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 2004UALA00779B-Nut · looseLANDED UNDER AMBER ALERT DUE TO LOSS OF HYDRAULIC SYSTEM. *S/D* AIRCRAFT EXPERIENCED GREEN HYDRAULIC QUANTITY LOSS INFLIGHT. FOUND B-NUT LOOSE AT BRAKE PRESSURE ACCUMULATOR. TIGHTENED B-NUT, NO LEAKS.Aug 20, 2004 · N417UA · Airbus A320232 · Hydraulic System, MainSDR YENA200444Odor · detectedCABIN CREW AND PASSENGERS SMELLED A BURNING ODOR LIKE PLASTIC OR CABLES BURNING IN THE MIDDLE PORTION OF THE CABIN DURING OUR DESCENT. INFO NOTICE 2004-TO23TR COMPLIED WITH NO DEFECTS NOTED. INSPECTED CABIN, COCKPIT, CARGO AND AVIONICS COMPARTMENTS IAW 24-00-Aug 19, 2004 · N542JB · Airbus A320232 · Air Distribution SystemSDR 2004UALA00777Oxygen Mask · misriggedFLIGHT DIVERTED DUE TO LOW COCKPIT OXYGEN PRESSURE. MASK WAS NOT STORED PROPERLY IN THE STORAGE BOX. IMPROPER STORAGE CAN ENGAGE THE 02 TEST VALVE, WHICH WILL ALLOW THE O2 TO VENT. THE MASK IS NOW STORED PROPERLY.Aug 19, 2004 · N437UA · Airbus A320232 · Crew Oxygen SystemSDR 2004UALA00776Hydraulic System · lowFLT EXPERIENCED LOSS OF ALL QTY GREEN HYDRAULIC SYSTEM. DECLARED EMERGENCY & CONTINUED TO PLANNED DESTINATION. AIRCRAFT LOST GREEN HYDRAULIC QUANTITY INFLIGHT. LANDING GEAR EXTENDED VIA GRAVITY. OAKLAND SERVICED GREEN SYSTEM TO FULL. RAN ALL SYSTEMS, VERIAug 18, 2004 · N417UA · Airbus A320232 · Hydraulic System, MainSDR 2004UALA00766Pump · inoperativeLEFT TANK PUMP NR 2 ECAM, NR 1 PUMP WAS PREVIOUSLY DEFERRED. THE LEFT WING TANK NR 2 FUEL BOOST PUMP WAS INOPERATIVE. REPLACED LEFT WING TANK FUEL NR 2 FUEL BOOST PUMP. OPERATIONS CHECK NORMAL.Aug 14, 2004 · N451UA · Airbus A320232 · Fuel Boost PumpSDR 2004UALA00735Hydraulic System · inoperativeRETURNED TO FIELD DUE TO LOSS OF BLUE SYSTEM HYDRAULICS. FOUND BLUE HYDRAULIC SYSTEM ELECTRIC PUMP PRESSURE FLEX LINE CHAFED. REPLACED CHAFED LINE AE707414-2. OPERATIONS CHECK NORMAL.Aug 11, 2004 · N409UA · Airbus A320232 · Hydraulic System, MainSDR 2004UALA00730Proximity Switch · out of adjustRETURNED TO FIELD TO SECURE AN OPEN AVIONICS DOOR. ADJUSTED DOOR PROXIMITY SWITCH. NO OTHER HISTORY OR FUTURE PROBLEMS.Aug 7, 2004 · N461UA · Airbus A320232 · Door Warning SystemSDR 2004UALA00718Cover · dislodgedEVAC SLIDE ON DR2L COVER WILL NOT STAY ON. THE FWD RETAINING HOLE IN THE IN THE SLIDE FIBERGLASS PACKBOARD WAS DAMAGED. THE PROBABLE CAUSE FOR THE PACKBOARD HOLE GETTING DAMAGED IS IN-SERVICE IMPACT BY FOREIGN OBJECTS, SUCH AS SERVICE CARTS OR PERSONNEL/PASSAug 4, 2004 · N446UA · Airbus A320232 · Escape SlideSDR 2004UALA00708Warning Light · illuminatedGREEN RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. LOST NOSE WHEEL STEERING. TOWED TO GATE. FOUND GREEN SYSTEM YAW DAMPER SERVO ACTUATOR LEAKING. YAW DAMPER SERVO ACTUATOR WAS REPLACED.Aug 1, 2004 · N405UA · Airbus A320232 · Hydraulic System, MainSDR 2004UALA00709Warning Light · illuminatedRETURN TO FIELD DUE TO NOSE GEAR NOT LOCKED INDICATION. THE SENSOR FAILED. REPLACED NLG UP LOCK ACTUATING SENSOR 12GA AND PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION OF THE NOSE LANDING GEAR. OPERATIONS CHECK NORMAL.Aug 1, 2004 · N432UA · Airbus A320232 · Landing Gear Position and WarningSDR YENA200442Electrical Box · odorPASSENGER IN ROW 19 COMPLAINED OF A UNUSUAL SMELL, TURNED OFF LIVE TV AND SMELL DISAPPEARED. PERFORMED LIVE TV SYSTEM FUNCTION CHECKS AND INTEGRITY INSPECTION OF ROW 17 THRU 21. NO EVIDENCE OF JAMMING OR ELECTRICAL ODOR. CHECK PERFORMED IAW JB INFO NOTICE 2Jul 30, 2004 · N516JB · Airbus A320232 · Entertainment SystemSDR 2004UALA00700Light · inoperativeEEL LIGHTS ON SEATS 15ABC AND 24ABC ARE INOPERATIVE. REPLACED LIGHT ASSY. OPERATIONS CHECK NORMAL.Jul 28, 2004 · N427UA · Airbus A320232 · Emergency LightingSDR 2004UALA00699Warning Light · illuminatedRT EMERGENCY OVERWING EXIT WARNING LIGHT ILLUMINATED. RETURN TO FIELD. DEBRIS IN DOOR SEAL CAUSED LEAK. NO OTHER FINDINGS, CLEANED DOOR SEAL, REINSTALLED COVER. OPERATIONS CHECK NORMAL.Jul 27, 2004 · N445UA · Airbus A320232 · Door Warning SystemSDR 2004UALA00690Hydraulic System · failedRETURN TO FIELD DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. LEAKING BYPASS VALVE, LOSS OF HYDRAULIC FLUID. REPLACED THE NOSE LANDING GEAR DOOR OPENING BYPASS VALVE. OPERATIONS CHECK NORMAL.Jul 24, 2004 · N445UA · Airbus A320232 · Hydraulic System, MainSDR 2004UALA00688Landing Gear · malfunctionedMANUAL GEAR EXTENSION ON APPROACH. UNABLE TO OBTAIN THREE DOWN AND LOCKED INDICATION. LANDED WITHOUT INCIDENT. LANDING GEAR SAFETY VALVE FAILED. REPLACED THE SAFETY VALVE. OPERATIONS CHECK NORMAL.Jul 22, 2004 · N459UA · Airbus A320232 · Main Landing GearSDR 2004UALA00670Blade · wornFLIGHT DIVERTED UNDER AMBER ALERT DUE TO NR 1 ENGINE COMPRESSOR STALL. C6 ABRADABLE SEPERATED AND ERODED THE TIPS OF THE BLADES.Jul 18, 2004 · N459UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2004UALA00691Light · inoperativeEMERGENCY LIGHT TEST FAULTED EXT LOADS FWD L. THE EPSU FAULTED. REPLACED POWER SUPPLY. OPERATIONS CHECK NORMAL.Jul 16, 2004 · N428UA · Airbus A320232 · Emergency LightingSDR 2004UALA00661Frame · dentedFOUND 3 DENTS AT FRAME 74 AREA, 2 DENTS WERE AT STR 32L, 1 DENT AT STR 32R. FRAME 73 SURROUNDING THE JACKING STABILIZATION POINT ON THE AFT FUSELAGE. INSTALLED SKIN DOUBLER AND FRAME DOUBLER. INSTALLED NEW SHEAR CLIPS.Jul 8, 2004 · N495UA · Airbus A320232 · Fuselage Main, FrameSDR AWXA200400712Engine · wornON TAKEOFF AT PHX EN ROUTE FOR OAK AT 1.05 EPR APPLICATION OF FLEX POWER NR 1 ENGINE EGT INDICATOR FLASHED AMBER AT APPROXIMATELY 610 DEGREES, REJECTED TAKEOFF AT 40 KNOTS. MAINTENANCE PERFORMED A HPC & HOT SECTION BORESCOPE INSPECTION IAW TSM 77-00-00-810-83Jul 5, 2004 · N642AW · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2004UALA00643Landing Gear · inoperativeUNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. NLG STRUT SEALS WERE TORN. REPL ACED THE NLG STRUT SEALS. OPERATIONS CHECK NORMAL.Jul 5, 2004 · N478UA · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR 2004UALA00642Landing Gear · inoperativeUNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. NOSE GEAR WOULD NOT CENTER BECAUSE THE LGCIU FAILED. REASSEMBLED NOSE GEAR, OPERATIONS CHECK NORMAL.Jul 2, 2004 · N486UA · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR 2004UALA00635Odor · detectedUPON CLIMBOUT, F/A'S REPORTED ODOR AND BECAME NAUSEOUS. CREW RETURNED TO FIELD. RECIRCULATION FILTERS BLOCKED. REPLACED RECIRCULATION FILTERS - NO FURTHER DISCREPANCIES REPORTED.Jul 1, 2004 · N480UA · Airbus A320232 · Air Distribution SystemSDR 2004UALA00624Line · leakingRETURN TO FIELD UNDER AMBER ALERT DUE TO GREEN HYDRAULIC SYSTEM FAILURE. FOUND CUT SEAL ON HYDRAULIC LINE. REPLACED SEAL, FOUND GREEN RESERVOIR WITH THREE GALLONS OF HYD FLUID. RESET MANUAL GEAR EXTENSION. SERVICED SYSTEM TO FULL. RAN ALL HYDRAULIC PUMPS, NJun 29, 2004 · N822UA · Airbus A319131 · Hydraulic System, MainSDR 2004UALA00622Door Frame · deformedFWD LOWER E AND E DOOR FWD FRAME SECTION AND CENTER INTERCOSTAL JUST FWD OF DOOR HANDLE DEFORMED DUE TO IMPACT WITH TOW BAR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FRAME AND INTERCOSTAL REPLACED.Jun 28, 2004 · N419UA · Airbus A320232 · Fuselage Main, StructureSDR 2004UALA00617Stringer · corrodedAFT PIT STR 43L EXFOLIATED FROM FR 53 TO 59. SPLICED IN NEW STRINGER SECTION.Jun 26, 2004 · N419UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2004UALA00616Warning Light · illuminatedFLIGHT DIVERTED DUE TO HYDRAULIC (G RSVR LO LVL) ECAM MESSAGE. LOW LEVEL SWITCH FAILED. REPLACED THE LOW LEVEL SWITCH ON THE GREEN HYDRAULIC SYSTEM . OPERATIONS CHECK NORMAL.Jun 25, 2004 · N407UA · Airbus A320232 · Hydraulic Quantity SensorSDR 2004UALA00602Engine · failedON TAKEOFF ROLL, APPROX 20 TO 30 KTS, HEARD LOUD POP & RT YAW. TAKEOFF ABORTED. ANOTHER AIRPLANE REPORTED NR 2 ENGINE WAS ON FIRE. SHUTDOWN NR 2 ENGINE AND FIRED THE BOTTLE. 3RD STAGE COMPRESSOR BLADE FAILED DUE TO PREVIOUS FOD. REPLACED NR 2 ENGINE. OPERAJun 22, 2004 · N411UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2004UALA00599Structure · damagedFUSELAGE DAMAGE IN NOSE AREA AFT OF THE E&E DOOR. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & SUPPLATE REPAIRS.Jun 22, 2004 · N461UA · Airbus A320232 · Fuselage Main, StructureSDR 2004UALA00594Wire Harness · failedDURING FLIGHT RECEIVED LOST NR 1 BRAKE SYSTEM ECAM MSG. PRECAUTIONARY LANDING. AIRCRAFT TOWED TO GATE & THE PROBLEM WAS ADDRESSED. ON SUBSEQUENT FLIGHT THE SAME SCENARIO OCCURRED. WIRING HARNESS FAILED DUE TO SHORT TO GROUND FROM FRETTING. REPLACED WIRING Jun 20, 2004 · N466UA · Airbus A320232 · Landing Gear System WiringSDR 2004UALA00590Door · openDURING CLIMB CREW WAS UNABLE TO RETRACT FLAPS/SLATS. FUEL DOOR WAS FOUND OPEN AND BENT AROUND WING FIXED L/E PREVENTING SLAT FROM RETRACTING FULLY. FUEL DOOR REPLACED. LEADING EDGE REPAIRED. SLAT REPLACED.Jun 17, 2004 · N419UA · Airbus A320232 · Fluid Service DoorsSDR YENA200435Engine · failedAT FLT 250 EXPERIENCED A POP SHUTTER, ENGINE 2 ECAM STALL, F/A CALLED UP REPORTED SMOKE IN CABIN. ENGINE REIGNITED THEN SHUTDOWN 2 OIL FILTER CLOG. THEN ENG 2 FAULT SHUTDOWN ECAM. REPLACED NR 2 ENGINE IAW WORK CARD 710020-J1-2 DUE METAL IN OIL CHIP DETECTJun 16, 2004 · N533JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2004UALA00552Bottle · dischargedDOOR 1R ASSIST BOTTLE PRESSURE AT 1500 PSI. SERVICED DOOR BOTTLE TO 1800 PSI. OPERATIONS CHECK NORMAL.Jun 7, 2004 · N415UA · Airbus A320232 · Escape SlideSDR 2004UALA00546Check Valve · inoperativeRETURN TO FIELD UNDER AMBER ALERT DUE TO LOSS OF YELLOW HYDRAULICS. YELLOW HYDRAULIC SYSTEM PUMP CHECK VALVE FAILED. REPLACED CHECK VALVE.Jun 6, 2004 · N441UA · Airbus A320232 · Hydraulic System, MainSDR 2004UALA00547Rib · lightning strikeLEFT ELEVATOR RIB 10 WAS DAMAGED BY LIGHTNING. REPLACED RIB AND INSTALLED BLIND FASTENERS.Jun 4, 2004 · N433UA · Airbus A320232 · Elevator, Spar/RibSDR 2004UALA00548Rib · lightning strikeRIGHT ELEVATOR RIB 10 WAS DAMAGED BY LIGHTNING. REPLACED RIB AND INSTALLED BLIND FASTENERS.Jun 4, 2004 · N433UA · Airbus A320232 · Elevator, Spar/RibSDR 2004UALA00515Valve · leakingARRIVED UNDER AMBER ALERT DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM. FOUND LEAK MEASUREMENT VALVE LEAKING, REPLACED VALVE. OPERATIONS CHECK NORMAL.May 30, 2004 · N487UA · Airbus A320232 · Hydraulic System, MainSDR 2004UALA00514Ram Air Turb · inoperativeRAT DOES NOT WORK. WOULD NOT PRESSURIZE BLUE SYSTEM OR PROVIDE ELECTRICAL POWER. TEST BOX MALFUNCTIONED CAUSING ERONOUS INDICATIONS.May 28, 2004 · N416UA · Airbus A320232 · Hydraulic System, AuxiliarySDR 2004UALA00503Yaw Damper · leakingFLT LANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. YAW DAMPER NR 1 WAS FOUND LEAKING. UNIT WAS REPLACED. OPERATIONS CHECK NORMAL.May 26, 2004 · N402UA · Airbus A320232 · Hydraulic System, MainSDR 2004UALA00489Terminal Block · contaminatedDURING EMERGENCY ESCAPE PATH LIGHT CHECK, ROWS 1, 2, 3, 6 AND 7 FAILED TO ILLUMINATE. FOUND SMALL PARTICLES IN TERMINAL BLOCK - CLEANED, INSTALLED NEW POWER SUPPLY AND OPERATIONS CHECK NORMAL.May 24, 2004 · N496UA · Airbus A320232 · Light System WiringSDR 2004UALA00487Scavenge Port · obstructedAFTER SHUT DOWN EXPERIENCED TAILPIPE FIRE IN NR 1 ENGINE. NR 5 BEARING COMPARTMENT FLOODED DUE TO BLOCKED OIL SCAVENGE PORT. MAINTENANCE IS INITIATING A MAINTENANCE TASK TO REPLACE SUSPECT OIL TUBES DURING C-CHECKS.May 22, 2004 · N424UA · Airbus A320232 · Turbine Engine Oil SystemSDR 2004UALA00488Computer · malfunctionedDURING DESCENT ACFT LOST FACS & EXPERIENCED DOWNGRADED NAVIGATION. EMERGENCY DECLARED. AIRSPEED DISAGREE OCCURRED BETWEEN ADR 1 AND ADR 2. ADIRU NR 1 WAS REPLACED AND NR 2 AIRSPEED FAULT WAS PRESENT. SHOP FINDINGS FOUND THE UNIT REMOVED FROM POSITION 2 REMay 20, 2004 · N462UA · Airbus A320232 · Air Data ComputerSDR 2004UALA00475Epsu · inoperativeEMERGENCY LIGHTS FAIL TEST INT LOADS LEFT. REPLACED POWER SUPPLY UNIT. CABIN EMERGENCY LIGHTS NOW PASS.May 16, 2004 · N420UA · Airbus A320232 · Emergency LightingSDR 2004UALA00479Wire · brokenDURING CHECK OF EMERGENCY LIGHTS, PTP PANEL FAULTED MESSAGE EXT LOADS FWD LEFT. FOUND WIRE 3351-5109 BROKEN AT DOOR 1-LEFT HINGE POINT UNDER CANVESS CONDUIT. THIS IS THE WIRE TO POWER DOOR 1-LEFT SLIDE LIGHTS. REPAIRED BROKEN WIRE WITH E-BUTT SPLICE, SYS OPMay 16, 2004 · N410UA · Airbus A320232 · Light System WiringSDR 2004UALA00474Pressure Switch · failedLANDED UNDER AMBER ALERT DUE TO GREEN HYDRAULIC SYSTEM LOW PRESSURE MESSAGE. THE SAME MESSAGE CAUSED DIVERSION OF NEXT FLIGHT DUE TO EN ROUTE WEATHER CONDITIONS AND TRADEWINDS AT PLANNED DESTINATION. HYDRAULIC PUMP PRESSURE SWITCH FAILED. REPLACED NR 1 ENGINEMay 14, 2004 · N824UA · Airbus A319131 · Hydraulic Indicating SystemSDR 2004UALA00472Warning Light · false activationENG 1 AGENT 1 DISCHARGE LIGHT STAYS ILLUMINATED. FLIGHT DIVERTED. CLEANED BOTTLE, RESET FDU, TESTED OK.May 12, 2004 · N417UA · Airbus A320232 · Fire Bottle, FixedSDR 2004UALA00466Wire Harness · failedFLIGHT DIVERTED DUE TO A POSSIBLE FUEL LEAK. UNWANTED FUEL TRANSFER AND DEGRADED FUEL INDICATIONS CAUSED BY LEFT HAND WING INNER FUEL QUANTITY HARNESSES FAILURE. REPLACED LEFT HAND WING INNER FUEL QUANTITY HARNESSES. OPERATIONS CHECK NORMAL.May 11, 2004 · N448UA · Airbus A320232 · Fuel System WiringSDR 2004UALA00420Sensor · obstructedRETURN TO FIELD DUE TO CARGO DOOR LIGHT INDICATION. CARGO NET WAS POSITIONED WHERE IT INTERFERED WITH DOOR PROXIMITY SENSOR. REPOSITIONED CARGO NET. OPERATIONS CHECK NORMAL.May 2, 2004 · N427UA · Airbus A320232 · Door Warning SystemSDR 2004UALA00392Bpsu · failedON TAXI OUT, COMPLETE LOSS OF NOSE WHEEL STEERING AND BRAKING. ALSO EXPERIENCED UNCOMMANDED LEFT TURN. BRAKE SYSTEM CONTROL UNIT (BSCU) FAILED. BRAKE SYSTEM CONTROL UNIT (BSCU) REPLACED, NOSE WHEEL ANTISKID STEERING SWITCH REPLACED. OPERATIONS CHECK NORMAL.Apr 24, 2004 · N494UA · Airbus A320232 · Landing Gear Brake SystemSDR 2004UALA00362Tab · brokenRT ELEVATOR UPPER ANTI-ROTATION TAB AT THE HINGE OUTBOARD OF THE INBD ACTUATOR IS BROKEN. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE.Apr 17, 2004 · N453UA · Airbus A320232 · Elevator, Tab StructureSDR 2004UALA00363Skin · punctured1 INCH BY 2 INCH HOLE PUNCTURED IN SKIN BETWEEN FRAME 20-21 AND STRINGERS 28-29 ON R-H SIDE OF FWD FUSELAGE APPROX 5 INCHES FWD OF AFT AVIONICS ACCESS DOOR. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER. FABRICATED & INSTALLED EXTERNAL SKIN DOUBLER.Apr 16, 2004 · N453UA · Airbus A320232 · Fuselage Main, Plate/Skin
Back to IAE V2527-A5