N810UA

Service difficulty reports · 146

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 = 'N810UA' 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 CALA2022032500793Floor Support · corroded(SDR) CORROSION ON RH SIDE FLOOR SUPPORT BEAM AT APPROX Y-1500 B ETWEEN FR65-FR66. CORROSION ON RH SIDE Y-1500 BTW FR65-FR66 FOUND OUT OF LIMITS IA STA: ST ENG BFM W SRM 53-00-14-283-002 FIG 001. REPLACED FLOOR BEAM FOR NEW FLOO R SUPPORT BEAM P/N: D5347207500Mar 25, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2022032500792Door · cracked(SDR)FOUND CRACK ON INTERNAL STRUCTURE OF LH EMERGENCY EXIT DOOR REMOVED INTERNAL STRUCTURE (SEGMENT ANGLE) THE EMERGENCY EXIT DO OR AND INSTALLED NEW SEGMENT ANGLE IAW SRM 51-42-11. EMP: V93387 0 WC: 0024009 STA: ST ENG BFMMar 25, 2022 · N810UA · Airbus A319131 · DoorsSDR CALA2022032500791Floor Support · corrodedCORROSION ON LH SIDE FLOOR SUPPORT BEAM Y765.0 AT FR66 REMOVED CORROSION ON BEAM 765.0 AT FR66 SIAW SRM 51-74-00-001 L= 2" W=1.5" DEPTH=0.055" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-1 4-283-002 FIG 001 SHEET 02. REPLACED WITH NEW BEAM IAW SRM 51-42 -11. EMP: Mar 25, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2022032500790Hinge · cracked(SDR) DURING INSPECTION OF AFT CARGO DOOR HINGE, NDT FOUND DISCR EPANCY IN 3EA HOLES. HOLE WITH DISCREPANCY DRILLED TO OVERSIZE IAW SRM 51-44-11/001 T ABLE 16 FINAL DIAMETER AT HOLE A: 0.213", AND HOLES B&C: 0.197". HFEC C/W - NO CRACKS OR OTHER DAMAGE NOTED. Mar 25, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2022032500789Floor Support · corroded(A3NB-53-3-6187) CORROSION ON LH SIDE FLOOR SUPPORT BEAM Y 1292. 0 AT FR66 (74-21) () CORROSION ON LH SIDE FLOOR SUPPORT BEAM Y1292 REMOVED IAW SRM 51 AND SRM 51-42-11. EMP: V933866 WC: 0024102 STA: ST ENG BFM -74-00. BEAM FOUND OUTSIDE LIMITS IAW SRM 53-00-14Mar 25, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2022032500788Shear Plate · corroded(SDR) CORROSION ON RH SIDE SHEAT PLATE BETWEEN FR69-FR70. REMOVED SHEAT PLATE RH BETWEEN FR69-FR70 FOR CORROSION TO BE OUT OF LIMITS AND REPLACED FOR NEW SHEAT PLATE IAW SRM 51-42-11. DI MENSION OF THE CORROSION L=0.5" W=0.5" D=0.015". EMP: V933870 WC : 002407Mar 25, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2022032300756Beam · corroded(A3NB-53-3-6187) CORROSION ON LH SIDE FLOOR SUPPORT BEAM Y 1292. 0 AT FR66 (74-21) ()Mar 22, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2022032300755None · none(SDR) DURING INSPECTION OF AFT CARGO DOOR HINGE, NDT FOUND DISCR EPANCY IN 3EA HOLES.Mar 22, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2022032300754None · none(SDR)FOUND CRACK ON INTERNAL STRUCTURE OF LH EMERGENCY EXIT DOORMar 22, 2022 · N810UA · Airbus A319131 · DoorsSDR CALA2022032300753Beam · corrodedCORROSION ON LH SIDE FLOOR SUPPORT BEAM Y765.0 AT FR66Mar 22, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2022032300752Beam · corroded(SDR) CORROSION ON RH SIDE FLOOR SUPPORT BEAM AT APPROX Y-1500 B ETWEEN FR65-FR66.Mar 22, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2022032300751Plate · corroded(SDR) CORROSION ON RH SIDE SHEAT PLATE BETWEEN FR69-FR70.Mar 22, 2022 · N810UA · Airbus A319131 · Standard Practices/StructuresSDR CALA2022031000625None · noneFOUND 2 AREAS OF CORROSION DAMAGE IN THE AFT CARGO COMPARTMENT O N THE INTERIOR LEDGE BETWEEN FR57 AND FR58. (SDR) REMOVED CORROSION LEDGE BETWEEN FR57/FR58 IAW SRM 51-24-00, CHEC SRM 51-23-11. EMP: V936136 WC: 0024017 STA: ST ENG BFM KED LIMITS IAW SRM 53-41-Mar 9, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2022030700588Beam · corroded(A3NB-53-3-6187) CORROSION ON L/H SIDE FLOOR SUPPORT BEAM Y 160. 5 HAS CORROSION BETWEEN FR68 AND FR70 (DOT74-16/74-17) () 1EA FLOOR BEAMNO Y160.5 REMOVED AND REPLACED IAW SRM 51-42-11/00 1 AND TREATED WITH PRIMER, PAINTING AND CIC IAW SRM 51-21-11/00 1. ACCOMar 5, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2022030700587Beam · corroded(SDR) CORROSION ON RH SIDE FLOOR SUPPORT DUMMY RAIL Y-179.0 AT F R66Mar 5, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2022030700586None · corroded(SDR) CORROSION AND CRACK ON LH SIDE SHEAT PLATE BETWEEN FR69-FR 70. REMOVED SHRDR PLATE FOR CRACK AND CORROSION LH SIDE BETWEEN FR69 -FR70 IAW SRM 51-42-11 AND INSTALLED NEW SHEAR PLATE IAW SRM 51- 42-11. ACCOMPLISHED BY AT BFM ST AEROSPACE MOBILE. N R#002408Mar 5, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2022030700585Fitting · cracked(AD 2020-18-06) LH FR43 FRAME FOOT HAS CRACK INDICATION AT 9 O?? CLOCK LOOING FWD.???REPAIR BEFORE NEXT FLIGHT???(REPAIR ON CONDI TION IAW DWG R53370233) REPAIRED L/H F.43 BY FREEZE PLUG IAW DWG R53370233, VAL EA5330-0 6692. ACCOMPLISHED BY EMP#V936761 AT ST BMar 5, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2021091301562Blower · failed*EMERGENCY DECLARED* ELECTRICAL SMELLIN FLIGHT DECKAND CABINDURING FLIGHT FOUND AVIONICS COOLING BLOWER FAN INOP. REQUIRES M&E 31-2126-9-9004 PART IS NIS IN PDX. DEFERRED IAW MEL 2126A. CRW REPORTED ACRID ODOR IN FLIGHT DECK AND CABIN BEFORE DESCENT STARTED. ASep 12, 2021 · N810UA · Airbus A319131 · Air Distribution FanSDR CALA2019111601992Pump · inoperativeCTR TK PUMP1 INOP. ECAMCOMPLETED. MEL REQUESTED. DISPATCH DESK: 35 NAME: JG DATE: 11-NOV-19- APPROVED PER MEL 2821C AND DD DDP COMPLIED WITH REF TSM28-21-00-810-813-A, TRANSFERED FUEL TO CTR TANK VERIFIED PUMP 1 SUPPLY C/B CLOSED AND 69QA Nov 15, 2019 · N810UA · Airbus A319131 · Fuel Boost PumpSDR CALA2019092301602Pressure Plate · crackedROTARY INSP FROM TASK CARD 14333 AT 35-36 FOUND 19 HOLES WITH CRACK INDICATIONS IN PRESSURE PLATE. HOLE 1,2,3,4,5,6,7,9,11,16,17 ,18,20,23,24,26,27,28 RT SIDE PER HGR NR 9294449. REPAIRED RT FR35-36 HOLES IAW SRM 51-42-11 REO L22287 REV IR ECRA 5331-02458 REV Sep 16, 2019 · N810UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2019092301597Intercostal · crackedRT FR16 DOOR STOP NR 7 IB UPPER AND IB LWR HOLES HAVE CRACK INDICATIONS AIMING IB AND APPEAR TO BE IN INTERCOSTAL LAYER AD RELATED TASK SPEC NR A3NB-53-4-0018 PER HGR NR 9294340. RMVD AND RPLD NR 7 RT INTERCOSTAL AT FR16 RT IAW SRM 51-72-11-91 1-001 AND ECRA 5Sep 16, 2019 · N810UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2019092301596Intercostal · crackedLT FR16 DOOR STOP NR 1, IB LWR HOLE HAS CRACK INDICATION IN THE 6 OCLOCK AD RELATED TASK SPEC NR A3NB-53-4-0017 PER HGR NR 9294 342. RMVD AND RPLD NR 1 LT INTERCOSTAL AT FR16 L1 IAW SRM 51-72-11-91 1-001 AND ECRA 5311-02250.Sep 16, 2019 · N810UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2019092301603Pressure Panel · crackedLT SIDE PRESSURE PNL BTWN FR35-36 HOLES. CRACK INDICATION IN THE FOLLOWING HOLES 2,3,4,14,15,17,20,21,22,23,27 CRACKS NO GREATER THAN 1.8 INCH OUT ROUND CRACK INDICATIONS IN THE FOLLOWING HOLE S 16,18,19,25,28. ALL INDICATIONS DIRECTIONS MARKED ON THE LOWER SUSep 16, 2019 · N810UA · Airbus A319131 · Fuselage Main, BulkheadSDR CALA2018032601022Power Supply · no testAFTER EMERGENCY LIGHT CHECK, TWO MESSAGES CAME UP, EPSU UNIT AFT L, AND ESPU BATTERY FWD L. REPLACED THE POWER SUPPLY AND BATTERY IAW MM 31-51-38, AND MM 33-51-00. TESTED OK.Mar 26, 2018 · N810UA · Airbus A319131 · Emergency LightingSDR CALA2018022000713Warning System · false activationCABIN EMERGENCY LIGHT CHECK EPSU BATTERY EMER L ATA 33-51-38 MESSAGE DISPLAYED. RESET SYSTEM OPS CHECK NORMAL PER AMM 33-51-00.Feb 20, 2018 · N810UA · Airbus A319131 · Emergency LightingSDR CALA2017041000950Lanyard · out of positionAFT SLIDE DOOR 2R WILL NOT DISARM FOUND LANYARD PROTRUDING AT BOTTOM OF GIRT BAR, RESTOWED LANYARD. ALSO LUBED GIRT ATTACH POINTS AND ROLLERS. DOOR ARMED DISARMED OK.Apr 10, 2017 · N810UA · Airbus A319131 · Emergency EquipmentSDR CALA2015072194144Battery · faultedEPSU BATTERY AFT L MSG WHEN EMERGENCY EXIT LIGHT TEST ACCOMPLISHED. REPLACED BATTERY, CHECKED GOOD.Jul 18, 2015 · N810UA · Airbus A319131 · Emergency LightingSDR CALA2014122392860Battery · failedEMERGENCY BATTERY PACKS 11WL & 12WL FAIL TEST. REPLACED EPSU BATTERIES IAW AMM 33-51-38-400-002-A.Dec 19, 2014 · N810UA · Airbus A319131 · Emergency LightingSDR CALA2013111592969Unknown · leakingNR 1 ENG PIECE OF RUBBER HANGING FROM BOTTOM OF COWLING & FLUID DRIPPING SAME AREA. IAW MM78-31-00-710-041 F0R OPERATIONAL CHECK OF REVERSER VIA CFDS. TROUBLE SHOOTING TO POSSIBLE LEAK ON NR 1 ENG RT LOWER THRUST REVERSER ACTUATOR. LOCKED OUT NR 1 THRUST RENov 14, 2013 · N810UA · Airbus A319131 · Engine Thrust ReverserSDR CALA2013111292849Flap · dentedLARGE DENT IN FLAP JUST INBD OF ENG 1 PYLON. DENT IS 1.5 IN WIDE, .030 IN DEEP. ACCOMPLISHED HFEC IAW NDT M PT6 51-10-08, NO CRACKS INDICATED. IAW SRM 57-52-00 PG 135 FIG 117. 2" DIAM DENT, .030 DEPTH, LOCATED 5" INBD OF LT INBD FLAP TRACK & 7" FWD OF TE. Nov 11, 2013 · N810UA · Airbus A319131 · Trailing Edge FlapsSDR CALA2013110892759Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN, F CTL. ELAC 2 FAULT HAPPEN WHEN AUTOPILOT ENGAGED RESETS WITH AP OFF BUT FAULTS AGAIN W AP PROG TEXT. ACCOMPLISHED CHRONIC REVIEW. R & R ELAC 2 COMPUTER IAW AMM 27-93-34-400-001 OPERATIONS CHECKED GOOD. UNABLE TNov 7, 2013 · N810UA · Airbus A319131 · Flight Control SystemSDR CALA2013110592686Actuator · leakingDRIPPING OIL UNDER NR 1 ENG. NR 1 ENG THRUST REVERSER OTBD ENG COWL OPENING ACTUATOR LEAKING. APPEARS CASE IS CRACKED ON OTBD END AT BASE OF ATTACH POINT. REQUIRES ACTUATOR PCN 644-010 5 IAW IPC 78-36-51-80A NR 70. PLACED ON DF IAW MEL 2522EZ.Nov 4, 2013 · N810UA · Airbus A319131 · Engine Thrust ReverserSDR CALA2013110892758Thrust Reverser · damagedNR 1 ENG REVERSER, INBOARD C DUCT, SEAL BETWEEN THE TRANSLATING SLEEVE & THE LOWER BIFURCATION FOUND PARTLY DELAMINATED. FIBERGLASS OUTER SECTION HAS SEPARATED FROM THE RED INNER CORE, OUTER SECTION IS GONE. INNER SECTION IS STILL ATTACHED TO THE REVERSER & Nov 1, 2013 · N810UA · Airbus A319131 · Engine Thrust ReverserSDR CALA2013091091188Fan · faultyAEVC BLOWER FAULT IN FLIGHT, CREW WENT TO OVERRIDE, FAULTED AGAIN ON GROUND. REPLACED BLOWER FAN IAW MM 21-26-51-000-001-A & TEMP SENSOR IAW MM.Sep 8, 2013 · N810UA · Airbus A319131 · Air Distribution FanSDR CALA2013091091187Unknown · malfunctionedFWD CABIN TEMP TRIM VALVE FAILED. ACCOMPLISHED CFDS TEMP CONTROL TEST. TESTED OK. OPERATED PACKS & RAN FWD TEMP COLD TO HOT & BACK TO COLD, VALVE OPERATIONS CHECKED NORMAL, NO FAULTS.Sep 8, 2013 · N810UA · Airbus A319131 · Cabin Temperature Control SystemSDR CALA2013091091185Solenoid Valve · leaking'G' SYSTEM FLUID LOSS, RTFL FOUND SOLENOID VALVE OF THE PTU BROKEN. REPLACED IAW MM. REPLACED PUMP IAW MM. RE-INITIALIZED SYSTEM & ACCOMPLISHED AVEC TEST & OK NO MESSAGES.Sep 8, 2013 · N810UA · Airbus A319131 · Hydraulic System, MainSDR CALA2013073090067Sliding Window · leakingF/O SLIDING WINDOW LEAKING WATER. EXCESSIVE WATER ON RT CONSOLE. PRESSURIZED ACFT AND NO LEAKS AT 406 PSI DIFFERENTIAL.Jul 27, 2013 · N810UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2013061904264Windshield · delaminatedF/O AFT WINDSHIELD DELAMINATING BOTTOM MIDDLE. LENGTH OF DELAM 3.5" RECHECK EVERY 2 SVC.Jun 19, 2013 · N810UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2013042202760O-Ring · damagedFUEL DRIPPING FROM UNDER RT ENGINE. FUEL LEAKS AT IDG FUEL COOLED OIL COOLER AT FUEL TUBE MATING SURFACE REF IPC 24-21-42-80 ITEM 100 AND 130, NEED 1EA O-RINGS PCN 222-1010 AND 2EA O-RINGS PCN 222-1006. REPLACED LP O-RINGS REF MM. RAN MOTOR REF JRH FOR LEAK Apr 19, 2013 · N810UA · Airbus A319131 · AC Generator-AlternatorSDR UALA2013041002427Bumper · unsecureCREW REPORT: SEAT BUMPER STRIP 27D COMING OFF. SEAT BUMPER REMOVED AND STOWED IN CLOSET. REPLACED BUMPER WITH NEW. OK TO CONTINUE.Apr 10, 2013 · N810UA · Airbus A319131 · Passenger Compartment EquipmentSDR UALA2013040102092Warning Light · false activationBLOWER FAULT DISPLAYED ON UPPER ECAM SCREEN. VENT REMOVED, REPLACED & TESTED BLOWER FAN IAW MM, OPS CHECKED GOOD, ALL INDICATIONS NORMAL.Mar 29, 2013 · N810UA · Airbus A319131 · Air Distribution FanSDR UALA2013032501844Skin · looseNUMEROUS LOOSE FASTENERS ON UNDERSIDE AND SIDES OF AIRCRAFT. RETORQUED AND SECURED NUMEROUS FASTENERS ON FUSELAGE BELLY PANEL 192 AREA.Mar 23, 2013 · N810UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2013030501300Gauge · out of positionL1 DOOR SLIDE PRESSURE GAUGE DIFFICULT TO VIEW. ADJUSTED GAUGE VIEW AND PRESSURE GOOD.Mar 3, 2013 · N810UA · Airbus A319131 · Emergency EquipmentSDR UALA2013011600264Knob · unknownCAPT SLIDING WINDOW NEEDS PART. REPLACED WINDOW KNOB 076 760.Jan 13, 2013 · N810UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2012041502263Battery Pack · dischargedPER GATE MECHANIC, EMERGENCY LIGHT TEST FAILS. REPLACED EMERGENCY LIGHT BATTERY PACK AT DOOR 1L, OPS NORMAL.Apr 15, 2012 · N810UA · Airbus A319131 · Emergency LightingSDR UALA2012041302247Structure · unsecureLOOSE TRIM IN FORWARD GALLEY CAUSING TRIPPING. TRIMMED LOOSE MATERIAL & APPLIED TAPE TO PREVENT FURTHER DAMAGE OR TRIPPING.Apr 12, 2012 · N810UA · Airbus A319131 · Buffet/GalleysSDR UALA2012032601921Floor Panel · delaminatedFWD GALLEY FLOOR HAS SOFT SPOT THAT FLEXES. FLOOR DELAMINATION MEASURES 10 INCHES BY 10 GALLEY FLOOR PANEL 222EF. TEMPORARY REPAIRED PER SRM.Mar 24, 2012 · N810UA · Airbus A319131 · Fuselage Floor PanelSDR UALA2012031901789Valve · faultyABORTED TAKEOFF ABOVE 80 KTS BELOW 110. MAX BRAKE TEMP 290 RT OUTBOARD. INSPECT WHEELS & BRAKES FOR DEFECTS RELATED TO MAX BRAKING, OVERHEAT. USE CAUTION APPROACHING LANDING GEAR AREA. ACCMP'D INSPECTION OF LANDING GEAR WHEELS, ALL FUSE PLUGS INTACT.Mar 18, 2012 · N810UA · Airbus A319131 · Airfoil Anti/De-ice SystemSDR UALA2012031901777Slat · dentedLEFT SLAT NR 2 HAS A DENT 18" FROM INBD EDGE 3" X 4 X .25" DEEP. SAMC TEXT: EDGE OF DENT IS 1.25" FROM NEAREST RIVET ROW AND IS IN AREA 3. REQUIRES TEMP FILLER REPAIR PER SRM AND APPLICATION OF SPEED TAPE PER SRM. ACP INTERIM REPAIR SRM. REQUIRES DAILY REMar 16, 2012 · N810UA · Airbus A319131 · Leading Edge DevicesSDR UALA2012012400499Pylon · gougedNR 1 ENG INBOARD PYLON HAS GAUGES FROM FLEXIBLE SEAL CONTACTING IT. SAMC TEXT: GOUGES ARE .031 MAX DEPTH & 2 3-4 INCH IN LENGTH. INSPECTED AREA: NO CRACKS. HAND BLENDED, REPAIR TO BE DETERMINED BY AIRBUS AT CONCLUSION OF FLT 498. CONTACT SFOLE FOR REPAIR Jan 24, 2012 · N810UA · Airbus A319131 · Nacelle/Pylon Miscellaneous Structure
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