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 2001UALA00630Crease Beam · corrodedFUSELAGE CREASE BEAM AND WEB CORRODED AT STA 934 STR 17L. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB AND REPAIRED CREASE BEAM.SDR 2001UALA00648Floorbeam · corrodedCABIN FLOORBEAM CAP CORRODED. STA 365 RBL 51 - 60. REMOVED DAMAGE AND INSTALLED NEW T CHORD.SDR 2001UALA00647Skin · dentedFUSELAGE SKIN DENTED STA 1593-1596 BETWEEN STR 14R AND 15R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER.SDR 2001UALA00605Intercostal · corrodedCABIN FLOOR INTERCOSTAL AT STA 365, RBL 42.45 CORRODED. REPLACED INTERCOSTAL.SDR 2001UALA00596Actuator · failedAIRCRAFT ARRIVED AT GATE WITH RIGHT MLG WHEEL WELL DOOR IN OPEN POSITION AND A HYDRAULIC LEAK IN THE SAME WHEEL WELL. GEAR DOOR EICAS MESSAGE ILLUMINATED. *S/D* DOOR RELEASE INTERLOCK ACTUATOR FAILED. REPLACED ACTUATOR.SDR 2001UALA00604Frame · corrodedAFT PIT FRAME HAS EXCESSIVE MATERIAL LOSS STA 1480 STR 27R. MAJOR REPAIR ACOMPLISHED. SPLICED REPAIR FRAME SECTION BETWEEN STR 22R TO 27R.SDR 2001UALA00603Skin · dentedDENT IN FUSELAGE SKIN. STA 615.REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER.SDR 2001UALA00597Skin · dentedDENT IN LT FUSELAGE TWO FEET FWD OF WING ILLUMINATION LIGHT. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER.SDR 2001UALA00573Bleed Valve · malfunctionedAFTER POWER REDUCED TO CLIMB THRUST THE LEFT ENGINE EXPERIENCED A COMPRESSOR STALL. *S/D* REPLACED 14TH STAGE BLEED VALVE (BEANPOT) PRECAUTIONARY.SDR 2001UALA00555Door Frame · crackedAFT CARGO DOOR INTERNAL FRAME CRACKED. STA 1410 AT HOLE FOR SWITCH. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER PER SRM.SDR 2001UALA00554Frame · damagedFRAME DAMAGED AT STA 365 ADJACENT TO STR 17R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED FRAME DOUBLER REPAIR.SDR 2001UALA00553Floorbeam · corrodedCABIN FLOORBEAM CORRODED STA 1640 RBL 10 TO CREASE BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP REPAIR PER SRM.SDR 2001UALA00552Floorbeam · corrodedCABIN FLOORBEAM CORRODED STA 345 RBL 45 AROUND FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR STRAP PER SRM.SDR 2001UALA00551Floorbeam · corrodedCABIN FLOORBEAM UPPER CHORD CORRODED STATION 365.25 BETWEEN BL 0 TO RBL 62. MAJOR REPAIR ACCOMPLISHED.INSTALLED T-CAP REPAIR PER SRM.SDR 2001UALA00550Crease Beam · damagedCREASE BEAM DAMAGED INBOARD ANGLE RIGHT SIDE STA 1130-1133. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED DAMAGE SECTION OF CREASE BEAM USING SRM 51-70-12 TYPICAL EXTRUDED SECTION REPAIR.SDR 2001UALA00549Floorbeam · corrodedFLOORBEAM CORRODED STA 1669-1673 RLB 40. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW FLOOR BEAM PER SRM.SDR 2001UALA00525Skin · dentedFUSELAGE SKIN DENTED LEFT SIDE AT FLOOR LINE BETWEEN STA 460 TO STA 492 STR 17L. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER PER SRM.SDR 2001UALA00524Floorbeam · corrodedFLOOR BEAM STA 324 BL 0 AND RBL 58 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP REPAIR PER AMM.SDR 2001UALA00523Floorbeam · corrodedFLOORBEAM STA 324.8 RBL 42 TO 49 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR ON T-CAP PER AMM.SDR 2001UALA00522Floorbeam · corrodedFLOORBEAM CAP STA 310.5 RBL 44 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR ON T-CAP PER AMM.SDR 2001UALA00497Crease Beam · corrodedCREASE BEAM WEB STA 1076 STR 17R HAS EXCESSIVE MATERIAL LOSS. REPLACED CREASE BEAM PER SRM.SDR 2001UALA00494Floor Support · corrodedMID CABIN FLOOR STRUCTURE SUPPORT ADJACENT TO DOOR 2R BS740 TO BS760 RBL 62 HAS EXCESSIVE MATERIAL LOSS. REPLACED ANGLES PER SRM.SDR 2001UALA00469Web · crackedNR 2 PYLON WEB IS CRACKED OUT OF THE FORWARD RIGHT HAND CUTOUT, ABOVE THE FORWARD MOUNT, AT THE ONE OCLOCK POSITION. MANUFACTURED AND INSTALLED DOUBLERS. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00465Web · crackedNR 1 PYLON WEB CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLERS TO THE AFFECTED AREA. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00464Crease Beam · damagedCREASE BEAM WEB STA 1076 STRINGER 17R HAS EXCESSIVE MATERIAL LOSS. REMOVED AND REPLACED AFFECTED CREASE BEAM WEB. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00463Angle · damagedMID CABIN SUPPORT STRUCTURE ADJACENT TO DOOR 2R BS 740 TO BS 760 RBL 62 HAS EXCESSIVE MATERIAL LOSS. REMOVED AND REPLACED TWO ANGLES. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00462Bulkhead · damagedNR 2 PYLON AFT BULKHEAD NACELLE STA 201.02 RIGHT HAND SIDE VERTICAL FLANGE LOWER CORNER HAS EXCESSIVE MATERIAL LOSS. FABRICATED AND INSTALLED REPAIR CRES PLATES. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00432Crease Beam · corrodedCREASE BEAM WEB STA 1021 STR 17L HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB PER SRM.SDR 2001UALA00431Frame · corrodedAFT CABIN FRAME BS 1681 STR 17R WL 208 IS EXFOLIATED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME PER SRM. INSTALLED DOUBLER ANGLE.SDR 2001UALA00421Skin · dentedFUSELAGE SKIN DENTED AT BS 650 JUST BELOW FLOORLINE STRINGER 17L. INSTALLED DOUBLER PER SRM.SDR 2001UALA00400Switch · failedAPU OIL QUANTITY STATUS MESSAGE ILLUMINATED. RIGHT GENERATOR PREVIOUSLY DEFERRED. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED APU OIL CONSUMPTION CHECK. APU WAS CHECKED ONCE FOR OIL CONSUMPTION AND EXTERNAL OIL LEAKS, AND NO DISCREPANCIES WERE FOUND. SUSPECT THE OSDR 2001UALA00422Skin · dentedDENT IN FUSELAGE SKIN 42 INCHES AFT OF DOOR 2L, STRINGER 16L. INSTALLED DOUBLER AND REPAIRED STRINGER 16L BS 770-780 PER SRM.SDR 2001UALA00388Skin · crackedNR 2 PYLON INBOARD SKIN ACCESS CUTOUT CRACKED. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR PER SRM.SDR 2001UALA00373Floorbeam · corrodedCABIN FLOORBEAM TOP SURFACE AT STA 365, CENTER TO RBL 61 CORRODED. MAJOR REPAIR ACCOMPLISHED.REPLACED T-ANGLE PER SRM.SDR 2001UALA00371Beam · crackedNR 2 ENGINE PYLON FAN COWL SUPPORT BEAM NAC STA 102 LT SIDE INNER ANGLE CRACKED AFT SIDE OF WEB NEAR CENTER CHORD. MAJOR REPAIR ACCOMPLISHED.REPLACED ANGLE PER SRM.SDR 2001UALA00356Floorbeam · corrodedAFT CABIN STA 1640 LBL 8 TO RBL 62 TOP CAP OF FLOOR BEAM HAS HEAVY CORROSION. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. CORROSION DAMAGE RESULTED IN REPLACEMENT OF THE DAMAGED SECTION OF THE UPPER CHORD. A REPLACEMENT SECTION OF THE UPPER CHORD WASSDR 2001UALA00352Doubler · misdrilled3 EACH FIELD FASTENERS ON LWR VHF ANTENNA DOUBLER HAVE NO EDGE DISTANCE TO FWD END OF CUTOUT. STA 1466 RBL 3.23. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.THE CUTOUT EXTENDED FORWARD TO REMOVE SHORT ED HOLES. THE REPAIR TRIPLER AND DOUBLER WERE EXTENSDR 2001UALA00358Channel · corrodedCABIN FLOOR STA 366 RBL 10 FLOOR CHANNEL CORRODED AT FLOOR BEAM ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR CHANNEL.SDR 2001UALA00357Skin · misrepairedRIGHT WING OTBD FLAP UPPER SURFACE NEAR LEADING EDGE HAS SCAB PATCH REPAIR DIRECTLY BELOW NR 10 SPOILER. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FLUSH REPAIR PER SRM.SDR 2001UALA00318Cooling Fan · failedSMOKE IN CABIN. SUPPLEMENTAL DATA UPDATE FOUND COOLING FAN SHAFT SHEARED AND FAN HOUSING BROKEN. THIS IS THE LATEST CONFIGURATION (-6) WHICH WAS INSTALLED ON THIS APU ON JUNE 11, 1999. THIS HAS BEEN A LONG TIME PROBLEM, AND HONEYWELL IS WORKING ON FIXING THESDR 2001UALA00319Frame · wornSTA 1640 STR 5L FRAME FLANGE WORN. MAJOR REPAIR ACCOMPLISHED.REPAIRED FRAME FLANGE PER AMM.SDR 2001UALA00370Actuator · corrodedHORIZONTAL STABILIZER TRIM ACTUATOR PRIMARY BRAKE FAILURE INSIDE UNIT. FOUND EXTREME CORROSION INSIDE AND OUTSIDE OF UNIT. BREAKDOWN OF GREASE DUE TO EXCESSIVE WATER INSIDE UNIT. REPLACED ACTUATOR.SDR 2001UALA00298Floorbeam · corrodedAFT CABIN STA 1661 RBL 0 TOP CAP OF FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR SPLICE PER AMM.SDR 2001UALA00302Spur Gear · failedAPU INOP. SUPPLEMENTAL DATA UPDATE REPLACED APU. FOUND STARTER AND COOLING FAN IDLER DRIVE GEAR BROKEN IN GEARBOX. GEARBOX HOUSING HAS DAMAGE AND WILL PROBABLY BE SCRAPPED.SDR 2001UALA00296Cooling Fan · failedSMOKE IN CABIN AND COCKPIT. SUPPLEMENTAL DATA UPDATE FOUND COOLING FAN SHAFT SHEARED AND FAN HOUSING BROKEN. THIS IS THE LATEST CONFIGURATION (-6) WHICH WAS INSTALLED ON THIS APU ON JUNE 11, 1999. THIS HAS BEEN A LONG TIME PROBLEM, AND HONEYWELL IS WORKING ISDR 2001UALA00293Shutoff Valve · leakingENGINE BLEED DUCT PRESSURE SPLIT. SUPPLEMENTAL DATA UPDATE TWO PRSOV SYSTEM FLEX LINES, HIGH PRESURE SHUTOFF VALVE, HIGH PRESSURE CONTROLLER AND MUSCLE LINE O-RING WERE REPLACED. HIGH POWER RUN ACCOMPLISHED, OPS CHECKED OK.SDR 2001UALA00283Bulkhead · wornNR 2 PYLON AFT BULKHEAD NAC STA 201.02 RIGHT SIDE VERTICAL FLANGE LOWER CORNER HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED.INSTALLED REPAIR PLATE PER SRM.SDR 2001UALA00282Cooling Fan · failedSMOKE IN THE COCKPIT AND CABIN. SUPPLEMENTAL DATA UPDATE FOUND COOLING FAN SHAFT SHEARED AND FAN HOUSING BROKEN. THIS IS THE LATEST -6 FAN WHICH WAS INSTALLED ON THIS APU. HONEYWELL IS WORKING ON THIS LONG TIME PROBLEM WHICH HAD CAUSED MANY DELAYS AND DISCRESDR 2001UALA00295Plate · damagedLOWER SURFACE OF DECK PLATE HAS TOOLING DAMAGE STA 1704 TO 1707 LBL 62. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. AFT DECK PLATE WAS BLENDED TO REMOVE TOOLING DAMAGE PER FORM 8110-3 .SDR 2001UALA00284Floorbeam · tool damageCABIN FLOORBEAM UPPER CAP AT STA 740 BETWEEN LT AND RT SEAT TRACK HAS TOOLING DAMAGE. MAJOR REPAIR ACCOMPLISHED. REPAIRED T CAP WITH SPLICE PER SRM.
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