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 2006UALA00670Sill · corrodedCORROSION ON L2 DOOR SILL AT FRAME 68. INSTALLED REINFORCING REPAIR ANGLE ON A PSE STRUCTURE.Apr 10, 2006 · N432UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2006UALA00663Sill · corrodedCORROSION ON R2 DOOR SILL AT NUT PLATE HOLE FWD OF FR 66. INSTALLED REINFORCING REPAIR ON A PSE STRUCTURE PER SRM 53-41-14.Apr 9, 2006 · N432UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2006UALA00662Sill · corrodedRIGHT AFT MED SILL BEAM HAS CORROSION IB OF AFT GIRT BAR FITTING. INSTALLED A REINFORCING REPAIR ON A PSE STRUCTURE PER SRM 53-41-14 FIG 201 PAR 5A.Apr 8, 2006 · N432UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2006UALA00627Compressor · stalledNR 1 ENG HAD A COMPRESSOR STALL DURING CLIMB AT APPROX 3000 FT AGL WITH A UPPER ECAM WARNING. UNDETERMINED CAUSE, TROUBLESHOOTING CHECKS RETURNED NO DEFECTS.Apr 1, 2006 · N406UA · Airbus A320232 · Turbine Engine Compressor SectionSDR AWXA200600596Bleed Valve · malfunctionedFLL - FLT 771 - CREW REPORTED THAT AT 5000 FT, NR 1 ENGINE STALLED, EPR ROLLED BACK TO IDLE AND CAPT PULLED THROTTLE BACK THEN WHEN ENG RECOVERED PUT THROTTLE BACK IN CLIMB DETENT. CREW RETURNED TO FLL AND LANDED W/O FURTHER EVENT. MX PERFORMED BOROSCOPE IAWMar 30, 2006 · N664AW · Airbus A320232 · Compressor Bleed ValveSDR 2006UALA00614Circuit Card · shortedAUDIO INOP IN ENTIRE CABIN, SOMETHING SHORTING OUT MUX BOX. MAIN MUX TRANSISTOR ON A4 CIRCUIT CARD FOUND BURNT. REPLACED MAIN MUX.Mar 30, 2006 · N459UA · Airbus A320232 · Communications SystemSDR 2006UALA00608Radome · bird strikeBIRD STRIKE AFTER TAKEOFF. IMPACT BELOW NOSE. RADAR ANTENNA MAKES GRINDING NOISE DURING SWEEP. RADOME DAMAGED.Mar 28, 2006 · N448UA · Airbus A320232 · Aerodynamic FairingsSDR AWXA200600569Bleed Valve · malfunctionedDURING CLIMB-OUT, APPROX 8500' REPORTED NR 1 ENG COMPRESSOR STALL WITH A LOUD BANG, FIREBALL, & EPR DROP TO NEARLY "0" THEN RECOVERY. REPORTED ECAM ANNUNCIATED "COMPRESSOR STALL" THEN CLEARED AS ENG RESUMED NORMAL OPS. RETURNED TO ATL. MX T/S IAW AIRBUS 320Mar 27, 2006 · N664AW · Airbus A320232 · Compressor Bleed ValveSDR 2006UALA00615Bottle · lowSLIDE AT DOOR 1R OUT OF GREEN BAND. REPLACED 1R SLIDE (MR25611-1035) WITH 1R SLIDE (MR25611-1191). SLIDES BEING REMOVED DUE TO LOW BOTTLE PRESSURE IS AN UNCOMMON EVENT. THE OPERATING ENVIRONMENT OF SLIDES SUCH AS VIBRATION, DOOR OPENING/CLOSING, CARTS IMPACMar 27, 2006 · N415UA · Airbus A320232 · Escape SlideSDR 2006UALA00616Battery · no testINT LOADS EMER R, FAILED SYSTEMS EMERGENCY TEST. REPLACED EPSU AND BATTERY AT 12WL. OPS CHECKED NORMAL.Mar 27, 2006 · N427UA · Airbus A320232 · Emergency LightingSDR 2006UALA00586Window · crackedRETURN TO FIELD DUE TO A CRACKED FLIGHT DECK WINDOW. SHOP FINDINGS INDICATE FOD DAMAGE. REPLACED WINDSHIELD.Mar 26, 2006 · N449UA · Airbus A320232 · Flight Compartment WindowsSDR 2006UALA00587Window · crackedFLIGHT DIVERTED DUE TO CRACKED WINDSHIELD AND POSSIBLE REVERSER PROBLEMS. SHOP FINDINGS INDICATE FOD DAMAGE. REPLACED WINDSHIELD.Mar 26, 2006 · N443UA · Airbus A320232 · Flight Compartment WindowsSDR 2006UALA00617Slide · low pressureDOOR 1 LEFT SLIDE PRESSURE GAUGE IS BELOW GREEN BAND. 1L SLIDE (MR25822-1005) WAS REPLACED WITH 1L SLIDE (MR25822-1002) IN DEN PER AMM 25-62-44. INSPECTION OF THE SLIDE INSTALLATION WAS ACCOMPLISHED. OPERATING ENVIRONMENT (VIBRATION, DOOR OPENING/CLOSING, CAMar 24, 2006 · N497UA · Airbus A320232 · Escape SlideSDR 2006UALA00556Floor Support · damagedTHE AFT CARGO PIT FLOOR CENTERLINE SUPPORT BEAM LOCATED JUST FWD OF FR56 HAS A HOLE DRILLED THRU THE UPPER CAP LEFT FLANGE. MAJOR REPAIR: INTERIM DOUBLER INSTALLED.Mar 23, 2006 · N463UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2006UALA00557Torque Box · damagedTHE AFT CARGO PIT THRESHOLD TORQUE BOX UPPER CAP AFT END INBOARD CORNER JUST FWD OF FR56 HAS A HOLE DRILLED THRU IT AND SEVERAL NICKS. MAJOR REPAIR: INTERIM REPAIR DOUBLER INSTALLED.Mar 23, 2006 · N463UA · Airbus A320232 · Fuselage Main, StructureSDR 2006UALA00565Light · inoperativeDOOR 1L SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED SLIDE, NO HELP. CONNECTOR 2871VC. FOUND DAMAGED, REPLACED. REINSTALLED DOOR 1R SLIDE, PER AMM 25-62-44. OPS CHECKED LIGHTS GOOD.Mar 23, 2006 · N428UA · Airbus A320232 · Escape SlideSDR 2006UALA00573Engine · surgesRTFL DUE TO NR 1 ENGINE POWER SURGE. ALL TROUBLESHOOTING CHECKS RETURN NO DEFECTS.Mar 23, 2006 · N486UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2006UALA00574Compressor · stalledENGINE NR 2 COMPRESSOR STALL - RTFL. ALL TROUBLE SHOOTING CHECKS RETURN NO DEFECTS.Mar 23, 2006 · N492UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2006UALA00544Bulb · inoperativeEMERGENCY LIGHTS AT SEATS 12 & 17 A,B,C HAVE ONE BULB INOP. RELAMPED. OPS CHECKED GOOD.Mar 22, 2006 · N466UA · Airbus A320232 · Emergency LightingSDR 2006UALA00512Valve · odorBURNED RUBBER ODOR IN CABIN REPORTED BY CREW. AFT TRIM AIR VALVE NOT OPERATING PROPERLY. REPLACED THE TRIM AIR VALVE.Mar 16, 2006 · N451UA · Airbus A320232 · Air Distribution SystemSDR 2006UALA00503Sill · corrodedR2 DOOR SILL HAS CORROSION AT NUT CLIP HOLE AT FRAME 66. TYPICAL UNDER FLOOR CORROSION. REPLACED FLOORBEAM ASSEMBLY.Mar 15, 2006 · N472UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2006UALA00509Control Unit · malfunctionedFWD CARGO PIT SMOKE WARNING ON FINAL. DISCHARGED AGENT 1 BOTTLE. ECAM WENT AWAY. FIRE DEPT ONSITE. TROULBESHOOTING PROCEDURES PERFORMED ON SMOKE DETECTION SYSTEM AND DISCOVERED SDCU CLASS II FAULT. REPLACED THE SDCU (10WQ) PCN:565-9019 PER AMM 26-17-34-40Mar 15, 2006 · N428UA · Airbus A320232 · Smoke DetectionSDR 2006UALA00510Connector · looseFLOOR EEL LIGHT INOP AT SEAT 1A. FOUND UNDER SEAT CONNECTOR DISCONNECTED. RESECURED UNDER SEAT CONNECTOR AND OPS CHECKED NORMAL.Mar 15, 2006 · N446UA · Airbus A320232 · Light System WiringSDR 2006UALA00478Radar · failedDUE TO WEATHER CONDITIONS AND LOSS OF WX RADAR, DECISION WAS MADE TO DIVERT THE FLIGHT. WEATHER RADAR TRANSCEIVER TESTS RETURNED "NO FAULT FOUND". TESTS FOUND WEATHER RADAR SCANNER HAD FAULTY AZ MOTOR AND THERMAL RESISTOR. REPLACED WEATHER RADAR TRANSCEIVEMar 13, 2006 · N438UA · Airbus A320232 · Weather Radar SystemSDR 2006UALA00426Blower · seizedBLOWER FAULT DISPLAYED ON UPPER ECAM SCREEN. BLOWER FAULT DISPLAYED ON UPPER ECAM SCREEN. MAINTENANCE CHECKED AND FOUND BLOWER FAN 20HQ SEIZED AND CIRCUIT BREAKER AD10 TRIPPED. REPLACED AEVC BLOWER FAN 20HQ (MR21211, 644-0089) PER MM 21-26-51. SYSTEM OP-CHMar 7, 2006 · N406UA · Airbus A320232 · Air Distribution FanSDR 2006UALA00418Power Supply · no testAFTER SLIDE INSPECTION, RAN EMERGENCY TEST ON THE PTP. MESSAGES -BATT EMER R- AND -INT LOADS EMER R- APPEARED. REPLACED POWER SUPPLY 12WL AND BATTERY PACK. EMERGENCY LIGHTS OPS CHECK OKAY.Mar 6, 2006 · N401UA · Airbus A320232 · Emergency LightingSDR 2006UALA00378Window · crackedFIRST OFFICER'S WINDOW CRACKED. FLIGHT DIVERTED. REPLACED NR 1 RT WINDOW PER AMM 56-11-11. NO FURTHER FINDINGS, OK FOR SERVICE.Mar 4, 2006 · N444UA · Airbus A320232 · Flight Compartment WindowsSDR 2006UALA00379Floorbeam · corrodedCORROSION AT STA Y1732 AND FRAME 66 OUTBOARD NUT PLATE HOLE. TYPICAL AFT GALLEY AREA CORROSION, REPLACED FLOORBEAM.Mar 4, 2006 · N470UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2006UALA00369Screw · shearedRETURN TO FIELD DUE TO A LOSS OF GREEN HYDRAULIC SYSTEM. LOSS GREEN HYD FLUID LEVEL. YELLOW AND BLUE SYS APPEARS OK. SECURED GREEN HYD SYS PER IRREG PROCEDURES. INSTALL GROUND SAFETY LOCKS PER AMM 32-00-00 AND TROUBLESHOOT. SOURCE OF GREEN HYD QTY LOSS. Mar 2, 2006 · N439UA · Airbus A320232 · Hydraulic System, MainSDR 2006UALA00370Lamp · inoperativeGROUND SCAN OF CIDS 1 DIRECTOR FAILS WITH : 115 VAC EMERG R EPSU, 115 VAC EMERG AFT L EPSU, EPSU UNIT R, EPSU UNIT AFT L, FAULT MSG'S. REPLACED AFT LEFT & MID RIGHT POWER SUPPLY'S AND BATTERY'S. RELAMPED RIGHT AFT OVERWING EMERGENCY EXIT LIGHT. OPS NORMAL.Mar 2, 2006 · N418UA · Airbus A320232 · Emergency LightingSDR 2006UALA00338Wire · brokenRETURN TO FIELD DUE TO NR 1 GENERATOR FAULT AND HISTORY ON NR 2 GENERATOR. SHOP FOUND BROKEN WIRE ON IDG CURRENT TRANSFORMER. NR 1 INTEGRATED DRIVE GENERATOR REPLACED. INSPECTED PYLON CONNECTORS FOR ARCING.Feb 25, 2006 · N445UA · Airbus A320232 · Electrical Power System WiringSDR 2006UALA00328Sill · damagedR2 DOOR SILL PLATE AT FRAME 68 APPROX RBL 50. APPLIED SIMPLE SRM DOUBLER ONTO DOOR SILL BEAM.Feb 22, 2006 · N429UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2006UALA00324Bearing · seizedDIVERTED DUE TO ODOR IN THE COCKPIT. FLIGHT CREW NOTICED ELECTRICAL ODOR IN CABIN. ECAM MESSAGE VENT EXTRACT FAULT, EXTRACT FAN SHOWING AMBER AND CREW SELECTED EXTRACT TO OVERRIDE. SUSPECT FAN/BEARING SEIZED UP. FOUND FAULT LIGHT ILLUMINATED ON EXTRACT FAFeb 21, 2006 · N495UA · Airbus A320232 · Air Distribution FanSDR 2006UALA00327Battery · no testCIDS MESSAGE: EPSU BATTERY AFT L WILL NOT CLEAR. REPLACED BATTERY PERFORMED SYSTEM TEST, TEST PASSED.Feb 21, 2006 · N465UA · Airbus A320232 · Emergency LightingSDR AWXA200600358Engine · malfunctionedPHX - ENGINE ANOMALY - CREW REPORTED A MOMENTARY ENGINE STALL ON THE NR 1 ENGINE AT ALTITUDE, WITH ASSOCIATED ECAM MESSAGE. MAINTENANCE INSPECTED AND BORESCOPED IAW AIRBUS TROUBLE SHOOTING MANUAL 71-00-00-810-803. FOUND STAGE 6 BLADE MISSING 50 PERCENT AND NFeb 20, 2006 · N665AW · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2006UALA00305Slide · no testAFTER CABIN EMERGENCY LIGHTS CHECK PER 3 SERVICE, MESSAGE -EXT LOADS AFT L- APPEARED ON CIDS CONTROL PANEL. ALTHOUGH THE EMERGENCY LIGHT TEST WAS CODED UNDER ATA-33, THE FAILURE OF THE TEST WAS DUE TO THE 2L (MR25614) SLIDE ASSY LIGHT SYSTEM. THE DEFECTIVE 2Feb 15, 2006 · N433UA · Airbus A320232 · Escape SlideSDR 2006UALA00281Battery · no testEPSU BATTERY EMER L DISPLAYED ON FAP AFTER EMERGENCY LIGHTS SYSTEM TEST. CYCLED FLIGHT DECK CIDS AND EMERGENCY LIGHT C-B'S. NO HELP. REPLACED BATTERY FOR LEFT AFT OVERWING EXIT. CIDS TESTS OK.Feb 14, 2006 · N471UA · Airbus A320232 · Emergency LightingSDR YENA200610Pressure Switch · malfunctionedOIL CLOG NR 1 ENG IN FLIGHT. REMOVED AND REPLACED NR 1 ENG SCAVENGE OIL FILTER ELEMENT IAW AMM 79-21-44 & ALSO REMOVED AND REPLACED NR 1 ENG SCAVENGE FILTER DIFF SWITCH IAW AMM 79-35-16, PERFORMED ENG IDLE RUN FAULTS CLEARED. A/C OK FOR SERVICE.Feb 13, 2006 · N612JB · Airbus A320232 · Engine Oil PressureSDR 2006UALA00276Skin · dentedEXTERNAL FUSELAGE SKIN DENTED IN TWO AREAS FWD OF DOOR 1L AT FRAMES 13 AND 14 AT LEVEL OF DOOR THRESHOLD. DENTS WERE FOUND IN ACCORDANCE WITH INSPECTIONS DRIVEN BY ALI ITEMS. REPAIR INSTALLED PER SRM 53-00-11 FIG 205 (DOUBLER OVER FRAME AND STRINGERS).Feb 13, 2006 · N482UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2006UALA00268Hydraulic System · leakingLANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. A/C TOWED TO GATE. GREEN SYS HYD QTY WENT TO ZERO. TROUBLESHOT GREEN SYS HYD LEAK. FOUND NR 2 ENG EDP PUMP LEAKING. FOUND PUMP HOUSING CRACKED. REPLCD PUMP. REPLACED LFT ENG HYD FILTER ASSY ANFeb 12, 2006 · N472UA · Airbus A320232 · Hydraulic System, MainSDR 2006UALA00269Apu · malfunctionedDIVERTED, APU AUTO SHUT DOWN & DEFERRED GENERATOR. APU 1660 HAS NO HISTORY SINCE INSTALLATION - FIRST HIT LAST SHOP VISIT 12APR05 NEW LOW OIL PRESSURE SWITCH & CONFIGURATION INSTALLED. APU HAS 661 HRS. TSHM & 890 CSHM. SFOEP CAPTURED UNIT & COMMUNICATED DFeb 12, 2006 · N471UA · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR 2006UALA00270Bulb · missingEMERGENCY FLOOD LIGHT ABOVE DOOR 2L HAS ONE BULB MISSING.Feb 12, 2006 · N412UA · Airbus A320232 · Emergency LightingSDR YENA200609Engine · stalledNR 1 ENG STALL DURING CLIMB THRU 4000 FT/250K. LOUD BANG-ROLLBACK. ENG RECOVERED NORMALLY. CONFIRMED NR 1 ENGINE STALL CAUSED BY WAKE TURBULANCE. NO EGT EXCEEDENCES NOTED. PERFORMED TSM TASK 71-00-10-710-019A, 71-00-00-810-808. ACCOMPLISHED BOROSCOPE, FUFeb 11, 2006 · N561JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2006UALA00261Power Supply · inoperativeAFT LEFT EMERGENCY LIGHT PWR SUPPLY INOPERATIVE.Feb 9, 2006 · N454UA · Airbus A320232 · Emergency LightingSDR 2006UALA00233Power Supply · no testDURING EEL TEST HALF OF ACFT SEATS LIGHTS FAILED TO ILLUMINATE. REPLACED AFT RT DOOR PWR SUPPLY AND BATTERY, LEFT MID BATTERY, SEAT EEL LIGHTS AT ROWS 18,20. OP CHECKS NORMALLY AT ALL SEATS.Feb 7, 2006 · N438UA · Airbus A320232 · Emergency LightingSDR 2006UALA00223Spring · brokenDOOR 2L FWD GIRT BAR FITTING SPRING LOADED LEVER HAS SPRING BROKEN. LEVER WILL NOT STAY UP. GIRT BAR SPRING FITTING CHANGED. THIS IS THE SUBJECT OF AD 2005-23-05 WHICH IS COVERED BY UNITED COA 405130. COA ASSIGNMENT TO BE MADE.Feb 4, 2006 · N411UA · Airbus A320232 · Escape SlideSDR 2006UALA00190Light · missingSEAT 10C HAS THE EMERGENCY PATHWAY LIGHT MISSING.Feb 3, 2006 · N448UA · Airbus A320232 · Emergency LightingSDR 2006UALA00191Light · no testEMERGENCY LIGHT TEST FAILS PER 3SVC.Feb 2, 2006 · N475UA · Airbus A320232 · Emergency LightingSDR 2006UALA00163Floor Support · corrodedSIX FLOOR SUPPORTS, AND FOUR FLOOR WEBS HAVE CORROSION FROM FRAMES 66 TO 70 AFT GALLEY FLOOR SUPPORTS. REPAIR ACCOMPLISHED PER SRM 51-72-11. SIX FLOOR SUPPORTS REPLACED BETWEEN FRAMES 66 AND 70. FOUR WEBS REPLACED BETWEEN FRAMES 69 AND 70.Jan 31, 2006 · N430UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2006UALA00162Lap Joint · damagedSKIN LAP DAMAGE JUST AFT OF AFT CARGO DOOR. RAMP CART HIT AIRCRAFT. REPAIR DOUBLER AND FILLER INSTALLED, REF SRM 53-00-11.Jan 30, 2006 · N424UA · Airbus A320232 · Fuselage Main, Plate/Skin
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