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 2001UALA02119Vane · fracturedNUMBER 1 ENGINE FAILED. UPON DISASSEMBLY THE ROOT CAUSE FOR THE FAILURE WAS LOW PRESSURE TURBINE (LPT) 4TH VANE SULFIDATION FRACTURE. WHEN THESE VANES FAILED, IT RESULTED IN HEAVY DAMAGE TO THE 5TH, 6TH, & 7TH STAGES OF THE LPT.SDR 2001UALA02125Skin · dentedFUSELAGE SKIN DENT STATION 1717 STRINGER 14L. MAJOR REPAIR ACCOMPLISHED. DAMAGED REMOVED DOUBLER AND FILLER INSTALLED, SKIN LAP AREA BEHIND DOOR 4L.SDR 2001UALA02118Frame · crackedAFT PIT STA 1400 JUST ABOVE STRINGER 25L, UPPER CHORD IS DENTED AND CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR SPLICE ON FRAME.SDR 2001UALA02117Frame · dentedAFT PIT FUSELAGE FRAME DENT IS OUT OF LIMITS STATION 1420 ABOVE STRINGER 26L LBL 35. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED ANGLE REPAIR ON FRAME.SDR 2001UALA02111ClipFRAME STATION 1400 STRINGER 26L CLIP REPLACE DUE TO FRAMESPLICE REPAIR. MAJOR REPAIR ACCOMPLISHED.REPLACED STRINGER 26L CLIP.SDR 2001UALA02110ClipFRAME STATION 1400 STRINGER 25L CLIP REPLACE DUE TO FRAME SPLICE REPAIR. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP.SDR 2001UALA02107Frame · dentedAFT PIT FRAME AT STATION 1420 DENTED BETWEEN STRINGER 25L AND 26L. MAJOR REPAIR ACCOMPLISHED.FORMED DOUBLER WAS INSTALLED ON FRAME.SDR 2001UALA02097Floorbeam · corrodedAFT CABIN FLOORBEAM WEB CORRODED STA 1685, RBL 51. MAJOR REPAIR ACCOMPLISHED. INSTALLED UPPER SURFACE DOUBLER STA 1685, RBL 47.5 TO RBL 54.SDR 2001UALA02096Floorbeam · corrodedCABIN FLOORBEAM AT STA 297, RBL 34 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED UPPER SURFACE STRAP REPAIR STA 297, RBL 41 TO RBL 47.5.SDR 2001UALA02093Control Unit · malfunctionedRUDDER REQUIRES 6 UNITS OF LEFT TRIM. ACCOMPLISHED TROUBLESHOOTING OF RUDDER TRIM AND RUDDER RATIO SYSTEMS AND EXAMINED RATIO CHANGER SHEAR PINS. NO DISCREPANCIES FOUND, AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER GRIPES ABOUT EXCESSIVE TRIM REQUIRED.SDR 2001UALA02086OvenCREW REPORTS LIGHT SMOKE COMING FROM FWD GALLEY AREA. FOUND CHEESE IN FWD GALLEY OVEN. CLEANED OVEN.SDR 2001UALA02073Floorbeam · corrodedFLOORBEAM TOP CAP CORRODED STA 680, RBL 9 TO LBL 9. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW TOP CAP.SDR 2001UALA02049Smoke · detectedSMOKE IN FLIGHT DECK AND MAIN CABIN. *S/D* UNABLE TO DUPLICATE PROBLEM. ALL SYSTEMS OPERATE NORMALLY. ACCOMPLISHED PACK BURNOUT.SDR 2001UALA01939Frame · damagedRT FUSELAGE FRAME AT BS 1682, CABIN FLOOR LEVEL, DAMAGED ON THE TOP OF THE INBD CAP. MAJOR REPAIR ACCOMPLISHED. BLENDED AREA. INSTALLED REPAIR ANGLE.SDR 2001UALA01938FrameAFT PIT FUSELAGE FRAME AT BS 1500, RBL28, GOUGED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. BLENDED AREA. INSTALLED REPAIR ANGLE.SDR 2001UALA01896Crease Beam · corrodedCABIN CREASE BEAM STATION 680-740 CORRODED. MAJOR REPAIR ACCOMPLISHED. CABIN CREASE BEAM REPLACED STATION 680-740.SDR 2001UALA01894Floorbeam · corrodedCABIN FLOOR BEAM T-CAP CORRODED AT STATION 324 RBL 59. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR.SDR 2001UALA01886Skin · damagedRIGHT ELEVATOR UPPER LEADING EDGE SKIN DAMAGED BY ELECTRO STATIC DISCHARGE 6 INCHES FROM TIP, HOLE DIA .25 INCH. MAJOR REPAIR ACCOMPLISHED. SEAL AND POT HOLE, OVERLAYED FIBERGLASS PLY, DRILLED FASTENER HOLE AND RESTORED FINISH.SDR 2001UALA01885Crease Beam · corrodedCABIN CREASE BEAM INBOARD CORD ANGLE AT BODY STATION 730-734 LBL72 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED INBOARD CREASE BEAM CORD ANGLE.SDR 2001UALA01884Crease Beam · corrodedCABIN CREASE BEAM STATION 1040 RBL 70 EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM.SDR 2001UALA01883Crease Beam · corrodedCABIN CREASE BEAM STATION 1170 RBL 65 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM.SDR 2001UALA01858Channel · corrodedCABIN FLOOR CHANNEL CORRODED, BODY STATION 401 RBL 56. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR CHANNEL STATION 395 TO STATION 415.SDR 2001UALA01849Warning System · malfunctionedCENTER EICAS "C HYD LOW QTY" RSVR LIGHT ON OVERHEAD. TURNED OFF CENTER HYD PUMPS, LOW PRESSURE LIGHTS CAME ON AT THAT TIME. LOWER EICAS STATUS CENTER QUANTITY ZEROSDR 2001UALA01846Hydraulic System · leakingEICAS MESSAGE 'L HYD SYS PRESS' DISPLAYED. LEFT HYDRAULIC QUANTITY DECREASED TO 0.02, QUANTITY STABLE WITH PUMPS OFF.SDR 2001UALA01840Web · corrodedCABIN STATION 984 SHEAR WEB CORRODED AT RBL 70. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB.SDR 2001UALA01844Crease Beam · corrodedSHEAR WEB CORRODED BETWEEN STATION 996 TO STATION 1020. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED SHEAR WEB OR CREASE BEAM WEB BETWEEN STATION 996 TO 1020.SDR 2001UALA01843Stringer · dentedSTRINGER 16 LH DAMAGED AT STA 605 FORWARD OF 2 LH DOOR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.STRINGER SPLICE INSTALLED.SDR 2001UALA01842ClipSTRINGER CLIP 16L REPLACED DUE TO STRINGER SPLICE STATION 600. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.NEW CLIP INSTALLED.SDR 2001UALA01841Crease Beam · corrodedFORWARD CABIN FLOOR CREASE BEAM CORROSION ON INNER CHORD. BS 367 & RBL 65 SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REMOVED AND REPLACED CREASE BEAM INNER CHORD AT BODY STATION 367 & RBL 65" TREATED, PRIMED & PAINTED.SDR 2001UALA01800Door · dented1 EA DENT IN FRONT OF DOOR 2L AT STATION 605 STRINGER 16LH. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.SDR 2001UALA01798Floorbeam · corrodedAFT CABIN FLOORBEAM STATION 1640, RBL 12 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCING ANGLE REPAIR.SDR 2001UALA01797Floorbeam · corrodedCABIN FLOORBEAM 365 CORRODED AT RBL 15, 24, 30, 36, 48. MAJOR REPAIR ACCOMPLISHED. REMOVED T-CAP, INSTALLED NEW T-CAP WITH SUPPORT ANGLES AND STRAPS.SDR 2001UALA01780Plate · corrodedCABIN AFT DECK PLATE CORRODED, STA 1681, RBL 1.5 TO RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER ON DECK PLATE.SDR 2001UALA01779Plate · corrodedCABIN AFT DECK PLATE CORRODED, STA 1681, RBL 1.5 TO RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER ON DECK PLATE.SDR 2001UALA01778Intercostal · corrodedCABIN FLOOR INTERCOSTAL BETWEEN STA 324 AND 418, BL 0, HAS CORROSION ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED. REMOVED AND INSTALLED NEW INTERCOSTAL.SDR 2001UALA01773Hose · kinked#2 ENGINE MAIN HYDRAULIC SUPPLY LINE, FROM FIREWALL TO RIGID LINES FOUND TWISTED AND KINKED WITH APPROXIMATELY 3/4 TWIST AND COLLAPSED BENEATH SHIELDING. REPLACED HYDRAULIC SUPPLY LINE.SDR 2001UALA01777Computer · failedLANDING FLARE CONTROL PRESSURE TWICE THE NORMAL EFFORT (PITCH PRESSURE EXTREMELY HIGH). FAILURE OF THE ELEVATOR FEEL COMPUTER CAUSED THE EXTRA FORCE REQUIRED TO OPERATE THE CONTROL COLUMN. REPLACED THE ELEVATOR FEEL COMPUTER.SDR 2001UALA01766Plug · looseLEFT EMERGENCY ESCAPE SQUIB DID NOT TEST IN TEST 1. ALL TEST IN TEST 2. FOUND CANNON PLUG ON SQUIB LOOSE, REINSTALLED CANNON PLUG, AND PERFORMED SQUIB TEST. TESTED NORMAL IN BOTH LEFT AND RIGHT IN TEST 1 AND 2.SDR 2001UALA01758Pump · failedLEFT ENGINE DRIVEN PUMP OVERHEAT LIGHT ILLUMINATED. PUMP DEACTIVATED, 30 MINUTES LATER LEFT SYSTEM LOST ALL FLUID. PUMP FAILED INTERNALLY. REPLACED LEFT ENGINE DRIVEN PUMP.SDR 2001UALA01757Turbine · damagedNUMBER 1 ENGINE LPT 3RD STAGE FAILED BORESCOPE INSPECTION.SDR 2001UALA01745Bracket · failedNR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. *S/D* LOSS OF OIL QUANTITY AND PRESSURE DUE TO A HOLE WORN IN THE LINE. REPLACED OIL OUT LINE FROM FOX TO AOX AND SUPPORT BRACKET ON NR 1 ENG.SDR 2001UALA01750Crease Beam · corrodedCABIN FLOOR INNER CREASE BEAM BELOW DOR 2L DRAIN GUTTER HAS EXCESSIVE CORROSION STA.700 TO 720 LBL70" STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. REMOVED SECTION OF INNER CREASE BEAM L-ANGLE Z ANGLE IN DOORWAY FROM STA.665 TO 754 AT FACTORY SPLICES INSTALLED NEWSDR 2001UALA01767SwitchLEFT EMERGENCY ESCAPE SLIDE SQUIB TEST FAILED IN #1 TEST POSITION. CLEANED TEST SWITCH, SLIDE SQUIB CHECK OK.SDR 2001UALA01751Crease Beam · corrodedRIGHT HAND CABIN FLOOR WEB BETWEEN INNER AND OUTER CREASE BEAM CORD WAS CORODED AT STA 1021 RBL 68. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED REPLACEMENT WEB FROM 7075-0 HEAT TREATED TO T6 INSTALLED NEW WEB BETWEEN STA.1020-1039 RBL68 STRINGER 17R.SDR 2001UALA01729Idg · failedNR 2 IDG FAILED. REPLACED NUMBER 2 INTEGRATED DRIVE GENERATOR (IDG).SDR 2001UALA01746Compressor · damagedNR 2 ENGINE FAILED TENTH STAGE BORESCOPE INSPECTION.SDR 2001UALA01713Turbine Blades · crackedNUMBER 1 ENGINE LPT 3 BLADE IS CRACKING WITH SULFIDATION. REPLACED ENGINE.SDR 2001UALA01682IdgL GEN OFF AND L GEN DRIVE EICAS MSG'S DISPLAYED. SUPPLEMENTAL DATA UPDATE IDG CHECK VALVE FITTING LEAKING.REPLACED IDG.SDR 2001UALA01662Skin · dentedLEFT FUSELAGE SKIN DENTED STA 618 STR 16L.SDR 2001UALA01646Oil System · overtempON DESCENT WITH POWER AT IDLE, LEFT OIL TEMPERATURE REDLINED TILL LANDING.
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