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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2001UALA00360Beam · bentFORWARD CARGO DOOR AFT ACTUATOR MOUNT BEAM IS BENT. REPLACED ACTUATOR ATTACH BEAM. MAJOR REPAIR ACCOMPLISHED.SDR CA010426009Bracket · chafed(CAN) DURING THE REMOVAL OF THE PREVIOUSLY INSTALLED MONITOR FOR LSTA C-LSA95-037/D THE NR 2 CENTRE ISLE BRACKET ASSEMBLY FORWARD OUTBOARD SUPPORT LEG WAS FOUND TO BE CHAFED BY AIRCRAFT ELECTRICAL WIRING. THE BRACKET WAS REPLACED AS PER SONY TRANSCOM DRAWING 6SDR 2001UALA00346Controller · failedCABIN PRESSURIZATION PROBLEM. SUPPLEMENTAL DATA UPDATE FOUND RED CAPS INSTALLED ON STATIC PORTS ON BOTH PRESSURE CONTROLLERS. REMOVED CAPS, AND PERFORMED OPERATIONAL TEST OF THE PRESSURE CONTROL AND MONITORING SYSTEM. TESTED GOOD.SDR 2001UALA00347Accumulator · failedAILERON PROBLEM. SUPPLEMENTAL DATA UPDATE BLUE HYDRAULIC SYSTEM ACCUMULATOR FAILED INTERNAL LEAK TEST ON AIRCRAFT. REPLACED BLUE HYDRAULIC ACCUMULATOR (P/N SB209L1A1-1483), AND BLUE AILERON SERVOCONTROL (P/N 31073-110).SDR 2001UALA00294Engine · failedNR 2 ENGINE FIRE INDICATION. SUPPLEMENTAL DATA UPDATE FIRE INDICATION CAUSED BY LIBERATED HIGH PRESSURE COMPRESSOR (HPC) AIRFOIL, CAUSING SIGNIFICANT DOWNSTREAM DAMAGE IN ENGINE CORE GAS PATH. THE AFFECTED ENGINE WAS REMOVED AND REPLACED.SDR 2001UALA00254Oven · smokeSMOKE SMELL IN THE GALLEY. SUPPLEMENTAL DATA UPDATE OVENS R41 AND R42 WERE CLEANED OF DEBRIS. OPS CHECKED GOOD. NO FURTHER INCIDENTS.SDR 2001UALA00237Seal · leakingRIGHT WING AIR LEAK. SUPPLEMENTAL DATA UPDATE FOUND ENGINE BLEED AIR SUPPLY DUCT JOINT LEAK IN RIGHT HAND WING LEADING EDGE. REPLACED DETERIORATED SEAL. NO FURTHER FAULTS REPORTED.SDR 2001UALA00196Skin · damagedAFT FUSELAGE SKIN DAMAGED FROM STRINGER 40R TO STRINGER 41R. THIS IS CLASSIFIED AS A MAJOR REPAIR. *S/D* THE DAMAGED AREA WAS CUT OUT AND REPAIRED BY THE INSTALLATION OF A FILLER AND ONE EXTERNAL DOUBLER. AN INSPECTION WAS PERFORMED AND THE REPAIR WAS APPRSDR 2001UALA00174Transceiver · inoperativeWEATHER RADAR SYSTEM INOPERATIVE. SUPPLEMENTAL DATA UPDATE REPLACED WEATHER RADAR TRANSCEIVER AND CONTROL PANEL. NO FURTHER FAULTS OCCURED.SDR 2001UALA00160Pump · intermittentWING BOOST PUMP FAILURE. *S/D* THE NR 2 FUEL BOOST PUMP WAS GROUND CHECKED WITH NO FAULTS FOUND. THE PUMP HAS NO HISTORY OF BEING INOPERATIVE AND HAS FLOWN 2 FLIGHTS SINCE IT WAS CHECKED AS NORMAL.SDR 2001UALA00127Outflow Valve · erraticRETURNED TO THE FIELD DUE TO A CABIN PRESSURIZATION PROBLEM. *S/D* FOUND OUTFLOW VALVE OPERATION ERRATIC. REPLACED THE OUTFLOW VALVE. NO FURTHER DISCREPANCIES REPORTED.SDR 2001UALA00114Pump · overheatedBLUE SYSTEM HYDRAULICS ELECTRIC PUMP OVERHEATED. *S/D* REPLACED BLUE SYSTEM ELECTRIC HYDRAULIC PUMP. SYSTEM CHECKS NORMAL.SDR 2001UALA00098Valve · failedUNABLE TO MAINTAIN CABIN PRESSURIZATION. *S/D* THE SKIN AIR VALVE WAS REPLACED. NO FURTHER DISCREPANCIES REPORTED.SDR 20010213CW012Brake · malfunctionedDURING LANDING OF FLIGHTAT HONDURAS AIRPORT, CREW REPORTED AT SPEED OF 80 KNOTS, THE BRAKING BECAME VERY POOR, DUE TO THIS SITUATION, HIGH SPEED EXIT OF RUNWAY WAS PERFORMED, BUT LEFT MAIN LANDING GEAR GOT STUCK OUTSIDE OF TAXIWAY. NOTE: FIRST REVENUE FLIGHT SDR 2001UALA00071Controller · failedCABIN PRESSURE SYSTEMS 1 AND 2 FAILED IN FLIGHT. *S/D* CABIN PRESSURE CONTROLLERS NR 1 AND NR 2 WERE BOTH REPLACED. THERE HAVE BEEN NO CABIN PRESSURE ANOMALIES SINCE THE REPAIR WAS ACCOMPLISHED.SDR 2001UALA00055Light · inoperativeEMERGENCY ESCAPE PATH LIGHT AT SEAT 9C IS INOPERABLE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK OK.SDR 2001UALA00109Switch · malfunctionedLANDED UNDER AMBER DUE TO LOSS OF THE GREEN HYDRAULIC SYSTEM. *S/D* SERVICED GREEN SYSTEM TO FULL LEVEL AND RAN SYSTEM FOR 4 CONTINUOUS HOURS. DUE TO NO POSITIVE DISCREPANCIES FOUND WITH GREEN HYDRAULIC SYSTEM QUANTITY INDICATION, REPLACED THE RESERVOIR LOWSDR 2001UALA00022Power Supply · failedCABIN EMERGENCY LIGHT TEST FAILED. REPLACED POWER SUPPLY 13WL. OPERATIONAL CHECK GOOD.SDR 2001UALA00007Sensor · failedLEFT WINDSHIELD ANTI-ICE ELECTRONIC CENTRALIZED AIRCRAFT MONITORING CAME ON DURING CRUISE. POST FLIGHT REPORT SHOWS LEFT WIND SHIELD SENSOR FAULT. *S/D* FOUND BAD TEMPERATURE SENSOR AT LEFT WINDSHIELD. CONNECTED SPARE SENSOR. ALL CHECKS NORMAL.SDR 2001UALA00001Battery · inoperativeBATTERY FWD L MESSAGE WHEN TESTING THE EMERGENCY LIGHT SYSTEM FROM THE FORWARD ATTENDANT PANEL. *S/D* REPLACED BATTERY AT 1L (10WLA). SYSTEM OPERATION CHECKED NORMAL.SDR 20001227SH018Engine · leakingBZE - FLT 573 - DURING CRUISE, ENGINE NR 2 OIL QUANTITY INDICATOR BEGAN TO DROP DOWN. A LOW OIL QUANTITY LEVEL WARNING WAS SHOWN ON THE ECAM MONITOR. ENGINE WAS SHUT DOWN. AIRCRAFT DIVERTED ITS NORMAL FLIGHT TO BELIZE STATION FOR MAINTENANCE. AFTER AN UNEVSDR 20001227SH019Control Unit · smokePTY - FLT 622 - DURING CRUISE, COCKPIT CREW OBSERVED SMOKE COMING FROM THE FLIGHT CONTROL UNIT. AIRCRAFT RETURNED TO PANAMA STATION FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING AT PTY STATION, MAINTENANCE TECHS PERFORMED AN INSPECTION OF THE FCU SYSTEM, THE SDR 20010111CW003Bearing · failedDURING FLT, OIL QNTY IND BEGAN TO DROP, ENG NR2 . LOW OIL QNTY LEVEL WARN ON ECAN MON. ENGINE SHUT DWN. AC DIVERTED, MAIN TECH CKD, NR5 BRG TO BE CHANGED. BRG CHGD, ENG RUN UP, CK OK, AC RETURNED TO NORMAL OPERATION.SDR 20001227SH021Shutoff Valve · damagedHAV - FLT 622 - DURING CRUISE, AIRCRAFT LOST THE GREEN HYDRAULIC SYTEM QUANTITY, FLIGHT CREW PERFORMED ABNORMAL PROCEDURES FOR GREEN HYDRAULIC SYSTEM LOSS. THE AIRCRAFT RETURNED TO LA HAVANA, CUBA, FOR MAINTENANCE. AT LA HAVANA STATION, MAINTENANCE TECHS FOUSDR 2000UALA00790Pressure Switch · leakingUNUSUAL SMELL NOTED IN THE CABIN. SUPPLEMENTAL DATA UPDATE AFTER ACCOMPLISHMENT OF TROUBLESHOOTING PROCEDURES, FOUND APU OIL PRESSURE SWITCH LEAKING AND OIL BEING INGESTED INTO APU AIR INLET. SWITCH WAS REPLACED AND NO FURTHER SMELL NOTED.SDR 2000UALA00791Stringer · corrodedSTRINGER REPAIR REQUIRED DUE TO CORROSION FOUND BELOW THE AFT CARGO PIT FLOOR PANEL. SUPPLEMENTAL DATA UPDATE PITTING CORROSION AND CHEMICAL CORROSION WAS FOUND ON STRINGER 41 BETWEEN FRAME FR56 AND FRAME FR59 NEXT TO THE AFT CARGO MANUAL SELECTOR VALVE (2504MSDR 2000UALA00773Computer · malfunctionedALL FUEL QUANTITY INDICATORS SHOW AMBER DASH LINES ACROSS THE LAST TWO DIGITS. SUPPLEMENTAL DATA UPDATE THE FUEL QUANTITY PROCESSOR (FQIC) FAILED. REPLACED FQIC.SDR 2000UALA00709Power Supply · failedLEFT EMERGENCY UNIT MESSAGE SHOWN DURING EMERGENCY LIGHTS TEST. REPLACED EMERGENCY POWER SUPPLY UNIT AND THE BATTERY PACK . TEST OK.SDR 2000UALA00708Unknown · odorSMOKE SMELL WAS DETECTED BOTH IN THE COCKPIT AND THE AFT CABIN. SUPPLEMENTAL DATA UPDATE REPLACED RECIRCULATION FILTERS AND RAN OVENS, NO SMOKE SMELL NOTED. RAN PACKS WITH APU BLEED AND ENGINE BLEEDS, OPERATION WAS NORMAL, NO SMOKE OR ABNORMAL ODORS NOTED. NO SDR 2000UALA00697Coffeemaker · shortedELECTRICAL SMELL COMING FROM AFT GALLEY OVEN AREA. *S/D* COFFEEMAKER M42, P/N 11225-1 HAD AN INTERNAL ELECTRICAL FAILURE (WIRING MELTED) WHICH CAUSED AN ELECTRICAL SMELL IN THE AFT GALLEY. THIS COFFEEMAKER WAS REMOVED AND REPLACED. NO REPEAT A/C WRITE-UPS.SDR 2000UALA00696Unknown · odorCHEMICAL SMELL IN ENTIRE CABIN. *S/D* FOUND DEICING FLUID ON APU INLET DOOR AND INLET DUCT. CLEANED INLET DOOR, DUCT AND SURROUNDING AIRCRAFT SKIN. TEST RUN APU AND BOTH ENGINES, RAN BOTH AIR CONDITIONING PACKS, NO FURTHER ODOR NOTED.SDR 2000UALA00690Power Supply · failedEMERGENCY POWER SUPPLY OVER LEFT WING EXIT FAILED. REPLACED POWER SUPPLY.SDR 2000UALA00665Window · delaminatedOUTER LAMINATE WINDOW R-3 PEELED OFF IN FLIGHT. SUPPLEMENTAL DATA UPDATE INITIAL FINDINGS SHOW STRONG PROBABILITY THAT THE FAILURE OCCURRED DUE TO SUBSTANDARD INTERLAYER BONDING DUE TO A BAD PRIMER USED DURING PRODUCTION. REPLACED WINDOW.SDR 2000UALA00643Light · will not testEMERGENCY LIGHTS FAIL TEST FROM THE PROGRAMMING AND TEST PANEL. REPLACED RIGHT HAND OVERWING EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL TEST NORMAL.SDR CA001106019Control Unit · failed(CAN) FLT 581 CUN TO YYZ WAS ON CLIMB FROM CANCUN AIRPORT EN ROUTE TO YYZ WHEN AN ECAM MESSAGE ENG 1 REV PRESSURIZED APPEARED.THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO CANCUN AIRPORT. THE CAPTAIN CONTACTED MAINTENANCE OPERATIONS CONTROL FOR ASSISTASDR 2000UALA00609Battery · dischargedDURING EMERGENCY LIGHT TEST HAD BATT FWD L, UNIT FWD L AND COM FWD L MESSAGES ON THE CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) PANEL AT DOOR 1 LEFT. *S/D* REPLACED EMERGENCY POWER SUPPLY UNIT AT DOOR 1 LEFT.SDR 2000UALA00590Engine · failedENGINE SHUTDOWN DUE TO LOSS OF OIL PRESSURE. *S/D* AIRCRAFT HAD DEFECTIVE ENGINE REPLACED WITH SERVICEABLE ENGINE. ENGINE IS AT OUTSIDE VENDOR SHOP VISIT FOR DETERMINATION OF CAUSE. PRELIMINARY RESULTS SHOW FAILED GEAR IN THE MAIN GEARBOX.SDR CA001018013Clamp · failed(CAN) THE AIRCRAFT ON A RETURN FLIGHT FROM MBJ, EXPERIENCED A FADEC FAILURE (OVER HEAT) IN CLIMB. THE ENGINE WENT TO IDLE POWER, UNCOMMANDED. THE CAPTAIN ELECTED TO SHUT DOWN THE ENGINE AND RETURN TO MBJ. MAINTENANCE WAS DISPATCHED FROM YYZ TO MBJ. INSPECTION SDR 2000UALA00587Engine · cokedCREW REPORTS INFLIGHT SHUTDOWN OF NR 2 ENGINE. ALL ENGINEPARAMETERS ARE NORMAL EXCEPT OIL QUANTITY WAS ZERO. *S/D* AIRCRAFT HAD DEFECTIVE ENGINE REPLACED WITH SERVICEABLE ENGINE. OFF ENGINE IS AT OUTSIDE VENDOR SHOP VISIT FOR DETERMINATION OF CAUSE. PRELISDR 2000UALA00663Skin · puncturedDUE TO CONTACT WITH GROUND EQUIPMENT, THE VERTICAL STABILIZER LT SIDE SKIN SUSTAINED SCRATCH, PUNCTURE AND DELAMINATION DAMAGE FROM AFT OF S-2 TO S-4, AND OVER A 7 INCHES REGION UP FROM RIB 4. THE SKIN ATTACH AND BOUND FLANGES OF S-3 WERE DAMAGED ABOUT 6 INCHSDR 2000UALA00571Light · damagedEXIT LIGHT DAMAGED NEAR FLOOR AT DOOR 1 LEFT. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK OK.SDR 2000UALA00560Valve · failedAVIONICS VENT SKIN FAULT AFTER TAKEOFF. UNABLE TO PRESSURIZE AIRCRAFT. *S/D* BOTH SKIN AIR VALVES WERE REPLACED. PRESSURIZATION WORKED FINE AFTER REPLACEMENT OF SKIN AIR VALVES.SDR CA000928034Cowling · separated(CAN) ITEM NR 1 P/N 745-4000-501 COWL LT ITEM NR 2 P/N 745-4000-502 COWL RT AFTER TAKE OFF NR 1 ENGINE LT AND RT FAN COWLING SEPARATED FROM AIRCRAFT. - LT SLATS 1, 2, 3 DAMAGED.- LT UPPER WING SURFACE DAMAGED.SDR 2000UALA00550Light · inoperativeSEAT EMERGENCY ESCAPE PATH LIGHT INOPERABLE ROW 20. REPLACED SEAT LIGHT ASSY.SDR 2000UALA00541Unknown · odorELECTRICAL ODOR NOTED BY THE FLIGHT CREW. *S/D* ALL CABIN AND GALLEY ELECTRICALS TURNED ON, NO ODOR NOTED. PERFORMED STAGE 1 CLEAN OF THE ENVIRONMENTAL CONTROL SYSTEM. NO SMOKE OR ODOR NOTED IN CABIN AFTER CLEANING.SDR 2000UALA00515Switch · failedB-HYDRAULIC PUMP LOW PRESSURE INDICATION. *S/D* REPLACED PRESS SWITCH FOR BLUE ELECTRIC PUMP.SDR 2000UALA00498Servo · failedAIRFRAME VIBRATION NOTED. *S/D* THE CENTER RUDDER SERVO WAS REPLACED. NO ADDITIONAL PROBLEMS NOTED.SDR 2000UALA00486Oven · contaminatedGALLEY OVEN SMOKING. *S/D* CLEANED SPILL IN THE OVEN (P/N: 2710-0001-01) AND PERFORMED AN OPERATIONAL CHECK. NO FURTHER FAULTS WERE FOUND.SDR 2000UALA00485Bottle · dischargedDOOR 1 LEFT EMERGENCY ESCAPE RESERVOIR PRESSURE IS LOW. *S/D* SERVICED BOTTLE.SDR 2000UALA00469Oxygen Mask · malfunctionedCREW REPORTED THAT WHEN THEY PUT ON THEIR OXYGEN MASK, THEY LOST ALL PRESSURE. *S/D* TESTED OXYGEN MASKS. FOUND OPERATION NORMAL. SERVICED OXYGEN CYLINDER, TESTED ON/OFF SWITCH, MASKS OPERATED NORMALLY.
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