N532AS
Service difficulty reports · 370
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N532AS' AND registry_match = 'registration' 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 n_number = 'N532AS' AND registry_match = 'registration' 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 ASAA12510882Panel · looseWHILE ACCOMPLISHING ENGINE INLET AND FAN BLADE INSP FOUND FAN DUCT PANELS LOOSE. PANELS NR 6, 7, 8, 9 AND 12. TIGHTEN SCREW ON FAN DUCT PANEL NR 1 ENG REF MM 72 23 07.SDR ASAA12510873Unknown · malfunctionedHF2 SHOWS FAIL WHEN SELECTED. PERFORMED HF COMMUNICATION SYSTEM TEST. OPS CHECK GOOD. REF AMM 23 11 00 730 801.SDR ASAA11510844Unknown · malfunctionedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATES ON RECALL. EXTINGUISHES ON RESET. BITE OF NR 2 PZTC SHOWS CONT CAB TRIM VALVE FAULT RESET & RETESTED PZTC REF FIM TASK 21 62TSK 842 NO FAULTS NOTED. SUCCESSFUL GROUND VERIFICATION CONFIRMED.SDR ASAA11510696Control Unit · faultyRIGHT SIDE WINDOW OVERHEAT ILLUMINATED. PERF WHCU BITE CHECK PROCEDURE PER FIM 30 41 00 810 801. FOUND RT SIDE SENSOR FAULT. PERF FIM TASK 30 41 00 810 811. WINDOW SENSOR FAULT ISOLATION. SWAPPED RT SIDE WINDOW TO SPARE SENSOR AND REPLACED COIL CORD. REPSDR ASAA11510701Jam-Nut · looseRIGHT SIDE WINDOW NR 2 OVERHEAT LIGHT ILLUMINATED. RIGHT SIDE WHCU BITE TEST OK. USING INFARED THERMOMETER FOUND RIGHT SIDE WINDOW TEMP WITHIN LIMITS REF MM 30 41 00 701 801. OPS CHECK OK. FOUND RIGHT SIDE WINDOW HEAT SWITCH JAM NUT LOOSE. REMOVED LIGHT PSDR ASAA11510338Shim · wornNR 2 ENGINE FAN BLADE LUBE 1EA FAN BLADE PLATFORM AND 24 FAN BLADE SHIMS REQUIRE REPLACEMENT. 1EA FAN BLADE PLATFORM MFG P/N 340 001 8YY 0 ARE INSTALLED 24EA FAN BLADE SHIMS MFG P/N 340 252 302 0 ARE INSTALLED ON NR 2 ENGINE.SDR ASAA11510333Filter · defectiveNR 1 ENG IDG DIFFERENTIAL PRESSURE INDICATOR IS EXTENDED. C/W FIM TASK 24 11 00 810 803 INSPECTED FILTER FOR CONTAMINATION NO CONTAMINATION FOUND CHANGED FILTERS AND OIL PER TASK CARD 78424000. DPI BUTTON RESET OK FOR SERVICE.SDR ASAA11510323Pump · leakingNR 2 ENGINE HAS HISTORY OF FUEL PUDDLING ON GROUND DURING ENGINE START. BAGGED FUEL & VENT DRAIN LINES ON NR 2 ENGINE & RAN AFTER 3 HR WAIT AFTER START HAD CONTINUOUS FUEL FLOW FROM PUMP PAD DRAIN UNTIL SHUTDOWN REF MM 71 71 00. REPLACED FUEL PUMP PACKAGE ASSDR ASAA11510260Pin · defectiveAPU HAD BEEN RUNNING FOR ABOUT 3 MINUTES APU SHUTDOWN FAULT LIGHT ON. REMOVED APU ECU AND SAW CONTINUITY FLUCTUATING TO 'OPEN' BETWEEN D3599A PINS C2 AND D2 WHILE SHAKING P15 REF WDM49 94 21. FOUND VERY LOW PIN TENSION AT P15 PIN B. REPLACED P15 PIN B REF CSDR ASAA11510257Oil Cooler · obstructedAPU SHUT OFF FAULT LIGHT ILLUMINATED. PERFORMED FIM TASK 49 90 00 810 801 FOUND APU OIL COOLER OBSTRUCTED WITH DEBRIS. REMOVED AND REPLACED APU OIL COOLER REF M/M 49 91 41, OPS AND LEAK CHECKS NORMAL.SDR ASAA11510096Computer · failed"FD" CAUTION FLAG ON CAPTAINS PFD + NO MA LIGHT ON FLIGHT DIRECTOR WHEN CAPTAINS F/D ON SWITCH SELECTED. FCC A CURRENT STATUS BITE FAILS MSG 22 11303 INTERNAL FAILURE. CYCLED FCC A C/B'S, NO HELP. REPLACED FCC A REF MM 22 11 33, OPS CHECK NORMAL.SDR ASAA11510081Unknown · malfunctionedWHILE ACCOMPLISHING ROUTINE CHECKS INTERROGATE, THE FMC CDU FOR ENIGINE FAULTS FOUND A SHORT TIME FAULT NR 73 30311 "THE START SWITCH SIGNAL AND ARINC BUS DATA DISAGREE." PERFORMED FIM 73 24 00 810 F00 INITIAL EVAL NO RECENT FAULT NO FAULT HISTORY. EXAMINED SDR ASAA1159933Bleed Air Sys · malfunctionedNO APU DUCT PRESSURE APU RUNNING NORMAL EGT 400 DEG. ACCOMPLISHED INITIAL EVALUATION & APU BITE PROCEDURES PER FIM 49 55 00 801 804 E (1) PGS 1 3 & 49 60 00 810 801 NO DEFECTS FOUND. INSPECTED BLEED AIR VALVE AREA NO LEAKS FOUND & CONNECTOR IS TIGHTENED & SESDR ASAA1159916Bleed Air Sys · malfunctionedZERO DUCT PRESSURE WHEN APU BLEED SWITCH SWITCHED ON. STARTED APU AND PERFORMED BLEED AIR VALVE OPERATIONAL CHECK OPS CHECK NORMAL IAW AMM 49 52 11 400 801 STEP F APU BITE TEST SHOW NO MAINTENANCE MESSAGE THERE WAS AN INTERMITTENT FAULT OK FOR SERVICE REF FIMSDR ASAA1159457Sensor · dirtyFLIGHT ATTENDANTS REPORT AFT CABIN TOO COLD. TURNED CONTROLLER TO NEARLY MAX WITHOUT MUCH EFFECT. CLEANED CABIN TEMP SENSORS IAW MM 21 61 10. CABIN TEMPERATURE CONTROL OPS NORMAL IAW REPAIR CONFIRMATION FIM 21 61 TASK 847.SDR ASAA1159380Warning System · intermittentCONT CAB ZONE TEMP LT ILLUMINATES ON RECALL EXTINGUISHES WITH MASTER CAUTION RESET. TROUBLESHOT PER FIM 21 62 00 810 842. FAULT APPEARS TO HAVE BEEN INTERMITTENT. BITE TEST SHOWS NO FAILURES PREVIOUS NINE FLTS. RESET LOGGED FAULT. GROUND VERIFICATION OF PSDR ASAA1159343Chip Detector · contaminatedDURING AGB/TGB MAGNETIC CHIP DETECTORS INSP ON NR 2 ENG FOUND FOUR MAGNETIC PARTICLES. TWO PARTICLES LARGER THAN 0.02 INCH IN THE FORWARD SUMP. REF LAB/COR REPORT 11.066 DEBRIS HAS BEEN IDENTIFIED AS 17 4PH STAINLESS STEEL. REF MM SUBTASK 79-00-00-240-001-F0SDR ASAA1158975Pcu · failedAMBER "ELEC" LIGHT ILLUMINATED AFTER ENGINE START. VERIFIED DISCREPANCY REMOVED AND INSTALLED NEW SPCU REF MM 24 34 11 000 801 AND 24 34 11 400 801. PERFORMED SPCU TEST PER SAME. SYS CHECKS NML.SDR ASAA1158932Filter · defectiveDURING PDC WALKAROUND FOUND NR 1 ENGINE IDG DELTA "P" INDICATOR EXTENDED. REPLACED NR 1 ENGINE IDG SCAVENGE AND CHARGE FILTER ELEMENT IAW ASAMM 24 11 41 400 801 AND INSPECTED THE FILTER ELEMENTS IAW ASAMM 24 11 41 200 801. FOUND NO VISUAL DEFECTS METAL PARTISDR ASAA1158873Sensor · out of toleranceAPU BLEED AIR INOP. CDU BITE PRODUCED FAULT CODE 49 52270 DELTA PRESSURE SENSOR SHOWS OUT OF RANGE DRIFT. REPLACED THE DELTA PRESSURE SENSOR OPS CHECK GOOD NO ACTIVE FAULTS. REF MM 49 52 33. VISUAL INSPECTION COMPLETED OF CONNECTOR AND WIRE HARNESS NO FAUL
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