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.

SDR 2005UALA00206Shear Tie · corrodedAFT PIT STA 1440 SHEAR TIE CORRODED BETWEEN STR 29L AND 30L. A REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED.Mar 2, 2005 · N582UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00205Floorbeam · corrodedFLOORBEAM STA 1640, RBL 44- 48 CORRODED. DAMAGED FLOOR BEAM WAS REMOVED AND A REPAIR USING SPLICE STRAPS AND ANGLES WAS INSTALLED.Mar 2, 2005 · N582UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00204Shear Tie · corrodedAFT PIT STA 1520, RBL 11, SHEAR TIE CORRODED. REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED.Mar 2, 2005 · N582UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00203Floorbeam · corrodedCABIN FLOORBEAM HAS CORROSION ON UPPER TEE CAP STA 324, RBL 46 - 59. TRIMMED TEE CAP AND INSTALLED ANGLE AND STRAP REPAIR FOR TEE CAP SPLICE.Mar 2, 2005 · N582UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00201Battery Pack · inoperativeEMERGENCY LIGHT ON EXTERIOR OF AFT CARGO DOOR, EMERGENCY AISLE LIGHT AT ROW 25, AND MID AISLE EXIT SIGN LIGHT INOP. REPLACED BATTERY PACK FOR POWER SUPPLY.Feb 27, 2005 · N572UA · Boeing 757222 · Emergency LightingSDR 2005UALA00193Compressor · surgesDIVERTED TO HNL DUE TO NR 2 COMPRESSOR SURGE. FOUND VSV SYSTEM 0.125 INCHES OUT OF RIG, ALL OTHER CHECKS OKAY.Feb 27, 2005 · N547UA · Boeing 757222 · Turbine Engine Compressor SectionSDR 2005UALA00190Floorbeam · corrodedFLOORBEAM AT STA 324 RBL 40 CORRODED. DAMAGED AREA OF FLOORBEAM WAS REMOVED AND REPAIR PARTS FABRICATED AND INSTALLED.Feb 27, 2005 · N583UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00191Skin · damagedFUSELAGE SKIN DAMAGE AT STA 600-660 STR 16L. CONSTANT THICKNESS SKIN WAS SPLICED INTO THE SKIN PANEL USING DOUBLER STRAPS AND TRIPLERS.Feb 25, 2005 · N581UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00189Skin · gougedLEFT FUSELAGE SKIN STA 754 HAS 2 EA DENTS WITH GOUGE JUST ABOVE STR 16L. SKIN WAS TRIMMED OUT AND EXTERNAL DOUBLER WAS INSTALLED.Feb 25, 2005 · N581UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00188Frame · dentedAFT PIT STA 1360 FRAME DENTED STR 26L. FRAME WAS TRIMMED AND ANGLE DOUBLERS WERE INSTALLED.Feb 25, 2005 · N581UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00187Skin · dentedFUSELAGE SKIN HAS DENTS STA 413, STR, 15L - 17L. FUSELAGE SKIN WAS TRIMMED AND AN EXTERNAL DOUBLER WAS INSTALLED.Feb 25, 2005 · N581UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00182Frame · dentedAFT PIT STA 1480 FRAME DENTED ON INBD FLANGE AT STR 26L. TYPICAL PIT FRAME UPPER INNER FRAME CAP DAMAGE. FRAME REPAIRED USING NESTED J-ANGLE REPAIR.Feb 23, 2005 · N581UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00181Frame · dentedAFT PIT STA 1460 LT FRAME DENTED AT STR 25L ON INBD FLANGE.TYPICAL PIT FRAME UPPER INNER FRAME CAP DAMAGE. FRAME REPAIRED USING NESTED J-ANGLE REPAIR.Feb 23, 2005 · N581UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00180Frame · dentedFWD PIT FRAME DENTED ON INBD FLANGE AT BS 660 AND STR 24L. TYPICAL PIT FRAME UPPER INNER FRAME CAP DAMAGE. FRAME REPAIRED USING NESTED J-ANGLE REPAIR.Feb 23, 2005 · N581UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00179Frame · dentedFWD PIT STA 640 FRAME DENTED ON INBD FLANGE AT STR 25R. TYPICAL PIT FRAME UPPER INNER FRAME CAP DAMAGE. FRAME REPAIRED USING NESTED J-ANGLE REPAIR.Feb 23, 2005 · N581UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00178Frame · dentedFWD PIT STA 600 FRAME DENTED AT STR 24L ON INBD FLANGE. TYPICAL PIT FRAME UPPER INNER FRAME CAP DAMAGE. FRAME REPAIRED USING NESTED J-ANGLE REPAIR.Feb 23, 2005 · N581UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00176Disc · rupturedLOW BOTTLE PRESSURE. RUPTURE DISC LEAKING. REPLACED RUPTURE DISC.Feb 23, 2005 · N506UA · Boeing 757222 · Escape SlideSDR 2005UALA00177Indicator · leakingLOW BOTTLE PRESSURE. PRESSURE LOSS WAS DUE TO LEAKAGE FROM PRESSURE GAUGE WINDOW. PRESSURE GAUGE WAS REPLACED.Feb 22, 2005 · N587UA · Boeing 757222 · Life RaftSDR 2005UALA00173Shear Web · corrodedAFT CABIN FLOOR, SHEAR WEB CORRODED AT BS 1681 RBL38. AFT PRESSURE DECK SHEAR WEB DAMAGE CAUSED BY TYPICAL GALLEY AREA CORROSION. CORROSION WAS REMOVED AND DECK WEB WAS REPAIRED USING DOUBLERS AND SHIMS.Feb 22, 2005 · N581UA · Boeing 757222 · Fuselage Main, StructureSDR 2005UALA00169Floorbeam · corrodedCABIN FLOORBEAM CORRODED AT BS 1640, RBL 42-57. DAMAGE CAUSED BY TYPICAL FLOORBEAM CORROSION. FLOORBEAM CAP REPAIRED WITH ANGLE AND FILLERS.Feb 20, 2005 · N581UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00167Shear Tie · corrodedAFT PIT SHEAR TIE HAS CORROSION AT BS 1480 BETWEEN STR 28L AND 28R. DAMAGE CAUSED BY TYPICAL AFT PIT CORROSION. SHEAR TIE REMOVED AND REPLACED TO ADDRESS CORROSION.Feb 20, 2005 · N581UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00166Floorbeam · corrodedCABIN STA 324 FLOORBEAM CORRODED BETWEEN RBL 38 AND RBL 44. TYPICAL FLOORBEAM CORROSION DAMAGE IN THE WET AREAS. FLOOR BEAM T-CAP WAS CUT AND REPAIRED USING ANGLES, FILLERS, AND A STRAP.Feb 20, 2005 · N581UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00165Crease Beam · corrodedCABIN LT CREASE BEAM AT STA 670-680, LBL 64 HAS CORROSION. DAMAGE CAUSED BY TYPICAL FLOOR AREA CORROSION AT DOOR SILL LOCATIONS. ANGLE WHICH IS PART OF THE LOWER DOOR SILL INSTALLATION WAS REMOVED AND REPLACED TO ADDRESS THE OUT OF LIMITS CORROSION.Feb 20, 2005 · N581UA · Boeing 757222 · Fuselage Main, StructureSDR 2005UALA00170Floor Support · corrodedCABIN RT FLOOR SUPPORT INNER CHORD AT CUSP AREA IS CORRODED FROM STA 686 TO 740, RBL 60 TO RBL 64.Feb 20, 2005 · N581UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2005UALA00168Floorbeam · corrodedCABIN LT FLOORBEAM CORRODED FROM STA 680-740 LBL 60-LBL64.Feb 20, 2005 · N581UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00162Floorbeam · corrodedAFT CABIN FLOORBEAM HAS CORROSION UPPER CAP STA 1640, RBL 11 TO RBL 12. TYPICAL FLOOR BEAM CORROSION. DAMAGE WAS TRIMMED. NEW SECTION OF FLOOR BEAM WAS SPLICED IN USING SPLICE ANGLES.Feb 16, 2005 · N581UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00161Shear Tie · corrodedAFT PIT SHEARTIE HAS CORROSION STA 1460, BETWEEN STR 28L AND 28R. REPLACED SHEAR TIE.Feb 16, 2005 · N581UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00154Frame · dentedAFT PIT STA 1620 FRAME IS DENTED ON INBD FLANGE AT STR 25R. INSTALLED NESTED J-ANGLE REPAIR.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00153Frame · dentedAFT PIT STA 1620, FRAME IS DENTED AT STR 25L ON INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00152Frame · dentedAFT PIT STA 1560 AT STR 26L FRAME IS DENTED ON INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00151Frame · dentedAFT PIT STA 1360 AT STR 26L FRAME INBD FLANGE IS DENTED. INSTALLED NESTED J-ANGLE REPAIR.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00150Frame · dentedAFT PIT STA 1580 AT STR 26L FRAME IS DENTED ON INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00149Skin · damagedCREASE NEAR BELLY SKIN CENTERLINE AT BS 1420 (EXTERIOR). SKIN DOUBLER REPAIRS AND STRINGER REPAIRS WERE ACCOMPLISHED.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00148Skin · damagedCREASE NEAR BELLY CENTERLINE AT BS 1385 (EXTERIOR). SKIN DOUBLER REPAIRS AND STRINGER REPAIRS WERE ACCOMPLISHED.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00146Shear Tie · corrodedSTA 1400 FRAME SHEAR TIE BETWEEN STR 29R AND 30R IS SEVERELY CORRODED. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00145Shear Tie · corrodedSTA 1400 SHEAR CLIP SEVERELY CORRODED. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00144Shear Tie · corrodedAFT CARGO PIT SHEAR TIE CORRODED AT BS 1340 AND RBL 27. DAMAGE CAUSED BY TYPICAL AFT PIT CORROSION. REPLACED SHEAR TIE.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00143Shear Tie · corrodedAFT PIT FRAME SHEAR TIE IN BILGE AREA IS CORRODED AT STA 1400 BETWEEN STR 28L AND 29L. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00142Shear Tie · corrodedAFT PIT FRAME SHEAR TIE IS CORRODED AT STA 1400 BETWEEN STRINGERS 27L AND 28L. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00141Splice · corrodedAFT PIT STA 1400 LBL 18 CIRCUMFERENTIAL SPLICE IS CORRODED. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. FABRICATED CIRCUMFRENTIAL SPLICE STRAP AND REPLACED CORRODED STRAP.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Main, Attach FittingsSDR 2005UALA00140Frame · dentedAFT PIT STA 1480 FRAME IS DENTED ON INBD FLANGE AT STR 26L. INSTALLED NESTED J-ANGLE REPAIR.Feb 13, 2005 · N578UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00139Frame · dentedFRAME FLANGE AT BS 1540 AND STR 25L DENTED. INSTALLED NESTED J-ANGLE REPAIR.Feb 12, 2005 · N598UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00137Frame · dentedAFT PIT STA 1460 AND STR 25L, FRAME IS DENTED ON THE INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR.Feb 10, 2005 · N598UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00135Skin · dentedEXTERIOR FUSELAGE SKIN AT STA 600 TO 620 BETWEEN STR 15L AND 18L HAS 8 EACH DENTS. PARTIAL SKIN REPLACEMENT ACCOMPLISHED. PARTIAL SKIN PANEL REMOVED AND NEW SECTION SPLICED IN USING SPLICE DOUBLERS AND TRIPLERS.Feb 10, 2005 · N598UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00138Light · inoperativeEMERGENCY SLIDE LIGHT ON EXTERIOR OF AIRCRAFT AFT OF LT WING INOP. RELAMPED PER AMM 33-51-06-201Feb 10, 2005 · N507UA · Boeing 757222 · Emergency LightingSDR 2005UALA00126Floorbeam · corrodedFLOORBEAM UPPER CAP IS CORRODED AT STA 365, RBL 16-73. SUPPLEMENTAL DATA UPDATE TYPICAL FLOORBEAM CORROSION DAMAGE. MAJOR REPAIR ACCOMPLISHED. REPAIRED USING NEW T-CAP SECTION AND SPLICE ANGLES.Feb 7, 2005 · N578UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00134Skin · damagedAREA 20 INCHES AFT OF DOOR 3 RIGHT IS DAMAGED. SKIN WAS HFEC INSPECTED FOR CRACKS AND A DOUBLER REPAIR WAS INSTALLED.Feb 6, 2005 · N598UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00124Floorbeam · corrodedCABIN FLOORBEAM STA 365 HAS CORROSION RBL 3 TO RBL 26 UPPER T-CAP. SUPPLEMENTAL DATA UPDATE DAMAGE CAUSED BY TYPICAL FLOORBEAM CORROSION. MAJOR REPAIR ACCOMPLISHED. DAMAGE TO THE T-CAP REMOVED. T-CAP REPLACEMENT SECTION FABRICATED AND INSTALLED USING SPLICFeb 5, 2005 · N581UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00123Pressure Panel · damagedAFT PRESSURE DECK HAS DAMAGE AT STA 1681 TO 1691, RBL 29 TO RBL 56. SUPPLEMENTAL DATA UPDATE DAMAGE CAUSED BY TYPICAL FLOOR CORROSION UNDER THE GALLEY AREA. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIRS AND INSTALLED NEW DOUBLERS ON THE AFT PRESSURE DFeb 5, 2005 · N578UA · Boeing 757222 · Fuselage Main, BulkheadSDR 2005UALA00122Floorbeam · damagedFLOORBEAM T-CAP IS DAMAGED AT STA 1640, BL-0 TO RBL 61. SUPPLEMENTAL DATA UPDATE EXISTING REPAIR REQUIRED MODIFICATION. ORIGINAL DAMAGE CAUSED BY TYPICAL FLOORBEAM CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR AND INSTALLED NEW T-CAP SECTIOFeb 5, 2005 · N578UA · Boeing 757222 · Fuselage Main, Floor Beam
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