IAE V2524-A5

Service difficulty reports · 893

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 = 'V2524A5'
  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 SIMA200528304Sill · corrodedTHE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. REMOVED THE EXISTING LOWER SILL AND CLEANED THE AREA. INSTALLED SERVICEABLE SILL IAW SRM. (SW21200600333) (K)Oct 4, 2005 · N823AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200528303Floorbeam · corrodedTHE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF THE FORWARD DIGITAL TO REMOVE THE CORROSION. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (SW21200600333) (K)Oct 3, 2005 · N823AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200528302Clip · corrodedTHE BAGGAGE DOOR FWD LATERIAL (SHEAR CLIP) LOWER SECTION AT FRAME 65 WAS FOUND CORRODED. REMOVED A SECTION OF THE SHEAR CLIP TO REMOVE THE CORROSION. PREPARED A SHEAR CLIP. FABRICATED A SHEAR CLIP SPLICE DOUBLER. REPAIR DONE IAW SRM. (SW21200600333) (K)Oct 2, 2005 · N823AE · Emb EMB135KL · Fuselage, Door HingeSDR YENA200569Computer · inoperativeF/CTL SLATS LOCKED, WING TIP BRK ON. HAPPENED ON DECENT ABOUT 2 HRS INTO FLIGHT. AFTER EXTENSIVE TROUBLESHOOTING REPLACED NR 2 SFCC. AIRCRAFT HAS BEEN OPERATED ON AN EVALUTION FLIGHT, NO ECAM SYSTEM WARNINGS, CAUTIONS OR FLAP INDICATION ANOMALIES NOTED. SFSep 23, 2005 · N624JB · Airbus A320232 · Leading Edge Slat Control SystemSDR YENA200568Support Bracket · damagedAFTER TAKEOFF, THE NOSE LANDING GEAR (NLG) DID NOT RETRACT AND WHEELS WERE OFFSET AT A 90 DEGREE ANGLE. THE AIRCRAFT WAS DIVERTED, WHERE IT LANDED WITH THE NLG AT ABNORMAL STEERING ANGLE. PRILIMINARY BORESCOPE INSPECTION FINDINGS INDICATE NLG UPPER SUPPORT Sep 21, 2005 · N536JB · Airbus A320232 · Fuselage, Landing Gear Attach FittingsSDR DJFA2005140Transducer · intermittentTHE CREW REPORTED THAT THE AIRCRAFT BRAKING FAILED UPON EXITING THE RUNWAY AFTER LANDING. WHEN THE ANTI-SKID SYSTEM WAS TURNED OFF, NORMAL BRAKING POWER WAS RESTORED. MAINTENANCE REPLACED BOTH ANTI-SKID WIRING HARNESSES, AND DISCOVERED BOTH MAIN LANDING GEARSep 18, 2005 · N501CW · Cessna 560CESSNA · Brake Anti-Skid SectionSDR YENA200551Coffeemaker · odorF/A REPORTED ACRID BURNING ODOR (NO SMOKE) FROM FWD GALLEY. ODOR SUBSIDED WHEN COFFEE POTS TURNED OFF. PERFORMED TSM TASK 24-00-00-810-823, CHECKED PINS AND NOSE TERMINALS BEHIND COFFEEEMAKERS. OK TO CONTINUE. PRECAUTIONARY REPLACED BOTH COFFEE MAKERS (S/NAug 18, 2005 · N621JB · Airbus A320232 · Buffet/GalleysSDR AWXA200500836Eec · malfunctionedNR 1 ENG STALLED. CREW RETURNED TO LAS WITHOUT INCIDENT. ENG BORESCOPED & FERRIED BACK TO PHX. MX R & R NR 1 ENG 7TH STAGE BLEED VALVE, 7A & 7C BLEED VALVE, & 7C BLEED VALVE SOLENOID. LUBED VSV ON NR 1 ENG & R & R NR 1 EEC. PERFORMED POWER RUNS IAW TASK CJul 19, 2005 · N802AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR AWXA200500781Wire Harness · inoperativeDURING 4 DAY, FOUND THE EMERGENCY EXIT SEAT LIGHTS AT ROW 19ABC WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED WIRING HARNESS AT SEAT 19ABE IAW MFG MM 33-51-00. OPERATIONAL CHECKS WERE GOOD. (OPEN)Jul 6, 2005 · N638AW · Airbus A320232 · Light System WiringSDR AWXA200500772Fmu · failedDURING TAKE OFF AFTER APPLYING POWER, RECEIVED MULTIPLE WARNINGS ALONG WITH NR 1 ENGINE OVERSPEED. ACFT ABORTED TAKEOFF AT APPROX 80 KNOTS. TAXIED BACK TO GATE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT IAW MFG MANUAL. R & R NR 1 FMU IAW TASK CARD R5M73308. Jul 3, 2005 · N650AW · Airbus A320232 · Fuel Controlling SystemSDR YENA200535Electrical Box · failedDURING CRUSE, DETECTED ELECTRICAL BURNING ODOR ROW 23-25. AFTER TURNING THE TV MASTER OFF THE ODOR WENT AWAY. INSPECTED ROW 23-25 ABC DEF AND NO FAULT FOUND. REMOVED AND REPLACED LIVE TV SEB AT 24E AS PRECAUTIONARY IAW INFO NOTICE 2004-T023TR. OPS CHECK NOJun 28, 2005 · N523JB · Airbus A320232 · Entertainment SystemSDR AWXA200500722Engine · malfunctionedDURING TAKEOFF AT T/O POWER SETTING, APPROX 1.04 EPR, ACFT VEERED LEFT. REJECTED TAKEOFF BEFORE FURTHER POWER. NO ABNORMAL INDICATIONS NOTED BUT SUSPECTED NR 1 ENG LAGGED NR 2 ENG IN SPOOLING UP. RAN ENGINES UP TO 70 PERCENT N1 PER MAINTENANCE CONTROL. ALLJun 17, 2005 · N822AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR AWXA200500192Actuator · failedON TAKEOFF ROLL, AT APPROXIMATELY 60 KTS PILOTS RECEIVED ECAM MESSAGE DUAL VSV FAULT. REJECTED TAKEOFF, & RETURNED TO GATE. MX R & R NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, PERFORMED AN ENGINE RUN & THE OPS AND LEAK CHK GOOD. CONFFeb 10, 2005 · N817AW · Airbus A319132 · Compressor Bleed ControlSDR 05024804Ring Assembly · lack of lubeENGINE 1 COMPRESSOR VANE ECAM MESSAGE ON TAKEOFF. ABORTED TAKEOFF. MX RESECURED AND RESAFTIED LOOSE LINE ON VGV ACT. LUBRICATED VGV RING ARMS AND PERFORMED GND ENG RUNS WITH NO FURTHER DEFECTS NOTED AT THIS TIME IAW TSM CH 75-30-00.Jan 24, 2005 · N804BR · Airbus A319132 · Compressor Bleed ControlSDR AWXA200500020Fmu · malfunctionedBOS - ABORTED TAKEOFF - FLT 0068 - ON TAKEOFF AT BOS EN ROUTE FOR PHX RECEIVED ECAM INDICATIONS, ENG 1 FADEC, ENG 1 COMPRESSOR, ENG 1 FAIL, ENG 1 FUEL CTRL FAULT. REJECTED TAKEOFF AT LOW SPEED. MAINTENANCE TROUBLESHOT AND REPLACED NR 1 ENGINE FUEL METERING UJan 8, 2005 · N820AW · Airbus A319132 · Fuel Controlling SystemSDR AWXA200401176Actuator · failedON TAKEOFF AT EWR EN ROUTE TO PHX, RECEIVED ECAM MESSAGE "ENG 1 COMPRESSOR VANE FAILURE", REJECTED TAKEOFF AT 68 KTS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, PERFORMED HIGH POWER ASSURANCE TEST, NOct 28, 2004 · N820AW · Airbus A319132 · Compressor Bleed ControlSDR AWXA200401131Wire Harness · brokenDURING E-01 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT HARNESS AT SEAT ROW 4 LT IAW AMM 33-51-18-04, OPERATIONAL CHECK WAS GOOD.Oct 16, 2004 · N656AW · Airbus A320232 · Light System WiringSDR AWXA200401095Flashlight · inoperativeEMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE L-1 DOOR EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Oct 4, 2004 · N825AW · Airbus A319132 · Emergency EquipmentSDR AWXA200401081Epsu · failedDURING 4-DAY CHECK RT OVER WING EMERGENCY POWER SUPPLY UNIT (EPSU) AND AFT ESPU FAILED EMERGENCY TEST. MAINTENANCE REMOVED AND REPLACED RT OVER WING EPSU (12WL) AND AFT EPSU (13WL) AND BATTERY PACKS; OPERATIONAL CHECK WAS GOOD. PART NAME; EPSU, MFG; DIEHL GSep 30, 2004 · N802AW · Airbus A319132 · Emergency LightingSDR 04FDEA02725Bleed Valve · malfunctionedBLEED VALVE 1 FAULTED AFTER TAKEOFF. NO RESET, RAN NR 1 ENG AT THE GATE. NO FAULTS NOTED. RAN ENGS AT T/O POWER FOR 5 MIN. NO FAULTS NOTED. INTERROGATED PNEU SYST CONTROLLERS. NO FAULTS STORE IN MEMORY FOR ANY FLIGHT LEG, STILL T/S. TALKED TO MOCC. SISep 17, 2004 · N716FD · Airbus A300B4622 · Compressor Bleed ValveSDR AWXA200400974Packing · leakingDIVERSION, ENROUTE, RECEIVED ECAM MESSAGE FOR YELLOW HYDRAULIC SYSTEM LOW LEVEL INDICATION, DIVERTED FOR REPAIR. MAINTENANCE FOUND FLUID LEAKING FROM AN O-RING AT THE YELLOW HYDRAULIC SYSTEM BRAKE SELECTOR VALVE, REPLACED O-RING AND PERFORMED LEAK CHECK IAW ASep 3, 2004 · N821AW · Airbus A319132 · Hydraulic System, AuxiliarySDR AWXA200400943Battery · dischargedDURING P-06 CHECK EMERGENCY LIGHT SYSTEM TEST THE SYSTEM OK LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LT AND RT OVER WING BATTERY PACKS AT EMERGENCY POWER SUPPLY UNITS 11WL AND 12WL, OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM WAS GOOD.Aug 22, 2004 · N823AW · Airbus A319132 · Emergency LightingSDR AWXA200400942Wire · brokenDURING P-05 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE FOUND A GROUND WIRE AT LIGHT ASSEMBLY CONNECTOR SEAT ROW 7 LT BROKEN, RE-TERMINATED GROUND WIRE, EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD.Aug 16, 2004 · N650AW · Airbus A320232 · Light System WiringSDR YENA200439Electrical Box · smokeFLT ATT REPORTED SMELLING SMOKE IN CABIN DURING APPROACH. PERFORMED INFO NOTICE 2004-TO23TR NO DISCREPANCY NOTICED. LIVE TV SYTEM FULLY OPERATIONAL. REMOVED AND REPLACED SEB AT 16E AS PRECAUTIONARY IAW INFO NOTICE. INSPECTED SEATS 14-18DEF.Jul 20, 2004 · N523JB · Airbus A320232 · Entertainment SystemSDR RJEF598HAAWarning Light · illuminatedDURING CRUISE, PILOT REPORTED INDICATION OF AFT AVIONICS DOOR. THE AC WAS DIVERTED. AFTER LANDING, INSPECTION OF THE DOOR WAS PERFORMED AND FOUND IT PROPERLY CLOSED AND INDICATIONS WERE NORMAL. ALSO PERFORMED PROXIMITY SENSORS CLEANING AND INSTALLATION OF TJul 15, 2004 · N477TA · Airbus A319132 · Door Warning SystemSDR RJE2004F00000Wheel · damagedDURING TRANSIT CHECK OF FLIGHT 390 AT TGU STATION, IT WAS FOUND ONE TIRED WITHOUT PRESSURE AND ANOTHER ONE WITH A CUT IN THE SHOULDER. AIRCRAFT REMAINS ON GROUND FOR MAINTENANCE AT TGU STATION. TECHS PERFORMED INSPECTION IAW AMM 05-51-15, AND FOUND MAIN WHEEJun 3, 2004 · N477TA · Airbus A319132 · Wheel/Ski/FloatSDR AWXA200400342Scavenge Pump · leakingBUR - TAILPIPE FIRE - FLT 0476 - NR 1 ENGINE HAD TAILPIPE FIRE AT ENGINE SHUTDOWN AFTER 5 MIN COOL DOWN. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE OIL SCAVENGE PUMP IAW T/C R5M79301. RAN ENGINE AT IDLE, NO TAILPIPE FIRE AT SHUTDOWN, LEAK CHECK OF PUMP WASApr 2, 2004 · N801AW · Airbus A319132 · Turbine Engine Oil SystemSDR AWXA200400312Bleed Valve · inoperativeEN ROUTE FROM PHX TO SFO AT FL 350 DURING MODERATE TURBULENCE ECAM INDICATED NR 2 ENG STALL & FLT ATTENDANT REPORTED HEARING A LOUD THUMP. PERFORMED FCOM 3 PROCEDURE, ENG OPS NORMAL, DID NOT DECLARE EMERGENCY. MAINT COMPLIED WITH AMM 72-22-49, EEC TEST & VISMar 27, 2004 · N818AW · Airbus A319132 · Compressor Bleed ValveSDR RYNA50885Engine · failedDURING TAKEOFF ROLL OUT, A LOUD BANG SHUDDERED THE AIRCRAFT ACCOMPANIED BY AN IMMEDIATE AND EXCESSIVE YAW TO THE LEFT OF CENTER LINE. TAKEOFF WAS ABORTED AND AIRCRAFT TAXIED CLEAR OF THE ACTIVE RUNWAY WITHOUT INCIDENT.Mar 3, 2004 · N381LF · Airbus A320232 · Engine (Turbine/Turboprop)SDR AWXA200300970Engine · malfunctionedON TAKEOFF ROLL AT ORD EN ROUTE FOR PHX RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 60 KTS. MAINTENANCE INSPECTED ENGINE INLET AREA, NO DAMAGE NOTED. PERFORMED FULL AUTHORITY DIGITAL ENGINE CONTROL TEST ON THE NR 2 ENGINE PER TSM 75-30-0Aug 21, 2003 · N814AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR 2003F00534Engine · making metalSAL - FLT 531 - FLIGHT CREW REPORTED ENGINE NR 2 N1 VIBRATION WHILE ARRIVING AT SAL STATION. TECHNICIANS PERFORMED INSPECTION OF ENGINE NR 2, AND FOUND SOME METALLIC DEBRIS AT THE EXHAUST AREA AND THE FAN BLADES COULD NOT BE TURNED BY HAND. ENGINE NR 2 ENGINAug 3, 2003 · N455TA · Airbus A320233 · Engine (Turbine/Turboprop)SDR AWXA200300437Engine · failedEN ROUTE FROM PHX TO DCA AT FL 370 A LOUD BANG WAS HEARD COMING FROM NR 1 ENGINE, IMMEDIATELY FOLLOWED BY A CLOGGED OIL MESSAGE, ALL OTHER PARAMETERS NORMAL. CREW CONTACTED MOC AND WERE TOLD TO MONITOR ENGINE. APPROXIMATELY 15 MINUTES LATER TWO MORE BANGS WEREApr 27, 2003 · N828AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR AWXA200201048Eec · failedFLT 0186 - DURING TAKEOFF ROLL AT PHX EN ROUTE FOR SAN, AT 80 KTS NR 1 ENGINE DID NOT REACH TAKEOFF EPR; TARGET WAS 1.399; AT 1.25 WITH STRONG DIRECTIONAL PULL WHEN ABORTED TAKEOFF. MAINTENANCE PERFORMED A FULL AUTHORITY DIGITAL ENGINE CONTROL AND ELECTRONIC EOct 24, 2002 · N825AW · Airbus A319132 · Fuel Controlling SystemSDR AWXA200200774Bearing · failedSTL - DIVERSION - FLT 0695 - EN ROUTE FROM CMH TO LAX THE NR 2 ENGINE COMPRESSOR STALLED TWO TIMES AT FL 370, EGT RED LINED AND OIL PRESSURE PEAKED AT 330 PSI THEN SLOWLY DROPPED TO -0- PSI, SHUTDOWN ENGINE PER ECAM INSTRUCTIONS AND DIVERTED TO STL. ENGINE ISAug 18, 2002 · N822AW · Airbus A319132 · Turbine Engine Compressor SectionSDR AWXA200200561Line · looseFLT 841 - ENROUTE FROM PHX TO RDU THE NR 1 ENGINE INDICATED LOW OIL QUANTITY, ENGINE WAS LOSING OIL AT A RATE OF 1 QUART OF OIL IN 5 MINUTES, DIVERTED AND LANDED AT BNA, UPON ARRIVAL AT GATE ENGINE HAD 7.5 QUARTS OF OIL REMAINING. MAINTENANCE INSPECTED THE Jun 23, 2002 · N804AW · Airbus A319132 · Turbine Engine Oil SystemSDR AWXA200200425Restrictor Valve · obstructedT/O ROLL APPROX 90 KTS, CAPT NOTICED NR 2 ENG HIGH OIL PRESSURE IND 332 PSI. AIRCRAFT RETURNED. MX REPLACED NR 2 ENG PRESSURE PUMP, NR 4 BEARING SCAVENGE VALVE & OIL FILTERS. PROBLEM PERSISTS, BUT OIL PRESSURE REDUCED TO ACCEPTABLE LIMITS FOR FERRY TO PHX. May 14, 2002 · N803AW · Airbus A319132 · Engine Oil Distribution (Airframe Furnished)SDR 2002F00365Engine · malfunctionedDURING CLIMB OF THE FLIGHT LR623, EGT ENGINE NR 2 WENT OUT OF LIMITS, AFTER THE CREW PERFORMED ALL NECESSARY CHECKLIST THE AIRCRAFT WAS RETURNED TO TORONTO AIRPORT. AT TORONTO STATION, THE AIRCRAFT REMAINS ON GROUND FOR MAINTENANCE CHECKS AND FURTHER DISPOSITMar 25, 2002 · N472TA · Airbus A319132 · Engine (Turbine/Turboprop)SDR AWXA200100565Bearing · fracturedEN ROUTE ECAM MESSAGE FOR NR 1 ENG OIL FILTER CLOG APPEARED, FOLLOWED BY NR 1 ENG OIL PRESSURE RISE INTO THE RED AREA, NR 1 ENG HIGH VIBRATION & SMOKE IN THE CABIN. EXECUTED EMERGENCY DESCENT & LANDED AT MAF. MX REMOVED MAIN OIL FILTER & CHIP DETECTORS AND FNov 2, 2001 · N814AW · Airbus A319132 · Turbine Engine Compressor SectionSDR AWXA0002166Engine · failedDEN - IN FLIGHT SHUTDOWN / UNSCHEDULED LANDING - FLT 534 - ORIG OPEN - EN ROUTE FROM PHX TO CLE THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND WENT TO IDLE, UPPER ECAM DISPLAYED ENG OIL FILTER (1) AND WAS SHUT DOWN. THE FLIGHT WAS DIVERTED TO DEN AND ON DAug 16, 2001 · N818AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR AWXA0001499Eec · malfunctionedOMA - DIVERTED FLIGHT - 3/15/01 - EN ROUTE FROM MKE TO PHX AT CRUISE FL 350 CREW GOT ECAM MSG, ENG 2 SENSOR FAULT; CREW ADVD MAINTENANCE AND DISPATCH AND FOLLOWED ECAM PROCEDURES; MADE PRECAUTIONARY LANDING IN OMA. OMA MAINTENANCE BLEW OUT THE NR2 ENG PB LINEMar 19, 2001 · N807AW · Airbus A319132 · Fuel Control/Turbine EnginesSDR AWXA0001481Relay · faultyPHX - AIR TURNBACK - 3/1/01 - THE CREW GOT A ENG NR 2 EPR MODE FAULT, N1 MODE XX AND RETURNED TO PHX. IN PHX DURING TROUBLESHOOTING OF NR 2 FADEC, HAD P2T2 SENSE/RELAY BOX/HC2 MESSAGE. INSPECTED THE FADEC WIRE HARNESS AND CONNECTOR FOR SECURITY AND NO DISCREMar 7, 2001 · N807AW · Airbus A319132 · Engine Pressure Ratio (EPR)SDR AWXA0001256Outflow Valve · malfunctionedCMH-DIVERTED FLIGHT- ON CLIMBOUT THE CABIN PRESSURE RATE FLUCTUATED FROM -600 FPM TO +1400 FPM. PRESSURIZATION SYSTEM 1 FAILED. AUTO SWITCH TO SYSTEM 2 AND CABIN PRESSURE FLUCTUATIONS CONTINUED. THE OUTFLOW VALVE CYCLED CONTINOUSLY, EVEN IN LEVEL FLIGHT AT Jan 24, 2001 · N822AW · Airbus A319132 · Pressure Regulator/Outflow ValveSDR 20001227SH020Engine · stalledLPB - FLT 030 - DURING DESCENT OF FLIGHT, A NOISE AND STALL WAS EXPERIENCED ON ENG NR 2 AND THE MESSAGE ENG 2 OIL FILTER CLOG (2) CAME ON THE ECAM. AFTER LANDING, TECHS PROCEEDED TO CHECK ENGINE OIL, FOUND SOME METAL PARTICLES AT THE CHIP DETECTOR AND ALSO MEDec 17, 2000 · N474TA · Airbus A319132 · Engine (Turbine/Turboprop)
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