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 2002UALA01464Skin · damagedINTERIM REPAIR INSTALLED BETWEEN FRAME 73 AND FRAME 75. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REPLACED.SDR 2002UALA01466Brake Assy · malfunctionedRETURNED TO FIELD UNDER AMBER ALERT DUE TO LEFT BRAKE WOULD NOT COOL. REPLACED NR 1 BRAKE ASSEMBLY. NO PREVIOUS HISTORY OF HIGH TEMPS. NO FURTHER DEFECTS ON SUBSEQUENT FLIGHTS.SDR 2002UALA01435Hydraulic Line · rupturedABORTED TAKEOFF DUE TO ECAM HYDRAULIC GREEN RESERVOIR LOW LEVEL WARNING. FOUND RIGHT HAND MLG DOOR RETRACT ACTUATOR AFT FLEX LINE RUPTURED. REPLACED FLEX LINE.SDR 2002UALA01389Computer · malfunctionedABORTED TAKEOFF AT 90 KNOTS DUE TO AN AVIONICS VENT MESSAGE. THE AVIONIC EQUIPMENT COOLING COMPUTER WAS RESET AND THE AIRCRAFT FLEW FUTURE FLIGHTS WITH NO INCIDENCE.SDR AWXA200200845Bleed Valve · lack of lubePHX - ABORTED TAKEOFF - FLT 0014 - ON TAKEOFF FROM PHX EN ROUTE FOR JFK THE NR 2 ENGINE EGT EXCEEDED LIMITATIONS, ABORTED TAKEOFF AT APPROXIMATELY 80 KTS. MAINTENANCE DOWNLOADED PREFLIGHT REPORT AND PERFORMED TROUBLESHOOTING TASKS 77-00-00-810-844 INSPECTION SDR 2002UALA01321Socket · defectiveEMERGENCY EXIT LIGHTS FLOOR LIGHT DAMAGED AT 01L. ALL TROUBLESHOOTING PROCEDURES WERE FOLLOWED AND THE LIGHT BASE WAS REPLACED.SDR 2002UALA01303Disk · rupturedFLIGHT DIVERTED UNDER AMBER ALERT DUE TO FUEL IMBALANCE. FOUND BURST DISC BETWEEN LEFT INNER AND CENTER FUEL TANKS BROKEN. REPLACED DISC.SDR AWXA200200746Pump · failedORD - ABORTED TAKEOFF - FLT 0060 - ON TAKEOFF FROM ORD EN ROUTE FOR PHX RECEIVED ECAM INDICATION FOR NR 2 ENGINE COMPRESSOR VANE FAULT. ABORTED TAKEOFF AT 60 KTS.SDR YENA200222Proximity Sensor · defectiveUpon configuration for landing, slats operated normally. Flaps locked at 1. Landed at flap 1 configured slats 3 per FCOMMaintenance removed and replaced interconnecting struct Prox Sensor 39CV IAW MM 27-51-44-400-002 and Ops Tested IAW MM 27-51-00-710-002, OpsSDR 2002UALA01277Smoke · detectedON DESCENT, FLIGHT ATTENDANT RELEASED HALON EXTINGUISHER IN AFT LAV DUE TO LIGHT HAZE/SMOKE AND HEAT. EMERGENCY PROCEDURES WERE PUT INTO EFFECT. SMOKE/HEAT HAD DISSIPATED ON LANDING. RAN ENGINES AND APU. CHECKED AFT FWD LAV FOR SIGNS OF SMOKE, ELECTRICAL SMSDR YENA200221Harness · overheatedFlt#94, OAK to JFK, Multiple faults occurred in flight including RA1, Nose wheel steering, #1 PFD, ND, #1 TLS, GPS, Blue electrical Hyd, #1 RMP, MCDU.Found phase "C" of eng and firewall disconnect plugs overheated. plug 400VC1 firewall plug pin "C" replaced peSDR 2002UALA01263Disk · burstRETURN TO FIELD WITH A FUEL IMBALANCE PROBLEM. OVER PRESSURE BURST DISC BETWEEN THE LEFT INNER WING FUEL TANK AND THE CENTER FUEL TANK RUPTURED. FUEL TRANSFERRED FROM THE LEFT WING TO THE CENTER CAUSING AN IMBALANCE BETWEEN THE INNER WING TANKS.SDR 2002UALA01207Controller · failedRETURNED TO FIELD. SMOKE ELECTRICAL SMELL IN CONTROL CABIN. CIRCUIT BREAKERS PHC2, AOA2, PITOT2, TAT2, AND PHC3 ALL POPPED. REPLACED NR 2 PHC AND TESTED ALL PROBE HEATERS FOR PROPER OPERATION. SYSTEM OPERATED NORMAL WITH NO ADDITIONAL FAILURES NOTED ON SUBSDR 2002UALA01203Skin · damagedFUSELAGE SKIN DAMAGED AT FRAME 67 TO FRAME 70 FROM STRINGER 42L TO 42R. MAJOR REPAIR ACCOMPLISHED. INSTALLED TWO DOUBLERS AND FILLERS.SDR 2002UALA01190Pump · malfunctionedRETURNED TO FIELD DUE TO OVERHEAT ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE OF GREEN HYDRAULIC PUMP. CHANGED GREEN SYSTEM LOW PRESSURE, HIGH PRESSURE AND CASE DRAIN FILTERS.SDR 2002UALA01191Valve · leakingLOSS OF YELLOW HYDRAULIC SYSTEM. REPLACED YELLOW SYSTEM PARK BRAKE VALVE 2579GM.SDR 2002UALA01185Idg · overtempABORTED TAKEOFF AT 80 KNOTS DUE TO LEFT ENGINE IDG FAULT LIGHT. NR 1 ENGINE IDG FAULT LIGHT CAME ON DURING TAKEOFF. NR 1 IDG REMOVED AND REPLACED.SDR YENA200217Engine · malfunctionedFLT 88 ONT TO JFK, DIVERTED TO SLC DUE NR 1 ENGINE AUTO SHUTDOWN IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE PER AMM 71-00-20 AND OPS CHECK OK PER AMM 71-00-00.SDR 2002UALA01133Engine · power lossABORTED TAKEOFF AT 90-100 KNOTS DUE TO NR 1 ENGINE NOT PRODUCING ENOUGH THRUST.SDR 2002UALA01079Radar · malfunctionedRETURN TO FIELD DUE TO LOSS OF WEATHER RADAR.SDR 2002UALA01067Rub Strip · debondedDIVERTED UNDER AMBER ALERT DUE TO VIBRATION IN NR 1 ENGINE. ENGINE REPLACED. HPC RUB STRIP DISBONDED CAUSING COMPRESSOR VIBRATION. ENGINE UPGRADED WITH RUB STRIP MODIFICATION.SDR 2002UALA01035Filter · collapsedABORTED TAKEOFF AT 90 KNOTS DUE TO VENT AVIONICS SYSTEM FAULT. THE AEVC SYSTEM FILTER WAS FOUND DIRTY AND COLLAPSED - REPLACED FILTER.SDR CA020618003Coffeemaker · failed(CAN) 20 MINS.,INTO FLT, CSM ADVISED CAPTAIN THAT STRONG ELECT. SMELL & SMOKE IN AFT GALLEY AREA. FLT CREW ADVISED ATC OF SMOKE IN CABIN & REQ IMMEDIATE RETURN TO VANCOUVER. FLT CREW TURNED GALLEY POWER OFF, AND CSM ADVISED THAT SMOKE HAD CEASED & SMELL HAD DESDR 2002UALA00975Light · inoperativeEMERGENCY EXIT LIGHT BETWEEN OVERWING DOORS INOPERATIVE ON TEST.SDR 2002UALA00957Battery · faultyAFT LEFT INT LOADS FAULT EMERGENCY LIGHT SYSTEM. REPLACED AFT LEFT EMERGENCY BATTERY. OPS CHECKS GOOD.SDR 2002UALA00945Blade · fracturedRETURNED TO FIELD DUE TO NR 1 ENGINE COMPRESSOR STALL. CAUSE OF STALL WAS FOUND TO BE LIBERATED SECTION OF HIGH PRESSURE COMPRESSOR (HPC) 5TH STAGE BLADE. LIBERATION CAUSED DOWNSTREAM DAMAGE, INCREASED TIP CLEARANCE, AND REDUCED SURGE MARGIN OF HPC TO STALL SDR 2002UALA00923Blade · failedRIGHT ENGINE FAILED. BORESCOPE INSPECTION REVEALED FAILED HIGH PRESSURE COMPRESSOR STAGE 4 BLADES, CAUSING MAJOR INTERNAL ENGINE DAMAGE AND AUTO-SHUTDOWN. ENGINE WAS REPLACED.SDR 2002UALA00919Control Unit · failedON FINAL GOT L-G LGCIU 1 FAULT. EXTENDED THE GEAR AND GOT REVERSER NR 1 AS INOP SYSTEM. REPLACED LGCIU-1.SDR 2002UALA00770Plate · stiffAFT CARGO DOOR ECAM WARNING ILLUMINATED. FOUND DOOR HANDLE PLATE STIFF. REMOVED PLATE, CLEANED, LUBED AND REINSTALLED.SDR 2002UALA00920Bleed Valve · failedNR 2 ENGINE EXPERIENCED A HUNG START. HPC BLEED VALVE TEST REVEALED FAILED HPC 7C BLEED VALVE AND WEAK HPC 7A SOLENOID VALVE. VALVES REPLACED.SDR 2002UALA00766Rub Strip · debondedNR 2 ENGINE EXPERIENCED A MAJOR COMPRESSOR STALL. THE THROTTLE WAS RETARDED TO IDLE SPEED. REPLACED ENGINE. CORRECTIVE ACTION FOR MAJOR CAUSE IS INCORPORATION OF UPGRADED HIGH PRESSURE COMPRESSOR (HPC) RUBSTRIP MATERIAL THAT IS MUCH MORE RESISTANT TO DISBONSDR 2002UALA00752Outflow Valve · failedAIRCRAFT UNABLE TO MAINTAIN PRESSURE. VALVE REPLACED ALONG WITH THE AVIONICS COMPUTER.SDR 2002UALA00706Handle · unsecureCARGO (FORWARD) DOOR ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE SHOWED OPEN PASSING 10,000 FEET. AIRCRAFT RETURNED TO FIELD. HANDLE WAS STOWED AND LIGHT EXTINGUISHED.SDR 2002UALA00570Wire · shortedNUMEROUS ECAM FAULT MESSAGES FROM THE NUMBER TWO ENGINE. FOUND NUMEROUS WIRES SHORTED IN THE RIGHT ENGINE OUTBOARD PYLON AREA. AREA WAS CHECKED FOR DAMAGE AND NEW WIRES INSTALLED AS REQUIRED.SDR 2002UALA00565Filter · cloggedABORTED TAKEOFF AT 73 KNOTS DUE TO AN AVIONICS COOLING FAN MESSAGE. FOUND AVIONICS COOLING SYSTEM FILTER CLOGGED. REPLACED SAME.SDR 2002UALA00537Bottle · lowDOOR ASSIST BOTTLE AT 2L LOW. SERVICED ASSIST BOTTLE PRESSURE TO 1750 PSI, CHECKS OK.SDR 2002UALA00368Cover · looseLOWER ECAM MESSAGE HAD AMBER EXIT DOOR WARNING ON DOOR PAGE FOR RIGHT AFT OVERWING DOOR. PROBLEM WAS CAUSED BY MOVEMENT OF THE OVERWING EXIT HANDLE COVER FLAP. REMOVED OVERWING HATCH AND INSPECTED WITH NO FINDINGS. REINSTALLED DOOR AND SECURED DOOR HANDLE CSDR 2002UALA00321Skin · crackedLEFT HAND EXTERNAL FUSELAGE BLIND FASTENER HOLE AT STATION 1270 STRINGER 38L HAS CRACK INDICATION AT 6:00 POSITION VERIFIED WITH NONDESTRUCTIVE TESTING. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN DOUBLER.SDR 2002UALA00536Fire Bottle · unserviceableCREW REPORTS ECAM MESSAGE INDICATES A FIRE BOTTLE DISCHARGE. REPLACED CARGO FIRE BOTTLE DUE TO LOW PRESSURE INDICATION.SDR 2002UALA00286Power Supply · dischargedDOOR 2L EMERGENCY EXIT LIGHT INOPERABLE. REINSTALLED POWER SUPPLY. OPERATIONAL CHECK NORMAL.SDR 2002UALA00279Switch · faultyDIVERTED TO MIA DUE TO HYDRAULIC QUANTITY LOSS INDICATION. CONFIRMED GREEN SYSTEM HYDRAULIC QUANTITY RESERVOIR FULL, NO EXTERNAL LEAKS NOTED. REPLACED LOW LEVEL SENSOR.SDR 2002UALA00250Outflow Valve · failedRETURNED TO FIELD DUE TO CABIN PRESSURIZATION PROBLEM. UNABLE TO MAINTAIN CABIN PRESSURE IN AUTO OR MANUAL MODE. SKIN AIR OUTLET VALVE WAS DEACTIVATED AND SUBSEQUENTLY REPLACED.SDR 2002UALA00214Light · inoperativeSEATS 19, 21 LEFT EMERGENCY ESCAPE PATH LIGHTING INOPERABLE. REPLACED EMERGENCY LIGHT ASSEMBLY.SDR 2002UALA00201Idg · overheatedNR 1 INTEGRATED DRIVE GENERATOR DISCONNECTED AND UNABLE TO START AUXILIARY POWER UNIT. REPLACED NR 1 ENGINE INTEGRATED DRIVE GENERATOR.SDR 2002UALA00182Odor · detectedSMELL OF SMOKE IN CABIN. NO SMOKE VISIBLE. FLIGHT ATTENDANT SMELLED SMOKE IN THE CABIN. NO SMOKE WAS SEEN, SMELL WAS PUNGENT AND LOCATED JUST AFT OF 1ST CLASS. ACCOMPLISHED BITE CHECK OF THE TEMPERATURE CONTROL SYSTEM, CHECKED ALL FANS FOR OPERATION, CHECKSDR 2002UALA00139Skin · dentedDENT FOUND AT AIRCRAFT ARRIVAL. DENT LOCATED ABOUT 20 INCHES ABOVE AVIONICS EQUIPMENT AIR INLET AND 9 INCHES AFT OF FRAME 20. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.SDR 2002UALA00132Carbon Seal · leakingNR 1 ENGINE HAD INFLIGHT SHUTDOWN DUE TO LOSS OF OIL QUANTITY AND DECREASE IN OIL PRESSURE. AFTER SHUTDOWN ENGINE WINDMILLED FOR 35 MINUTES, OIL TEMPERATURE 110-115, OIL PRESSURE 9.5 PSI AND OIL QUANTITY ZERO. INTERFACE BETWEEN FUEL PUMP AND MAIN ENGINE GEARSDR 2002UALA00011Monitor · malfunctionedCREW REPORTS HOT BRAKES ON CLIMB OUT WITH GEAR DOWN. SUPPLEMENTAL DATA UPDATE ORIG INDICATION 370 DEG, CLIMBED TO 425 DEG. SUSPECTED INDICATION PROBLEM, BRAKE TEMP CHECKS NORMAL. BSCU BITE CHECK AND PREVIOUS LEG REPORT FAULT BRAKE TEMPERATURE MONITORING UNIT SDR 2001UALA02501Power Supply · failedRIGHT OVERWING EMERGENCY LIGHT POWER SUPPLY FAILS TEST AFTER REPLACEMENT OF THE BATTERY PACK. REPLACED POWER SUPPLY.SDR 2001UALA02442Structure · damagedABORTED TAKEOFF AT 140 KNOTS DUE TO NR 1 ENGINE COMPRESSOR STALL. SUPPLEMENTAL DATA UPDATE INITIAL BORESCOPE INFORMATION INDICATES DISBOND OF C6 ABRADABLE RUBSTRIP MATERIAL, CAUSING C6 BLADE DAMAGE AND COMPRESSOR STALL.
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