IAE V2522-A5

Service difficulty reports · 3,465

Newest first. General aviation reporting is voluntary.

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 engine_model_key = 'V2522A5'
  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 2001UALA01934Hydraulic System · failedLANDED UNDER AMBER ALERT DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM.Sep 3, 2001 · N816UA · Airbus A319131 · Hydraulic System, MainSDR 2001UALA01929Line · crackedUNSCHEDULED LANDING DUE TO A FUEL LEAK. NR 1 ENGINE SHUTDOWN. *S/D* AFTER IN FLIGHT SHUTDOWN, THE FUEL TUBE WAS FOUND BROKEN. MAJOR CONTRIBUTOR FOR TUBE FAILURE CONSIDERED TO BE IMPROPER CLAMP CONFIGURATION. CLAMP WAS FOUND TO BE APPROXIMATELY 2 SIZES TOSep 2, 2001 · N821UA · Airbus A319131 · Engine Fuel DistributionSDR 2001UALA01995Skin · damagedFUSELAGE SKIN DAMAGED FWD OF APU COMPARTMENT AFT OF FRAME 76, STRINGER 30. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.Sep 1, 2001 · N843UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR 2001UALA01672Blower · defectiveUNUSUAL SMELL IN THE COCKPIT. REPLACED AVIONICS BLOWER FAN. NO FURTHER DISCREPANCIES REPORTED.Aug 11, 2001 · N809UA · Airbus A319131 · Air Distribution FanSDR 2001UALA01659Warning System · activatedFORWARD CABIN DOOR PRESSURE FAULT DISPLAYED ON UPPER ELECTRONIC CENTRALIZED AIRCRAFT MONITORING SCREEN.Aug 8, 2001 · N841UA · Airbus A319131 · Door Warning SystemSDR 2001UALA01416Blower · failedAVIONICS VENT FAULT AND A SUBSEQUENT AVIONICS EXTRACT FAULT. *S/D* REPLACED AVIONICS BLOWER FAN AND SYSTEM FILTER, NO OTHER DAMAGE NOTED. NO FURTHER FAULTS.Jul 18, 2001 · N827UA · Airbus A319131 · Air Distribution FanSDR 2001UALA00670Skin · dentedLT FUSELAGE SKIN DENT BETWEEN FRAME 23 AND FRAME 24 AND BETWEEN STRINGER 22LT AND STRINGER 23LT. REPAIRED FUSELAGE SKIN DENT.May 9, 2001 · N819UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR 2001UALA00623Outflow Valve · failedAIRCRAFT DIVERTED TO CLE DUE TO LOSS OF CABIN PRESSURE. *S/D* CFDS FAULTED OUTFLOW VALVE, REPLACED SAME AND BOTH CABIN PRESSURE CONTROLLERS PRECAUTIONARY, NO FURTHER DEFECTS REPORTED.May 2, 2001 · N807UA · Airbus A319131 · Pressure Regulator/Outflow ValveSDR 2001UALA00299Skin · damagedLOWER SKIN OF THE RIGHT HAND HORIZONTAL STABILIZER DAMAGED APPROXIMATELY 1.5 FEET FROM THE OUTBOARD TIP. SUPPLEMENTAL DATA UPDATE INSTALLED STRINGER REPAIR AND SKIN DOUBLER. MAJOR REPAIR ACCOMPLISHED.Mar 22, 2001 · N830UA · Airbus A319131 · Horizontal Stabilizer, Plate/SkinSDR 2001UALA00175Thermostat · failedNR 2 ENGINE BLEED AIR LOW TEMPERATURE INDICATION. SUPPLEMENTAL DATA UPDATE REPLACED FAN AIR VALVE THERMOSTAT. NO FURTHER DISCREPANCIES NOTED SINCE THERMOSTAT REPLACEMENT.Mar 4, 2001 · N805UA · Airbus A319131 · Pneumatic Indicating SystemSDR 2001UALA00173Duct · damagedUNABLE TO PRESSURIZE AFTER TAKEOFF. *S/D* FOUND AVIONICS COOLING SYSTEM EXTRACT DUCT DAMAGED. REPLACED DUCT. NO FURTHER PRESSURIZATION PROBLEMS REPORTED.Mar 2, 2001 · N821UA · Airbus A319131 · Air Distribution SystemSDR 2001UALA00149Wire · damagedEMERGENCY EXIT LIGHTS NOT WORKING IN ROWS 1, 2, 5, AND 6. REPLACED THE POWER SUPPLY AND REPAIRED EMERGENCY LIGHT WIRES IN ROW 1. OPS CHECKED NORMAL.Feb 26, 2001 · N821UA · Airbus A319131 · Light System WiringSDR 2001UALA00148Warning Light · illuminatedDOOR 1R PRESSURE LIGHT ILLUMINATED. *S/D* CHECKED THE GIRT BAR FOR DEBRIS, CYCLED THE DOOR CLOSED, AND ARMED AND DISARMED THE DOOR. ALL OPERATED NORMALLY.Feb 26, 2001 · N814UA · Airbus A319131 · Door Warning SystemSDR 2000UALA00824Slide · leakingLEFT HAND OFF WING SLIDE FAILED AIR RETENTION CHECK IN THE SHOP. HOLE WAS CUT BY ASPIRATOR DURING PACKING. SENT SLIDE TO VENDOR FOR REPAIR.Dec 29, 2000 · N812UA · Airbus A319131 · Escape SlideSDR 2000UALA00808Smoke · detectedELECTRICAL SMELL IN AFT GALLEY. *S/D* FLIGHT ATTENDANT REPORTED SMOKE ODOR WAS SMELLED FOR APPROXIMATELY TWO MINUTES FOLLOWING TAKEOFF THEN SUBSIDED. MAINTENANCE PULLED CEILING PANELS DOWN AND EXAMINED GENERATOR POWER LINES, NO FAULTS OR DAMAGE FOUND. AIRCDec 23, 2000 · N820UA · Airbus A319131 · Air Conditioning SystemSDR 2000UALA00809Sensor · failedON APPROACH FOR LANDING, GOT AN ECAM GEAR NOT DOWN LOCKED MESSAGE. RECYCLED GEAR HANDLE, AND GEAR INDICATED DOWN AND LOCKED. *S/D* POST FLIGHT REPORT INDICATES NLG DOOR PROXIMITY SENSOR 39GA FAULTED DURING THE GEAR EXTENSION SEQUENCE. THIS SENSOR WAS REPLADec 23, 2000 · N820UA · Airbus A319131 · Landing Gear Position and WarningSDR 2000UALA00811Computer · failedCAPTAIN LOST INDICATIONS FROM FMGC. IN ADDITION, RECEIVED GPWS INOP ECAM WARNING, FOLLOWED BY NAV MODE DEGRADE ON BOTH ND''S. *S/D* THE FLIGHT MANAGEMENT GUIDANCE COMPUTER 1 AND THE GEAR PROX SENSOR 39GA WERE REPLACED.Dec 23, 2000 · N820UA · Airbus A319131 · Flight Management Computing Hardware SystemSDR 2000UALA00799Computer · failedDIVERTED DUE TO AN AVIONICS SMOKE WARNING. *S/D* REPLACED AVONICS EXTRACT FAN. PERFORMED AVIONICS EQUIPMENT VENTILATION COMPUTER (AEVC) CHECK IN THE CENTRAL FAULT DISPLAY SYSTEM AND SYSTEM CHECKED OK. ALSO REPLACED AEVC COMPUTER. (PRECAUTIONARY)Dec 21, 2000 · N821UA · Airbus A319131 · Air Distribution FanSDR 20010111CW004Engine · damagedDURNING DESCENT OF FLT, ENG NR2 EXPER STALL,ON ECAM,MSG OF NR2 OIL FLTR CLOG. MAIN TECH INSPD ENG MSTR CHIP DECTRS, FOUND STRONG METAL CONTAMINATION. ENGINE NR2 WAS REPLACED. NO DISCREP DETECTED. AC RETRN TO NORMAL OPERATION.Dec 16, 2000 · N474TA · Airbus A319132 · Engine (Turbine/Turboprop)SDR 2000UALA00695Transmitter · defectiveNUMBER 1 OIL QUANTITY INDICATOR INOP. SUPPLEMENTAL DATA UPDATE FOUND LOOSE PIN ON OIL QUANTITY TRANSMITTER CONNECTOR. TRANSMITTER WAS ALSO REPLACED.Nov 17, 2000 · N828UA · Airbus A319131 · Engine Oil QuantitySDR 2000UALA00659Wire · damagedHYDRAULIC INDICATION PROBLEM. *S/D* FOUND OPEN WIRE TO LOW PRESSURE SWITCH 1074GK. REPAIRED AS REQUIRED.Nov 5, 2000 · N815UA · Airbus A319131 · Hydraulic Power System WiringSDR 2000UALA00569Light · inoperativeEMERGENCY EGRESS LIGHT OUT AT SEAT 12A, B AND C. REPLACED EMERGENCY EGRESS LIGHT AT SEAT 12A, B AND C. OPERATIONAL CHECK OK.Sep 29, 2000 · N804UA · Airbus A319131 · Emergency LightingSDR 2000UALA00562Wire · failedBLUE SYSTEM HYDRAULIC LOW PRESSURE ELECTRIC CENTRALIZED AIRCRAFT MONITORING MESSAGE. *S/D* FINAL FIX WAS A RETERMINATION OF THE WIRES CONNECTING TO THE PUMP PUSHBUTTON SWITCH IN THE COCKPIT. ALL OTHER WIRING CHECKS WERE COMPLETED WITHOUT FINDINGS.Sep 21, 2000 · N826UA · Airbus A319131 · Hydraulic Power System WiringSDR 2000UALA00573Pin · missingTHREE MISSING INNER PINS IN 3 LOCATIONS ON THE AFT ENGINE MOUNT ASSEMBLY. *S/D* ROOT CAUSE HAS BEEN DETERMINED TO BE IMPROPER INSTALLATION DURING INSTALLATION OF MOUNTS ON THE SPARE ENGINE. THIS ERROR WAS NOT FOUND ON ANY OF 12 OTHER ENGINES SIMILARLY PROCUSep 21, 2000 · N821UA · Airbus A319131 · Engine Mount SectionSDR 2000UALA00561Power Supply · inoperativeEMERGENCY LIGHT POWER SUPPLY IS INOPERABLE AT RIGHT EMERGENCY EXIT ROW. REPLACED EMERGENCY LIGHT POWER UNIT. OPERATIONAL CHECK OK.Sep 20, 2000 · N829UA · Airbus A319131 · Emergency LightingSDR 2000UALA00546Valve · leakingPOSSIBLE FUEL LEAK IN THE RIGHT WING. *S/D* RIGHT HAND AIR VENT VALVE WAS CHANGED.Sep 11, 2000 · N813UA · Airbus A319131 · Fuel StorageSDR 2000UALA00455Thermostat · inoperativeNR 2 ENGINE BLEED FAULT. *S/D* NR 2 ENGINE FAN AIR THERMOSTAT WAS REPLACED. BLEED SYSTEM CHECKED GOOD.Jul 31, 2000 · N810UA · Airbus A319131 · Engine Bleed Air SystemSDR 2000UALA00421Cover · looseRIGHT HAND EMERGENCY OVERWING EXIT ELECTRONIC CENTRALIZED AIRCRAFT MONITORING DOOR PAGE INOPERATIVE AND LIGHT ABOVE EXIT DOOR IS FLASHING. *S/D* THE EMERGENCY HATCH HANDLE COVER WAS SECURED AND THE SYSTEM OPERATED OK.Jul 14, 2000 · N821UA · Airbus A319131 · Emergency ExitsSDR 2000UALA00393Slide · deployedDOOR NR 2 RIGHT INADVERTENT SLIDE DEPLOYMENT. *S/D* THE SLIDE DEPLOYED NORMALLY. SLIDE WAS REPLACED PRIOR TO RETURNING AIRCRAFT TO SERVICE.Jul 13, 2000 · N829UA · Airbus A319131 · Escape SlideSDR 2000UALA00407Unknown · odorOIL SMELL AND HAZE IN CABIN. OPERATED PACKS WITH APU, NO ODOR. CHECKED APU FOR LEAKS AND ODORS, CHECKED INTERIOR LIGHTS, RELAMPED INOP LIGHTS TO ENSURE NO BALLAST WERE BAD. CHECKED HISTORY, NONE FOUND. OPERATED PACKS FOR 3 HOURS, NO SMELLS.Jul 8, 2000 · N812UA · Airbus A319131 · Air Distribution SystemSDR 2000UALA00350Engine · contaminatedDURING CLIMB THE CREW EXPERIENCED A BURNING ODOR IN THE COCKPIT. *S/D* REPLACED NUMBER ONE ENGINE PER MM 71-00-20 ON ACCOUNT OF OIL BEING FOUND AT HIGH PRESSURE COMPRESSOR STAGES 3 & 4. ACCOMPLISHED TEST NR 13. OPERATIONAL CHECK NORMAL.Jun 22, 2000 · N812UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR 2000UALA00312Pressure Switch · leakingGREEN HYDRAULIC SYSTEM LOSS IN CRUISE. QUANTITY AND PRESSURE READING ZERO. *S/D* CHECKED NR 1 ENGINE FOR EXTERNAL HYDRAULIC LEAKS. FOUND LOW PRESSURE SWITCH LOOSE AND LEAKING. REPLACED SHREDDED O RING AND INSTALLED SWITCH WITH PROPER TORQUE. SERVICED GREJun 5, 2000 · N821UA · Airbus A319131 · Hydraulic Pressure Regulator, MainSDR 2000UALA00306Acm · odorSEVERAL PASSENGERS MOMENTARILY SMELLED SULPHER. *S/D* REMOVED AND REPLACED NR 2 AIR CYCLE MACHINE. LEAK AND OPERATIONAL CHECK OK.Jun 4, 2000 · N807UA · Airbus A319131 · Cabin Cooling SystemSDR 2000UALA00294Fillet · looseRETURNED TO SFO AFTER NR 1 ENG COWL FILLET AT TOP PYLON TO COWL SECTION CAME LOOSE.May 31, 2000 · N818UA · Airbus A319131 · Nacelle/Pylon, Plate/SkinSDR 2000UALA00277Gcu · failedAPPROX 15 MINS AFTER TAKEOFF, AC LOST NR 2 ELECTRICAL GENERATOR. APU WAS INEFFECTIVE IN POWERING ESSENTIAL SYSTEMS ON THE PLANE, SO CAPT ELECTED TO RETURN TO DEN FOR REPAIRS. *S/D* REPLACED GENERATOR LINE CONTACTOR NR 2 (GLC2) AND NR 2 GENERATOR CONTROL UNIMay 21, 2000 · N805UA · Airbus A319131 · AC Generation SystemSDR 2000UALA00265Coupling · leakingDIVERTING WITH LOSS OF YELLOW SYSTEM. *S/D* FOUND DAMAGED O-RING AT POWER TRANSFER UNIT QUICK DISCONNECT FITTING. REPLACED O-RING, SERVICED SYSTEM AND LEAK CKD. NO FURTHER LEAKS NOTED.May 17, 2000 · N805UA · Airbus A319131 · Hydraulic System, MainSDR 2000UALA00245Probe · failedBOTH AUTOPILOTS AND AUTO THROTTLE FAILED DURING CLIMB. FLIGHT DIVERTED TO DEN. *S/D* TOTAL AIR TEMPERATURE (TAT) PROBE FIN NR 11FP1 WAS REPLACED. OPERATIONAL TEST AND AUTOLAND TEST PASSED SATISFACTORILY.May 11, 2000 · N806UA · Airbus A319131 · Auto Flight SystemSDR 2000UALA00162Control Box · failedCREW REPORTS NOSE STEERING DISCONNECT MESSAGE COMES AND GOES. WHEN MESSAGE APPEARS UNABLE TO STEER ACFT. NECESSARY TO CHECK AND CORRECT. *S/D* REPLACED NOSE WHEEL STEERING ELECTRICAL BOX.Mar 30, 2000 · N828UA · Airbus A319131 · Steering UnitSDR 2000UALA00083Blade · separatedDIVERSION TO STL DUE TO N2 COMPRESSOR STALL AT FL350. AFTER PATCH WITH SAMC ALL AGREED TO NR 2 ENGINE SHUT DOWN AND STL DIVERT. AN AMBER ALERT WAS DECLARED AND EMERGENCY EQUIPMENT WAS REQESTED BY DISPATCH THROUGH STL TRACON. *S/D* A HPC 4TH STAGE BLADE FAIFeb 21, 2000 · N803UA · Airbus A319131 · Turbine Engine Compressor SectionSDR 2000UALA00075Battery · inoperativeAFTER PERFORMING EMERGENCY LIGHT TEST 3 SVC GOT EPSU INT LOAD AFT L NARRATIVE. *S/D* REPLACED EPSU 13WL PER MM 31-51-38 AND BATTERY. TEST PASSED AND ALL LIGHTS OPS CHECKED GOOD.Feb 17, 2000 · N806UA · Airbus A319131 · Emergency LightingSDR 2000UALA00006Downlock Sensor · failedON APPROACH TO ATL, FLT EXPERIENCED UNSAFE NOSE LANDING GEAR INDICATION. FLT DECLARED AMBER ALERT WITH ATL TOWER AND REQUESTED EQUIPMENT AND LONG RUNWAY. *S/D* A SUCCESSFUL LANDING WAS ACCOMPLISHED BY MANUAL LANDING GEAR EXTENSION. THE POST FLIGHT REPORT FJan 5, 2000 · N806UA · Airbus A319131 · Landing Gear Position and WarningSDR 99UAL900644Cone · crackedNR 2 ENG HAS INLET CONE FAIRING CRACKED AROUND BOLT HOLE. *S/D* THE CAUSE OF THE INLET CONE CRACKING IS VIBRATION OF THE INLET CONE FAIRING AGAINST THE INLET CONE SEATING. THE MANUFACTURER ISSUED SERVICE BULLETIN V2500-ENG-72-0318 WHICH MODIFIED THE FAIRINGDec 10, 1999 · N818UA · Airbus A319131 · Turbine Engine Compressor SectionSDR 99UAL900636Blade · failedLOST NR 2 ENGINE ON CLIMBOUT PASSING 17,000 FT. LOUD BANG AND HIGH EGT. SHUTDOWN ENGINE. *S/D* STAGE 4 BLADE FAILED IN FATIGUE IN ROOT ATTACHMENT AREA, LIBERATING AIRFOIL AND PLATFORM AND CAUSING EXTENSIVE DOWNSTREAM DAMAGE. THE MANUFACTURER HAS ISOLATED Dec 6, 1999 · N812UA · Airbus A319131 · Turbine Engine Compressor SectionSDR AWXA9900379Engine · damagedAIR TURNBACK, AFTER TAKEOFF 5 MIN & 6000 RT ENG CLASS 1 EGT OVERLIMIT WITH LOUD BANG AND ENG SPOOL DOWN. REPLACED NR 2 ENG IAW R5M71302, 4TH STAGE BLADE DAMAGE.Oct 22, 1999 · N801AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR 99UAL900473Epsu · failedEPSU UNIT FWD L FAILED TEST PER NR 3 SVC. EPSU UNIT WAS THE CAUSE OF THIS MALFUNCTION. THE EPSU WAS REPLACED AND THE SYSTEM TESTED GOOD.Sep 12, 1999 · N810UA · Airbus A319131 · Emergency LightingSDR 99UAL900466Tire · failedON TAKEOFF CREW HEARD A LOUD BANG AND ANOTHER AIRCRAFT OBSERVED DEBRIS DEPARTING AIRCRAFT. SAN AIRPORT RECOVERED TIRE DEBRIS FROM RUNWAY. LEFT NOSE LANDING GEAR TIRE TREAD SEPARATED ON DEPARTURE. FLIGHT DIVERTED TO LAX UNDER AMBER ALERT. *S/D* LT NLG TIRESep 7, 1999 · N828UA · Airbus A319131 · TireSDR 99UAL900465Coupling · looseDIVERTED TO DEN DUE TO LOW HYDRAULIC QUANTITY. *S/D* FOUND A COUPLING LOOSE. RETIGHTENED AND REPLACED AN O-RING ON RETURN LINE.Sep 5, 1999 · N812UA · Airbus A319131 · Hydraulic System, MainSDR 99UAL900459Blade · failedRETURNED TO SFO DUE TO NR 1 ENGINE FAILURE. *S/D* STAGE 4 BLADE FAILED IN FATIGUE IN ROOT ATTACHMENT AREA, LIBERATING AIRFOIL AND PLATFORM AND CAUSING EXTENSIVE DOWNSTREAM DAMAGE. THE MANUFACTURER HAS ISOLATED THE CAUSE TO A VSV SCHEDULE INTRODUCED WITH EECSep 2, 1999 · N818UA · Airbus A319131 · Turbine Engine Compressor SectionSDR 99UAL900447Air Dist · odorFLIGHT EN ROUTE TO YVR, CREW DISCOVERED A HEATED PANEL AFT OF CB PANEL 49VU. *S/D* ACTUAL ODOR WAS NOT CONFIRMED. AS PRECAUTION, LIGHT BALLAST FIN NR 6LF WAS REPLACED AS WELL AS THE RECIRCULATION FAN FILTERS.Aug 25, 1999 · N810UA · Airbus A319131 · Air Distribution SystemSDR 99UAL900446Carbon Seal · leakingAFTER SHUTDOWN NOTICED FIRE IN TAILPIPE OF NR 1 ENGINE. DRY MOTORED ENG 3 TIMES TO EXTINGUISH FIRE. FIRE LASTED APPROX 15 MINS INTERMITTENLY DURING MOTORING. *S/D* FOUND OIL LEAKING PAST NR 5 BEARING CARBON SEAL INTO EXHAUST CASE GASPATH. REPLACED CARBON Aug 24, 1999 · N807UA · Airbus A319131 · Turbine Engine Compressor Section
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