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 2002UALA01464Skin · damagedINTERIM REPAIR INSTALLED BETWEEN FRAME 73 AND FRAME 75. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REPLACED.Sep 17, 2002 · N430UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2002UALA01466Brake Assy · malfunctionedRETURNED TO FIELD UNDER AMBER ALERT DUE TO LEFT BRAKE WOULD NOT COOL. REPLACED NR 1 BRAKE ASSEMBLY. NO PREVIOUS HISTORY OF HIGH TEMPS. NO FURTHER DEFECTS ON SUBSEQUENT FLIGHTS.Sep 17, 2002 · N402UA · Airbus A320232 · BrakeSDR 2002UALA01435Hydraulic Line · rupturedABORTED TAKEOFF DUE TO ECAM HYDRAULIC GREEN RESERVOIR LOW LEVEL WARNING. FOUND RIGHT HAND MLG DOOR RETRACT ACTUATOR AFT FLEX LINE RUPTURED. REPLACED FLEX LINE.Sep 8, 2002 · N429UA · Airbus A320232 · Hydraulic System, MainSDR 2002UALA01389Computer · malfunctionedABORTED TAKEOFF AT 90 KNOTS DUE TO AN AVIONICS VENT MESSAGE. THE AVIONIC EQUIPMENT COOLING COMPUTER WAS RESET AND THE AIRCRAFT FLEW FUTURE FLIGHTS WITH NO INCIDENCE.Aug 30, 2002 · N463UA · Airbus A320232 · Cabin Cooling SystemSDR AWXA200200845Bleed Valve · lack of lubePHX - ABORTED TAKEOFF - FLT 0014 - ON TAKEOFF FROM PHX EN ROUTE FOR JFK THE NR 2 ENGINE EGT EXCEEDED LIMITATIONS, ABORTED TAKEOFF AT APPROXIMATELY 80 KTS. MAINTENANCE DOWNLOADED PREFLIGHT REPORT AND PERFORMED TROUBLESHOOTING TASKS 77-00-00-810-844 INSPECTION Aug 28, 2002 · N660AW · Airbus A319132 · Compressor Bleed ValveSDR 2002UALA01321Socket · defectiveEMERGENCY EXIT LIGHTS FLOOR LIGHT DAMAGED AT 01L. ALL TROUBLESHOOTING PROCEDURES WERE FOLLOWED AND THE LIGHT BASE WAS REPLACED.Aug 18, 2002 · N445UA · Airbus A320232 · Emergency LightingSDR 2002UALA01303Disk · rupturedFLIGHT DIVERTED UNDER AMBER ALERT DUE TO FUEL IMBALANCE. FOUND BURST DISC BETWEEN LEFT INNER AND CENTER FUEL TANKS BROKEN. REPLACED DISC.Aug 13, 2002 · N481UA · Airbus A320232 · Fuel StorageSDR AWXA200200746Pump · failedORD - ABORTED TAKEOFF - FLT 0060 - ON TAKEOFF FROM ORD EN ROUTE FOR PHX RECEIVED ECAM INDICATION FOR NR 2 ENGINE COMPRESSOR VANE FAULT. ABORTED TAKEOFF AT 60 KTS.Aug 12, 2002 · N660AW · Airbus A319132 · Engine Fuel PumpSDR YENA200222Proximity Sensor · defectiveUpon configuration for landing, slats operated normally. Flaps locked at 1. Landed at flap 1 configured slats 3 per FCOMMaintenance removed and replaced interconnecting struct Prox Sensor 39CV IAW MM 27-51-44-400-002 and Ops Tested IAW MM 27-51-00-710-002, OpsAug 11, 2002 · N531JB · Airbus A320232 · Trailing Edge Flap Control SystemSDR 2002UALA01277Smoke · detectedON DESCENT, FLIGHT ATTENDANT RELEASED HALON EXTINGUISHER IN AFT LAV DUE TO LIGHT HAZE/SMOKE AND HEAT. EMERGENCY PROCEDURES WERE PUT INTO EFFECT. SMOKE/HEAT HAD DISSIPATED ON LANDING. RAN ENGINES AND APU. CHECKED AFT FWD LAV FOR SIGNS OF SMOKE, ELECTRICAL SMAug 4, 2002 · N448UA · Airbus A320232 · Air Distribution SystemSDR YENA200221Harness · overheatedFlt#94, OAK to JFK, Multiple faults occurred in flight including RA1, Nose wheel steering, #1 PFD, ND, #1 TLS, GPS, Blue electrical Hyd, #1 RMP, MCDU.Found phase "C" of eng and firewall disconnect plugs overheated. plug 400VC1 firewall plug pin "C" replaced peAug 3, 2002 · N521JB · Airbus A320232 · AC Generation SystemSDR 2002UALA01263Disk · burstRETURN TO FIELD WITH A FUEL IMBALANCE PROBLEM. OVER PRESSURE BURST DISC BETWEEN THE LEFT INNER WING FUEL TANK AND THE CENTER FUEL TANK RUPTURED. FUEL TRANSFERRED FROM THE LEFT WING TO THE CENTER CAUSING AN IMBALANCE BETWEEN THE INNER WING TANKS.Jul 31, 2002 · N479UA · Airbus A320232 · Fuel StorageSDR 2002UALA01207Controller · failedRETURNED TO FIELD. SMOKE ELECTRICAL SMELL IN CONTROL CABIN. CIRCUIT BREAKERS PHC2, AOA2, PITOT2, TAT2, AND PHC3 ALL POPPED. REPLACED NR 2 PHC AND TESTED ALL PROBE HEATERS FOR PROPER OPERATION. SYSTEM OPERATED NORMAL WITH NO ADDITIONAL FAILURES NOTED ON SUBJul 26, 2002 · N447UA · Airbus A320232 · Instrument PanelSDR 2002UALA01203Skin · damagedFUSELAGE SKIN DAMAGED AT FRAME 67 TO FRAME 70 FROM STRINGER 42L TO 42R. MAJOR REPAIR ACCOMPLISHED. INSTALLED TWO DOUBLERS AND FILLERS.Jul 19, 2002 · N467UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2002UALA01190Pump · malfunctionedRETURNED TO FIELD DUE TO OVERHEAT ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE OF GREEN HYDRAULIC PUMP. CHANGED GREEN SYSTEM LOW PRESSURE, HIGH PRESSURE AND CASE DRAIN FILTERS.Jul 18, 2002 · N440UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR 2002UALA01191Valve · leakingLOSS OF YELLOW HYDRAULIC SYSTEM. REPLACED YELLOW SYSTEM PARK BRAKE VALVE 2579GM.Jul 18, 2002 · N464UA · Airbus A320232 · Landing Gear Brake SystemSDR 2002UALA01185Idg · overtempABORTED TAKEOFF AT 80 KNOTS DUE TO LEFT ENGINE IDG FAULT LIGHT. NR 1 ENGINE IDG FAULT LIGHT CAME ON DURING TAKEOFF. NR 1 IDG REMOVED AND REPLACED.Jul 17, 2002 · N416UA · Airbus A320232 · AC Generator-AlternatorSDR YENA200217Engine · malfunctionedFLT 88 ONT TO JFK, DIVERTED TO SLC DUE NR 1 ENGINE AUTO SHUTDOWN IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE PER AMM 71-00-20 AND OPS CHECK OK PER AMM 71-00-00.Jul 11, 2002 · N520JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2002UALA01133Engine · power lossABORTED TAKEOFF AT 90-100 KNOTS DUE TO NR 1 ENGINE NOT PRODUCING ENOUGH THRUST.Jul 5, 2002 · N414UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2002UALA01079Radar · malfunctionedRETURN TO FIELD DUE TO LOSS OF WEATHER RADAR.Jun 25, 2002 · N460UA · Airbus A320232 · Weather Radar SystemSDR 2002UALA01067Rub Strip · debondedDIVERTED UNDER AMBER ALERT DUE TO VIBRATION IN NR 1 ENGINE. ENGINE REPLACED. HPC RUB STRIP DISBONDED CAUSING COMPRESSOR VIBRATION. ENGINE UPGRADED WITH RUB STRIP MODIFICATION.Jun 22, 2002 · N801UA · Airbus A319131 · Turbine Engine Compressor SectionSDR 2002UALA01035Filter · collapsedABORTED TAKEOFF AT 90 KNOTS DUE TO VENT AVIONICS SYSTEM FAULT. THE AEVC SYSTEM FILTER WAS FOUND DIRTY AND COLLAPSED - REPLACED FILTER.Jun 18, 2002 · N433UA · Airbus A320232 · Air Distribution SystemSDR CA020618003Coffeemaker · failed(CAN) 20 MINS.,INTO FLT, CSM ADVISED CAPTAIN THAT STRONG ELECT. SMELL & SMOKE IN AFT GALLEY AREA. FLT CREW ADVISED ATC OF SMOKE IN CABIN & REQ IMMEDIATE RETURN TO VANCOUVER. FLT CREW TURNED GALLEY POWER OFF, AND CSM ADVISED THAT SMOKE HAD CEASED & SMELL HAD DEJun 13, 2002 · Airbus A320232 · Buffet/GalleysSDR 2002UALA00975Light · inoperativeEMERGENCY EXIT LIGHT BETWEEN OVERWING DOORS INOPERATIVE ON TEST.Jun 9, 2002 · N438UA · Airbus A320232 · Emergency LightingSDR 2002UALA00957Battery · faultyAFT LEFT INT LOADS FAULT EMERGENCY LIGHT SYSTEM. REPLACED AFT LEFT EMERGENCY BATTERY. OPS CHECKS GOOD.Jun 6, 2002 · N415UA · Airbus A320232 · Emergency LightingSDR 2002UALA00945Blade · fracturedRETURNED TO FIELD DUE TO NR 1 ENGINE COMPRESSOR STALL. CAUSE OF STALL WAS FOUND TO BE LIBERATED SECTION OF HIGH PRESSURE COMPRESSOR (HPC) 5TH STAGE BLADE. LIBERATION CAUSED DOWNSTREAM DAMAGE, INCREASED TIP CLEARANCE, AND REDUCED SURGE MARGIN OF HPC TO STALL Jun 1, 2002 · N822UA · Airbus A319131 · Turbine Engine Compressor SectionSDR 2002UALA00923Blade · failedRIGHT ENGINE FAILED. BORESCOPE INSPECTION REVEALED FAILED HIGH PRESSURE COMPRESSOR STAGE 4 BLADES, CAUSING MAJOR INTERNAL ENGINE DAMAGE AND AUTO-SHUTDOWN. ENGINE WAS REPLACED.May 29, 2002 · N435UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2002UALA00919Control Unit · failedON FINAL GOT L-G LGCIU 1 FAULT. EXTENDED THE GEAR AND GOT REVERSER NR 1 AS INOP SYSTEM. REPLACED LGCIU-1.May 27, 2002 · N437UA · Airbus A320232 · Landing Gear Position and WarningSDR 2002UALA00770Plate · stiffAFT CARGO DOOR ECAM WARNING ILLUMINATED. FOUND DOOR HANDLE PLATE STIFF. REMOVED PLATE, CLEANED, LUBED AND REINSTALLED.May 27, 2002 · N429UA · Airbus A320232 · Cargo/Baggage DoorsSDR 2002UALA00920Bleed Valve · failedNR 2 ENGINE EXPERIENCED A HUNG START. HPC BLEED VALVE TEST REVEALED FAILED HPC 7C BLEED VALVE AND WEAK HPC 7A SOLENOID VALVE. VALVES REPLACED.May 27, 2002 · N435UA · Airbus A320232 · Compressor Bleed ValveSDR 2002UALA00766Rub Strip · debondedNR 2 ENGINE EXPERIENCED A MAJOR COMPRESSOR STALL. THE THROTTLE WAS RETARDED TO IDLE SPEED. REPLACED ENGINE. CORRECTIVE ACTION FOR MAJOR CAUSE IS INCORPORATION OF UPGRADED HIGH PRESSURE COMPRESSOR (HPC) RUBSTRIP MATERIAL THAT IS MUCH MORE RESISTANT TO DISBONApr 28, 2002 · N411UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2002UALA00752Outflow Valve · failedAIRCRAFT UNABLE TO MAINTAIN PRESSURE. VALVE REPLACED ALONG WITH THE AVIONICS COMPUTER.Apr 23, 2002 · N416UA · Airbus A320232 · Pressure Regulator/Outflow ValveSDR 2002UALA00706Handle · unsecureCARGO (FORWARD) DOOR ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE SHOWED OPEN PASSING 10,000 FEET. AIRCRAFT RETURNED TO FIELD. HANDLE WAS STOWED AND LIGHT EXTINGUISHED.Apr 12, 2002 · N417UA · Airbus A320232 · Door Warning SystemSDR 2002UALA00570Wire · shortedNUMEROUS ECAM FAULT MESSAGES FROM THE NUMBER TWO ENGINE. FOUND NUMEROUS WIRES SHORTED IN THE RIGHT ENGINE OUTBOARD PYLON AREA. AREA WAS CHECKED FOR DAMAGE AND NEW WIRES INSTALLED AS REQUIRED.Mar 27, 2002 · N420UA · Airbus A320232 · Turbine Engine System WiringSDR 2002UALA00565Filter · cloggedABORTED TAKEOFF AT 73 KNOTS DUE TO AN AVIONICS COOLING FAN MESSAGE. FOUND AVIONICS COOLING SYSTEM FILTER CLOGGED. REPLACED SAME.Mar 26, 2002 · N458UA · Airbus A320232 · Cabin Cooling SystemSDR 2002UALA00537Bottle · lowDOOR ASSIST BOTTLE AT 2L LOW. SERVICED ASSIST BOTTLE PRESSURE TO 1750 PSI, CHECKS OK.Mar 22, 2002 · N418UA · Airbus A320232 · Passenger/Crew DoorsSDR 2002UALA00368Cover · looseLOWER ECAM MESSAGE HAD AMBER EXIT DOOR WARNING ON DOOR PAGE FOR RIGHT AFT OVERWING DOOR. PROBLEM WAS CAUSED BY MOVEMENT OF THE OVERWING EXIT HANDLE COVER FLAP. REMOVED OVERWING HATCH AND INSPECTED WITH NO FINDINGS. REINSTALLED DOOR AND SECURED DOOR HANDLE CMar 20, 2002 · N412UA · Airbus A320232 · Emergency ExitsSDR 2002UALA00321Skin · crackedLEFT HAND EXTERNAL FUSELAGE BLIND FASTENER HOLE AT STATION 1270 STRINGER 38L HAS CRACK INDICATION AT 6:00 POSITION VERIFIED WITH NONDESTRUCTIVE TESTING. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN DOUBLER.Mar 3, 2002 · N456UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2002UALA00536Fire Bottle · unserviceableCREW REPORTS ECAM MESSAGE INDICATES A FIRE BOTTLE DISCHARGE. REPLACED CARGO FIRE BOTTLE DUE TO LOW PRESSURE INDICATION.Feb 23, 2002 · N475UA · Airbus A320232 · Fire Bottle, FixedSDR 2002UALA00286Power Supply · dischargedDOOR 2L EMERGENCY EXIT LIGHT INOPERABLE. REINSTALLED POWER SUPPLY. OPERATIONAL CHECK NORMAL.Feb 17, 2002 · N476UA · Airbus A320232 · Emergency LightingSDR 2002UALA00279Switch · faultyDIVERTED TO MIA DUE TO HYDRAULIC QUANTITY LOSS INDICATION. CONFIRMED GREEN SYSTEM HYDRAULIC QUANTITY RESERVOIR FULL, NO EXTERNAL LEAKS NOTED. REPLACED LOW LEVEL SENSOR.Feb 16, 2002 · N403UA · Airbus A320232 · Hydraulic Quantity SensorSDR 2002UALA00250Outflow Valve · failedRETURNED TO FIELD DUE TO CABIN PRESSURIZATION PROBLEM. UNABLE TO MAINTAIN CABIN PRESSURE IN AUTO OR MANUAL MODE. SKIN AIR OUTLET VALVE WAS DEACTIVATED AND SUBSEQUENTLY REPLACED.Feb 9, 2002 · N409UA · Airbus A320232 · Pressure Regulator/Outflow ValveSDR 2002UALA00214Light · inoperativeSEATS 19, 21 LEFT EMERGENCY ESCAPE PATH LIGHTING INOPERABLE. REPLACED EMERGENCY LIGHT ASSEMBLY.Feb 4, 2002 · N435UA · Airbus A320232 · Emergency LightingSDR 2002UALA00201Idg · overheatedNR 1 INTEGRATED DRIVE GENERATOR DISCONNECTED AND UNABLE TO START AUXILIARY POWER UNIT. REPLACED NR 1 ENGINE INTEGRATED DRIVE GENERATOR.Feb 3, 2002 · N404UA · Airbus A320232 · AC Generator-AlternatorSDR 2002UALA00182Odor · detectedSMELL OF SMOKE IN CABIN. NO SMOKE VISIBLE. FLIGHT ATTENDANT SMELLED SMOKE IN THE CABIN. NO SMOKE WAS SEEN, SMELL WAS PUNGENT AND LOCATED JUST AFT OF 1ST CLASS. ACCOMPLISHED BITE CHECK OF THE TEMPERATURE CONTROL SYSTEM, CHECKED ALL FANS FOR OPERATION, CHECKFeb 1, 2002 · N429UA · Airbus A320232 · Air Distribution SystemSDR 2002UALA00139Skin · dentedDENT FOUND AT AIRCRAFT ARRIVAL. DENT LOCATED ABOUT 20 INCHES ABOVE AVIONICS EQUIPMENT AIR INLET AND 9 INCHES AFT OF FRAME 20. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.Jan 24, 2002 · N475UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2002UALA00132Carbon Seal · leakingNR 1 ENGINE HAD INFLIGHT SHUTDOWN DUE TO LOSS OF OIL QUANTITY AND DECREASE IN OIL PRESSURE. AFTER SHUTDOWN ENGINE WINDMILLED FOR 35 MINUTES, OIL TEMPERATURE 110-115, OIL PRESSURE 9.5 PSI AND OIL QUANTITY ZERO. INTERFACE BETWEEN FUEL PUMP AND MAIN ENGINE GEARJan 21, 2002 · N441UA · Airbus A320232 · Turbine Engine Accessory DriveSDR 2002UALA00011Monitor · malfunctionedCREW REPORTS HOT BRAKES ON CLIMB OUT WITH GEAR DOWN. SUPPLEMENTAL DATA UPDATE ORIG INDICATION 370 DEG, CLIMBED TO 425 DEG. SUSPECTED INDICATION PROBLEM, BRAKE TEMP CHECKS NORMAL. BSCU BITE CHECK AND PREVIOUS LEG REPORT FAULT BRAKE TEMPERATURE MONITORING UNIT Jan 1, 2002 · N462UA · Airbus A320232 · Landing Gear Brake SystemSDR 2001UALA02501Power Supply · failedRIGHT OVERWING EMERGENCY LIGHT POWER SUPPLY FAILS TEST AFTER REPLACEMENT OF THE BATTERY PACK. REPLACED POWER SUPPLY.Dec 30, 2001 · N454UA · Airbus A320232 · Emergency LightingSDR 2001UALA02442Structure · damagedABORTED TAKEOFF AT 140 KNOTS DUE TO NR 1 ENGINE COMPRESSOR STALL. SUPPLEMENTAL DATA UPDATE INITIAL BORESCOPE INFORMATION INDICATES DISBOND OF C6 ABRADABLE RUBSTRIP MATERIAL, CAUSING C6 BLADE DAMAGE AND COMPRESSOR STALL.Dec 21, 2001 · N426UA · Airbus A320232 · Turbine Engine Compressor Section
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