N762US

Service difficulty reports · 289

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 = 'N762US' 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 USAA2014031100002Bottle · low pressureTHE 2R DOOR ASSIST BOTTLE PRESS LOW. SERVICED 2R DOOR ASSIST BOTTLE TO PROPER PRESS IAW AMM 52-10-00, LEAK CHECKED OK.Mar 11, 2014 · N762US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2014021100004Filter · dirtyCREW REPORTED A SMOKE DETECTOR FAULT. CLEANED & CHANGED ALL LAVATORY SMOKE DETECTOR FILTERS & RESET IAW 26-17-02, CHECKED NORMAL.Feb 10, 2014 · N762US · Airbus A319112 · Smoke DetectionSDR USAA2013092500002Smoke Detector · false activationCREW REPORTED SMOKE DETECTOR WARNING ON ECAM. MX REPLACED LAVATORY SMOKE DETECTOR FILTERS AND RESET SYS. ACFT OK FOR SERVICE.Sep 24, 2013 · N762US · Airbus A319112 · Smoke DetectionSDR USAA2013070200015Skin · saturated2S CHECK - 6 AREAS OF MOISTURE INGRESS ON LT SIDE OF RUDDER BETWEEN RUDDER STA 8 THRU TOP OF RUDDER ALONG T/E & AT ALL 3 HOIST POINT LOCATIONS. REPLACED RUDDER IAW AMM 27-21-41.Jun 30, 2013 · N762US · Airbus A319112 · Rudder, Plate/SkinSDR USAA2013070200014Skin · saturated2S CHECK -4 AREAS OF MOISTURE INGRESS ON RT SIDE OF RUDDER BETWEEN RUDDER STA 206 THRU TOP OF RUDDER ALONG T/E. REPLACED RUDDER IAW AMM 27-21-41.Jun 30, 2013 · N762US · Airbus A319112 · Rudder, Plate/SkinSDR USAA2013070100022Frame · cracked2S CHECK - CRACK ON LT EMERGENCY EXIT DOOR 844 FRAME SEGMENT BETWEEN FR40 TO FR41. REPAIRED LT EMERGENCY EXIT DOOR 844 FRAME SEGMENT IAW US EO 5209Y173.Jun 30, 2013 · N762US · Airbus A319112 · Emergency ExitsSDR USAA2013070100021Frame · cracked2S CHECK - CRACK ON RIGHT EMERGENCY EXIT DOOR NR 844 FRAME SEGMENT 1 BETWEEN FR40 TO FR41. REPAIRED RIGHT EMERGENCY EXIT DOOR NR 844 FRAME SEGMENT 1 IAW EO 5120Y228, REV. A.Jun 30, 2013 · N762US · Airbus A319112 · Emergency ExitsSDR USAA2013070200018Lens · missing2S CHECK - SEAT 20ABC EMERGENCY LIGHT LENS MISSING. INSTALLED LENS FOR EMERGENCY LIGHT AT SEAT 20ABC IAW AMM 33-51-18. OPS CHECK GOOD.Jun 29, 2013 · N762US · Airbus A319112 · Emergency LightingSDR USAA2013070200017Wire · broken2S CHECK - DURING CHECKS FOUND BROKEN WIRE AT ROW 17 LT. WIRE IDENTIFIED AS 3351-1033 BELONGING TO EMERGENCY POWER SUPPLY UNIT 13WL. REPLACED BROKEN WIRE NR 3351-1033 AT ROW 17L. SYS OPS CHECK OF AFT CABIN EMERGENCY LIGHTS CHECKED NORMAL IAW ESPM 20-53-21, 2Jun 29, 2013 · N762US · Airbus A319112 · Light System WiringSDR USAA2013070200016Lens · cracked2S CHECK - SEVERAL EMERGENCY EXIT LIGHT LENSES CRACKED. REPLACED R2,L2, L1 & R1 OVERWING WALL MOUNTED EMERGENCY EXIT LIGHT LENSES IAW AMM 33-15-13.Jun 29, 2013 · N762US · Airbus A319112 · Emergency LightingSDR USAA2013070100023Slide · out of position2S CHECK - DURING GAP CHECK OF L-2 DOOR GIRT BAR FITTINGS, SLIDE FELL OUT OF PACK. REPLACED L2 DOOR SLIDE IAW AMM 25-62-44, OPS CHECK NORMAL IAW AMM 25-62-44.Jun 16, 2013 · N762US · Airbus A319112 · Escape SlideSDR USAA2013070100020Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR35.4 BETWEEN S40R & S41R. REPLACED CLEAT AT FR35.4 BETWEEN S40R & S41R IAW SRM 51-72-11 & DWG D53235027.May 15, 2013 · N762US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2013021800031Tru · faultyCREW REPORTED AN INFLIGHT LOSS OF TR 1 AT 16,000 FEET. LOSS OF ELEC AND ND. IMMEDIATE ACTION ITEMS EXECUTED AND STARTED APU. POWER WAS RE-ESTABLISHED. FLIGHT LANDED NORMAL AT DCA. MAINTENANCE REMOVED AND REPLACED NR 1 TR PER AMM TASK 24-32-51-000-001-A ANFeb 15, 2013 · N762US · Airbus A319112 · DC Rectifier/ConverterSDR USAA2013012200020Bottle · low pressureMAINTENANCE REPORTED THE R1 DOOR SLIDE BOTTLE IS LOW. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR SLIDE. REFERENCE J/C 26L00025010.Jan 19, 2013 · N762US · Airbus A319112 · Escape SlideSDR USAA2013011400029Computer · malfunctionedON APPROACH, CREW REPORTED ECAM F/CTRL FLAPS LOCKED - WING TIP BRAKE ON. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED RESET OF SFCC NR 1 AND NR 2. REFERENCE AMM 27-51-00-710-002. FLAPS AND SLATS SYSTEM OP CHECK NORMAL.Jan 12, 2013 · N762US · Airbus A319112 · Trailing Edge Flap Control SystemSDR USAA2012110200017Sign · missingEXIT SIGN ON RIGHT DOOR MISSING (FWD RIGHT GALLEY DOOR R1). INSTALLED NEW EXIT SIGN AT DOOR R1.Nov 1, 2012 · N762US · Airbus A319112 · Emergency LightingSDR USAA2012100100047Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, Y512. REPLACED FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES IAW A319 SRM 51-42-11 PAR 5.Sep 26, 2012 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012100100046Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK AT FR21, Y765. REPLACED SEAT TRACK AT FR21, Y765 IAW A319 SRM 51-42-11 PAR 7B FIG 12.Sep 21, 2012 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012100100063Attach Fitting · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON ATTACH CLIP AT FR20, -Y1584. REPLACED ATTACH CLIP AT FR20, -Y1584 IAW A319 SRM 51-42-11, PAR 7B, FIG 12.Sep 19, 2012 · N762US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012100100034Floor Panel · corrodedC11 CHECK - CORROSION ON FLOOR PANEL 261FF BETWEEN FR66 TO FR68 & BETWEEN Y1292 TO Y1732. REPLACED FLOOR PANEL 261FF IAW JOB CARD 26C26053014.Sep 19, 2012 · N762US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012100100033Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN Y1162 TO -Y1162. REPLACED FLOOR PANEL 261PF IAW JOB CARD 26C26053014.Sep 19, 2012 · N762US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012100200008Sill · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE AT FR66, -Y1732. REPAIRED SILL PLATE AT FR66, -Y1732 IAW A319 SRM 53-41-14 FIG 101 & 201.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012100200007Sill · corrodedC11 CHECK - LEVEL 2 FILIFORM CORROSION ON SILL PLATE AT L2 DOORWAY AT FR68, Y1732. REPAIRED SILL PLATE AT L2 DOORWAY AT FR68, Y1732 IAW A319 SRM 53-41-11 FIG 201.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012100100072Bearing · frozenC11 CHECK - RIGHT HORIZONTAL STABILIZER NR 5 ELEVATOR UPPER HINGE BEARING IS FROZEN. REPLACED NR 5 ELEVATOR UPPER HINGE ARM FITTING ASSEMBLY IAW A319 AMM 55-16-42-000-001-A, 55-16-42-400-001-A.Sep 18, 2012 · N762US · Airbus A319112 · Elevator StructureSDR USAA2012100100071Bearing · wornC11 CHECK - LEFT HORIZONTAL STABILIZER NR 5 ELEVATOR HINGE BEARING IS WORN. REPLACED NR 5 ELEVATOR HINGE ARM FITTING ASSEMBLY IAW A319 AMM 55-16-42-0000-001-A, 55-16-42-400-001-A.Sep 18, 2012 · N762US · Airbus A319112 · Elevator StructureSDR USAA2012100100070Bearing · wornC11 CHECK - LEFT HORIZONTAL STABILIZER NR 3 ELEVATOR HINGE BEARING IS WORN. REPLACED NR 3 ELEVATOR HINGE ARM FITTING ASSEMBLY IAW A319 AMM 55-16-42-000-001-A, 55-16-42-400-001-A.Sep 18, 2012 · N762US · Airbus A319112 · Elevator StructureSDR USAA2012100100069Bearing · wornC11 CHECK - RIGHT HORIZONTAL STABILIZER NR 2 ELEVATOR HINGE BEARING IS WORN. REPLACED NR 2 ELEVATOR HINGE ARM FITTING ASSEMBLY IAW A319 AMM 55-16-42-000-01-A, 55-16-42-400-001-A.Sep 18, 2012 · N762US · Airbus A319112 · Elevator StructureSDR USAA2012100100068Hinge Fitting · wornC11 CHECK - LEFT HORIZONTAL STABILIZER NR 2 ELEVATOR HINGE BEARING IS WORN. REPLACED NR 2 ELEVATOR HINGE ARM FITTING ASSEMBLY IAW A319 AMM 55-16-42-000-001-A, 55-16-42-400-001-A.Sep 18, 2012 · N762US · Airbus A319112 · Elevator StructureSDR USAA2012100100066Skin · saturatedC11 CHECK - AREAS OF WATER INGRESS ON LEFT ELEVATOR UPPER SURFACE APPROX 19 INCHES TO 191 INCHES FROM INBOARD END. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11 PARA 5D & 5E, FIGS 204 & 205.Sep 18, 2012 · N762US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2012100100060Splice Plate · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SILL SPLICE PLATE AT FR66, Y1732. REPLACED SILL SPLICE PLATE AT FR66, Y1732 IAW A319 SRM 53-41-14 FIG 101 & 201.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012100100059Shear Pin · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Y1162. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Y1162 IAW A319 SRM 51-42-11 PAR 6.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012100100058Shear Plate · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1162. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1162 IAW A319 SRM 51-42-11 PAR 6.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012100100057Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y1292 IAW A319 SRM 51-42-11 PAR 5.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012100100056Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, -Y765 IAW A319 SRM 51-42-11 PAR 5.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012100100055Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, Y1732 IAW A319 SRM 51-42-11 PG 25-27 & 30 FIG 8 & 12.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012100100054Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, -Y765 IAW A319 SRM 51-42-11 PAR 5.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012100100053Floorbeam · corrodedC11 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1162 IAW A319 SRM 51-42-11.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012100100052Floorbeam · corrodedC11 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1162 IAW A319 SRM 51-42-11 PAR 5.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012100100051Floorbeam · corrodedC11 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A319 SRM 51-42-11 PAR 5.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012100100050Floorbeam · corrodedC11 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Y1292 IAW A319 SRM 51-42-11 PAR 5.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012100100049Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, Y765 IAW A319 SRM 51-42-11 PAR 5.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012100100048Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y765 IAW A319 SRM 51-42-11 PAR 5.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012100100038Seat Track · corrodedC11 CHECK - CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPAIRED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A319 SRM 53-21-15 FIG 204.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012100100036Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT RAIL BEAM ASSEMBLY BETWEEN FR64 TO FR66, -Y1292. REPLACED SEAT RAIL BEAM ASSEMBLY BETWEEN FR64 TO FR66, -Y1292 IAW A319 SRM 51-42-11 PAR 5.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012100100035Floor Panel · corrodedC11 CHECK - CORROSION ON FLOOR PANEL 222FF BETWEEN FR16 TO FR20 & BETWEEN -Y1262 TO -Y1584. REPLACED FLOOR PANEL 222FF IAW JOB CARD 26C22053014.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012100100032Floor Panel · corrodedC11 CHECK - CORROSION ON FLOOR PANEL 262FF BETWEEN FR66 TO FR68 & BETWEEN -Y1292 TO -Y1732. REPLACED FLOOR PANEL 262FF IAW JOB CARD 26C26053014.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012100100031Floor Panel · corrodedC11 CHECK - CORROSION ON FLOOR PANEL 221FF BETWEEN FR16 TO FR20 & BETWEEN Y1262 TO Y1584. REPLACED FLOOR PANEL 221FF IAW JOB CARD 26C22053014.Sep 18, 2012 · N762US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012100100067Skin · saturatedC11 CHECK - AREAS OF WATER INGRESS ON RIGHT ELEVATOR UPPER SURFACE APPROX 23 INCHES TO 159 INCHES FROM INBOARD END. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11 PARA D & E, FIGS 204 & 205.Sep 17, 2012 · N762US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2012100100065Attach Angle · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON ATTACH ANGLE AT FR20, Y1584. REPLACED ATTACH ANGLE AT FR20, Y1584 IAW A319 SRM 5151-42-11 PARA 7B FIG 12.Sep 17, 2012 · N762US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012100100064Attach Angle · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON ATTACH ANGLE PLATE AT FR16, -Y1379.5. REPLACED ATTACH ANGLE PLATE AT FR16, -Y1379.5 IAW A319 SRM 51-42-11 FIG 3.Sep 17, 2012 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
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