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 2005UALA00576Hose · brokenTHE HOSE WAS FOUND BROKEN AT SWIVEL AND BY ASPIRATOR DURING UNPACKING PROCEDURE. HOSE WAS FOUND BROKEN AT SWIVEL AND AT ASPIRATOR CONNECTION DURING MAINTENANCE OF THE SLIDE IN THE SHOP. PROBABLE CAUSES COULD BE MISHANDLING DURING TRANSPORTATION OR THAT THE SDR 2005UALA00569Engine · stalledNR 2 ENGINE OVERTEMPTED & STALLED ON TAKEOFF. ENGINE WAS REPLACED AND AIRCRAFT CONTINUED FUTHER FLYING WITHOUT INCIDENT. THE ENGINE FAILURE WAS CONFIRMED AS A HIGH PRESSURE COMPRESSOR 3RD STAGE BLADE (R3 BLADE) FAILURE. THIS IS AN INDUSTRY-WIDE AND KNOWN ISDR 2005UALA00567Hose · brokenBROKEN HOSE AT ASPIRATOR. THE HOSE WAS FOUND BROKEN AT ASPIRATOR CONNECTION DURING MAINTENANCE OF THE SLIDE IN THE SHOP. A PROBABLE CAUSE IS KINKED ROUTING OF THE HOSE DURING THE PREVIOUS PACKING OF THE ASSEMBLY. THE STRESS ON THE HOSE RESULTED IN ITS BREAKSDR 2005UALA00556Fan · failedBOTH AVIONICS BLOWER AND EXTRACT FANS BECAME INOPERATIVE. PFR SHOWS ECAM VENT AVIONICS SYS FAULT WITH ASSOCIATED FAILURE MSG NO AEVC DATA. TSM SHOWS POSSIBLE COMPUTER FAULT 10HQ. REPLACED AEVC AND BITE TEST CHECKS GOOD. NO FAILURES OR FAULTS NOTED.SDR 2005UALA00565Hose · brokenTHE HOSE WAS FOUND BROKEN BY ASPIRATOR DURING THE UNPACKING PROCESS. DURING UNPACKING OF THE SLIDE IN THE SHOP, THE HOSE WAS FOUND BROKEN FROM PLATE. THE PROBABLE CAUSE IS KINKED ROUTING OF THE HOSE DURING THE PREVIOUS PACKING OF THE ASSEMBLY. THE CONTINUESSDR 2005UALA00536Engine · stalledNR 1 ENGINE EXPERIENCED TWO COMPRESSOR STALLS, ONE IN CRUISE AND ONE AT TOP OF DESCENT. ENGINE WAS CHANGED AND AIRCRAFT CONTINUED FLYING AFTERWARDS WITHOUT FURTHER INCIDENT. COMPRESSOR STALL WAS CAUSED BY HIGH-PRESSURE COMPRESSOR (HPC) BLADE DAMAGE PRIMARILYSDR 2005UALA00509Engine · failedLOUD BANG ON CLIMBOUT FROM NR 1 ENGINE. OIL QUANTITY AND PRESSURE WENT TO ZERO, EGT RED LINED. ENGINE WAS REPLACED AND AIRCRAFT CONTINUED FUTHER FLYING WITHOUT INCIDENT. THE ENGINE FAILURE WAS CONFIRMED AS A HIGH PRESSURE COMPRESSOR 3RD STAGE BLADE (R3 BLADSDR 2005UALA00589Hose · brokenHOSE FOUND BROKEN DURING THE PACKING PROCEDURE. HOSE WAS FOUND BROKEN AT END NEAR ASPIRATOR CONNECTION DURING MAINTENANCE OF THE SLIDE IN THE SHOP. PROBABLE CAUSES COULD BE MISHANDLING DURING TRANSPORTATION OR THAT THE ROUTING OF THE HOSE DURING THE PREVIOUSDR 2005UALA00573Elec Connector · disconnectedSKIN VALVE FAULT DISPLAYED ON UPPER ECAM. FOUND CONNECTOR ON SKIN EXCHANGER ISOLATION VALVE 24HQ NOT CONNECTED. RECONNECTED CONNECTOR AND REACTIVATED SKIN VALVE. ALL TEST PASSED.SDR 2005UALA00482Electrical Sys · unknownFLIGHT ATTENDANT SHOCKED WHILE HOLDING THE G1 AND G2 GALLEY COUNTER TOPS, DURING POWER TRANSFER FROM GROUND TO APU. INSPECTION AND VERIFICATION OF THE ELECTRICAL GROUNDING OF BOTH HOT GALLEY AND COLD GALLEY SECTIONS WERE ACCOMPLISHED IN ACCORDANCE WITH THE ASDR 2005UALA00469Pump · failedLOST GREEN HYD SYSTEM WHILE IN A HOLDING PATTERN ABOVE PLANNED DESTINATION. GREEN SYSTEM EDP REPLACED AWAITING FINDINGS FROM THE VENDOR (ARINC). REPLACED NR 1 ENG DRIVEN PUMP, REF MM29-11-51. REPLACED CASE DRAIN FILTER, PDI NOT POPPED. NO DEBRIS FOUND IN FILSDR 2005UALA00474Aspirator · damagedFOUND ASPIRATOR CRUSHED, FLAPS STUCK AND HOLE IN ASPIRATOR. THE PROBABLE CAUSE OF ASPIRATOR DAMAGE IS INCORRECT PREVIOUS PACKING OF THE SLIDE ASSEMBLY THAT RESULTED IN THE ASPIRATOR DEFORMATION. THE SHOP REPORT THAT THE SLIDE WOULD NOT HAVE DEPLOYED IS UNFOUSDR 2005UALA00413Limiter · failedBOTH RUDDER LIMITERS FAILED. MAINTENANCE FOUND FAULT "AFS: FAC2-RTL ACTR 4CC". ELECTRONIC MODULE OF RUDDER TRAVEL LIMITATION UNIT (RTLU) WAS SUBSEQUENTLY REPLACED. OPERATIONAL CHECK WAS NORMAL.NO FURTHER ANOMALY WAS REPORTED. SUBSEQUENT SHOP FINDING FOUND A SDR 2005UALA00411Compressor · stalledCREW HAD MOMENTARY ENGINE STALL ECAM FOR BOTH ENGINES. EVENT LASTED 2 SECONDS AND SUBSEQUENT PARAMETERS WERE NORMAL. CAUSED BY A COMBINATION OF UNIQUE FLIGHT CONTROL INPUT , AND ENVIRONMENTAL FACTORS , AND SPECIFIC ENGINE CONDITIONS . THE FIX FOR THIS PROSDR 2005UALA00412O-Ring · failedYELLOW RESERVOIR LOW LEVEL FAILURE WITH BLUE SYS LOW AND GREEN FLUCTUATING AS WELL. FLIGHT LANDED WITHOUT INCIDENT. REPLACED B-NUT AND O-RING ON PTU MANIFOLD REF MM 29-13-15-991-001 PTU MANIFOLD ITEM 5 AND 52 LEAK CHECK OK. FOUND BAD O-RING SOURCE OF LEAK. SSDR 2005UALA00405Fluid · leakingDIVERTED FLIGHT DUE TO LOSS OF GREEN ENGINE HYDRAULIC FLUID. CREW REPORTED IN MSY AFTER NR 1 ENG START GREEN HYD PUMP WOULD NOT COME ONLINE. CYCLED SWITCH SEVERAL TIMES CAME ONLINE. AT FL10 ECAM WARNING GREEN PUMP FAILED CYCLED SWITCH OFF. PTU TOOK OVER OPS NSDR 2005UALA00386Outflow Valve · faultyUNABLE TO CONTROL CABIN PRESSURE IN AUTO OR MANUAL MODE. OXYGEN MASKS MANUALLY DEPLOYED. CABIN PRESSURE SYSTEM 1 AND 2 WARNING WITH ASSOCIATED FAULT OF THE OUTFLOW VALVE. REPLACED THE OUTLFOW VALVE 10HL.SDR 2005UALA00382Transducer · failedCREW RECEIVED LOW PRESSURE GREEN HYDRAULIC PUMP INDICATION. GREEN SYSTEM PRESSURE TRANSDUCER FAILED. REPLACED THE TRANSDUCER.SDR 2005UALA00375Light · malfunctionedEMERGENCY LIGHTS FAILING TEST IN AFT CABIN. AFTER SYSTEM RESET SYSTEM TESTED OK .SDR 2005UALA00306Actuator · failedNUMBER 1 ENGINE SHUT DOWN DUE TO ECAM WARNING FOR COMPRESSOR VANE, STALL AND EGT OVER LIMIT. REPLACED VSV ACTUATOR AND ACCOMPLISHED POWER ASSURANCE TEST. HISTORY SHOWED CLASS 2 FAULT MESSAGE ON VSV ACTUATOR FUNCTIONING ON ONE CHANNEL. A SUBSEQUENT STALL WASSDR 2005UALA00381Skin · dentedDENT AFT OF DOOR 1L, APPROX 20 INCHES AFT OF DOOR BOTTOM. INSTALLED DOUBLER REPAIR.SDR 2005UALA00277Blade · failedABORTED INITIAL TAKEOFF ROLL DUE TO COMPRESSOR STALL AND REPORTED FLAMES FROM NR 2 ENGINE. ENGINE TEARDOWN CONFIRMED A HPC STAGE 3 BLADE FAILURE. THIS FAILURE MODE IS AN INDUSTRY KNOWN PROBLEM AS A RESULT OF WEAR ON THE BLADE MIDSPAN SHROUD. A PROGRAM ISSDR 2005UALA00280Insert · missingLT OFFWING SLIDE, METAL INSERTS IN ENCLOSURE FOR MOUNTING STUDS ARE MISSING IN 4 HOLES, ALLOWING MOUNTING STUDS TO CRUSH ENCLOSURE AGAINST MOUNTING PLATE. INSERTS COULD GET FOULED UP AND GETTING LOST DURING ENCLOSURE REMOVAL AND/OR TRANSPORT. THE SHOP DOCUMSDR 2005UALA00267Idg · shutdownAPU AUTO SHUTDOWN WITH THE NR 2 IDG DEFERRED. REPLACED PRECAUTIONARY PER SFOLM THE APU OIL PRESS SWITCH, OIL SUMP TEMP SENSOR, OIL LEVEL SENSOR, AND ECB. RAN APU ON GROUND FOR ONE HOUR WITH ELEC AND PNEU LOADS NO AUTO SHUTDOWNS. APU HAD 2 PREVIOUS GRND ASD. SDR 2005UALA00261Duct · disconnectedLT WING LEAK DISPLAYED ON UPPER ECAM. FOUND DUCT DISCONNECTED AT GROUND BLEED AIR CONNECTOR. RECONNECTED DUCT.SDR 2005UALA00266Duct · looseLEFT WING LEAK DISPLAYED ON UPPER ECAM. FOUND DUCT LOOSE AT FIRST CLAMP AFT OF THE GROUND AIR CONNECTOR. REPOSITIONED DUCT AND RESECURED CLAMPS.SDR AWXA200500368Actuator · malfunctionedON TAKEOFF ROLL RECEIVED ECAM MESSAGE FOR NR 2 ENGINE COMPRESSOR VANE, REJECTED TAKEOFF BELOW 70 KTS AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, OPERATIONAL CHECK WAS GOOD. VENDORS TEAR DOWN RESDR 2005UALA00254Separator · wornAUTO SHUTDOWN OF APU WITH NR 2 ENG DRIVEN GENERATOR ALREADY INOPERATIVE. CONFIRMED NO EXTERNAL OIL LEAKAGE. GEARBOX MODULE 756407J, S/N SP-G 970369 WAS PARTIALLY DISASSEMBLED FOR INSPECTION AND REPLACEMENT OF THE BEARING TABS AND AIR-OIL SEPARATOR SEAL. AIR-OSDR 2005UALA00252Seal · leakingCABIN PRESSURE INCREASED RAPIDLY DURING CLIMB FROM FL300-370. PRESSURIZED AIRCRAFT AND FOUND FWD CARGO DOOR LEAKING. REPLACED FWD CARGO DOOR SEAL AND PRESSURIZED AIRCRAFT, NO LEAKS NOTED.SDR 2005UALA00237Outflow Valve · out of adjustUNABLE TO PRESSURIZE THE CABIN. PFR SHOWED THE AVIONICS SKIN AIR OUTLET VALVE FAILED. ADJUSTED VALVE DOOR 3 QUARTER TURN TO FULL OPEN STOP.SDR 2005UALA00229Warning Light · illuminatedNR 2 ENGINE REVERSER FAULT INDICATION. SENSOR 23GA WAS REPLACED.SDR 2005UALA00202Bearing · failedNR 2 ENGINE COMPRESSOR STALL FOLLOWED BY OIL FILTER CLOGGED MESSAGE. SHUTDOWN ENGINE. NR 4 MAINLINE ROLLER BEARING FAILED, CAUSING ENGINE TO AUTO-SHUTDOWN. NR 4 BEARING HAD 1417 FLT HOURS FROM LAST OVERHAUL. BEARING FAILURE CONFIRMED AS CAUSED BY BEARING CSDR 2005UALA00185Door · noisyRETURN TO FIELD DUE TO LOUD NOISE BY DOOR 1R. ON SECOND ATTEMPT LOUD BANGING DETECTED FROM DOORS 1R AND 1L. APPEARS TO BE NORMAL NOISES FROM FUSELAGE DURING TAKEOFF AND CLIMB. ENGINEERING FLIGHT TEST CREW SHOWED NOTHING ABNORMAL.SDR 2005UALA00163Duct · chafedLEFT WING BLEED LEAK MESSAGE AFTER TAKEOFF. A SMALL HOLE WAS FOUND IN A WING-ANTI ICE DUCT FLANGE. THE HOLE WAS CAUSED BY A CLAMP CHAFING THE DUCT FLANGE. THE DEFECTIVE DUCT WAS REPLACED AND A NEW CLAMP INSTALLED.SDR 2005UALA00131Indication Sys · failedLOST ALL FUEL QUANTITY INDICATIONS. REVIEW OF THE POST FLIGHT REPORT RESULTED IN THE INDICATION OF BOTH THE FQIC 3QT AND FWC1 AS BEING FAULTED. FURTHER TROUBLESHOOTING ALONG WITH SOME ADDITIONAL WIRING CHECKS CONFIRMED NO DATA WAS AVAILABLE FOR CHANNEL 1A OR SDR 2005UALA00102Warning Light · illuminatedVENT AVIONICS FAULT WITH VENT SKIN VALVE MESSAGE. ECAM PAGE SHOWS SKIN AIR OUTLET VALVE (22HQ) AT FAULT. PERFORMED CFDS TEST, CONFIRMED VALVE AT FAULT AND REPLACED.SDR 2005UALA00101Proximity Sensor · malfunctionedAFT CARGO DOOR WARNING LIGHT ILLUMINATED. REPLACED THE AFT CARGO DOOR PROXIMITY SENSOR 32WV AND CONNECTOR.SDR CA050124006Recorder · burned(CAN) TROUBLE SHOOTING THE AFT VIDEO MONITOR NOT EXTENDING REVEALED THAT THE TAPEING UNIT WAS SHOWING SIGNS OF SMOKE DAMAGE. CLOSER INVESTIGATION REVEALED THAT THE TAPEING UNIT HAD GIVEN OF SUFFICIENT HEAT TO CAUSE BURNING OF THE INSULATION BLANKET DIRECTLY ABSDR 2005UALA00303Slide · tornPREDEPLOYED, FOUND BOTTLE GAUGE BROKEN AND BAG TORN. ASPIRATOR BENT. ALL FLANGABLE LINKS POPPED A HOLE IN THE TOP TUBE, BLOWN OUT SEAM AND TORN FABRIC. DEFECTS REPORTED BY THE OSV SHOP (WINSLOW) ARE OF A SLIDE/RAFT PREVIOUSLY INADVERTENTLY DEPLOYED BY CREW SDR 2005UALA00038Battery · inoperativeEMERGENCY EXIT AISLE LIGHT INOP AT SEAT 1C. REPLACED BATTERY AND CHARGER 110WL1.SDR 2005UALA00012Blade · failedAT 10,000 FT THROTTLE AT NORMAL SETTING JUST ABOVE IDLE, LOUD NOISE WAS HEARD FROM NR 1 ENGINE. EGT WENT RED AND VIBRATION INDICATION STAYED AT 6.0. REPLACED NR 1 ENGINE. TEARDOWN REVELAED A STAGE THREE BLADE FAILED IN THE DOVE TAIL AREA. THIS PROBLEM IS NOTSDR 2004UALA01238Aspirator · damagedLOWER CHAMBER ASPIRATOR (60322-105) CRUSHED AND RENDERED UNREPAIRABLE. PACKBOARD DAMAGED AT BOTH OUTBOARD CORNERS AND BOTTOM SHAFT SUPPORTS DAMAGED FROM SERVICE HANDLING. ASPIRATORS APPEAR DAMAGED FROM LAST PACKING. REPLACED THE ASPIRATORS AND PACKBOARD.SDR AWXA200401412Stator Vane · lack of lubeON TAKEOFF AT BOS EN ROUTE FOR LAS JUST PRIOR TO 80 KTS RECEIVED ECAM MESSAGE NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT NR 2 ENGINE COMPRESSOR VANE FAULT IAW TSM 75-30-08-810-846, TSM RECOMMENDED A VARIASDR 2004UALA01235Controller · faultyFLIGHT DIVERTED DUE TO NR 2 PACK SLOWLY OVERHEATING AND NR 1 PACK PREVIOUSLY DEFERRED. REPLACED FAULTY CONTROLLERSDR 2004UALA01234Proximity Sensor · malfunctionedLANDED UNDER AMBER ALERT DUE TO NOSE GEAR INDICATION. NORMAL LANDING BUT NO NOSE WHEEL STEERING AND HAD TO BE TOWED IN. MLG UNSAFE INDICATION ON FWD PANEL WITH ECAM DOOR NOT CLOSED AND NW STEERING FAULT PER POST FLIGHT REPORT, FOUND NLG DOWNLOCK PROX SENSOR 1SDR 2004UALA01208O-Ring · leakingFLIGHT DIVERTED WITH A WING LEAK, RESTRICTED TO NO ICING. FOUND FAN AIR VALVE THERMOSTAT LEAKING ONTO OVERHEAT LOOP - REPLACED SENSOR AND O-RING.SDR 2004UALA01180Line · out of positionMOORING LINE LOOP UNDER LOWER LACING COVER. SLIDE REPACKED WITH MOORING LINE LOOP INSTALLED ON TOP OF LACING.SDR 2004UALA01181Bulb · burned out6 BULBS BURNED OUT. MOORING LINE NOT IN POCKET, PLACED IN BETWEEN GIRT HALVES. HOSE WAS TAPED OVER SWIVEL 6 INCES FROM MAT DOWN HOSE. INFLATION CABLE NOT RUN IN CABLE GUIDE AND RAN THROUGH LACING GROMMET, THEREFORE SLIDE WOULD NOT HAVE FIRED, WAS 10 INCHES SDR 04UALA01181Slide · unserviceableDURING OVERHAUL OF DOOR TWO LEFT SLIDE THE MOORING LINE WAS FOUND TO BE PACKED IN BETWEEN GIRT HALVES. THE INFLATION CABLE WAS NOT RUN IN CABLE GUIDE BUT RUN THROUGH LACING GROMMET INSTEAD, THE SLIDE WAS FOLDED INSTEAD OF ROLLED AND WAS PACKED OVER BOTTLE ANSDR 2004UALA01169Fitting · stuckDOOR 1L AFT GIRT BAR ATTACH FITTING IS STUCK OPEN AND WILL NOT SPRING BACK TO CLOSED OR LOCKED POSITION. REMOVED DEBRIS TRAPPED IN THE INTERFACE AND LUBED GIRT BAR.
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