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 2003UALA00451Bearing · leakingNUMBER 1 ENGINE OIL LEAK IN FLIGHT. QUANTITY DECREASED FROM 10.5 TO 3.5. SMOKE IN TAILPIPE AND TURBINE AREA AFTER SHUTDOWN. OIL LEAK CAUSED BY OIL LEAKING FROM NR 5 BEARING COMPARTMENT INTO HOT GASPATH AREA, GENERATING SMOKE AT ENGINE SHUTDOWN. LEAK CAUSEDMay 30, 2003 · N462UA · Airbus A320232 · Turbine Engine Oil SystemSDR 2003UALA00450Outflow Valve · malfunctionedAVIONICS VENT FAULT ECAM MESSAGE ILLUMINATED. FOUND SKIN AIR OUTLET VALVE MALFUNCTIONING AS REPORTED BY CFDS AND REPLACED SAME.May 24, 2003 · N481UA · Airbus A320232 · Pressure Regulator/Outflow ValveSDR AWXA200300584Control Unit · malfunctionedON TAKEOFF AT LAS EN ROUTE FOR CMH WITH THRUST SET TO FLEX, NR 2 WENT TO TOGA, AND NR 1 WENT TO FLEX OR REDUCED SETTING (10 O'CLOCK ON GAUGE). HAD ECAM MESSAGE NO FLEX TEMP SET, BUT FLEX WAS SET AT IDLE. UPPER ECAM POWER INDICATOR VARIED FROM TOGA TO CLIMB WIMay 23, 2003 · N650AW · Airbus A320232 · Fuel Controlling SystemSDR 2003UALA00390Cable · burnedFLIGHT DIVERTED DUE TO SMOKE ODOR IN THE CABIN. FOUND PIN 'A' OF CONNECTOR 400VCA SEVERELY BURNED, ALONG WITH RECEPTICLE. REPLACED IDG POWER CABLE AND PYLON POWER CABLE.Apr 23, 2003 · N463UA · Airbus A320232 · Electrical Power System WiringSDR 2003UALA00386Bracket · damagedRETURN TO FIELD DUE TO LANDING GEAR SHOCK ABSORBER FAULT INDICATIONS. REPLACED SENSOR BRACKET FOR LANDING GEAR EXTENSION SENSOR (24GA & 25GA) CAUSED BY FOD.Apr 20, 2003 · N497UA · Airbus A320232 · Landing Gear Position and WarningSDR 2003UALA00385Computer · malfunctionedDIVERSION DUE TO LOSS OF CABIN PRESSURE. AIRCRAFT EXPERIENCED DUAL BLEED SYSTEM FAILURE - LT BLEED LEAK & ENG 2 BLEED FAULT. THE BLEED MANAGEMENT COMPUTER WAS REPLACED FOR THE REPORTED BLEED LEAK (NO LEAKS WERE FOUND) AND THE FAN AIR THERMOSTAT WAS REPLACED FApr 17, 2003 · N475UA · Airbus A320232 · Cabin Pressure ControllerSDR 2003UALA00348Damper · leakingLANDED UNDER AMBER ALERT DUE TO A GREEN HYDRAULIC SYSTEM INDICATION AND LOSS OF QUANTITY. YAW DAMPER NR 1 WAS FOUND LEAKING. UNIT WAS REPLACED.Mar 28, 2003 · N422UA · Airbus A320232 · Autopilot SystemSDR 2003UALA00251Outflow Valve · failedRETURN TO FIELD DUE TO LOSS OF CABIN PRESSURE. REPLACED OUTFLOW VALVE.Mar 9, 2003 · N486UA · Airbus A320232 · Pressure Regulator/Outflow ValveSDR 2003UALA00233Pump · leakingECAM WARNING, GREEN HYDRAULIC LOW PRESSURE. NR 1 ENGINE HYDRAULIC PUMP LEAKING. REPLACED PUMP.Mar 3, 2003 · N426UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR 2003UALA00229Duct · damagedLEFT WING LEAK ECAM DISPLAYED. FOUND LEFT HAND CROSSBLEED DUCT DAMAGED AT HIGH PRESSURE GROUND CONNECTION. REPLACED DUCT.Feb 28, 2003 · N415UA · Airbus A320232 · Pneumatic Distribution SystemSDR 2003UALA00244Skin · dentedSKIN ON NR 1 LT SLAT LEADING EDGE IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLUSH SKIN REPAIR ON #1LH SLAT L/E.Feb 27, 2003 · N410UA · Airbus A320232 · Leading Edge DevicesSDR 2003UALA00179Wire · damagedINTERIOR EMERGENCY LIGHTS WILL NOT TEST, FOUND CIRCUIT BREAKER, H5 POPPED. RESET AND TRIED AGAIN NO HELP CIRCUIT BREAKER POPPED AGAIN. SUPPLEMENTAL DATA UPDATE FOUND WIRE PINCHED BETWEEN SEAT AND SEAT TRACK AT ROW 10. REMOVED DAMAGED WIRE AND SPLICED WIRE. Feb 15, 2003 · N430UA · Airbus A320232 · Light System WiringSDR 2003UALA00152Odor · detectedRETURNED TO FIELD DUE TO ELECTRICAL ODOR IN COCKPIT.Feb 6, 2003 · N439UA · Airbus A320232 · Air Distribution SystemSDR 2003UALA00155Warning System · activatedFLIGHTS ABORTED ON TAKEOFF ROLL DUE TO ECAM VENT SKIN VALVE FAULT.Feb 6, 2003 · N439UA · Airbus A320232 · Central WarningSDR 2003UALA00145Skin · damagedFUSELAGE SKIN DAMAGED AT FRAME 61 AT STRINGER 40L & STRINGER 41L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLERS AND DOUBLER.Feb 5, 2003 · N412UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2003UALA00123Fan · inoperativeVIBRATION FELT UNDER FORWARD GALLEY FLOOR AND FLIGHT DECK AND SMOKE ODOR IN FLIGHT DECK. REPLACED AVIONICS BLOWER FAN (18HQ).Jan 30, 2003 · N449UA · Airbus A320232 · Air Distribution FanSDR 2003UALA00130Frame · damagedDAMAGED FRAME SECTIONS AT FRAME 60 ON STRINGER 40 LT & STRINGER 41 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR ON FRAME.Jan 29, 2003 · N412UA · Airbus A320232 · Fuselage Main, FrameSDR 2003UALA00067Target · out of adjustCABIN EMERGENCY EXIT RIGHT AFT ECAM ILLUMINATED. ADJUSTED TARGET ON THE RIGHT AFT EMERGENCY EXIT DOOR.Jan 18, 2003 · N497UA · Airbus A320232 · Door Warning SystemSDR 2003UALA00062PipeFLIGHT DIVERTED DUE TO GREEN HYDRAULIC SYSTEM LOW. SUPPLEMENTAL DATA UPDATE FOUND LINE FROM HYD PRESSURE MODULE #1 ENG LEAKING AT FITTING. THE LINE WAS REPLACED. THE ENGINE PUMP CASE DRAIN AND HYDRAULIC CONTROL UNIT FILTERS WERE ALSO REPLACED PRECAJan 15, 2003 · N423UA · Airbus A320232 · Hydraulic Power SystemSDR 2003UALA00045Blade · fracturedCOMPRESSOR STALL NR 2 ENGINE. THROTTLED TO IDLE, ENGINE WAS NOT SHUTDOWN. ENGINE TEARDOWN REVEALED C6 BLADE FAILURE RESULTING FROM NICKED C6 VANE. BIRD INGESTION 17 DAYS PRIOR HAD BEEN BORESCOPED WITH NO FINDINGS IN FIRST THREE STAGES.Jan 13, 2003 · N404UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2003UALA00043Wire · chafedFLIGHT DIVERTED DUE TO ELECTRICAL ODOR IN THE REAR CABIN. REPLACED 9A READING LIGHT POWER SUPPLY, FOUND ARCING WHEN WIRES MOVED. SHOP FINDINGS, FOUND WIRE LEADS CHAFED IN POWER SUPPLY.Jan 11, 2003 · N434UA · Airbus A320232 · Light System WiringSDR 2003UALA00015Actuator · leakingLOSS OF GREEN HYDRAULIC SYSTEM INFLIGHT. GREEN HYD RSVR LOW LEVEL ECAM. REPLACED GREEN SYSTEM RETURN FILTER ELEMENT AND YAW DAMPER SERVO ACTUATOR. RESERVICED HYDRAULIC SYSTEM. THE EVENT REOCCURED ON THE NEXT FLIGHT. AN INTERNAL HYD LEAK CHECK AND A VERJan 4, 2003 · N450UA · Airbus A320232 · Hydraulic System, MainSDR 2003UALA00007Oil Cooler · leakingNOXIOUS ODOR IN CABIN AFTER TAKEOFF. SUBJECT APU OIL LEAK WAS CONFIRMED AT TEST. OIL COOLER WAS LEAKING SEVERELY (APPROX 1/2 QT. / MINUTE) FROM THE INLET SIDE OF THE PRESSURE REGULATOR. FURTHER DISASSEMBLY REVEALED SEVERAL DEEP VERTICAL SCRATCHES EVIDENT AJan 2, 2003 · N404UA · Airbus A320232 · APU Oil SystemSDR CA021230003Proximity Sensor · failed(CAN) FIVE CASES OF FLAP LOCK WITH NO MOVEMENT HAVE BEEN REPORTED SINCE 01 NOVEMBER. THERE WAS NO HARD FAULT AND FAULT COULD NOT BE DUPLICATED ON THE GROUND. ITEMS CHANGED OR TESTED INCLUDE THE SLAT FLAP CONTROL COMPUTER (SFCC), ASYMMETRY POSITION PICK OFF UNIDec 28, 2002 · Airbus A320232 · Trailing Edge Flap Control SystemSDR 2002UALA01902Pseu · failed'PSEU EXT LOAD EMER L' DISPLAYED DURING OPS TEST OF EMERGENCY ESCAPE LIGHTING FOR NR 3 SERVICE. REPLACED UNIT.Dec 26, 2002 · N457UA · Airbus A320232 · Emergency LightingSDR 2002UALA01889Skin · damagedCREASE UNDER LEFT HAND SIDE WINDOW. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIR DOUBLER.Dec 23, 2002 · N497UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2002UALA01890Engine · inoperativeRETURNED TO FIELD DUE TO NR 2 ENGINE INDICATION PROBLEM.Dec 23, 2002 · N432UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2002UALA01866Apu · malfunctionedRETURNED TO FIELD UNDER AMBER ALERT DUE TO APU AUTO SHUTDOWN.Dec 21, 2002 · N401UA · Airbus A320232 · APU Core EngineSDR 2002UALA01856Computer · malfunctionedFLIGHT CREW SUSPECTED FUEL LEAK INFLIGHT. SUPPLEMENTAL DATA UPDATE INSPECTED AIRPLANE AND FOUND NO FUEL LEAK. TRANSFERRED FUEL AND TAXI CHECKED AIRPLANE AND UNABLE TO FIND A FUEL LEAK. FUEL QUANTITY CHECKED AND FOUND WITHIN LIMITS BY COMPARING INDICATION ADec 13, 2002 · N410UA · Airbus A320232 · Fuel Quantity IndicatorSDR 2002UALA01848Fan · failedBURNING ELECTRICAL SMELL IN THE COCKPIT ACCOMPANIED BY AIRCRAFT VIBRATION. REPLACED AEVC BLOWER FAN, WHICH HAD EXPERIENCED BEARING FAILURE.Dec 12, 2002 · N463UA · Airbus A320232 · Air Distribution FanSDR YENA200232Connector · dirtyRTO AT CLOSE TO 80KTS -ECAM MESSAGE OF ENG 1 COMPRESSOR VANE. CFDS MESSAGE BOTH CHANNELS CH A/B VSV/HC/EEC1. T/S PER CAATS TASK 75-30-00-810-852. EXAMINED AND CLEANED CONNECTORS ON VSV ACTUATOR PER STEP 1 OF TASK & LUBED VSV UNISON RING PER AMM TASK. POWERDec 10, 2002 · N507JB · Airbus A320232 · Compressor Bleed ControlSDR 2002UALA01735Floorbeam · crackedCABIN FLOOR STRUCTURE FRAME 12+2, LBL 9 TRANSVERSE FLOORBEAM CRACKED FWD FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTION OF TRANSVERSE FLOORBEAM WITH 4EA NESTED ANGLES.Nov 16, 2002 · N467UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2002UALA01731Skin · damagedSKIN IS DAMAGED FROM STRINGER 41R TO 40L, FRAMES 58 THROUGH 61. MAJOR REPAIR ACCOMPLISHED. REPLACED DAMAGED SKIN SECTION.Nov 15, 2002 · N467UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA200228Service difficultyFlight #88, ONT to JFK, had fairly strong smell of burnt oil during inter stages of take off and climb out, Smell persisted and aircraft returned to ONT. Landing weight was aprx 155.500. Touchdown was smooth with minimun vertical speed. Preliminary report indiNov 14, 2002 · N520JB · Airbus A320232 · Powerplant SystemSDR 2002UALA01729Skin · damagedAIRCRAFT SUSTAINED DAMAGE TO AFT LWR BELLY SKIN BETWEEN FRAME 58 AND 64 BETWEEN STRINGER 41R AND 40L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKINS AND DOUBLER.Nov 14, 2002 · N467UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2002UALA01730Control Unit · malfunctionedFLIGHT MADE AN EMERGENCY LANDING DUE TO A FIRE WARNING IN THE AFT CARGO PIT. SMOKE DETECTOR CONTROL UNIT WAS REPLACED.Nov 14, 2002 · N417UA · Airbus A320232 · Smoke DetectionSDR 2002UALA01723Fitting · gougedAFT CARGO DOOR CUT OUT LOWER SILL 3RD FROM FRONT LUG HAS GOUGE AFT LOWER END. MAJOR REPAIR ACCOMPLISHED. 3RD FROM FRONT LOWER LUG BLENDED & ROTO PEENED.Nov 13, 2002 · N467UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR 2002UALA01718Duct · leakingFLIGHT DIVERTED DUE TO A LEFT WING BLEED MESSAGE. FOUND SOURCE OF LEAK AT HIGH PRESSURE GROUND AIR CONNECTION DUCT/CLAMP. REPLACED DUCT AND CLAMPS.Nov 12, 2002 · N435UA · Airbus A320232 · Pneumatic Distribution SystemSDR 2002UALA01715Ballast · overheatedFLIGHT DIVERTED DUE TO BURNING ODOR. REPLACED BALLAST AT SEAT ROWS 9 & 10ABC, BALLAST HAD ELECTRICAL ODOR .Nov 11, 2002 · N478UA · Airbus A320232 · Passenger Compartment LightingSDR 2002UALA01689Shear Tie · bentAFT PIT FRAME 58 AT STRINGER 41L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED NEW SHEAR TIE. REPLACED BENT SHEAR TIE.Nov 8, 2002 · N467UA · Airbus A320232 · Fuselage Main, StructureSDR 2002UALA01690Shear Tie · bentAFT PIT FRAME 59 AT STRINGER 42L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. NEW SHEAR TIE MANUFACTURED. REPLACED SHEAR TIE.Nov 8, 2002 · N467UA · Airbus A320232 · Fuselage Main, StructureSDR 2002UALA01691Shear Tie · bentAFT PIT FRAME 59 AT STRINGER 43L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. NEW SHEAR TIE MANUFACTURED. SHEAR TIE REPLACED.Nov 8, 2002 · N467UA · Airbus A320232 · Fuselage Main, StructureSDR 2002UALA01692Shear Tie · bentAFT PIT FRAME 59 AT STRINGER 41L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. NEW SHEAR TIE MANUFACTURED. SHEAR TIE REPLACED.Nov 8, 2002 · N467UA · Airbus A320232 · Fuselage Main, StructureSDR 2002UALA01631Fmc · malfunctionedFLIGHT DIVERTED DUE TO A FLIGHT CONTROL UNIT FAULT. UPPER ECAM MESSAGE AUTO FLIGHT "FCU 1 FAULT". REPLACED FLIGHT MANAGEMENT & GUIDANCE COMPUTER FMGC NR 1.Oct 29, 2002 · N452UA · Airbus A320232 · Flight Management Computing Hardware SystemSDR 2002UALA01632Skin · dentedDENT TO FUSELAGE APPROXIMATELY 1 FOOT BELOW FORWARD CUTOUT OF DOOR 2L. DAMAGE CONSISTS OF AN APPROXIMATE 2 INCH DIAMETER DENT. DENT IS DEEP BORDERING ON PUNCTURE. UNDERLYING RIB IS ALSO DENTED. MAJOR REPAIR ACCOMPLISHED, MANUFACTURED DOUBLER & INSTALLED FAOct 25, 2002 · N465UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2002UALA01607Sensor · damagedRETURNED TO FIELD DUE TO LEFT MAIN GEAR DOOR NOT UPLOCKED AFTER GEAR RETRACTION. SUPPLEMENTAL DATA UPDATE FOUND LH MAIN GEAR DOOR PROXIMITY SENSOR (29GA) AND CONNECTOR DAMAGED. REPLACED SENSOR AND CONNECTOR. ALSO DETERMINED LH MAIN LANDING GEAR UPLOCK ASSEMOct 18, 2002 · N405UA · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR 2002UALA01593Battery Pack · dischargedEMERGENCY LIGHTS FAIL SYSTEM TEST AT 3 SVC. REPLACED BATTERY PACK AT RT OVERWING EXIT.Oct 15, 2002 · N427UA · Airbus A320232 · Emergency LightingSDR 2002UALA01597Fire Loop · malfunctionedNUMBER 2 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING DESCENT WITH NO SECONDARY INDICATIONS. THE FIRE DETECTION UNIT WAS CHANGED.Oct 12, 2002 · N407UA · Airbus A320232 · Fire DetectionSDR 2002UALA01559Damper · leakingLANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. NR 1 YAW DAMPER WAS FOUND LEAKING HYDRAULIC FLUID. NEW YAW DAMPER ACTUATOR WAS INSTALLED AND OPERATIONAL CHECK WAS GOOD.Oct 10, 2002 · N448UA · Airbus A320232 · Autopilot SystemSDR 2002UALA01561Valve · leakingLOST GREEN HYDRAULIC PRESSURE AND QUANTITY ON TAXI OUT. RETURNED TO GATE UNDER TOW. SUPPLEMENTAL DATA UPDATE #2 MAIN LANDING GEAR DOOR GROUND OPENING BYPASS VALVE LEAKING. REPLACED VALVE ASSEMBLY.Oct 10, 2002 · N802UA · Airbus A319131 · Landing Gear Door Retract Section
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