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 2001UALA02437Bellows · blownCABIN ALTITUDE COULD NOT BE MAINTAINED BELOW 10,000 IN AUTO. PACK NR 2 WAS DEFERRED INOPERATIVE, PACK NR 1 WOULD NOT PRESSURIZE THE CABIN, FOUND BLOWN COOLING DUCT BELLOWS NR 1 PACK, REPLACED AND OPERATIONALLY CHECKED NORMAL. PACK NR 2 WAS LATER OPERATIONALLDec 18, 2001 · N406UA · Airbus A320232 · Cabin Cooling SystemSDR 2001UALA02408Control Unit · failedCREW REPORTED ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM) SMOKE LAVATORY & CARGO DETECTION FAULT WITH THE REPORT FROM A FLIGHT ATTENDANT OF SMOKE IN AFT CABIN. REPLACE THE SDCU (SMOKE DETECTOR CONTROL UNIT). AIRCRAFT FREE OF PROBLEMS SINCE REMOVAL.Dec 13, 2001 · N434UA · Airbus A320232 · Smoke DetectionSDR 2001UALA02392Sensor · failedAIR CONDITIONING STUCK FULL HOT IN CABIN. SUPPLEMENTAL DATA UPDATE AFTER TROUBLESHOOTING AND IN CONJUNCTION WITH ASSOCIATED CFDS FAULT, REPLACED PACK NR 2 INLET PRESSURE SENSOR (36HH). NO FURTHER CFDS OR CREW REPORTED FAULTS.Dec 7, 2001 · N482UA · Airbus A320232 · Cabin Temperature Control SystemSDR 2001UALA02383Pump · failedYELLOW HYDRAULIC RESERVOIR OVERHEAT WARNING IN FLIGHT. REPLACED YELLOW SYSTEM ENGINE DRIVEN HYDRAULIC PUMP.Dec 4, 2001 · N447UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR 2001UALA02358Actuator · faultyRESERVOIR OVERHEAT DISPLAYED ON UPPER ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM) SCREEN. FOUND GREEN HYDRAULIC SYSTEM PRESSURE INDICATING 2000 PSI WITH GEAR DOORS UP. DISCOVERED THAT BY OPENING THE RIGHT HAND MAIN LANDING GEAR DOOR, PRESS RETURNS TO 3Dec 3, 2001 · N436UA · Airbus A320232 · Landing Gear Door ActuatorSDR 2001UALA02359Wire · looseEMERGENCY EXIT LIGHTS ON LAST 3 ROWS OF SEATS ARE INOP. RESECURED WIRES AT SEATS 24C AND 26C. LIGHTS OPERATIONAL CHECK NORMAL.Dec 2, 2001 · N431UA · Airbus A320232 · Light System WiringSDR 2001UALA02356Actuator · faultyCREW REPORTS LANDING GEAR DOORS NOT CLOSED ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM) MESSAGE AFTER TAKEOFF. FOUND GREEN HYDRAULIC SYSTEM PRESSURE INDICATING 2000 PSI WITH GEAR DOORS UP. DISCOVERED THAT BY OPENING THE RIGHT HAND MAIN LANDING GEAR DOOR,Dec 1, 2001 · N436UA · Airbus A320232 · Landing Gear Door ActuatorSDR 2001UALA02355Actuator · faultyELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM) - GREEN HYDRAULIC SYSTEM RESERVOIR OVERHEAT. FOUND GREEN HYDRAULIC SYSTEM PRESSURE INDICATING 2000 PSI WITH GEAR DOORS UP. DISCOVERED THAT BY OPENING THE RIGHT HAND MAIN LANDING GEAR DOOR, PRESS RETURNS TO 30Nov 30, 2001 · N436UA · Airbus A320232 · Landing Gear Door ActuatorSDR 2001UALA02354Valve · failedONCE GEAR SELECTED DOWN FOR LANDING ALL THREE GEAR DOORS WOULD NOT RETRACT. NOSE WHEEL STEERING INOP BUT NO ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM). AFTER ENGINES SHUT DOWN GEAR DOORS RETRACTED. REPLACED LANDING GEAR SAFETY VALVE (49GA). LEAK CHENov 28, 2001 · N445UA · Airbus A320232 · Landing Gear Door Retract SectionSDR 2001UALA02326Stringer · bentDEEP GOUGE 2 FT AFT OF DR 2L, AND 1 FT UP FROM DOOR BOTTOM.. MAJOR REPAIR ACCOMPLISHED. FRAME 69, STRINGER 23 REMOVED. REWORKED STRINGER & MFG DOUBLER AND INSTALLED.Nov 21, 2001 · N444UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2001UALA02191Skin · dentedFUSELAGE SKIN DENTED AT FUSELAGE STATION 3320 BETWEEN STRINGER 3 AND 4 LEFT. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT TO AREA. NO CRACKS EXIST. INSTALLED DOUBLER.Oct 31, 2001 · N460UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2001UALA02193Proximity Switch · out of adjLEFT AFT OVERWING EMERGENCY EXIT OPEN ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM) WARNING DURING CLIMB THROUGH FL 200. NO DEPRESSURIZATION. ECAM DISAPPEARED IN DESCENT BELOW 8000 FEET. FOUND EMERGENCY HANDLE COVER PROXIMITY SWITCH OUT OF TARGET. ADJUSOct 31, 2001 · N453UA · Airbus A320232 · Door Warning SystemSDR 2001UALA02144Pressure SwitchOIL SMELL IN CABIN. FOUND APU OIL PRESS SWITCH LEAKING INTO APU INLET. REPLACEDSWITCH AND RAN PACKS. NO LEAKS OR SMELL NOTED.Oct 17, 2001 · N825UA · Airbus A319131 · APU Oil SystemSDR 2001UALA02087Servo · malfunctionedUNCOMMANDED RIGHT ROLL IN EXCESS OF 10 DEGREES EXPERIENCED AFTER ENCOUNTER WITH TURBULENCE. THE RT GREEN AILERON SERVO CONTROL WAS REPLACED AND THE OPERATIONAL CHECK WAS GOOD.Sep 27, 2001 · N442UA · Airbus A320232 · Aileron Control SystemSDR 2001UALA02075Blade · crackedNR 1 ENGINE FAILURE. IN FLIGHT SHUT DOWN DUE TO ENGINE FAILURE CAUSED BY HIGH PRESSURE COMPRESSOR (HPC) 6TH STAGE BLADE CRACKING/LIBERATION AT ROOT. INSTALLATION OF NEW DESIGN OF C6 BLADES.Sep 21, 2001 · N435UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2001UALA02074Computer · malfunctionedON CLIMBOUT FELT STRONG VIBRATION IN RUDDER PEDALS. STRONG VIBRATION WAS FELT IN THE REAR OF THE CABIN. THE VIBRATION WAS REPORTED AS BEING A SIDE-TO-SIDE MOTION. FAC (FLIGHT AUGMENTATION COMPUTER) WAS REPLACED.Sep 19, 2001 · N404UA · Airbus A320232 · Flight Management Computing Hardware SystemSDR 2001UALA02040Thermostat#1 ENGINE BLEED FAULT LIGHT ILLUMINATED, HAD BLEED 1OVERHEAT. UNABLE TO RESET SYSTEM. SUPPLEMENTAL DATA UPDATE REPLACED FAN AIR THERMOSTAT, RAN ENGINES, BLEED PARAMETERS NORMAL.Sep 14, 2001 · N412UA · Airbus A320232 · Pneumatic Indicating SystemSDR 2001UALA02004Relief Valve · brokenFUEL AUTO FEED FAULT ECAM MESSAGE. FUEL IMBALANCE BETWEEN LEFT AND RIGHT WING TANKS OF 1500 POUNDS. FOUND FUEL TANK PROTECTOR-OVERPRESSURE DISC BROKEN BETWEEN THE LEFT WING AND CENTER FUEL TANKS. THIS ALLOWED FUEL TO MIGRATE FROM THE LEFT WING TANK INTO THE Sep 9, 2001 · N478UA · Airbus A320232 · Fuel StorageSDR 2001UALA01964Blade · debondedUNSCHEDULED LANDING DUE TO NR 1 ENGINE COMPRESSOR STALL. *S/D* BORESCOPE INSPECTION REVEALED DAMAGED HIGH PRESSURE COMPRESSOR SIXTH STAGE BLADES AND DISBONDED RUBSTRIP, WITH ASSOCIATED DOWNSTREAM DAMAGE. REPLACED ENGINE.Sep 4, 2001 · N436UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2001UALA01854Door · vibrationLOUD BUZZING NOISE AND VIBRATION COMING FROM DOOR 1 LEFT.Aug 27, 2001 · N443UA · Airbus A320232 · Passenger/Crew DoorsSDR 2001UALA01853Control Unit · failedINTERMITTENT MASTER CAUTION CHIME LIGHT. INTERMITTENT BLINKING OF FEATURES DISPLAYED ON CAPTAINS PRIMARY FLIGHT DISPLAY AND NAVIGATION DISPLAY. FLIGHT CONTROL UNIT LIGHTS FLASHING ALSO. THE FCU WAS REPLACED AND GROUND CHECK WAS NORMAL.Aug 27, 2001 · N446UA · Airbus A320232 · Flight ControllerSDR 2001UALA01852Light · smokeSMOKE FROM FORWARD ENTRY LIGHTS. CIRCUIT BREAKER PULLED AND SMOKE APPEARS TO BE DISSIPATING.Aug 24, 2001 · N414UA · Airbus A320232 · Passenger Compartment LightingSDR 2001UALA01768Light · will not testEMERGENCY LIGHT TEST FAILED.Aug 21, 2001 · N415UA · Airbus A320232 · Emergency LightingSDR 2001UALA01744HoseGREEN HYDRAULIC SYSTEM LOSS OF FLUID. SUPPLEMENTAL DATA UPDATE LEFT MAIN LANDING GEAR LOCKSTAY ACTUATOR HYDRAULIC LINE SWIVEL SHEARED.REPLACED LINE ASSEMBLY AND LEAK CHECKED. NO LEAKS NOTED.Aug 18, 2001 · N418UA · Airbus A320232 · Hydraulic System, MainSDR 2001F00229Harness · damagedSAL - FLT 390 - DURING CLIMB, THE CAPTAIN REPORTED AIR ENGINE 1 BLEED ABNORMAL PRESSURE, AIR ENGINE 1 BLEED FAULT AND HYD GREEN ENG 1 PUMP LOW PRESSURE. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING, MAINT TECH PERFORMED FAULT ANALYSIS, Aug 16, 2001 · N941LF · Airbus A320233 · Bleed Air Indicating SystemSDR 2001UALA01661Servo · defectiveELEVATOR AILERON COMPUTER WARNING FAULT. A/C HAD HISTORY OF ELAC 1 PITCH FAULT AND ELAC 2 -RELATED PROBLEMS. IT WAS DETERMINED THAT THE LEFT GREEN ELEVATOR SERVO CONTROL 34CE1 NEEDED TO BE REPLACED. OPS TEST WAS ACCOMPLISHED.Aug 9, 2001 · N457UA · Airbus A320232 · Elevator Control SystemSDR 2001UALA01647IndicatorON CLIMB, RECEIVED YELLOW HYDRAULIC RESERVOIR OVERHEAT WARNING. SUPPLEMENTAL DATA UPDATE FOUND YELLOW SYSTEM OVER SERVICED. REMOVED EXCESS HYDRAULIC FLUID AND ALSO REPLACED REMOTE HYDRAULIC QUANTITY INDICATOR FOR A STUCK NEEDLE TO PREVENT RECURRENCE.Aug 6, 2001 · N447UA · Airbus A320232 · Hydraulic System, MainSDR 2001UALA01616Skin · damagedFUSELAGE SKIN DAMAGED AT FRAME 73 TO FRAME 74 BETWEEN STRINGER 31 LEFT TO 33 LEFT. MAJOR REPAIR ACCOMPLISHED. FOUR SHEAR TIES REPLACED AND STRINGER SPLICE ACCOMPLISHED. FILLER AND DOUBLER INSTALLED.Aug 5, 2001 · N443UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2001UALA01586Computer · faultyUNSCHEDULED LANDING DUE TO LOSS OF NR 1 ENGINE BLEED. *S/D* FOUND LEAKING CLAMPS AT GROUND AIR START CONNECTION (FIXED PROBLEM ON NR 1 BLEED), AND REPLACED NR 2 BLEED AIR MONITORING COMPUTER FOR NR 2 BLEED PROBLEM. NO FURTHER DISCREPANCIES HAVE BEEN REPORTEAug 1, 2001 · N435UA · Airbus A320232 · Pneumatic Distribution SystemSDR 2001UALA01415B-Nut · looseFLIGHT CREW REPORTING LOSS OF GREEN HYDRAULIC SYSTEM. FOUND LEFT LANDING GEAR DOOR UPLOCK HYDRAULIC LINE B-NUT LOOSE. TIGHTENED NUT AND SERVICED SYSTEM. PRESSURIZED AND NO LEAKS FOUND.Jul 18, 2001 · N460UA · Airbus A320232 · Hydraulic System, MainSDR 2001UALA01394Thermostat · failedNR 1 ENGINE BLEED FAULT DISPLAYED ON UPPER ECAM SCREEN. *S/D* REPLACED CONTROL THERMOSTAT AS FAULTED IN CENTRALIZED FAULT DISPLAY SYSTEM. IN ADDITION, THE HEAT EXCHANGER OUTLET TEMPERATURE SENSOR AND BLEED MANAGEMENT COMPUTER WERE REPLACED PRECAUTIONARY. Jul 14, 2001 · N406UA · Airbus A320232 · Pneumatic Distribution SystemSDR 2001UALA01297Sensor · failedRT AFT OVER WING EXIT SLIDE IS NOT INDICATING ARMED. REPLACED RIGHT AFT EMERGENCY EXIT DOOR ARM SENSOR.Jul 1, 2001 · N439UA · Airbus A320232 · Emergency EquipmentSDR 2001UALA01254Compressor · stalledCOMPRESSOR STALL ON NUMBER TWO ENGINE.Jun 30, 2001 · N401UA · Airbus A320232 · Turbine Engine Compressor SectionSDR CA010629039Pressure Switch · failed(CAN) DEPARTED YUL FOR KEF. WHILE IN CLIMB THE ENGINE NR 2 YELLOW HYDRAULIC PUMP FAULT LIGHT ILLUMINATED. THE PUMP WAS DE-ACTIVATED AND THE AIRCRAFT DIVERTED TO YHZ. MAINTENANCE TROUBLESHOOTING LOCATED A HYDRAULIC LEAK FROM THE HYDRAULIC PUMP NR 2 PRESSURE SWJun 29, 2001 · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR 2001UALA01196AileronRH AILERON ASSEMBLY UPPER SKIN DAMAGE BY HAIL RESULTING IN A DENT 1 INCH IN DIAMETER ON THE UPPER SKIN, .5 INCHES FROM THE INBOARD EDGE AND 5 INCHES FROM THE TRAILING EDGE. THERE IS ALSO A CRACK AT THE BOTTOM OF THE DENT MEASURING .5 INCHES LONG. ACCOMPLISHEJun 20, 2001 · N451UA · Airbus A320232 · AileronsSDR AWXA0001856Bleed Valve · fluctuatesPHX - AIR TURNBACK - 6/10/01 - FLT 234 - DURING LEVEL OFF AT FL 370, NR 2 BLEED FAULTED W/ ECAM MSG; PER THE FCOM CREW TURNED OFF BLEED SWITCH AND DUE TO ICING CONDITIONS EN ROUTE TO DTW, THE A/C RETURNED TO PHX; IN PHX THE NR 2 BLEED AIR SYS WAS PLACED ON MELJun 14, 2001 · N642AW · Airbus A320232 · Compressor Bleed ValveSDR 2001UALA00885Power Supply · dischargedCABIN EMERGENCY LIGHT TEST FAILED. REPLACED DOOR 1 LEFT SLIDE AND EMERGENCY LIGHT SYSTEM POWER SUPPLY ASSEMBLY.Jun 1, 2001 · N428UA · Airbus A320232 · Emergency LightingSDR 2001UALA00782Tube · unserviceableSLIDE/RAFT D30665-105 TOP INFLATION TUBE RT SIDE SEAM FAILED DURING PROOF PRESSURE TEST. TOP TUBE HAS A 4 FOOT SEAM RIP ON RT SIDE ABOVE THE REDUCER BULKHEAD FROM THE FAILURE. UNIT IS BEING SENT TO THE VENDOR FOR REPAIR.May 18, 2001 · N404UA · Airbus A320232 · Escape SlideSDR 2001UALA00799Skin · dentedDENT IN FUSELAGE SKIN, 13 INCHES AFT OF FRAME 65 AND BETWEEN STRINGER 23R AND 24R WAS FOUND CRACKED.May 4, 2001 · N434UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2001UALA00657Power Supply · dischargedFWD LT EMERGENCY POWER SUPPLY UNIT, EMERGENCY LIGHT TEST FAILS. REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY, TESTS OK.May 3, 2001 · N463UA · Airbus A320232 · Emergency LightingSDR CA010529006Manifold · leaking(CAN) YELLOW SYSTEM LOW LEVEL ECAM ON DESCENT INTO YYC - MAJOR HYDRAULIC LEAK EVIDENT AT BLOCK IN ON RAMP. FOUND YELLOW LEAK MEASUREMENT MANIFOLD LEAKING. REPLACED HYDRAULIC LEAK MEASUREMENT MANIFOLD. SYSTEM CHECKS SERVICEABLE IAW 29-19-41-401.. . . .Apr 26, 2001 · Airbus A320232 · Hydraulic System, MainSDR YENA0105Light · missingROW 1ABC EMERGENCY LIGHT BULB MISSING WITH TERMINAL PIN BROKEN OFF.Apr 23, 2001 · N507JB · Airbus A320232 · Emergency LightingSDR 2001UALA00468Harness · chafedNR 2 ENGINE EXHAUST GAS TEMPERATURE OVERTEMP INDICATION. SUPPLEMENTAL DATA UPDATE EXHAUST GAS TEMPERATURE (EGT) HARNESS EXHIBITED UNUSUAL PHYSICAL CHAFING. REPLACED THE EGT HARNESS.Apr 11, 2001 · N409UA · Airbus A320232 · Engine EGT/TIT Indicating SystemSDR 2001UALA00453Windshield · crackedCAPTAINS WINDSHIELD CRACKED. REPLACED CRACKED WINDSHIELD AND NR 1 WINDOW HEAT CONTROL.Apr 9, 2001 · N436UA · Airbus A320232 · Flight Compartment WindowsSDR 2001UALA00452Radar · failedFAILURE OF THE WEATHER RADAR. WEATHER RADAR TRANSCEIVER WAS REPLACED AND THE SYSTEM CHECKED GOOD.Apr 9, 2001 · N470UA · Airbus A320232 · Weather Radar SystemSDR YENA0104Skin · damagedDURING WALKAROUND FOUND DAMAGE TO AIRCRAFT SKIN BETWEEN FRAMES 61-62 AND STRINGERS P41 AND P43. AIRCRAFT MAINTENANCE FERRY FROM OAK TO JFK FOR REPAIR. ACCOMPLISHED MAJOR REPAIR PER SRM 53-00-11, FIG 202 AND 209.Apr 5, 2001 · N507JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2001UALA00411Heater · arcedLEFT WINDSHIELD HEAT STARTED ARCING ON DESCENT. SUPPLEMENTAL DATA UPDATE INSTALLED NEW LEFT WINDSHIELD. HEAT OPS CHECKED GOOD.Apr 4, 2001 · N444UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR 2001UALA00412Oxygen Mask · leakingFLIGHT DECK LOW OXYGEN PRESSURE. *S/D* REMOVED CREW FULL FACE OXYGEN MASK (WITH SECONDARY REGULATOR) AND REPLACED. ALSO REMOVED AND REPLACED THE STOWAGE BOX.Apr 4, 2001 · N453UA · Airbus A320232 · Crew Oxygen SystemSDR 2001UALA00401Controller · failedLOST NOSE WHEEL STEERING AND BRAKING CONTROL. SUPPLEMENTAL DATA UPDATE REPLACED CAPTAINS STEERING TILLER. OPS CHECKS OK.Apr 3, 2001 · N470UA · Airbus A320232 · Landing Gear Steering SystemSDR 2001UALA00798Pump · burnedFOUND CONNECTOR FOR NR 1 CENTER TANK BOOST PUMP BURNED AND DAMAGED.Apr 2, 2001 · N418UA · Airbus A320232 · Fuel Boost Pump
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