IAE V2527-A5

Service difficulty reports · 8,011

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 = 'V2527A5'
  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 2006UALA01603Power Supply · failedTHE 1L EPSU FAILS TEST. REPLACED 1L EPSU AND BATT.Aug 16, 2006 · N440UA · Airbus A320232 · Emergency LightingSDR 2006UALA01594Cap · damagedAFT PIT THRESHOLD TORQUE BOX UPPER CAP DAMAGED AT AFT END IB CORNER. MAJOR REPAIR. REPLACED THRESHOLD COVER AND INSPECTED.Aug 15, 2006 · N463UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2006UALA01574Engine · flamed outNR 1 ENGINE FLAMED OUT. CREW WAS ABLE TO RELIGHT AND TURNBACK. ENGINES RUNNING NORMAL.Aug 11, 2006 · N403UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2006UALA01562Unknown · malfunctionedFLT ABORTED TAKEOFF AT APPROX 140 KNOTS DUE TO SUDDEN RIGHT TURN. INITIATED HIGH SPEED ABORT. REPLACED NR 3 BRAKE DUE TO E XCESSIVE DRAGGING. REPLACED ALL MAIN LANDING GEAR TIRES DUE TO OVERHEAT, PERFORMED TSM TASK, NO ADDITIONAL FAULTS NOTED.Aug 10, 2006 · N440UA · Airbus A320232 · Landing Gear SystemSDR 2006UALA01552Battery · faultyWHILE PERFORMING EMERGENCY SYSTEM TEST FOR SLIDE CHANGE BY-BACK, MESSAGE (BATTERY AFT LEFT ATA 33-51-48) CAME INTO VIEW ON CIDS PANEL. REPLACED EPSU BATTERY 13WL AFT LEFT. OPS CHECKS NORMAL.Aug 9, 2006 · N423UA · Airbus A320232 · Emergency LightingSDR 2006UALA01553Connector · looseEMERGENCY LIGHTS SYS FAILED TEST IND EPSU 115 VAC FWD L. RESEATED CONNECTOR AT 1L POWER SUPPLY PASSED TEST.Aug 8, 2006 · N442UA · Airbus A320232 · Light System WiringSDR 2006UALA01523Connector · unsecureSYSTEM FAILED 3 SERVICE EMERGENCY CHECK. FAULT SHOWS COMM FWD L, EMER L, COMM AFT L. TRIED RESETTING SYSTEM, NO HELP.Aug 7, 2006 · N419UA · Airbus A320232 · Light System WiringSDR 2006UALA01539Warning System · activatedON TAXI OUT AIR ENG 1 BLEED FAULT UPPER ECAM. UPON RETURN TO GATE, ACCOMPLISHED FWC RESET, BLEED MESSAGE NO LONGER PRESENT. ACCOMPLISHED ENGINE RUN CONFIDENCE CHECK, NO BLEED MESSAGE PRESENT.Aug 7, 2006 · N435UA · Airbus A320232 · Pneumatic Indicating SystemSDR 2006UALA01541A/C Pack · overheatedPACK 2 OVERHEAT ON TAXI OUT. PACK OUTLET TEMP CONTINUED TO CLIMB AFTER PACK WAS SELECTED OFF. PERFORMED TROUBLESHOOTING AND FOUND FLOW CONTROL VALVE BAD. REPLACED FLOW CONTROL VALVE. OPS CHECK AND LEAK CHECK GOOD.Aug 7, 2006 · N432UA · Airbus A320232 · Cabin Cooling SystemSDR 2006UALA01542Light · odorHOT ELEC SMELL AT DOOR 1L. ENTRY LIGHT WARM. TURNED OFF LIGHT AND SMELL GONE. DROPPED LIGHT PANEL AND INSPECTED AREA NO SMELL NOTED, ALSO BALLEST NOT HOT.Aug 7, 2006 · N417UA · Airbus A320232 · Passenger Compartment LightingSDR 2006UALA01543Control Unit · malfunctionedON SHORT FINAL GEAR DOWN AND LOCKED BUT -LG DOORS NOT CLOSED- ECAM AND THEN LGCIU 1 AND 2 FAIL MESSAGES. REPLACED LGCIU 1.Aug 7, 2006 · N410UA · Airbus A320232 · Landing Gear Door Retract SectionSDR 2006UALA01521Engine · fireON SHUTDOWN NR 1 ENG HAD A TAILPIPE FIRE AROUND THE INNER TURBINE EXHAUST AREA.Aug 6, 2006 · N409UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2006UALA01520Hydraulic System · leakingLOST GREEN HYDRAULIC SYSTEM ON GEAR EXTENSION. REQUIRED A TOW TO THE GATE.Aug 4, 2006 · N454UA · Airbus A320232 · Hydraulic System, MainSDR 2006UALA01503Skin · puncturedA L-SHAPED PUNCTURE IN FUSELAGE, 22 IN AFT OF AFT LEFT ENTRY DOOR FRAME AT FLOOR LEVEL, BETWEEN STATION FR70 AND FR72. PUNCTURE MEASURES 6 IN LONG BY 1.5 IN HIGH WITH A .75 IN CRACK EXTENDING OUT OF IT TO THE RIVET LOCATED JUST BELOW IT. INSTALLED PERMENANTAug 2, 2006 · N452UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2006UALA01507Plate · corrodedR2 DOOR SILL PLATE HAS CORROSION AT FASTENER HOLE AT FRAME 66. INSTALLED DOUBLER REPAIR.Aug 2, 2006 · N452UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2006UALA01480Battery · failedAIRCRAFT EMERGENCY LIGHTS FAILED 3 SVC TEST. EPSU BATTERY AFT LEFT. REPLACED 13WL AND IT'S BATTERY. OPS CHECK OK.Jul 31, 2006 · N445UA · Airbus A320232 · Emergency LightingSDR 2006UALA01491Battery · failedEMERGENCY LIGHTS FAIL TEST EPSU FWD L. SUPPLEMENTAL DATA UPDATE REPLACED EPSU BATTERY.Jul 29, 2006 · N458UA · Airbus A320232 · Emergency LightingSDR 2006UALA01479Fastener · installedLEFT EXT FUSELAGE SKIN HAS 1 EA TEMP RIVET INSTALLED AT STA 503 AT STR 36L. TEMP RIVET REMOVED, HOLE ROTARY PROBE INSPECTED. STR 36L REPAIRED, AND SKIN HAS BUSH REPAIR.Jul 28, 2006 · N492UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2006UALA01481Battery Pack · failedEMERGENCY LIGHT TEST FAILS WITH EPSU AFT L MESSAGE ANNUNCIATED. REPLACED THE AFT LEFT EPSU AND BATTERY PACK. CHECKS OK ON TEST.Jul 28, 2006 · N481UA · Airbus A320232 · Emergency LightingSDR 2006UALA01467Epsu · faultyFOUND EPSU COMM FWD LEFT MESSAGE ON PTP PANEL, FOUND ON 3 SVC. REPLACED EPSU AND BATTERY.Jul 27, 2006 · N454UA · Airbus A320232 · Emergency LightingSDR 2006UALA01468Battery · faultyFOUND 1L EMERGENCY LIGHT BATTERY FAULT. REPLACED BATTERY, SYSTEM TESTS OK.Jul 26, 2006 · N406UA · Airbus A320232 · Emergency LightingSDR AWXA200601306Stator · surgesAT 900' AGL, NR 1 ENG "BANG" ACCOMPANIED BY ECAM "COMPRESSOR" & "ENG STALL" WITHIN 5 SECS. SHUT DOWN NR 1 ENG IAW FCOM & DECLARED EMERG. A/C RETURNED. MX EXAMINED INLET, EXHAUST, BLEED VALVES & FOUND NO DAMAGE. BORESCOPE OF HIGH PRESS COMPRESSURE 3 & 6 PERJul 25, 2006 · N667AW · Airbus A320232 · Turbine Engine Compressor SectionSDR 2006UALA01469Battery · dischargedFOUND EMERGENCY SYSTEM CHECK FAILED TEST, BATT COMM LEFT. REPLACED BATTERY ON EPSU 11WL. TEST NORMAL.Jul 25, 2006 · N424UA · Airbus A320232 · Emergency LightingSDR 2006UALA01451Battery · faultyFOUND FWD LEFT EPSU BATTERY IS FAULTING ON EMERGENCY LIGHT TEST ON THE PTP PANEL. REPLACED BATTERY.Jul 23, 2006 · N460UA · Airbus A320232 · Emergency LightingSDR 2006UALA01452Epsu · failedL FWD EPSU FAILED ON EMERGENCY LIGHT TEST. REPLACED EPSU AND BATTERY.Jul 23, 2006 · N463UA · Airbus A320232 · Emergency LightingSDR 2006UALA01458Battery Pack · dischargedFOUND EMERGENCY LIGHTS TEST FAILED. FAULTING EPSU BATTERY FWD LEFT. REPLACED BATTERY PACK AT FWD LEFT POSITION. TEST PASSED.Jul 23, 2006 · N466UA · Airbus A320232 · Emergency LightingSDR 2006UALA01443A/C Pack · failedDIVERTED FLIGHT DUE TO FAILURE OF BOTH PACKS.Jul 22, 2006 · N435UA · Airbus A320232 · Cabin Cooling SystemSDR 2006UALA01449Connector · faultyFOUND CABIN EMERGENCY LIGHT FAILED, EPSU COMM AFT LEFT. RESEATED THE AFT EMERGENCY LIGHT BATTERY PACK CONNECTOR. ACCOMPLISHED EMERGENCY LIGHT SYSTEM TEST ON CIDS PANEL. TEST PASSED, NO FAULT MESSAGES SHOWN.Jul 22, 2006 · N449UA · Airbus A320232 · Light System WiringSDR 2006UALA01450Light · inoperativeEMERGENCY LIGHTS FAIL 3SVC CHECK AFT LOAD. FOUND RIGHT AFT SLIDE LIGHTS BAD. REPLACED DOOR 2R SLIDE. TEST PASSED.Jul 22, 2006 · N433UA · Airbus A320232 · Emergency LightingSDR 2006UALA01457Battery · dischargedFOUND CABIN EMERGENCY LIGHTS TEST FAILED PER NR 3 CHECK FORM. REPLACED BATTERY PACK AT 10WL.Jul 22, 2006 · N433UA · Airbus A320232 · Emergency LightingSDR 2006UALA01442A/C Pack · malfunctionedEMERGENCY DECLARED DUE TO CABIN DEPRESSURIZATION. REPLACED RT PACK FLOW CONTROL VALVE. OPS CHECKED OK. REPLACED APU COMPRESSOR DISCHARGE SENSOR [4951546], AND SPEED SENSOR [4950009]. OPS CHECKED GOOD. RAN BOTH PACKS AND MOTORED ENGINE, HAD GOOD DUCT PRESSJul 21, 2006 · N433UA · Airbus A320232 · Cabin Cooling SystemSDR 2006UALA01439Antenna · inoperativeWEATHER RADAR SYSTEM INOPERATIVE. RTFL. REPLACED ANTENNA, SYSTEM TESTED GOOD ON GROUND.Jul 20, 2006 · N415UA · Airbus A320232 · Weather Radar SystemSDR 2006UALA01427Power Supply · faultyEMERGENCY LIGHT TEST FAIL, EPSU INT LOAD FWD L. TEST OF EPSU SHOWS INT LOAD.Jul 19, 2006 · N471UA · Airbus A320232 · Emergency LightingSDR 2006UALA01414Battery · failedAFT L EMERGENCY BATTERY FAILED EMERGENCY TEST.Jul 17, 2006 · N405UA · Airbus A320232 · Emergency LightingSDR 2006UALA01415Power Supply · faultyRIGHT OVERWING EMERGENCY EXIT LIGHT STAYS ILLUMINATED.Jul 17, 2006 · N454UA · Airbus A320232 · Emergency LightingSDR 2006UALA01398Battery Pack · failedEMERGENCY LIGHT TEST FAILS WITH MSG EPSU COMM AFT L.Jul 16, 2006 · N439UA · Airbus A320232 · Emergency LightingSDR 2006UALA01428Odor · detectedAFTER TAKEOFF HAD MULTIPLE REPETITIVE ECAMS AND CHIMES. FIRST CLASS PASS AND FWD FLT ATTENDANT REPORTED A STRONG RUBBER SMELL IN FIRST CLASS CABIN. CHECKED NOSE LANDING GEAR, MAIN LANDING GEAR AREAS & PROX. SWITCHES NO DEFECTS NOTED. ACCOMPLISHED SDAC 1 & 2Jul 15, 2006 · N480UA · Airbus A320232 · Air Distribution SystemSDR 2006UALA01385Skin · damagedEXTERNAL FUSELAGE BETWEEN FR 63 AND FR 64, STR 7R-8R IS DAMAGED. ACCOMPLISHED DOUBLER REPAIR.Jul 13, 2006 · N490UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2006UALA01396Power Supply · failedMID CABIN L EPSU FAILS EEL SYSTEM TEST.Jul 13, 2006 · N442UA · Airbus A320232 · Emergency LightingSDR 2006UALA01369Beam · corrodedR2 DOOR SILL BEAM HAS CORROSION ON UPPER SURFACE AT FRAME 66. DOOR SILL BEAM REPAIRED PER SRM 53-41-14 FIG 201.Jul 11, 2006 · N462UA · Airbus A320232 · Fuselage Main, StructureSDR 2006UALA01370Warning Light · illuminatedRETURNED TO FIELD DUE TO FWD CARGO DOOR INDICATION.Jul 11, 2006 · N421UA · Airbus A320232 · Door Warning SystemSDR 2006UALA01371Compressor · stalledRETURNED TO FIELD DUE TO NR 1 ENG COMPRESSOR STALL.Jul 11, 2006 · N479UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2006UALA01372Wire · brokenEMERGENCY LIGHT AT 15C HAS WIRE BROKEN AT CONNECTOR.Jul 11, 2006 · N444UA · Airbus A320232 · Light System WiringSDR 2006UALA01381Compressor · stalledNR 1 ENG COMPRESSOR STALL AT 7500 FT. FLAME SEEN AT FRONT AND BACK OF ENGINE FROM THE CABIN.Jul 11, 2006 · N447UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2006UALA01362Slide · dislodgedDOOR 1R SLIDE FELL OUT OF DOOR.Jul 10, 2006 · N463UA · Airbus A320232 · Escape SlideSDR 2006UALA01355Structure · vibrationFLIGHT REPORTED A VIBRATION ON CLIMBOUT IN THE COCKPIT & A STRONGER VIBRATION IN THE TAIL & AFT GALLEY. ACCOMPLISHED AMM5-50-00. VIBRATION DECICION TREE SUGGESTS TYPE 1 ELEVATOR AS MOST PROBABLE CAUSE. MAINTENACE TIP 53-005 ALSO ACCOMPLISHED. AM27-34-00-20Jul 9, 2006 · N402UA · Airbus A320232 · Aircraft StructuresSDR 2006UALA01540Control Panel · inoperativeTAKEOFF CONFIG WILL NOT TEST. CYCLED CBS F1 AND Q7 AND SYSTEM RETURNED AND T/O CONFIG CHECKED OK. RE-CYCLED CB AND T/O CONFIG AGAIN WOULD NOT RESPOND. REPLACED FAULTY ECAM CONROL PANEL.Jul 8, 2006 · N461UA · Airbus A320232 · Central WarningSDR 2006UALA01347Power Supply · failedFOUND EMERGENCY LIGHT TEST FAILED. REPLACED LEFT EPSU, TEST PASSED.Jul 7, 2006 · N437UA · Airbus A320232 · Emergency LightingSDR 2006UALA01348Connector · dirtyDURING 3SVC CHK, FOUND EPSU EXT LOAD FAULT ON PTP PANEL WITH OVERWING FAILURE ON LEFT SLIDE. CLEANED AND SECURED CONNECTOR AT TOP PART OF SLIDE TO BOTTOM PART OF SLIDE. OPS TESTED EMERGENCY LIGHT SYSTEM. TEST OK .Jul 6, 2006 · N442UA · Airbus A320232 · Light System WiringSDR 2006UALA01320Power Supply · failed11WL EPSU FAILED OPS CK. REPLACED EPSU 11WL. OPS CHECKED OK.Jul 5, 2006 · N449UA · Airbus A320232 · Emergency Lighting
Back to IAE V2527-A5