED IN TEST CELL AT 12:00 WHEN GEARBOX PRESSURIZED (SIMULATES APU OPERATION IN ALTITUDE). STAT-O-SEALS AT THE 12:00 POSITION, BETWEEN THE GEARBOX AND DRIVEN COMPRESSOR WERE LEAKING IN THE THApr 15, 2005 · N574UA · Boeing 757222 · APU Oil SystemSDR 2005UALA00339Stringer · crackedSTRINGER 16L AT BS 758 IS CRACKED.Apr 14, 2005 · N585UA · Boeing 757222 · Fuselage Main, Longeron/StringerSDR 2005UALA00334Girt Bar · damagedGIRT BAR ENGAGEMENT LIGHT EXTINGUISHED WITH EVACUATION SLIDE ARMING LEVER IN ENGAGED POS AT DOOR. DOOR 3R GIRT BAR ENGAGEMENT LIGHT INOP.Apr 13, 2005 · N572UA · Boeing 757222 · Escape SlideSDR 2005UALA00332Skin · damagedEXTERNAL FUSELAGE AT BS 274 BETWEEN STR 21L AND 22L HAS IMPROPER FASTENER INSTALLED, COUNTERSUNK CHERRY MAX RIVET. MAJOR REPAIR ACCOMPLISHED. REMOVED BLIND RIVET AND CUT OUT SKIN DAMAGE AND INSTALLED DOUBLER AND FILLER.Apr 12, 2005 · N585UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00329Skin · damagedEXTERNAL FUSELAGE SKIN HAS BLIND FASTENER INSTALLED AT APPROX BS 746 BETWEEN STR 24L AND STR 25L. MAJOR REPAIR ACCOMPLISHED. REMOVED BLIND FASTENERS, CUT OUT SKIN DAMAGE AND INSTALLED DOUBLER AND FILLER.Apr 12, 2005 · N585UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00321Frame · dentedAFT CARGO FRAME IS DENTED AT STA 1420 AT STR 25-26L. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED.Apr 9, 2005 · N584UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00320Frame · dentedAFT CARGO FRAME STA 1500 AT STR 25L-27L. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED.Apr 9, 2005 · N584UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00319Frame · dentedAFT CARGO FRAME STA 1520 AT STR 25L, FRAME IS DENTED. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED.Apr 9, 2005 · N584UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00318Frame · dentedAFT CARGO FRAME STA 1540, NEAR STR 26L, FRAME DENTED. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED.Apr 9, 2005 · N584UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00315Skin · damagedLT FUSELAGE STA 599 TO 618 STRINGER 16L TO 17L. DAMAGE CAUSED BY CONTACT WITH GROUND EQUIPMENT. DAMAGE WAS CUTOUT AND DOUBLER REPAIR INSTALLED.Apr 8, 2005 · N594UA · Boeing 757222 · Fuselage Main, Plate/Skin
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