IAE V2522-A5
Service difficulty reports · 3,465
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 = 'V2522A5' 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 = 'V2522A5' 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 99UAL900422Brakes · locked upBRAKES LOCKED UP UPON LANDING. *S/D* AFTER LANDING SHUT DOWN NR 2 ENG ON TAXI HOLDING SHORT OF RUNWAY. BRAKES WERE SET, BRAKES WOULD NOT RELEASE. BSCU WAS RESET, NO HELP. BRAKES WERE BLED AND TAXI TESTED OK.SDR 99UAL900412Windshield · crackedCRACKED RIGHT WINDSHIELD. *S/D* CAUSE OF CRACKED RIGHT WINDSHIELD WAS FOD AS THERE WAS NUMEROUS HITS ALONG LOWER EDGE.SDR 99UAL900342Battery · dischargedMID LEFT OVERWING EXIT EMERGENCY POWER SUPPLY UNIT BATTERY INOP. REPLACED BATTERY (PSU P/N IS 565-0038).SDR 99UAL900308Switch · failedCREW REPORTS SMOKE IN THE CABIN. EXTERNALLY LEAKING LOW OIL PRESSURE (LOP) SWITCH CAUSED OIL TO FLOW OVER LOAD COMPRESSOR CASE WHICH WAS REINJESTED INTO THE APU AND CAUSED ODOR OR SMOKE. THE APU (APS3200 SERIAL NUMBER 1413) WAS REMOVED AND ROUTED THROUGH SUNSDR 99UAL900178Battery · dischargedCABIN EMERGENCY LIGHT TEST FAILS FROM PTP PANEL. *S/D* EPSU AND BATTERY WERE REPLACED.SDR 99UAL900131Fmgc · malfunctionedAUTOPILOT DISENGAGED ON APPROACH ALONG WITH THE MAP NOT AVAIL FLAG ON THE CAPTAIN SIDE NAV DISPLAY. PFR SHOWS FAILURE MESSAGES FMGC2 AND FAC2. *S/D* THE POSTFLIGHT REPORT IDENTIFIED THE FLIGHT MANAGEMENT AND GUIDANCE COMPUTER (FMGC) NR 2 AND FLIGHT AUGMENTATISDR 99UAL900114Power Supply · inoperativeEMERGENCY LIGHTS TEST SHOWS EPSU COMM FWD L AND EPSU COMM EMER R, L. COMMUNICATION FAULT OCCURED BETWEEN EPSU'S (FWD L - 10WL, EMER R - 12WL AND EMER L - 11WL) AND CIDS. ALL THESE EPSU'S AND THEIR BATTERIES WERE REPLACED, AND SUBSEQUENT EMERGENCY LIGHT TEST SDR 99UAL900102Valve · failedRIGHT SIDE FUEL BURNING MUCH FASTER THAN LEFT SIDE. IN 2:30 FLT TIME, FUEL IMBALANCE BECAME GREATER THAN 300 LBS AND CAUSED A FUEL IMBALANCE ECAM WARNING. AT THAT TIME, THE XFEED VALVE INDICATED CLOSED. CROSSFEED VALVE FAILED OPEN. ECAM AND PB SWITCH BOTH SDR 99UAL900057Valve · malfunctionedFUEL TRANSFERRING FROM RT WING TANK TO LT WING TANK IN FLIGHT WITH CROSSFEED VALVE CLOSED. NO ECAM WARNINGS.SDR 99UAL900020Door · misinstalledOVERWING EMERGENCY EXIT DOOR AIR LEAK. SEATS 9BC AND 10ABC NOT TO BE OCCUPIED DURING FLIGHT UNTIL REPAIRS ARE COMPLETE. FOUND DOOR INSTALLED INCORRECTLY WITH SEAL STUCK IN THE GAP BETWEEN THE DOOR AND FUSELAGE. DOOR WAS REINSTALLED CORRECTLY.SDR 98UAL900603O Ring · failedLOST YELLOW SYS HYD QTY, NO QTY OR PRESS, TURNED PUMP OFF. DIVERTED TO DEN. *S/D* FOUND O-RING DAMAGED AT COUPLING QUICK DISCONNECT ON YELLOW MAIN HYDRAULIC POWER REF IPC 29-13-03. REPLACED O-RING PER MM 29-13-15, OPS CK GOOD.SDR 98UAL900533Pfd · failedCREW REPORTS PFD AND ND ON F-O'S SIDE WENT BLANK. *S/D* SECURED TERMINAL BLOCK 2VG. TERMINAL BLOCK HAD HIGH RESISTANCE ON GND PIN 102 OF F/O ND, PFD, AND LOWER DU. AIRCRAFT THEN TESTED OK.SDR 98UAL900507Indication · malfunctionedAFTER TAKEOFF, ECAM WARNING: GEAR NOT DOWN. RETURNED TO FIELD. *S/D* ACCOMPLISHED LGCIU1 AND LGCIU2 TEST. NO FAULTS FOUND. REPLACED EEC DUE TO EPR PROBLEMS. TESTED FMGC AND AFS SYSTEM, ALL OK.SDR 98UAL900438Lgciu · malfunctionedCREW REPORTS LANDING GEAR DID NOT COMPLETELY EXTEND ON FIRST ATTEMPT. CYCLED GEAR, OPS NORMAL. *S/D* LGCIU REPORTED NLG R DOOR PROX SENSOR 38GA TARGET POSITION. CHECKED GAPS AND FOUND WITHIN TOLERANCE PER AMM 32-31-73. BITE TEST OK. NO FURTHER PROBLEMS.SDR 98UAL900250Engine · stalledNR 2 ENGINE STALL AT FL330, OVER TEMP LIGHT ILLUMINATED. ENGINE SHUTDOWN, DIVERTED TO SMF. OVERWEIGHT LANDING.
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