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 USAA2012100100061Floor Support · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT WEB AT FR20, -Y1584. REPLACED FLOOR SUPPORT WEB AT FR20, -Y1584 IAW A319 SRM 51-42-11 PARA 6 FIG 2 & 3.Sep 17, 2012 · N762US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012100100045Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK ASSEMBLY AT FR20, -Y254. REPLACED SEAT TRACK ASSEMBLY AT FR20, -Y254 IAW A319 SRM 51-42-11 PAR 7B FIG 12.Sep 17, 2012 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012100100044Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK ASSEMBLY AT FR20, -Y765. REPLACED SEAT TRACK ASSEMBLY AT FR20, -Y765 IAW A319 SRM 51-42-11 PAR 7B FIG 12.Sep 17, 2012 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012100100043Dummy Rail · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON DUMMY RAIL ASSEMBLY AT FR16, Y503.2. REPLACED DUMMY RAIL ASSEMBLY AT FR16, Y503.2 IAW A319 SRM 51-42-11 PAR 7B FIG 12 & 20.Sep 17, 2012 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012100100042Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK ASSEMBLY BETWEEN FR20 TO FR21+15 INCHES, Y1292. REPLACED SEAT TRACK ASSEMBLY BETWEEN FR20 TO FR21+15 INCHES IAW A319 SRM 51-42-11 PAR 7B FIG 12.Sep 17, 2012 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012100100041Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK ASSEMBLY BETWEEN FR16 TO FR24, Y254. REPLACED SEAT TRACK ASSEMBLY BETWEEN FR16 TO FR24, Y254 IAW A319 SRM 51-42-11 PAR 7B FIG 12.Sep 17, 2012 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012100100040Seat Track · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK ASSEMBLY BETWEEN FR16 TO FR20, -Y1292. REPLACED SEAT TRACK ASSEMBLY BETWEEN FR16 TO FR20, -Y1292 IAW A319 SRM 51-42-11 PAR 7B FIG 12.Sep 17, 2012 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012100100039Dummy Rail · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON DUMMY RAIL AT FR20, -Y189. REPLACED DUMMY RAIL AT FR20, -Y189 IAW A319 SRM 51-42-11, PAR. 7, B & D, FIG 12 & 20.Sep 17, 2012 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012100100037Dummy Rail · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON RAIL DUMMY AT FR16, -Y81. REPLACED RAIL DUMMY AT FR16, -Y81 IAW A319 SRM 51-42-11 PAR 7D FIG 12.Sep 17, 2012 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012100100062Support Bracket · brokenC11 CHECK - BROKEN R-2 DOOR UPPER DOOR HANDLE BRACKET SUPPORT AT FR68, S17R. REPLACED R-2 DOOR UPPER DOOR HANDLE BRACKET SUPPORT AT FR68, S17R IAW A319 SRM 51-44-11 FIG 2.Sep 16, 2012 · N762US · Airbus A319112 · Service DoorsSDR USAA2012100100030Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 151VG BETWEEN FR53 TO FR56 & BETWEEN S40L TO S40R IN AFT CARGO COMPARTMENT. REPLACED FLOOR PANEL 151VG, IAW A319 SRM 51-42-11 & AMM 53-42-14-400-001-A.Sep 15, 2012 · N762US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012100100029Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 151ZG BETWEEN FR56 TO FR58 & BETWEEN S40L TO S40R IN AFT CARGO COMPARTMENT. REPLACED FLOOR PANEL 151ZG IAW A319 SRM 51-42-11 & AMM 53-42-14-400-001-A.Sep 15, 2012 · N762US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012032600019Valve · overheatedLANDING GEAR WOULD NOT RETRACT. LGCIU 1 & LGCCIU SYS 1 GROUND SUPPLY CIRCUIT BREAKERS TRIPPED DURING RETRACTION. FOUND SAFETY VALVE GREEN SYSTEM 49GA GETS EXTREMELY HOT DURING GEAR SWING. SUSPECT PROBLEM WITH CIRCUIT BREAKERS C-09 AND C-034 POPPING. REMOVEMar 21, 2012 · N762US · Airbus A319112 · Landing Gear Retraction/Extension SystemSDR USAA2012030100002Crossbeam · brokenBEAM BROKEN AT FRAME C20 TO FRAME 20. UPPER LEFT AFT CORNER NOSE LANDING GEAR STRUCTURE. REPLACED CROSS BEAM AT FR20 AT NOSE LANDING GEAR STRUCTURE IAW A319 SRM 51-72-11.Feb 28, 2012 · N762US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012010900015Megaphone · inoperativeFORWARD PORTABLE MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE WITH SERVICEABLE UNIT.Jan 6, 2012 · N762US · Airbus A319112 · Emergency EquipmentSDR USAA2011101300012Unknown · odorFAINT ODOR ON TAKEOFF PASSING APPROXIMATELY 10,000 FT AND ON ARRIVAL DESCENDING THROUGH 10,000 FT. SLIGHT ELECTRICAL BURNING ODOR LASTING APPROXIMATELY 3 TO 5 MINUTES. ACCOMPLISHED CABIN AIR QUALITY CHECK. NO DEFECTS NOTED. UNABLE TO VERIFY SOURCE OF ODOR.Oct 11, 2011 · N762US · Airbus A319112 · Air Distribution SystemSDR USAA2011050491749Hydraulic Line · leakingFLT 1785 - IND-IND - EMERGENCY LANDING - LOST GREEN HYDRAULIC FLUID. FOUND RIGHT GEAR DOOR LINE LEAKING. REMOVED AND REPLACED LINE. AS PRECAUTIONARY, REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP. OPERATIONAL CHECK WAS GOOD.May 1, 2011 · N762US · Airbus A319112 · Hydraulic System, MainSDR USAA2011022890885Unknown · malfunctionedFLT 1222 - CLT-BWI - EMERGENCY LANDING - EXPERIENCED PROBLEMS WITH STABILIZER, EXTREME AIRFRAME BUFFET INCURRED. COMPLETED TASK CARDS 26T00027002 (ELEVATOR AND AILERON SERVO CONTROLS), 26T00027003 (OPERATIONAL TEST OF RUDDER SERVO, STAB TRIM, AND CARGO SMOKE Feb 24, 2011 · N762US · Airbus A319112 · Stabilizer Control SystemSDR USAA2011022290851Battery · dischargedFLT 1406 - PHL-BOS - EMERGENCY LIGHTS - RECHARGEBLE FLASHLIGHT AT L1 DOOR INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.Feb 19, 2011 · N762US · Airbus A319112 · Emergency EquipmentSDR USAA2011012490321Cylinder · low pressureFLT 2048 - DCA-BOS - EMERGENCY EGRESS SYSTEM - R2 DOOR DAMPER CYLINDER PRESSURE LOW. SERVICED R2 DOOR DAMPER CYLINDER PER AMM 52-10-00-614-001.Jan 21, 2011 · N762US · Airbus A319112 · Service DoorsSDR USAA2010052191001Bottle · low pressureMCN - EES - GEAR CHANGE - L1 DOOR POWER ASSIST BOTTLE READS ZERO. REPLACED THE L1 DOOR ASSIST BOTTLE PERCUSSION MECHANISM DIAGRAM AND SERVICED THE BOTTLE IAW A319 AMM 52-10-00.May 20, 2010 · N762US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2010052591031Pin · wornMCN - LANDING GEAR CHANGE - MAJOR REPAIR - LEFT MAIN LANDING GEAR AFT PINTLE PIN SCORED & WORN. REPLACED LEFT MAIN LANDING GEAR AFT PINTLE PIN.May 14, 2010 · N762US · Airbus A319112 · Main Landing Gear Attach SectionSDR USAA920081781Battery · dischargedFLT NR 9172 - FLL-DCA - EEL FOUR CABIN BREAKAWAY CABIN FLASHLIGHTS USED AND DEPLETED. REMOVED AND REPLACED BATTERIES FOR EMERGENCY FLASHLIGHTS. OPS CHECK GOOD.Sep 29, 2008 · N762US · Airbus A319112 · Emergency EquipmentSDR USAA061182Shear Tie · corrodedLT SHEAR TIE AT FRAME 69, SEVERAL SPOTS OF 1 INCH DIA CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORR TASK JA-260-53500, DEFECT SIZE: 1 INCH DIA, SEVERAL SPOTS.Sep 21, 2006 · N762US · Airbus A319112 · Fuselage Internal Mounting StructureSDR USAA061183Floor Support · corrodedFRAME 20 & FLOOR SUPPORT Y254 CORROSION. INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-11-15 FIG 203, DEFECT SIZE: .375 INCH.Sep 21, 2006 · N762US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061184Floorbeam · corrodedFR 20 AT -Y1292 CORROSION. REPLACED FLOORBEAM PER SR 51-72-11; CORR LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 2 SQ INCHES.Sep 21, 2006 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061185Seat Track · corrodedSEAT TRACK FLOORBEAM Y1292 BETWEEN FRAMES 66-69 CORROSION. REMOVED AND REPLACED 3 ATTACHED FLOORBEAMS PER SRM 51-72-11; CORR LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 3 SQ INCHES.Sep 21, 2006 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA061186Floorbeam · corrodedFR 68 ON RIGHT O/B FLOORBEAM CORROSION. REPLACED PART WITH IDENTICAL PART PER SRM 51-72-11, DEFECT SIZE: 1 INCH DIA X .040 INCH DEEP AT CENTER.Sep 21, 2006 · N762US · Airbus A319112 · Fuselage Main, Floor BeamSDR SA05114Slide · reads lowTHE AFT RIGHT DOOR EMERGENCY ESCAPE SLIDE INDICATED LOW PRESSURE DURING INSPECTION. MAINTENANCE REPLACED THE AFT RIGHT DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE.Nov 14, 2005 · N762US · Airbus A319112 · Escape SlideSDR 2005FA0000575Placard · failedDEBRIS (PLASTIC RIB AND MANHOLE DOOR IDENTIFICATION DECALS) FOUND ON THE INLET STRAINER OF THE LT AND RT WING FUEL TANK, NR 2 MAIN FUEL PUMP AFT SCREENS DURING C-CHECK. OIT ISSUED BY AIRBUS AND IS APPLICABLE TO MSN1136. (K)Apr 4, 2005 · N762US · Airbus A319112 · Fuel StorageSDR 2005FA0000577Quick Disconnect · looseDURING A C-CHECK, THE QUICK DISCONNECT WHICH CONNECTS THE SLIDE RELEASE CABLE TO THE RELEASE MECHANISM ON THE PACKBOARD ASSY WAS FOUND LOOSE. THE ELECTRICAL LOOM WAS CONFIGURED FOR A LT DOOR. (K)Mar 29, 2005 · N762US · Airbus A319112 · Escape SlideSDR 2005FA0000576Quick Disconnect · missingWHILE CARRYING OUT A SAMPLE INFLATION ON THE AFT ENTRY DOOR, THE ESCAPE SLIDE FAILE TO RELEASE FROM THE PACK DUE TO THE QUICK DISCONNECT, PN 25C150911, WHICH CONNECTS THE SLIDE RELEASE CABLE TO THE RELEASE MECHANISM ON THE PACKBOARD ASSY BEING MISSING.(K)Mar 29, 2005 · N762US · Airbus A319112 · Escape SlideSDR 2005FA0000574Light · failedTHE ESCAPE SLIDE LIGHTS DID NOT WORK DUE TO THE CONNECTOR NOT FULLY HOME. THE ELECTRICAL LOOM AND THE CONNECTOR WERE NOT STOWED PROPERLY. (EA33200501197) (K)Mar 29, 2005 · N762US · Airbus A319112 · Escape SlideSDR USAA040566Skin · dentedPIT - FOUND SKIN DENTED 7 INCH BY 8 INCH BY .331 INCH, BETWEEN FRAME 3 AND 4, STRINGERS 22 AND 23 IN PITOT STATIC PORT RED BAND. TEMPORARY REPAIR, INSTALLED L ANGLES AND DOUBLERS PER EA 79115. (M)Sep 9, 2004 · N762US · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA040564Skin · dentedPIT - FOUND SKIN DENTED 7 INCH BY 7 INCH BY .250 INCH DEEP, BETWEEN FRAME 4/5 AND STRINGERS 22 AND 23 IN RED STATIC PORT BAND. TEMPORARY REPAIR INSTALLED L ANGLES AND DOUBLER PER EA 79115. (M)Sep 9, 2004 · N762US · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAASA04007Wire · inoperativeTHE SEAT MOUNTED EMERGENCY LIGHT ON SEAT 3L WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED THE WIRING TO THE LIGHT ASSEMBLY. OPERATIONALLY CHECKS OK. (M)Jan 25, 2004 · N762US · Airbus A319112 · Light System WiringSDR USAADUPE1Blower · failedFLT 147 - EN ROUTE CLT-PHX, AN ACRID ODOR WAS DETECTED IN THE COCKPIT, FOLLOWED BY AN ECAM MESSAGE OF VENT BLOWER INOPERATIVE. FLIGHT LANDED IN PHX WITHOUT FURTHER INCIDENT. (M)Dec 3, 2002 · N762US · Airbus A319112 · Air Distribution FanSDR USAASA02104Blower · malfunctionedEN ROUTE, AN ACRID ODOR WAS DETECTED IN THE COCKPIT, FOLLOWED BY AN ECAM MESSAGE OF VENT BLOWER INOPERATIVE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AVIONICS VENT BLOWER FAN, FIN20HQ. SYSTEM BITE CHECKS, OK.Dec 3, 2002 · N762US · Airbus A319112 · Air Distribution FanSDR USAASA01054Light · wrong partCLT - AFTER REPLACEMENT OF SEAT ROW 3 ABC, IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHT INSTALLED ON THE SEAT WAS AN INCORRECT PART AND WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE BULBS. OPERATIONALLY CHECKED OK. (M)Oct 9, 2001 · N762US · Airbus A319112 · Emergency Lighting
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