N763US
Service difficulty reports · 243
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 = 'N763US' 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.
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 = 'N763US' AND registry_match = 'registration' 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 USAA2012100300005Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 261DF IAW A319 SRM 53-02-00.SDR USAA2012100300004Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261BG BETWEEN FR64 TO FR66 & BETWEEN -Y765 TO Y1732. REPLACED FLOOR PANEL 261BG IAW A319 SRM 53-02-00.SDR USAA2012100300003Floor Panel · damagedC11 CHECK - ELONGATED HOLE IN FLOOR PANEL 231CF BETWEEN FR20 TO FR24 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 231CF IAW A319 SRM 53-02-00.SDR USAA2012100500022Floorbeam · corrodedC11 CHECK - LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 65 & FR 66 AT Y 1292. REMOVED AND REPLACED BEAM IAW A319 SRM 53-00-14, 51-72-11, 51-42-11, 51-44-11.SDR USAA2012100500021Floorbeam · corrodedC11 CHECK - LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 65 & FR 66 AT Y 1732. REMOVED AND REPLACED BEAM IAW A319 SRM 51-42-11, 51-44-11, 51-75-12.SDR USAA2012100500020Seat Track · corrodedC11 CHECK - SEAT TRACK CORRODED BETWEEN FR 16 & FR 24 AT Y -1292. REMOVED AND REPLACED TRACK IAW A319 SRM 53-11-14, 51-44-11, 51-42-11.SDR USAA2012100300007Shear Plate · crackedC11 CHECK - CRACK ON SHEAR PLATE BETWEEN FR68 TO FR69, S23L. REPLACED SHEAR PLATE BETWEEN FR68 TO FR69, S23L IAW A319 SRM 51-42-11 & 51-44-11.SDR USAA2012100500019Dummy Rail · corrodedC11 CHECK - SEAT TRACK DUMMY RAIL CORRODED BETWEEN FR 14 & FR 16 AT Y -81. REMOVED AND REPLACED RAIL IAW A319 SRM 53-11-14 FIGURE 102 & 51-42-11.SDR USAA2012100500018Floorbeam · corrodedC11 CHECK - LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 65 & FR 66 AT Y -765. REMOVED AND REPLACED BEAM IAW A329 SRM 53-00-14 FIGURE 102 & 51-42-11.SDR USAA2012100500017Sill · corrodedC11 CHECK - R2 DOOR SILL CORRODED AT FR 66 & Y -1732. REPAIRED SILL IAW A319 SRM 53-41-14 FIGURE 101, 53-41-14 FIGURE 201 & 51-42-11.SDR USAA2012100500016Floorbeam · corrodedC11 CHECK - LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 65 & FR 66 AT Y -1292. REMOVED AND REPLACED BEAM IAW A319 SRM 53-00-14 FIGURE 102 & 51-42-11.SDR USAA2012100500015Floorbeam · corrodedC11 CHECK - LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 67 & FR 68 AT Y -1292. REMOVED AND REPLACED BEAM IAW A319 SRM 53-00-14 FIGURE 102 & 51-42-11.SDR USAA2012100500014Floorbeam · corrodedC11 CHECK - LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 66 & FR 67 AT Y -1292. REMOVED AND REPLACED BEAM IAW A319 SRM 53-00-14 FIGURE 102 & 51-42-11.SDR USAA2012100300006Shear Plate · crackedC11 CHECK - CRACK ON AFT CABIN LATERAL SHEAR PLATE BETWEEN FR68 TO FR69, S23R. REPLACED AFT CABIN LATERAL SHEAR PLATE BETWEEN FR68 TO FR69, S23R IAW A319 SRM 51-42-11.SDR USAA2012100500013Floorbeam · corrodedC11 CHECK. LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 64 & FR 65 AT Y 765. REMOVED AND REPLACED BEAM IAW SRM 53-00-14 FIGURE 102 & 51-42-11.SDR USAA2012100500012Floorbeam · corrodedC11 CHECK - LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 68 & FR 70 AT Y 765. REMOVED AND REPLACED BEAM IAW A319 SRM 53-00-14 FIGURE 102 & 51-42-11.SDR USAA2012100300010Shear Plate · damagedC11 CHECK - ELONGATED HOLE ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A319 SRM 53-41-17 FIG 101 & 51-42-11.SDR USAA2012100300009Shear Plate · chafedC11 CHECK - CHAFING & ELONGATED HOLES ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A319 SRM 53-41-17 FIG 101 & 51-42-11.SDR USAA2012100300008Shear Plate · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A319 SRM 53-41-17 FIG 101 & 51-42-11.SDR USAA2012082900011Hinge · wornFLT/CHK 2049 - AIRFRAME VIBRATION - SEE FORM- FL 220-260 310-320 KIAS STOPS WHEN RUDDER TRIM IS NOT .2R OR .3R. NO ENGINE OR FLIGHT CONTROL INDICATIONS. INSPECTED NLG DOORS AND ACCOMPLISHED TR320- 5280-10-0005A SECTION (I) REMOVED AND REPLACED BOTH FWD HINGESDR USAA2012070500024Lens · missingEMERGENCY LIGHT LENS COVER MISSING AT DOOR L4. INSTALLED EMERGENCY LIGHT LENS COVER AT DOOR 4L. OPS CHECKED GOOD.SDR USAA2012040600014Lens · unsecureEMERGENCY EXIT LIGHT LENS FELL OFF L2 DOOR AFT SIDE PANEL. SECURED LENS COVER ON L2 DOOR EXIT LIGHT. OPS CHECKED GOOD.SDR USAA2012030900012Lens · missingSMALL EMERGENCY EXIT LIGHT IS MISSING FROM LOWER WALL POSITION, AFT SIDE OF AFT LEFT LAV DOOR. REPLACED MISSING EMERGENCY EXIT LIGHT LENS ON LOWER LAV WALL.SDR USAA2011120100004Hinge Fitting · wornENGINE AND AIRFRAME VIBRATION NOTED DURING CLIMB, ENGINE NR 1 VIB N1 (1) 2.3 (2) .7. ALL OTHER ENGINE PARAMETERS WERE MATCHED. DURING CRUISE VIB N1(1) 2.1 (2) .7. REPLACED LEFT AFT NOSE GEAR DOOR HINGES IAW A319 AMM 32-22-13.SDR USAA2011022190848Skin · debondedPIT - MAJOR REPAIR - RUDDER DISBOND CHECK- RUDDER HAS AREA OF DISBOND, 3.11INCHES ABOVE BR1 AND 13.25 INCHES FWD OF THE TRAILING EDGE. REPAIRED RUDDER, 3.11 INCHES ABOVE BR1 AND 13.25 INCHES FWD OF THE TRAILING EDGE IAW EA 117296.SDR USAA2010081691667Bottle · low pressureFLT 2048 - DCA-BOS - EMERGENCY EGRESS SYSTEM - L2 DOOR BOTTLE NEEDS SERVICING. SERVICED L2 DOOR ASSIST BOTTLE PER AMM 52-10-00-614.SDR USAA2009083192297Lens · missingFLT 1406 - MIA-PHL - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT LENS ON SEAT 4C IS MISSING AND LIGHT IN SEAT RECESSED INTO SEAT. REPLACED EMERGENCY LIGHT LENS. OPERATIONAL CHECK WAS GOOD.SDR USAA2009081792139Lens · missingFLT 2169 - LGA-DCA - EMERGENCY LIGHTS - FLOOR PATH EMERGENCY LIGHT LENS MISSING AT 1C. REMOVED AND REPLACED FLOOR PATH EMERGENCY LIGHT LENS AT 1C.SDR USAA2009072791933Acm · overheatedFLT 1420 - PHL-CLT - ELECTRICAL SMELL - OILY OR HOT ELECTRICAL SMELL FROM NR 1 PACK, TURNED PACK OFF AND SMELL DISSIPATED. REMOVED AND REPLACED AIR CYCLE MACHINE (ACM) PER MAINTENANCE MANUAL 21-52-21. OPERATIONAL CHECK WAS GOOD.SDR USAA2009062691607Brake · overheatedFLT 1937 - PHL-PHL - ABORTED TAKEOFF - AT APPROXIMATELY 100 KNOTS IAS BRAKE TEMPERATURE INDICATED AS: NR 1 BRAKE-995 DEGREES, NR 2 BRAKE-995 DEGREES, NR 3 BRAKE 700 DEGREES, AND NR 4 BRAKE-685 DEGREES. REMOVED AND REPLACED NR 1 & 2 BRAKE ASSEMBLY IAW MAINTENSDR USAA2009062691603Brake · overheatedFLT 1937 - PHL-PHL - ABORTED TAKEOFF - AT APPROXIMATELY 100 KNOTS IAS BRAKE TEMPERATURE INDICATED AS: NR 1 BRAKE-995 DEGREES, NR 2 BRAKE-995 DEGREES, NR 3 BRAKE 700 DEGREES, AND NR 4 BRAKE-685 DEGREES. REMOVED AND REPLACED NR 1 & 2 BRAKE ASSEMBLY IAW MAINTENSDR USA09021690341Wire · disconnectedAC LT SEAT MOUNTED EMERGENCY MOUNTED EMERGENCY AISLE LIGHTING INOPERATIVE. FOUND WIRE DISCONNECTED. REATTACHED WIRE TO PLUG. OPS CHECK WAS GOOD. (K)SDR USAASA06094Proximity Switch · faultyCLT FLT900 AFTER TAKEOFF FROM MBJ, EN ROUTE TO CLT, CREW RECEIVED ECAM WARNINGS: -ENGINE 2 REVERSER FAULT-, -ANTI-ICE CAPTAIN'S PITOT- AND -GEAR WOULD NOT RETRACT-. CREW RECYCLED LANDING GEAR AND A NORMAL GEAR RETRACTION COMMENCED. FIVE MINUTES LATER, BOTHSDR USAA061223Beam · corrodedLEFT STA 1292 Z-BEAM 3 SECTIONS, 6 PLACES CORROSION. REMOVED & REPLACED Z-BEAM SECTIONS PER AIRBUS DWG D53472815 & SRM 51-72-11; CORR TASK JA-260-53500, DEFECT SIZE: 2 INCHES AT 6 PLACES.SDR USAA061208Seat Track · corrodedFOUND CORROSION 55" FROM RT OUTBD FWD END SEAT TRACK. INSTALLED 2 SPLICES IN SEAT TRACK PER SRM 53-00-15; CORROSION TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 1" BY 3" AND 1" BY 1".SDR USAA061209Web · corrodedFOUND CORROSION LT SHEAR WEB BETWEEN C69 AND C70. REPLACED WITH IDENTICAL PART AND PER DWG.; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 12" BY 12".SDR USAA061210Floorbeam · corrodedFOUND FLOORBEAM CORRODED, 10" LEFT OF CENTER, BETWEEN FS 12 AND 16. FLOORBEAM REMOVED AND INSTALLED PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 1" BY 18" BY .075".SDR USAA061211Floorbeam · corrodedFOUND FLOORBEAM CORRODED Y254 TOP FACE ABOVE C21. CUT OUT DAMAGE, INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-00-14; CORROSION TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 1/2" BY 1-3/4".SDR USAA061198Beam · corrodedRT STA 1292 Z-BEAM - 2 SECTIONS; CORR TASK JA-260-53500; LEVEL 1. REMOVED & REPLACED Z-BEAM SECTION PER AIRBUS DWG D53472815 & D53472780 & SRM 51-72-11, DEFECT SIZE: 2 X 3 INCHES.SDR SA05037Battery · installedDCA - FOUND AN EPSU BATTERY (13WLA) WHICH NEEDED TO BE REPLACED. MAINTENANCE REPLACED THE EPSU BATTERY.SDR SA04111Windshield · crackedCLT FLT 473 ENROUTE PIT TO TPA, DURING THE FLIGHT, THE FIRST OFFICER'S WINDSHIELD BEGAN TO ARC, FOLLOWED BY THE OUTER PANE CRACKING. CREW ALSO RECEIVED ECAM WARNINGS "R WINDSHIELD" AND "R WINDOW". QRH PROCEDURES WERE FOLLOWED AND THE FLIGHT DIVERTED TO CLT.SDR USAASA04077Diaphragm · rupturedUPON ATTEMPT TO ENTER THE AIRCRAFT, THE MAINTENANCE CREW FOUND THAT THE R1 DOOR WOULD NOT OPEN FROM THE OUTSIDE. PRESSURE WAS FELT AGAINST THE DOOR AS THE ATTEMPT TO OPEN WAS MADE. MAINTENANCE FOUND THE DOOR ASSIST BOTTLE DIAPHRAM DISK PUNCTURED. SUSPECT PRSDR USAASA03127Cable · brokenDURING INSPECTION, FOUND THE CABLE END ON THE LEFT OVERWING SLIDE BROKEN NEAR THE SLIDE BOTTLE. MAINTENANCE REPLACED THE LEFT OVERWING SLIDE BOTTLE. OK FOR SERVICE. (M)
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