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 2007UALA00954Sill · corrodedR2 DOOR SILL PLATE HAS CORROSION BEYOND LIMITS AT FRAME 68. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR.Mar 30, 2007 · N472UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2007UALA00960Battery · faultyFWD EPSU BATTERY FAULT & EPSU BATTERY L DISPLAYED ON PTP. REPLACED BATTERY.Mar 30, 2007 · N458UA · Airbus A320232 · Emergency LightingSDR 2007UALA01003Starter · faultyON START NR 1 ENG HAD REPORTED SPARKS COMING FROM THE BOTTOM OF THE ENG. [SUP 06-01-07] REPLACED START VALVE AND STARTER.Mar 30, 2007 · N474UA · Airbus A320232 · Engine StarterSDR 2007UALA00943Stringer · corrodedSTRINGER 42 LEFT HAS CORROSION ON THE INNER SURFACE OF THE FLANGE.Mar 29, 2007 · N432UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2007UALA00926Compressor · stalledPOSSIBLE ENGINE COMPRESSOR STALL ON TAKEOFF. SUSPECT LEFT ENG. NO ECAM, PFR SHOWS NR 2 ENGINE COMPRESSOR STALL. [SUP 05-18-07] QTY 2 STAGE 6 HPC BLADES LIBERATED AT MID-SPAN WITH DOWNSTREAM DAMAGE.Mar 28, 2007 · N416UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2007UALA00934Controller · inoperativeCAPTAIN'S SLIDING WINDOW HEATING INOPERATIVE. [SUP 06-01-07] INITIALLY REPLACED THE NR 1 WINDOW HEAT CONTROLLER BUT LATER DETERMINED THAT SLIDING WINDOW WAS DEFECTIVE. WINDOW INTERNAL TEMPERATURE SENSORS MISREPORTING TEMP TOO LOW, CAUSING HEAT CONTROLLER TOMar 28, 2007 · N474UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR 2007UALA00941Controller · malfunctionedNOSE WHEEL STEERING FAULT AT GEAR DOWN. [SUP 06-01-07] REPLACED NOSE WHEEL STEERING SERVO CONTROL 6GC.Mar 28, 2007 · N428UA · Airbus A320232 · Landing Gear Steering SystemSDR 2007UALA00876Connector · disconnectedINVESTIGATING SMC 003 FAULT. FOUND BOTH THE LEFT AND RIGHT OVERWING EMERGENCY EXIT EPSU UNIT CONNECTOR DISCONNECTED. [SUP 06-01-07] ALL EMERGENCY POWER SUPPLY UNITS WERE CHANGED DURING A REGULARLY SCHEDULED HMV VISIT 2 WEEKS PRIOR. STATION PERFORMING HMV DIMar 25, 2007 · N446UA · Airbus A320232 · Light System WiringSDR 2007UALA00896Warning System · activatedAFTER TAKEOFF RECEIVED ECAM FOR GREEN HYDRAULIC LOW LEVEL. AMBER ALERT AND EMERGENCY DECLARED WITH ATC WITH EMERGENCY EQUIPMENT MEETING FLIGHT AT PLANNED DESTINATION. [SUP 06-01-07] A HYDRAULIC PRESSURE LINE IN THE UPPER FORWARD LT PYLON WORN THROUGH FROM CMar 24, 2007 · N407UA · Airbus A320232 · Hydraulic Indicating SystemSDR 2007UALA00878Power Supply · faultyMID CABIN OVERHEAD EXIT FLASHING ON-OFF; EXIT DOOR LIT TOO. REPLACED LEFT WING POWER SUPPLY UNIT.Mar 24, 2007 · N473UA · Airbus A320232 · Emergency LightingSDR 2007UALA00858Slide · dischargedSLIDE DISCHARGED 1L. [SUP 06-01-07] REPLACED DOOR 1L SLIDE AND ASSIST MECHANISM SEALING DIAPHRAGM. FILLED ASSIST BOTTLE TO PROPER PRESSURE.Mar 23, 2007 · N426UA · Airbus A320232 · Escape SlideSDR 2007UALA00874Light · brokenCABIN EEL BACKSHELLS ARE BROKEN AT CABIN FLOOR LEVEL BY LEFT SIDEWALL AT SEAT ROWS 13 AND 26. [SUP 5-1-07] BACKSHELLS REPLACED AND OP CHECKED GOOD.Mar 23, 2007 · N415UA · Airbus A320232 · Emergency LightingSDR 2007UALA00875Connector · dirtyCIDS TEST FAULTS BPSU BATTERY AFT LT. CONNECTOR DIRTY. CLEANED CONNECTION FOR BATTERY POWER SUPPLY UNIT.Mar 23, 2007 · N438UA · Airbus A320232 · Light System WiringSDR 2007UALA00877Light · faultyFWD EMERGENCY EXIT LIGHTS ARE ON WITH SEAT BELT SWITCH ON. SUP.4-17-07. RESET CIDS SYS. AND LIGHTS CKD NORMAL.Mar 23, 2007 · N458UA · Airbus A320232 · Emergency LightingSDR 2007UALA00856Compressor · stalledNR 2 ENGINE HAD A COMPRESSOR STALL WITH AN AUDIBLE BANG. [SUP 06-01-07] INSPECTED ENGINE PER AMM TASK FOR STALL CONDITION AND FOUND NO DEFECTS. LUBED VARIABLE STATOR VALVE MECHANISM AND PERFORMED IDLE RUN CHECK. NO FURTHER IRREGULARITIES NOTED.Mar 22, 2007 · N411UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2007UALA00855Engine · hung startNR 2 ENG HAD A OVERTEMP. EGT WAS 738C ON ECAM. N1 6-7%, N2 41-42%. ENG APPEARED TO HAVE A HUNG START AND WAS OVER 635C FOR APPROX 6-8 SECONDS BEFORE SHUTTING DOWN. [06-14-07] REPLACED NR 2 ENGINE DUE TO POSSIBLE DAMAGE TO TURBINES AND DOWNSTREAM ITEMS.Mar 21, 2007 · N453UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2007UALA00818Power Supply · failedEMERGENCY LIGHTS TEST FAILED. REPLACED EPSU AND BATTERY 11WL.Mar 19, 2007 · N443UA · Airbus A320232 · Emergency LightingSDR YENA2007018Cowling · detachedFLT 830, PBI-JFK, AIR RETURN TO PBI. ENGINE COWL SEPARATED FROM ENGINE NR 1. DAMAGE NOTED ON INBOARD LEADING EDGE ON LEFT WING AND OTHER AREA'S OF ENGINE COWL.Mar 18, 2007 · N635JB · Airbus A320232 · Powerplant SystemSDR 2007UALA00796Unknown · smokeFLIGHT CREW REPORTING SMOKE IN AFT GALLEY IN OVEN AREA. [SUP 06-01-07] REMOVED BOTH OVENS, CEILING PANELS AND CIRCUIT BREAKER PANEL AND FOUND NO EVIDENCE OF FIRE. OPERATED OVENS, HOT PLATES AND CHILLERS FOR 4.5 HOURS ON GROUND AND DID NOT NOTICE ANY SMOKE ORMar 18, 2007 · N408UA · Airbus A320232 · Air Distribution SystemSDR 2007UALA00793Control Module · malfunctionedRTFL DUE TO NW STEERING FAULT DISPLAYED ON UPPER ECAM SCREEN. REQUESTED TOW. [SUP 06-01-07] REPLACED NOSE STEERING SERVO CONTROL MODULE. AT OVERHAUL, FOUND A CRUSHED ELECTRICAL CONNECTOR AND SIGNIFICANT CORROSION DAMAGE ON ELECTRO SELECTOR.Mar 17, 2007 · N454UA · Airbus A320232 · Landing Gear Steering SystemSDR 2007UALA00799Wire · shortedCABIN EMERGENCY LIGHTING DOES NOT TEST OK. SEAT FOUND MOUNTED ON TOP OF POWER (RED) WIRE, CAUSING SHORT. RESPLICED ALL THREE SEATS TO POWER AND GROUND WIRE FROM WALL CONNECTOR. ROUTED PROPERLY AND SECURED. ALL LIGHTS TEST NORMAL. EMER LIGHT TEST AT ATTNDT PAMar 17, 2007 · N404UA · Airbus A320232 · Light System WiringSDR 2007UALA00832Cover · out of positionTHE 2L SLIDE COVER FELL OFF. [SUP 05-18-07] SECURED SLIDE COVER.Mar 17, 2007 · N402UA · Airbus A320232 · Escape SlideSDR 2007UALA00785Unknown · vibrationHIGH FREQ LATERAL VIBRATION FROM TAIL OF ACFT DURING CLIMBOUT. VIBRATION DECREASES WITH DECREASE IN AIR SPEED. [SUP 06-01-07] REPLACED YELLOW HYDRAULIC SYSTEM RT ELEVATOR SERVO VALVE AFTER FINDING OSCILLATIONS TO BE OUT OF LIMITS.Mar 16, 2007 · N443UA · Airbus A320232 · Standard Practices/StructuresSDR 2007UALA00786Unknown · vibrationHIGH FREQUENCY VIBRATION STARTED 23,500- 330 KNOTS WENT AWAY 24,500-300 KNOTS RETURNED AGAIN 25,000-315 KNOTS AND STOPPED 30,500-290 KNOTS .76 MACH. VIBRATION VERY NOTICEABLE THROUGHOUT CABIN. FLT CONTROLS SEEMED OK. CREW REPORTED UP & DOWN OSCILLATION THRMar 16, 2007 · N446UA · Airbus A320232 · Standard Practices/StructuresSDR 2007UALA00791Idg · leakingRTFL DUE TO A IDG LOW OIL PRESSURE PROBLEM. [SUP 06-01-07] REPLACED NR 1 IDG. AT OVERHAUL, FOUND A LEAKING SEAL THAT WAS ALLOWING FLUID TO ESCAPE THE SYSTEM.Mar 16, 2007 · N401UA · Airbus A320232 · AC Generation SystemSDR 2007UALA00800Frame · crackedAFT BULK CARGO COMPT 2ND FRAME FWD OF AFT PRESSURE BULKHEAD [F68] APPROX 12 INCHES INBOARD LEFT FUSE FLOORBEAM ATTACH CRACKED. [SUP 06-14-07] MAJOR REPAIR ACCOMPLISHED. CUTOUT DAMAGED FLANGE. HFEC TRIMMED SURFACE. FABRICATED AND HEAT TREATED REPAIR ANGLESMar 16, 2007 · N452UA · Airbus A320232 · Fuselage Main, FrameSDR 2007UALA00788Hydraulic System · reads lowGREEN HYDRAULIC LOW LEVEL QTY ECAM ON FINAL. PRESSURE STILL GOOD ON GREEN SYSTEM. EMERGENCY DECLARED. AMBER ALERT. [SUP 06-01-07] PERFORMED A LEAK CHECK WITH ELECTRIC AND ENGINE DRIVEN PUMPS OPERATING AND DID NOT FIND ANY LEAKS. 2 DAYS PRIOR, NR 2 ENGINEMar 15, 2007 · N412UA · Airbus A320232 · Hydraulic System, MainSDR 2007UALA00798Bleed Valve · dirtyENG 2 COMPRESSOR VANE IMPENDING ENG STALL. WARNING CAME ON-OFF 3 TIMES DURING DESCENT. *S/D* REPLACED LPC BLEED MASTER ACTUATOR. FOUND HEAVY FUEL LACQUERING ON PRESSURE DROP REGULATOR DURING OVERHAUL.Mar 15, 2007 · N448UA · Airbus A320232 · Compressor Bleed ValveSDR 2007UALA00737Control Unit · malfunctionedGEAR DID NOT RETRACT PROPERLY ON DEPARTURE. ALL OK ON 2ND ATTEMPT. [SUP 05-29-07] REPLACED NR 2 LANDING GEAR CONTROL AND INDICATING UNIT AND LANDING GEAR SELECTOR VALVE. AT OVERHAUL, NOTHING WAS FOUND TO BE OUT OF SPEC WITH THE LGCIU OR THE SELECTOR VALVE. Mar 12, 2007 · N410UA · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR 2007UALA00735Battery · faultyOVERWING EXIT LIGHT IN CEILING AND LEFT OVERWING EXIT LIGHT ON SIDEWALL FLICKER WITH SWITCH IN OFF-ON-ARMED POSITIONS. REPLACED EMERGENCY LIGHT BATTERY ON LEFT SIDE OVERWING.Mar 10, 2007 · N473UA · Airbus A320232 · Emergency LightingSDR 2007UALA00708Connector · disconnectedCABIN SEATS 3AB, 3CD, 17ABC FAILED O2 MASK RELEASE CHECK. [SUP 05-29-07] ADJUSTED THE OXYGEN CONTAINER DOOR SPACERS AND REPLACED THE RELEASE SOLENOIDS AS A PRECAUTIONARY MEASURE. AT SEATS 17ABC, FOUND THE ELECTRICAL CONNECTOR DISCONNECTED. RECONNECTED & PEMar 9, 2007 · N421UA · Airbus A320232 · Oxygen System WiringSDR 2007UALA00702Pump · failedGREEN HYDRAULIC PUMP FAILURE JUST AFTER DEPARTURE. REPLACED NR 1 ENGINE PUMP PRESSURE SWITCH. RAN ENGINE PRESSURE AND INDICATION NORMAL.Mar 8, 2007 · N406UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR 2007UALA00715Pump · failedLANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC ENGINE PUMP. [SUP 05-29-07] REPLACED ENG NR 1 HYDRAULIC PUMP AND CASE DRAIN FILTER. HYDRAULIC PUMP WAS OVERHAULED, BUT NOTHING WAS FOUND TO BE OUT OF SPEC. SEVERAL FLIGHTS LATER, THE ERROR MESSAGE REOCCMar 8, 2007 · N487UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR 2007UALA00691O-Ring · failedRTFL DUE TO GREEN HYDRAULIC SYSTEM FAILURE. GEAR WAS MANUALLY EXTENDED. REPLACED NR 1 ENGINE HYDRAULIC PUMP, AND NR 1 ENGINE HYDRAULIC PUMP CASE DRAIN FILTER PRECAUTIONARY. LEAK WAS DETERMINED TO BE CAUSED BY A CHECK VALVE PACKING IN THE NR 1 ENGINE PYLON. Mar 7, 2007 · N498UA · Airbus A320232 · Hydraulic System, MainSDR 2007UALA00692Light · no testEMERGENCY LIGHT TEST FAULTED LEFT UNIT. REPLACED EPSU. OPS CHECKS NORMAL.Mar 7, 2007 · N403UA · Airbus A320232 · Emergency LightingSDR 2007UALA00664Seat Track · corrodedFRAME C20, RBL 31 HAS EXFOLIATED CORROSION. MAJOR REPAIR ACCOMPLISHED: REPLACED SEAT TRACK.Mar 6, 2007 · N477UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR 2007UALA00690Bleed Air Sys · leakingDIVERTED DUE TO A LEFT WING BLEED LEAK. LT WING LEAK DISPLAYED ON UPPER ECAM SCREEN-AIR. FOUND LOOSE DUCTING AND CLAMPS JUST ABOVE THE EXTERNAL AIR CART HOOK UP. RESEATED DUCT AND RESECURED CLAMPS NO FURTHER DEFECTS NOTED. ACCOMPLISHED LEAK CHECK OF DUCMar 6, 2007 · N410UA · Airbus A320232 · Airfoil Anti/De-ice SystemSDR 2007UALA00662Unknown · unknownRTFL DUE TO BLEED 1 & 2 EMAC FAULT ON CLIMB. RESET BMC, BLEED 1 RESTORED IMMEDIATELY FOLLOWED BY BLEED 2 IN FLIGHT. SUPPLEMENTAL DATA UPDATE ON ENGINE NR 1, BITE TEST INDICATED FAULT OF EITHER FAN AIR VALVE, CONTROL THERMOSTAT OR SENSE LINE. FOUND FILTER FOR CMar 5, 2007 · N472UA · Airbus A320232 · Cabin Pressure Control SystemSDR 2007UALA00663Floorbeam · damagedCABIN FLOORBEAM EXFOLIATED, STA FRAME C21 TO C22, LBL 9 IN. [SUP 05-24-07] REMOVED AND REPAIRED DAMAGED AREA IN ACCORDANCE WITH SRM.Mar 5, 2007 · N477UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2007UALA00674Light · no testEMERGENCY LIGHT TEST FAILED -EXT LOADS AFT L- NO GREEN SYS OK LIGHT CIDS RESET, NO HELP. [SUP 05-24-07] FAULT TRACED TO A FAULTY SLIDE PACK AT DOOR 2L. OVERHAUL OF THE SLIDE PACK FOUND THE GREEN SYSTEM LIGHTS TO BE DAMAGED.Mar 5, 2007 · N433UA · Airbus A320232 · Emergency LightingSDR 2007UALA00675Extinguisher · misinstalledNR 1 ENGINE FWD FIRE EXTINGUISHER BOTTLE SAFETY RELIEF VALVE FOUND WITH A METAL CAP STILL INSTALLED. [SUP 05-27-07] REMOVED METAL CAP AND REINSTALLED FIRE EXTINGUISHER BOTTLE. AT THE PREVIOUS C-CHECK ON 9/13/2005, THE NR 1 ENGINE FWD BOTTLE WAS ACCIDENTALLY Mar 5, 2007 · N411UA · Airbus A320232 · Fire Bottle, FixedSDR 2007UALA00677Bleed Valve · faultyA 'THUD' NOISE NOTED ON TAKEOFF, DEADHEADING CAPT ON 23A NOTICED WHAT APPEARED TO BE A FIREBALL FROM ENG 1 EXHAUST. CREW REPORTED NO ABNORMAL PARAMETERS. NO DEBRIS FOUND ON RUNWAY. SUPPLEMENTAL DATA UPDATE CHECKED FOR EVIDENCE OF COMPRESSOR FAILURE WITH NO FINMar 5, 2007 · N421UA · Airbus A320232 · Compressor Bleed ValveSDR 2007UALA00657Oxygen Mask · no testF/O'S OXYGEN HARNESS FAILS TO INFLATE (LEAKING). DOES NOT TEST CORRECTLY WHEN PRESS TO TEST IS PUSHED. [SUP 05-24-07] REPLACED FIRST OFFICER'S MASK WITH A NEW UNIT. AT REPAIR, MASK WAS FOUND TO HAVE A LEAKING AIR BLADDER INSIDE THE HARNESS.Mar 3, 2007 · N487UA · Airbus A320232 · Crew Oxygen SystemSDR 2007UALA00632Wire Harness · unserviceableNR 2 ENG HP VLV FAULT. FOUND DAMAGED CONNECTOR AND BURNED WIRES. [SUP 05-18-07] FOUND THE WIRING HARNESS BACKSHELL CONNECTOR ON THE HP VALVE WAS STRIPPED. INITIALLY ATTEMPTED TO REPLACE BACKSHELL CONNECTOR, BUT FOUND BURNT WIRES INSIDE CONNECTOR. DETERMINEMar 2, 2007 · N427UA · Airbus A320232 · Pneumatic System WiringSDR 2007UALA00637Connector · looseCREW REPORTS FWD CARGO DOOR ECAM ON CLIMB. FOUND A LOOSE CONNECTOR ON DOOR SWITCH. RESECURED, INDICATES OKAY.Mar 2, 2007 · N405UA · Airbus A320232 · Door Warning SystemSDR 2007UALA00633Unknown · unknownENG NR 1 STALL ON POWER REDUCTION DESCENDING OUT OF FL 380, 1 SECONDS THUD HEARD AND STALL ECAM FOR 5 SECONDS. THEN ALL INDICATIONS NORMAL. [SUP 05-18-07] INITIALLY ATTRIBUTED TO POSSIBLE 7TH OR 10TH STAGE BLEED VALVE SOLENOID FAILURE. DID FIND THAT 7TH STAMar 1, 2007 · N454UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2007UALA00620Seat · misinstalledPAX SEAT ROW 10R FOUND INSTALLED TOO FAR FWD AND INTERFERES WITH THE REMOVAL OF THE FWD RIGHT OVERWING EMERGENCY EXIT HATCH. ERROR WAS MADE WHEN ATTACHMENT SCREWS FOR SEATS 10DEF WERE REMOVED FOR USE ON ANOTHER AIRCRAFT ON 1/19/2007 AT IAD. SEAT ROW WAS ACCIFeb 28, 2007 · N420UA · Airbus A320232 · Passenger Compartment EquipmentSDR 2007UALA00597Support Bracket · crackedBELLY FAIRING SUPPORT BRACKET UPPER ANGLE -Y127 (LT SIDE) AT FRAME 46 IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPAIRED UPPER ANGLE PER SRM 53-35-11-FIG 229.Feb 26, 2007 · N420UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2007UALA00593Bulb · inoperativeMIDSHIP OVERHEAD EXIT SIGN FWD SIDE HAS 1 BULB, AFT FACE HAS 3 BULBS & AFT BULKHEAD OVERHEAD EXIT SIGN HAS 1 BULB INOPERATIVE. [5-1-07] REPLACED LAMPS OPS GOOD.Feb 25, 2007 · N409UA · Airbus A320232 · Emergency LightingSDR 2007UALA00594Lighter · inoperativeTHE 2L EXIT SIGN HAS 1 BULB, 2R EXIT SIGN HAS 4 BULBS & RIGHT OVERWING EXIT SIGN HAS 1 BULB INOPERATIVE. [5-1-07] REPLACED LAMPS OPS GOOD.Feb 25, 2007 · N409UA · Airbus A320232 · Emergency Lighting
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