N764US

Service difficulty reports · 221

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N764US' AND registry_match = 'registration'
  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 USAA2015032100001Power Supply · failedEMERGENCY POWER SUPPLY 12WL FAILED WEEKLY BITE CHECK ON CIDS. REPLACED 12WL EMER POWER SUPPLY IAW AMM 33-51-38.Mar 20, 2015 · N764US · Airbus A319112 · Emergency LightingSDR USAA2014061600030Battery · dischargedTHE FWD FLIGHT ATTENDANT FLASHLIGHT NOT SHOWING CHARGE. REPLACED BATTERY.Jun 16, 2014 · N764US · Airbus A319112 · Emergency EquipmentSDR USAA2014030300016Bypass Valve · faultyAT FL340, 112 MILES FROM MSY, FLIGHT ATTENDANT COMPLAINED OF PLASTIC BURNING SMELL ROWS 5 - 7DEF. ALSO, HEARD CRACKLING SOUND WITHIN 3 MINUTES. INITIATED DESCENT & DECLARED EMERGENCY. DIVERTING TO MSY, OVERHEAD BINS CHECKED, NO HEAT DISCOVERED. COMPLIED WITMar 2, 2014 · N764US · Airbus A319112 · Cabin Cooling SystemSDR USAA2013102100010Battery · dischargedCREW REPORTED THE AFT RT GALLEY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY IN AFT RT GALLEY FLASHLIGHT. CHECKS OK.Oct 19, 2013 · N764US · Airbus A319112 · Emergency EquipmentSDR USAA2013050900017Attach Angle · corroded2S CHECK - R1 DOOR THRESHOLD ATTACH ANGLE CORRODED BETWEEN FR 16 AND FR 20. REMOVED, FABRICATED AND INSTALLED ATTACH ANGLE IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53112198.May 8, 2013 · N764US · Airbus A319112 · Fuselage Main, Attach FittingsSDR USAA2013050900016Sill · corroded2S CHECK - CABIN DOOR SILL CORRODED BETWEEN FR 16 AND FR 20 AT Y 1820. REMOVED AND REPLACED SILL IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53112109.May 8, 2013 · N764US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2013050600010Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251RF BETWEEN FR58 TO FR62, -Z500 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 251RF IAW IRM 9701 REV G.May 5, 2013 · N764US · Airbus A319112 · Fuselage Floor PanelSDR USAA2013050600011Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261CG BETWEEN FR64 TO FR66, -Z500, Y=0. REPLACED FLOOR PANEL 261CG IAW IRM 9701 REV G.May 3, 2013 · N764US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012120700017Cover · misinstalledCREW REPORTED THE EXIT SIGN COVERS OVER FRONT ENTRY DOOR AND CENTER AISLE ROW 1 ARE REVERSED. NOTE: THE SIGN WITH THE ARROWS OVER DOOR. MAINTENANCE INSTALLED EXIT SIGNS IN PROPER LOCATION AS REQUIRED.Dec 7, 2012 · N764US · Airbus A319112 · Emergency LightingSDR USAA2012091000045Lens · missingR2 SERVICE DOOR EMERGENCY EXIT LENS MISSING. REPLACED R2 SERVICE DOOR EMERGENCY EXIT LENS.Sep 7, 2012 · N764US · Airbus A319112 · Emergency LightingSDR USAA2012090600008Strut · wornRON CHECK - LEFT WING INTERCONNECTING STRUT BETWEEN INBOARD & OUTBOARD FLAP IS WORN TO LIMITS PER JOB CARD. REPLACED LEFT WING INTERCONNECTING STRUT IAW A319 AMM 27-57-44-000-001-A.Sep 6, 2012 · N764US · Airbus A319112 · Trailing Edge FlapsSDR USAA2012090600007Bottle · low pressureC11 CHECK - R2 DOOR DAMPER ASSIST BOTTLE HAS PRESSURE LOW. SERVICED R2 DOOR DAMPER ASSIST BOTTLE IAW A319 AMM 52-10-00-614-001-A.Aug 27, 2012 · N764US · Airbus A319112 · Service DoorsSDR USAA2012090600006Bottle · low pressureC11 CHECK - L2 DOOR DAMPER ASSIST BOTTLE HAS PRESSURE LOW. SERVICED L2 DOOR DAMPER ASSIST BOTTLE IAW A319 AMM 52-10-00-614-001-A.Aug 27, 2012 · N764US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2012082900014Seat Track · corrodedC11/SY6 CHECK - INTERGRANULAR CORROSION ON SEAT TRACK BETWEEN FR16 TO FR20, Y765. REPLACED SEAT TRACK BETWEEN FR16 TO FR20, Y765 IAW A319 SRM 51-42-11 PARAGRAPH 7, FIGURE 12.Aug 21, 2012 · N764US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012082700001Lens · crackedC11/SY6 CHECK - L1 DOOR FRAME EMERGENCY LIGHT LENS IS CRACKED. REPLACED L1 DOOR FRAME EMERGENCY LIGHT LENS IAW A319 AMM 33-51-11-0401.Aug 21, 2012 · N764US · Airbus A319112 · Emergency LightingSDR USAA2012082800038Fitting · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON R2 AFT LOWER CORNER FITTING AT FR68, -Y1732. REPLACED R2 AFT LOWER CORNER FITTING AT FR68, -Y1732 IAW A319 SRM 51-42-11 FIG 8 & 12, A319 AMM 53-45-15-00.Aug 20, 2012 · N764US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012082400010Web · corrodedC11 CHECK - LEVEL 2 FILIFORM CORROSION ON ATTACH WEB AT FR14, -Y81. REPLACED SHAPE ATTACH WEB AT FR14, -Y81 IAW A319 SRM 51-42-11 PAR 4 FIG 2 & 3.Aug 17, 2012 · N764US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012082800040Coupling · corrodedC11 CHECK - LEVEL 2 FILIFORM CORROSION ON COUPLING AT FR68, Y1292. REPLACED COUPLING AT FR68, Y1292 IAW A319 SRM 51-42-11 PAR 5 & 51-45-00 TABLE 14.Aug 16, 2012 · N764US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012082800037Fitting · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT SHAPE SILL AFT CORNER FITTING AT FR68, Y1732. REPLACED LEFT SHAPE SILL AFT CORNER FITTING AT FR68, Y1732 IAW A319 SRM 51-42-11 FIG 17, 19.Aug 16, 2012 · N764US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012090600001Shear Plate · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON RIGHT AFT SHEAR PLATE BETWEEN FR69 TO FR70, Y1162. REPLACED RIGHT AFT SHEAR PLATE BETWEEN FR69 TO FR70, Y1162 IAW A319 SRM 51-42-11 PARA 6B.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012082900019Shear Plate · corrodedC11/SY6 CHECK - INTERGRANULAR CORROSION ON LEFT SHEAR PLATE BETWEEN FR69 TO FR70, Y1162. REPLACED LEFT SHEAR PLATE BETWEEN FR69 TO FR70, Y1162 IAW A319 SRM 51-42-11 PARAGRAPH 6D, FIGURE 8, 14F AND 85.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012082900017Seat Track · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR64 TO FR66, -Y765. REPLACED SEAT TRACK BETWEEN FR64 TO FR66, -Y765 IAW A319 SRM 51-42-11 FIGURE 20, 51-21-11, AND 51-42-11 FIGURE 3.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012082900015Seat Track · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON SEAT RAIL BETWEEN FR64 TO FR66, Y1292. REPLACED SEAT RAIL BETWEEN FR64 TO FR66, Y1292 IAW A319 SRM 51-42-11 FIGURE 10 AND 51-49-00 TABLE 14.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012082900013Floorbeam · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1162 IAW A319 SRM 51-42-11 FIGURE 10 AND 51-49-00 TABLE 14.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012082900012Floorbeam · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR67 +10 INCHES, -Y765. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR67 +10 INCHES, -Y765 IAW A319 SRM 51-42-11 PARAGRAPH 5.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012082800041Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, -Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, -Y1732 IAW A319 SRM 51-74-00, 51-44-11, 51-42-11 FIG 1, 2 & 10.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012082800039Web · crackedC11 CHECK - CRACK ON WEB BETWEEN FR68 TO FR69, Y1162. REPLACED WEB BETWEEN FR68 TO FR69, Y1162 IAW A319 SRM 51-42-11 FIG 2 & 3.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012082800032Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 232MH BETWEEN FR24 TO FR30 & BETWEEN -Y1292 TO -Y1735. REPLACED FLOOR PANEL 232MH & INSTALLED ON LOG PAGE 6545353.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012082800026Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR70, -Y765. REPLACED FLOORBEAM AT FR70, -Y765 IAW A319 SRM 51-42-11 FIG 20, 51-44-11 FIG 2 & 51-42-11 FIG 3.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012082800023Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y765 IAW A319 SRM 51-49-00 TABLE 14 & 51-42-11 FIG 10.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012082800022Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR67 TO FR68, -Y1162. REPLACED FLOORBEAM BETWEEN FR67 TO FR68, -Y1162 IAW A319 SRM 51-42-11 FIG 10 & 51-49-00 TABLE 14.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012082800021Seat Track · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON BEAM SEAT RAIL ASSEMBLY BETWEEN FR64 TO FR66, -Y1292. REPLACED BEAM SEAT RAIL ASSEMBLY BETWEEN FR64 TO FR66, -Y1292 IAW A319 SRM 51-42-11 PAR 5, 7; FIG 10, 51-49-00 TABLE 14.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012082400009Sill · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHAPE SILL BETWEEN FR66 TO FR68, Y1732. REPLACED SHAPE SILL BETWEEN FR66 TO FR68, Y1732 IAW A319 SRM 51-42-11 FIG 2, 3.Aug 15, 2012 · N764US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012082900018Seat Track · corrodedC11/SY6 CHECK - INTERGRANULAR CORROSION ON SEAT TRACK BETWEEN FR16 TO FR24, Y254. REPLACED SEAT TRACK BETWEEN FR16 TO FR24, Y254 IAW A319 SRM 51-42-11 PARAGRAPH 7B, FIGURE 12.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012082900016Seat Track · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR16 TO FR20, Y1292. REPLACED SEAT TRACK BETWEEN FR16 TO FR20, Y1292 IAW A319 SRM 51-42-11 FIGURE 12.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012082800036Floor Panel · corrodedC11 CHECK - CORROSION ON FLOOR PANEL 261FF BETWEEN FR66 TO FR68 & BETWEEN Y1732 TO Y765. REPLACED FLOOR PANEL 261FF & INSTALLED ON JOB CARD 26C26053014.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012082800035Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 261DF & INSTALLED ON JOB CARD 26C26053014.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012082800034Floor Panel · corrodedC11 CHECK - CORROSION ON FLOOR PANEL 262FF BETWEEN FR66 TO FR68 & BETWEEN -Y765 TO -Y1732. REPLACED FLOOR PANEL 262FF & INSTALLED ON JOB CARD 26C26053014.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012082800033Floor Panel · corrodedC11 CHECK - CORROSION ON FLOOR PANEL 261BG BETWEEN FR64 TO FR66 & BETWEEN Y765 TO Y1732. REPLACED FLOOR PANEL 261BG & INSTALLED ON JOB CARD 26C2653014.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012082800031Floor Panel · delaminatedC11 CHECK - DELAMINATION ON TOP SHEET OF FLOOR PANEL 222CF BETWEEN FR12 TO FR16 & BETWEEN -Y1732 TO Y0. REPLACED FLOOR PANEL 222CF IAW JOB CARD 26C22053014.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012082800030Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK ASSEMBLY BETWEEN FR20 TO FR24, -Y189. REPLACED SEAT TRACK ASSEMBLY BETWEEN FR20 TO FR24, -Y189 IAW A319 SRM 51-42-11, PAR 7B, FIG 9.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012082800029Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK ASSEMBLY BETWEEN FR18 TO FR20, -Y254. REPLACED SEAT TRACK ASSEMBLY BETWEEN FR18 TO FR20, -Y254 IAW A319 SRM 51-42-11, PAR 7B, FIG 12.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012082800028Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK ASSEMBLY BETWEEN FR18 TO FR21, -Y1292. REPLACED SEAT TRACK ASSEMBLY BETWEEN FR18 TO FR21, -Y1292 IAW A319 SRM 51-42-11, PAR 7B, FIG 9.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012082800027Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK ASSEMBLY BETWEEN FR18 TO FR21, -Y765. REPLACED SEAT TRACK ASSEMBLY BETWEEN FR18 TO FR21, -Y765 IAW A319 SRM 51-42-11 PAR 7 FIG 12.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012082800025Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, Y1292. REPLACED FLOORBEAM AT FR68, Y1292 IAW A319 SRM 51-49-00 TABLE 14 & 51-42-11 FIG 10.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012082800024Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Y1292 IAW A319 SRM 51-49-00 TABLE 14 & 51-42-11 FIG 10.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012082400008Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 221EF BETWEEN FR16 TO FR20 & BETWEEN Y254 TO Y1292. REPLACED FLOOR PANEL 221EF IAW JOB 26C22053014.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012082000022Floorbeam · corrodedC11 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR12 TO FR16, Y503. REPLACED FLOORBEAM BETWEEN FR12 TO FR16, Y503 IAW A319 SRM 51-42-11, FIG 9.Aug 14, 2012 · N764US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070200004Cylinder · low pressureR2 DOOR EMERGENCY CYLINDER/ACCUMULATOR PERSSURE LOW. PRESSURE 1000 PSI AT 65F. SERVICED R2 DOOR EMERGENCY CYLINDER/ACCUMULATOR TO 1850 PSI PER AMM 52-10-00-614-001-A.Jun 28, 2012 · N764US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2012052500023Megaphone · inoperativeAFT MEGAPHONE INOPERATIVE. REMOVED AND REPLACED AFT MEGAPHONE AS REQUIRED.May 22, 2012 · N764US · Airbus A319112 · Emergency Equipment
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