N765US

Service difficulty reports · 299

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 = 'N765US' 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 USAA2012091400016Angle · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON ANGLE AT FR68, -Y1732. REPLACED ANGLE AT FR68, -Y1732 IAW A319 SRM 51-42-11.Sep 3, 2012 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091400026Fitting · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON CORNER FITTING AT FR68 TO Y1732. REPLACED CORNER FITTING AT FR68 TO Y1732 IAW A319 SRM 51-42-11.Sep 2, 2012 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091400019Sill · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON SILL BETWEEN FR66 TO FR68, Y1732. REPLACED SILL BETWEEN FR66 TO FR68, Y1732 IAW A319 SRM 51-42-11.Sep 2, 2012 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091400010Tray · crackedC11/SY6 CHECK - CRACK ON SHEET TRAY BETWEEN FR68 TO FR69, -Y1695. REPLACED SHEET TRAY BETWEEN FR68 TO FR69, -Y1695 IAW A319 SRM 51-42-11.Sep 2, 2012 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091400007Tray · crackedC11/SY6 CHECK - CRACK ON SHEET TRAY BETWEEN FR68 TO FR69, Y1695. REPLACED SHEET TRAY BETWEEN FR68 TO FR69, Y1695 IAW A319 SRM 51-42-11.Sep 2, 2012 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091400036Web · corrodedC11/SY6 CHECK - INTERGRANULAR CORROSION ON WEB AT FR20, -Y1584. REPLACED WEB AT FR20, -Y1584 IAW A319 SRM 51-42-11 PARAGRAPH 6D, FIGURE 2 AND 8.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091400035Floorbeam · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 PLUS 10 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 PLUS 10 INCHES, Y1292 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091400034Floor Panel · corrodedC11/SY6 CHECK - DELAMINATION ON FLOOR PANEL 221FF BETWEEN FR16 TO FR20, -Y1584 TO -Y1292. REPLACED FLOOR PANEL 221FF BETWEEN FR16 TO FR20, -Y1584 TO -Y1292 IAW JOB CARD 26C22053014.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012091400032Floorbeam · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, -Y465 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091400031Floorbeam · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, -Y160. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, -Y160 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091400030Seat Track · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y254. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y254 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012091400027Floorbeam · 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.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091400025Seat Track · corrodedC11/SY6 CHECK - INTERGRANULAR CORROSION ON SEAT TRACK AT FR16, Y254. REPLACED SEAT TRACK AT FR16, Y254 IAW A319 SRM 51-42-11, PARAGRAPH 7B, FIGURE 12.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012091400024Floorbeam · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR65 TO FR67, -Y318. REPLACED FLOORBEAM BETWEEN FR65 TO FR67, -Y318 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091400023Floorbeam · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1162. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1162 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091400021Sill · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON SILL BETWEEN FR66 TO FR68, -Y1732. REPLACED SILL BETWEEN FR66 TO FR68, -Y1732 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091400020Floor Panel · delaminatedC11/SY6 CHECK - DELAMINATION ON FLOOR PANEL 261BG BETWEEN FR64 TO FR65, Y1732 TO Y765. REPLACED FLOOR PANEL 261BG IAW JOB CARD 26C26053014.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012091400018Floor Panel · corrodedC11/SY6 CHECK - CORROSION ON FLOOR PANEL 262EF SCREW HOLES BETWEEN FR66 TO FR68, -Y795 TO -Y1292. REPLACED FLOOR PANEL 262EF IAW JOB CARD 26C26053014.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012091400017Floorbeam · corrodedC11/SY6 CHECK - FILIFORM CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, -Y765 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091400013Shear Plate · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091400011Floorbeam · corrodedC22/SY6 CHECK - EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 PLUS 4 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR64 PLUS 4 INCHES TO FR70, Y765 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091400009Floorbeam · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, -Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, -Y1292 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091400008Floorbeam · 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.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091400005Floorbeam · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67 PLUS 10 INCHES, Y512. REPLACED FLOORBEAM BETWEEN FR64 TO FR67 PLUS 10 INCHES, Y512 IAW A319 SRM 51-41-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091400004Floor Panel · corrodedC11/SY6 CHECK - CORROSION ON FLOOR PANEL 262BG SCREW HOLES BETWEEN FR64 TO FR66, -Y132 TO -Y765. REPLACED FLOOR PANEL 262BG IAW JOB CARD 26C26053014.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012091400003Floorbeam · corrodedC11/SY6 CHECK - EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 10 INCHES TO FR68, Y1162. REPLACED FLOORBEAM BETWEEN FR66 PLUS 10 INCHES TO FR68, Y1162 IAW A319 SRM 51-42-11.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091000011Floor Panel · corrodedC11 CHECK - CORROSION ON FLOOR PANEL 262FF BETWEEN FR66 TO FR68 & BETWEEN -Y765 TO -Y1292. REPLACED FLOOR PANEL 262FF IAW JOB CARD 26C26053014.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012091000010Floor Panel · corrodedC11 CHECK - CORROSION ON FLOOR PANEL 261FF BETWEEN FR66 TO FR68 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL 261FF IAW JOB CARD 26C26053014.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012091000008Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON CABIN FLOOR TRACK ASSEMBLY AT FR16, -Y503.2. REPLACED CABIN FLOOR TRACK ASSEMBLY AT FR16, -Y503.2 IAW A319 SRM 51-42-11, PAR 7, FIG 12.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012091000007Stiffener · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON STIFFENER ASSEMBLY AT FR12+4.0 INCHES, -Y1292. REPLACED STIFFENER ASSEMBLY AT FR12+4.0 INCHES, -Y1292 IAW A319 SRM 51-42-11, PAR 5, FIG 10A.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091000006Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON CABIN FLOOR RAIL AT FR14, -Y81. REPLACED CABIN FLOOR RAIL AT FR14, -Y81 IAW A319 SRM 51-42-11, PAR 6B, FIG 2, 3 & 8.Sep 1, 2012 · N765US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012040600016Manifold · faultyYELLOW HYDRAULIC LOW PRESSURE LIGHT EN ROUTE TO PHL. DECLARED EMERGENCY LANDING. REMOVED AND REPLACED YELLOW SYSTEM GROUND LEAK MEASUREMENT MANIFOLD (3146GM) PER AMM 29-19-41. OPS CHECKED GOOD.Apr 2, 2012 · N765US · Airbus A319112 · Hydraulic System, MainSDR USAA2012012700014Power Supply · inoperativeEMERGENCY LIGHTS INOPERATIVE AT SEAT 8 & 10 LEFT & 10 RIGHT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK MID CABIN RIGHT PER AMM 33-51-38-400-001.Jan 24, 2012 · N765US · Airbus A319112 · Emergency LightingSDR USAA2011030790981Lens · missingFLT 1406 - PHL-BOS - EMERGENCY LIGHTS - AFT LEFT PASSENGER DOOR EMERGENCY LIGHT LENS IS MISSING ABOVE DOOR. REPLACED LENS.Mar 3, 2011 · N765US · Airbus A319112 · Emergency LightingSDR USAA2010112292633Pin · corrodedPIT - TRIPLE GEAR CHANGE - MAJOR REPAIR - JOB CARD 26T00032001 - CORROSION ON RIGHT MAIN LANDING GEAR PINTLE PIN. REPLACED RIGHT MAIN LANDING GEAR PINTLE PIN IAW JOB CARD 26T00032001.Nov 20, 2010 · N765US · Airbus A319112 · Main Landing Gear Attach SectionSDR USAA2010111592605Lens · missingFLT 2049 - BOS-DCA - EMERGENCY LIGHTS - FORWARD RIGHT DOOR EMERGENCY EXIT LENS MISSING. INSTALLED NEW LENS AT FORWARD RIGHT DOOR.Nov 14, 2010 · N765US · Airbus A319112 · Emergency LightingSDR USAA2009081792141Lens · missingFLT 1260 - LGA-PIT - EMERGENCY LIGHTS - SEAT 10C EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED SEAT 10C EMERGENCY EXIT LIGHT LENS.Aug 16, 2009 · N765US · Airbus A319112 · Emergency LightingSDR USAA2009060991441Lens · missingFLT 894 - ATL - EEL - EMERGENCY LIGHT ON SEAT 3-L MISSING LENS. MAINTENANCE INSTALLED NEW LENS ON SEAT 3-L.Jun 8, 2009 · N765US · Airbus A319112 · Emergency LightingSDR USAA2009041090849Power Supply · dischargedFLT 1403 - BOS-PHL - EMERGENCY LIGHTS - MID CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY UNIT (2WL). OPERATIONAL CHECK WAS GOOD.Apr 10, 2009 · N765US · Airbus A319112 · Emergency LightingSDR USAA920081714Pin · vibrationFLT NR 2134 - EMERGENCY LANDING, AT CRUISE POWER, A BANG WAS HEARD AND SEVERE VIBRATION FELT. THE FLT CREW PULLED POWER BACK TO IDLE AND VIBRATION STOPPED. ON ATTEMPT TO RESTORE POWER TO CLIMB, WHILE TRANSITIONING THRU 40-45% N1, VIBRATION AND BANG RESUMED. Sep 19, 2008 · N765US · Airbus A319112 · Turbine Engine Compressor SectionSDR USAA920081493Battery · dischargedFLT 1774 CLT-EEL- OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED TEST STEP 5A, EPSU LOAD AFT LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT 13WL BATTERY PER AIRBUS MAINTENANCE MANUAL 33-51-38. OPERATIONAL TEST GOOD. (S)Aug 7, 2008 · N765US · Airbus A319112 · Emergency LightingSDR USAA061156Threshold · corrodedFR 66 DOOR THRESHOLD RT SIDE. INSTALLED FILLER, DOUBLER IAW SRM 53-41-14 PG. 202; CORR TASK JA-260-53500; LEVEL 1 DEFECT SIZE: 1 SQ. IN.Sep 12, 2006 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061155Floor Support · corrodedFLOOR SUPPORT FROM FR. 64 -66 AT - Y1292 REPLACED FLOOR SUPPORT IAW SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 4 SQ. IN.Sep 12, 2006 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061154Floor Support · corrodedFLOOR SUPPORT FROM 66-68 AT -Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1 DEFECT SIZE: 6 SQ. IN.Sep 12, 2006 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061153Floor Support · corrodedFLOOR SUPPORT FROM FR 68-69 AT -Y1292. REPLACED SUPPORT IAW SRM 51-72-11; TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 3 SQ. IN.Sep 12, 2006 · N765US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061152Floorboard · torn3 INSERTS TORN OUT, AND TEAR - FLOOR BOARD 262EF MAUFACTURED NEW FLOORBOARD IAW IRM 9701 REV. F. DEFECT SIZE: .7500 INCH AREA EACH.Sep 12, 2006 · N765US · Airbus A319112 · Fuselage Floor PanelSDR USAA061151Floorboard · tornFLOORBOARD D261 HG - 4 EA. INSERTS TORN OUT. MANUFACTURED NEW FLOORBOARD IAW IRM 9701 REV. F DEFECT SIZE: .7500 INCH TEAR (4 EA.)Sep 12, 2006 · N765US · Airbus A319112 · Fuselage Floor PanelSDR USAA061158Floorbeam · corrodedLOCATION: 7 INCH FWD OF FR 20 ON TOPSIDE OF BEAM -Y254. REMOVED CORROSION AND INSTALLED FILLER AND REPAIR ANGLES IAW SRM 53-00-14; CORR TASK JA-220-53500 DEFECT SIZE: .75 INCH X .75 INCH.Sep 12, 2006 · N765US · Airbus A319112 · Fuselage Main, Floor BeamSDR SA04105Proximity Sensor · faultyPHL - FLT 77 ,EN ROUTE CUN - PHL, UPON LANDING GEAR EXTENSION IN PHL, RECEIVED ALL THREE GEAR DOWN UNSAFE LIGHT INDICATIONS. THE CREW RECYCLED THE LANDING GEAR AND SUBSEQUENTLY RECEIVED THREE GREEN, DOWN AND LOCKED INDICATIONS. FLIGHT CONTINUED TO LANDING WINov 10, 2004 · N765US · Airbus A319112 · Landing Gear Position and Warning
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