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 2004UALA00024Control Unit · malfunctionedFLIGHT DIVERTED DUE TO FWD CARGO SMOKE WARNING. *S/D* THE SMOKE DETECTOR CONTROL UNIT (SDCU, FIN 10WQ) WAS REPLACED.Jan 9, 2004 · N425UA · Airbus A320232 · Smoke DetectionSDR 2004UALA00020Slide · will not testLT OVERWING EXIT SLIDE DID NOT DEPLOY AUTOMATICALLY WHEN HATCH WAS REMOVED AND DID DEPLOY WHEN MANUAL OVERRIDE WAS ENGAGED. SLIDE BOTTLE ASSY INFLATION CABLE WAS FOUND KINKED INSIDE THE PULLEY OF THE WIRE CONTROL ASSY AND THE END OF CABLE WAS FOUND TWISTED. TJan 8, 2004 · N474UA · Airbus A320232 · Escape SlideSDR 2004UALA00014Damper · leakingAIRCRAFT LANDED UNDER AMBER ALERT DUE TO FAILURE OF GREEN HYDRAULIC SYSTEM. YAW DAMPER NR 1 WAS FOUND LEAKING. SUBSEQUENT REPLACEMENT WITH NEW YAW DAMPER AND OPS CHECK WERE ACCOMPLISHED WITH NO FURTHER ANOMALY.Jan 7, 2004 · N401UA · Airbus A320232 · Auto Flight SystemSDR 2004UALA00002Bypass Valve · leakingFLIGHT DIVERTED DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. FOUND NOSE LANDING GEAR BYPASS VALVE LEAKING, REPLACED BYPASS DOOR . ACCOMPLISHED GEAR SWING ALL GEAR OPERATIONS CHECK NORMAL.Jan 3, 2004 · N802UA · Airbus A319131 · Hydraulic System, MainSDR AWXA200301636Engine · malfunctionedPHX - ABORTED TAKEOFF - FLT 0075 - ON TAKEOFF AT PHX EN ROUTE FOR SEA WHEN THRUST LEVERS ADVANCED TO 1.05 EPR THE LT ENGINE WAS SLOWER TO SPOOL THAN RT ENGINE, NO ECAM WARNINGS OR CAUTIONS OF ANY KIND, REJECTED TAKEOFF. RECONFIGURED SETTINGS, TAXIED BACK TO RDec 29, 2003 · N655AW · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2003UALA00989Actuator · out of limitsSLATS FAILED TO DEPLOY, S-CTRL FAULT ILLUMINATED. THE TORQUE LIMITER OF THE LT NR 2 SLAT OUTBOARD ACTUATOR WAS FOUND TRIPPED. THE SLAT STOP TO FWD ROLLER DIMENSION WAS ALSO FOUND OUT OF LIMIT. REPLACEMENT OF THE FAULTY SLAT ACTUATOR AND SUBSEQUENT ADJUSTMENT Dec 29, 2003 · N421UA · Airbus A320232 · Leading Edge Slat ActuatorSDR 2003UALA00963Light · inoperativeROW 21 ABC ESCAPE PATCH EEL LIGHT IS INOPERATIVE. REPLACED EEL PATCH LIGHT.Dec 16, 2003 · N459UA · Airbus A320232 · Emergency LightingSDR 2003UALA00953Structure · damagedRT ELEVATOR MR55500-006 HAD 4 AREAS OF WATER INGRESS FOUND DURING ACP OF COA 40535. UPPER SURFACE HAD AN AREA 2.6 BY 1.3 INCH LOCATED 160.5 INCHES FROM I/B EDGE, AND 3.5 INCHES FROM T/E LWR SURFACE HAD 3 AREAS, ONE 4.0 BY 1.5 INCH FROM 113 INCHES FROM I/B EDGDec 13, 2003 · N406UA · Airbus A320232 · Elevator StructureSDR 2003UALA00954Structure · damagedLEFT ELEVATOR MR55501-006 HAD 2 AREAS OF WATER INGRESS FOUND DURING ACP OF COA 40535. ONE ON THE UPPER SURFACE 2.3 BY 1.4 INCH, 154 INCHES FROM THE I/B EDGE, AND 3.5 INCHES FROM THE T/E. ONE ON THE LWR SURFACE 2.9 BY 1.9 INCH, 139 INCHES FROM THE I/B EDGE ANDec 13, 2003 · N406UA · Airbus A320232 · Elevator StructureSDR 2003UALA00933Battery Pack · dischargedEMERGENCY LIGHT TEST FAILS. REPLACED BATTERY PACK 10WL.Dec 7, 2003 · N446UA · Airbus A320232 · Emergency LightingSDR 2003UALA00931Sill · corrodedR-2 DOOR SILL PLATE CORRODED. MAJOR REPAIR ACCOMPLISHED. AREA REPAIRED PER EVA IMC 30161 AND MAE EA 20-5341-13-A1060.Dec 3, 2003 · N405UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2003UALA00913Structure · contaminatedLT ELEVATOR HAD 3 AREAS OF WATER INGRESS. ALL AREAS ABOUT 1 INCH BY 1 INCH IN SIZE. TWO AREAS ON UPPER SURFACE: 1 LOCATED 98 INCHES FROM I/B EDGE & 2.5 INCHES FROM T/E, & 1 AT 177 INCHES FROM T/E & 10.5 INCHES FROM T/E, ONE AREA ON LWR SKIN 53 INCHES FROM INov 28, 2003 · N405UA · Airbus A320232 · Elevator, Plate/SkinSDR 2003UALA00900Skin · dentedLEFT FUSE SKIN IS CREASED & DENTED AT STA 359 (FR 23), STR 22L. MAJOR REPAIR ACCOMPLISHED. REPAIR ACCOMPLISHED PER MAE EA 47-5381-13-A1053 & UAL EVA IMC 30150.Nov 25, 2003 · N403UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2003UALA00901Skin · contaminatedRT ELEVATOR UPPER SKIN HAD 2 AREAS OF WATER INGRESS. MAJOR REPAIR ACCOMPLISHED. DAMAGE REPAIRED PER SRM 55-21-11, REP 5E, PG 226, FIG 205 SHEET 3 & 4.Nov 25, 2003 · N404UA · Airbus A320232 · Elevator, Plate/SkinSDR 2003UALA00902Skin · contaminatedLEFT ELEVATOR UPPER SKIN HAD ONE AREA OF WATER INGRESS. MAJOR REPAIR ACCOMPLISHED. DAMAGE REPAIRED PER SRM 55-21-11, REP 5E, PG 226, FIG 205, SHEET 3.Nov 25, 2003 · N404UA · Airbus A320232 · Elevator, Plate/SkinSDR 2003UALA00886Stringer · corrodedAFT PIT STRINGER 43 LT CORRODED BETWEEN FRAMES 56 & 57. MAJOR REPAIR ACCOMPLISHED. EXTRUDED STRINGER REPAIR.Nov 23, 2003 · N403UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2003UALA00887Skin · dentedFUSELAGE SKIN DENTED FROM FRAME 23 TO FRAME 24 BETWEEN STRINGERS 21L & 23L. DIMENSIONS ARE LENGTH 24.8 INCHES BY 10 INCHES HEIGHT WITH 5 SMALLER SHARP EDGES. MAJOR REPAIR ACCOMPLISHED. REPLACED STR 22L & FABRICATED EXTERNAL DOUBLER REPAIR UTILIZING SHIMS & Nov 23, 2003 · N403UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2003UALA00885Stringer · corrodedAFT CARGO COMPARTMENT STRINGER 42 LEFT CORRODED BETWEENN FRAMES 59 & 60. MAJOR REPAIR ACCOMPLISHED. EXTRUDED STRINGER SPLICE REPAIR.Nov 22, 2003 · N403UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2003UALA00881Structure · contaminatedLOWER PANEL OF LT ELEVATOR FOUND WITH WATER INGRESSION IN AREA APROX 1.5 BY 1.4 INCHES LOCATED APPROXIMATELY 2 IN FROM I/B EDGE AND 33 INCHES FROM TRAILING EDGE. MAJOR REPAIR ACCOMPLISHED. A REINFORCING REPAIR WAS ACCOMPLISHED PER SRM 55-21-11. REPAIR NR 5DNov 21, 2003 · N403UA · Airbus A320232 · Elevator StructureSDR YENA200338Actuator · failedENGINE ONE COMPRESSOR VANE ECAM ON TAKEOFF AT ABOUT 50 KTS. DID LOW SPEED RTO. REMOVED AND REPLACED NR 1 ENG VARIABLE STATOR ACTUATOR IAW AMM 75-32-41, AS PART OF TSM 75-30-00. PERFORMED TEST NR 11 (HIGH POWER ASSURANCE TEST) ON NR 1 ENGINE IAW 71-00-00-710Nov 17, 2003 · N507JB · Airbus A320232 · Engine Air Intake SystemSDR YENA200334Wire Harness · shortedTAKEOFF ABORTED DUE TO NR 1 ENG OVERHEAT ECAM, ABOUT 90 KT. PERFORMED TSM TASK 77-00-00-810-817. EIS(DMC1) REPORT SHOWED NR ENG 1 OVERTEMP. CHECKED REPORTS 4, 6, 10 ON AIDS. NO OVERTEMP NOTED. PERFORMED VISUAL INSP OF EGT JUNCTION BOX ON NR 1 ENG, NO DEFECNov 7, 2003 · N521JB · Airbus A320232 · Engine Temperature Indicating SystemSDR 2003UALA00844Dampener · leakingLANDED UNDER AMBER ALERT DUE TO FAILURE OF GREEN HYDRAULIC SYSTEM. YAW DAMPER NR 1 WAS FOUND LEAKING. SUBSEQUENT REPLACEMENT WITH NEW YAW DAMPER AND OPERATIONS CHECK WERE ACCOMPLISHED WITH NO FURTHER ANOMALY.Nov 7, 2003 · N410UA · Airbus A320232 · Hydraulic System, MainSDR AWXA200301374Engine · malfunctionedDURING CRUISE, A LOUD BANG HEARD & A/C SHUDDERED, FOLLOWED BY ECAM MESSAGE NR 2 ENG STALL & NR 2 ENG OIL FILTER CLOG MESSAGE. NR 2 ENG SHUTDOWN INFLT, DIVERTED, A/C LANDED SAFELY & TAXIED TO GATE UNDER OWN POWER. MAINT FOUND DEBRIS ON CHIP DETECTORS & IN OILNov 5, 2003 · N663AW · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2003UALA00821Smoke Detector · malfunctionedRETURN TO FIELD DUE FWD CARGO SMOKE ECAM MESSAGE. REPLACED FORWARD CARGO DETECTOR AS FAULTED BY CENTRALIZED SMOKE DETECTOR CONTROL UNIT. OPERATIONS CHECK NORMAL.Oct 29, 2003 · N409UA · Airbus A320232 · Smoke DetectionSDR 2003UALA00808Outflow Valve · malfunctionedRETURN TO FIELD DUE TO INABILITY TO PRESSURIZE AIRCRAFT. REPLACED FAULTY SKIN AIR OUTFLOW VALVE.Oct 28, 2003 · N402UA · Airbus A320232 · Pressure Regulator/Outflow ValveSDR 2003UALA00789Light · inoperativeROWS 2AB, 11ABC, 21ABC, 22ABC, 25ABC EELS ARE INOPERATIVE. REPLACED EEL LIGHTS. CHECKS OKAY.Oct 22, 2003 · N429UA · Airbus A320232 · Emergency LightingSDR 2003UALA00755Light · inoperativeROWS 21ABC AND 19ABC EEL LIGHTS ARE INOPERATIVE. REPLACED EEL LIGHTS.Oct 7, 2003 · N422UA · Airbus A320232 · Emergency LightingSDR 2003UALA00754Windshield · crackedAT FL370, .80 MACH, HEARD LOUD POP AND NOTED CAPT'S FWD WINDSCREEN HAD CRACKED MORE THAN .750 INCH OF OUTER PANEL SURFACE AREA. ALSO NOTED 7-8 INCH BURN MARK AT LOWER LEFT. BUS BAR ARCED CAUSING CRACK. WINDSHIELD WAS REPLACED.Oct 6, 2003 · N473UA · Airbus A320232 · Flight Compartment WindowsSDR 2003UALA00740Skin · damagedWATER INGRESS WAS FOUND AT 2 LOCATIONS ON THE RT ELEVATOR. DAMAGE ON UPPER SKIN IS 2.8 BY 2 INCHES AND IS 127 INCHES FROM IB EDGE AND 20 FROM TRAILING EDGE. MAJOR REPAIR ACCOMPLISHED. REPAIR DAMAGED AREAS PER SRM 55-21-11 TO ELIMINATE WATER INGRESSION.Oct 3, 2003 · N402UA · Airbus A320232 · Elevator, Plate/SkinSDR 2003UALA00741Structure · contaminatedINDICATIONS OF WATER INGRESS WERE FOUND IN 4 AREAS. ALL AREAS WERE APPROX 2.5 X 2 INCHES AND WERE APPROX 3 INCHES FROM THE TRAILING EDGE. THE FIRST AREA WAS ON THE LT UPPER SURFACE 102 INCHES FROM THE INBOARD EDGE. THE OTHER 3 AREAS WERE ON THE LT LOWER SUROct 3, 2003 · N402UA · Airbus A320232 · Elevator StructureSDR 2003UALA00734Structure · contaminated8 AREAS OF WATER INGRESS WERE FOUND ON THE RT ELEVATOR. UPPER SURFACE - 5 EACH AREAS 2 BY 2 INCHES, ALL 3.5 INCHES FWD OF THE TE, AND 132, 153.5, 1 61,168.8, 175 INCHES FROM IB EDGE. 3 EACH AREAS 2 BY 2 INCHES ON THE LWR SURFACE, ALL 3.5 INCHES FROM TE ANDSep 30, 2003 · N401UA · Airbus A320232 · Elevator StructureSDR 2003UALA00735Skin · contaminatedWATER INGRESSION FOUND AT THE FOLLOWING LOCATIONS: LT ELEVATOR UPPER SURFACE - 2 2" BY 2" AREAS, 3.5 INCHES FWD OF TRAILING EDGE, 160.8 AND 187.6 " FROM THE IB END. LWR SURFACE HAS 7 2' BY 2" AREAS, 3.5 " FWD OF TE AND 139.2, 146.2, 153.6, 160.7, 175.3, 181Sep 30, 2003 · N401UA · Airbus A320232 · Elevator StructureSDR 2003UALA00721Coffeemaker · failedRETURN TO FIELD DUE TO ELECTRICAL ODOR IN CABIN. REPLACED COFFEEMAKER M11 IN FORWARD GALLEY.Sep 26, 2003 · N431UA · Airbus A320232 · Air Distribution SystemSDR 2003UALA00699Light · inoperativeEEL LIGHTS ARE OUT AT 6ABC AND 17ABC. REPLACED BAD EEL LIGHTS.Sep 20, 2003 · N463UA · Airbus A320232 · Emergency LightingSDR AWXA200301061Engine · malfunctionedON TAKEOFF AT PHX EN ROUTE FOR BWI NR 2 ENGINE DID NOT PRODUCE FLEX TAKEOFF POWER, EPR ONLY REACHED 1.2, EPR OF 1.4 REQUIRED, REJECTED TAKEOFF AT 78 KTS. MAINTENANCE PERFORMED A HIGH POWER ASSURANCE TEST IAW T/C F5M71312, NO FAULTS WERE NOTED, NR 2 ENGINE EPR Sep 15, 2003 · N660AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR 2003UALA00666Switch · malfunctionedWITH NO SMOKING SWITCH IN THE ON POSITION, EMERGENGY EXIT SIGNS WERE ILLUMINATED DURING TAXI & FOR THE FIRST 30 MIN OF FLIGHT. FLIGHT ATTENDANT CALLED TO REPORT THAT ALL EMERGENCY EXIT SIGNS EXTINGUISHED AT SAME TIME WITH NO CHANGE IN COCKPIT SWITCH POSITION.Sep 2, 2003 · N467UA · Airbus A320232 · Emergency LightingSDR 2003UALA00625Filter · cloggedRETURN TO FIELD DUE TO AVIONICS VENT FAULT. AVIONICS COOLING SYSTEM FILTER REPLACED.Aug 13, 2003 · N429UA · Airbus A320232 · Air Distribution SystemSDR 2003UALA00617Actuator · failedABORTED TAKEOFF DUE TO NR 1 ENGINE N2 OVERSPEED AND EGT AMBER. DUE TO 2.5 BLEED ACTUATOR MALFUNCTION THE BLEED VALVE FAILED IN OPEN POSITON RESULTING IN HIGH EGT. DEN MAINTENANCE REPLACED THE 2.5 BLEED ACTUATOR AND LUBRICATED THE 2.5 BLEED VALVE ACTUATING MECAug 12, 2003 · N452UA · Airbus A320232 · Compressor Bleed ValveSDR 2003UALA00615Warning System · activatedECAM FWD CARGO DOOR AFTER TAKEOFF. ACCOMPLISHED OPERATIONAL CHECKS, NO FAULT MESSAGES INDICATED.Aug 11, 2003 · N801UA · Airbus A319131 · Door Warning SystemSDR 2003UALA00590Transformer · malfunctionedRETURN TO FIELD DUE TO LOSS OF BLUE HYDRAULIC PRESSURE. REPLACED CURRENT TRANSFORMER. 2706GJJul 26, 2003 · N426UA · Airbus A320232 · Hydraulic System, MainSDR 2003UALA00585Warning System · activatedRETURNED TO FIELD DUE TO NR 2 BLEED INOPERATIVE ECAM MESSAGE. AIRCRAFT RETURNED DUE TO NON-ICING RESTRICTIONS, NR 2 PRV REPLACED.Jul 22, 2003 · N430UA · Airbus A320232 · Pneumatic Distribution SystemSDR AWXA200300804Engine · overheatedDURING TAKEOFF AT LAS EN ROUTE FOR SEA, AT TAKEOFF POWER NR 1 ENGINE TEMPERATURE REACHED APPROXIMATELY 620 DEGREE'S FOR LESS THAN 2 SECONDS. FLIGHT CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE INLET AND EXHAUST SJul 14, 2003 · N657AW · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2003UALA00550Smoke Detector · malfunctionedFLIGHT DIVERTED DUE TO CARGO PIT SMOKE INDICATION. REPLACED FAILED SDCU (SMOKE DETECTOR CONTROL UNIT)Jul 10, 2003 · N418UA · Airbus A320232 · Smoke DetectionSDR 2003UALA00551Skin · lightning strikeLIGHTNING STRIKE DAMAGE AT FRAME 24, 3 INCHES BELOW STRINGER 36L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SOLID FASTENER.Jul 10, 2003 · N419UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2003UALA00519Transceiver · inoperativeRETURNED TO FIELD DUE TO INOPERATIVE WEATHER RADAR. INOPERATIVE WEATHER RADAR CAUSED BY FAULT IN RECEIVER/TRANSMITTER. RECEIVER/TRANSMITTER REPLACED. SHOP TEST CONFIRMED PREAMP FAILURE IN RECEIVER/TRANSMITTER.Jun 25, 2003 · N474UA · Airbus A320232 · Weather Radar SystemSDR 2003UALA00515Odor · detectedFLIGHT DIVERTED DUE TO REPORTS OF BURNING SMELL IN AFT GALLEY AREA. BURNED GUM WAS FOUND ON HOT PLATE. CLEANED HOT PLATE.Jun 21, 2003 · N419UA · Airbus A320232 · Air Distribution SystemSDR 2003UALA00512Engine · bird ingestionRETURN TO FIELD DUE TO NR 1 ENGINE COMPRESSOR STALL AND SUBSEQUENT SHUTDOWN. REPLACED ENGINE. DISASSEMBLY OF REMOVED ENGINE REVEALED FRACTURED 3RD STAGE BLADE AS ROOT CAUSE. FURTHER ANALYSIS OF BLADE FRACTURE AREA REVEALED BIRD DEBRIS AS MOST LIKELY SOURCE OJun 19, 2003 · N442UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2003UALA00501Latch · contaminatedFWD CARGO DOOR WARNING LIGHT CAME ON. DOOR HANDLE LATCH FOUND CONTAMINATED WITH DEBRIS OF AN UNKNOWN NATURE PREVENTING FULL SEATING. LATCH WAS CLEANED OF DEBRIS AND LUBRICATED.Jun 15, 2003 · N420UA · Airbus A320232 · Cargo/Baggage DoorsSDR 2003UALA00490Fmu · failedNR 1 ENGINE EXPERIENCED A FLAMEOUT. REPLACED FMU. REMOVED FMU DISASSEMBLED AT OEM, REVEALING A BUILD ERROR IN THE SPILL VALVE SLEEVE.Jun 11, 2003 · N437UA · Airbus A320232 · Fuel Controlling SystemSDR 2003UALA00473Seal · defectiveRETURN TO FIELD DUE TO ECAM RIGHT WING LEAK. WITH NR 1 BLEED SYSTEM ALREADY DEFERRED INOPERATIVE, AIRCRAFT EXPERIENCED LOSS OF BLEED SYSTEM NR 2 DUE TO RIGHT WING AIR LEAK. REPLACED SEALS AND COUPLING AT RIGHT PACK HEAT EXCHANGER. SUBSEQUENT MAINTENANCE INCJun 5, 2003 · N445UA · Airbus A320232 · Pneumatic Distribution System
Back to IAE V2527-A5