N584AS
Service difficulty reports · 569
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 = 'N584AS' 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 = 'N584AS' 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 ASAA0853223Computer · malfunctionedFMC DISAGREE MSG WHEN FLAPS LOWERED VERIFIED DISCREPANCY. PERFORMED FMC RESET PROCEDURES IAW FIM 34-61-00-810-835. SYSTEM RESET OK. AC OK FOR SERVICE.SDR ASAA0853170Controller · malfunctionedAUTO FAILED ON PRESSURIZATION ALTN MODE SELECTED AUTO FAIL LIGHT OUT. UNABLE TO DUPLICATE DISCREPANCY NR 2 CONTROLLER LOGGED FAULT CODE 101 FOR FLIGHT 479. ACCOMPLISHED FIM 31 803 FOUND FAULT TO BE INTERMITTENT. GROUND VERIFICATION TEST PASSED REF MM 21 31 SDR ASAA0853107Hydromech Unit · faultyENG NR 2 SHORT TERM FAULT MSG NO. FAULT CODE NR 73 20342. THE FMV
POSITION SIGNAL OUT OF RANGE. PERFORMED TEST 12 ACTUATORS TEST CONFIRMED FAULT. VERIFIED ROTABLE COMPONENT MFG NR 442369 S/N NR 3219 REF IPC 73 21 10 01 ITEM 25T. REPLACED HMU REF MM 73 21SDR ASAA0852970Apu · oil consumptionAPU OIL COMSUMPTION INDICATE ALERT. STRIP AC FROM ETOPS SERVICES INSP, APU INTAKE EXHAUST AND APU AREA, NO OIL LEAKS NOTED AT THIS TIME. AC RESTRICTED FROM ETOPS UNTIL NEW APU OIL COMSUMPTION RATE IS CALULATED. INSPECTED APU, APU OIL LEVEL FULL CONSUMPTION SDR ASAA0852937Filter · dirtyCONT CABIN ZONE TEMP ILLUM ON RECALL BITE CHECK BOTH TEMP CONTROLLERS RT CONTROLLER SHOWED FLT DECK TRIM VALVE FAULT WHICH CLEARED. DUE PREVIOUS HISTORY 15 APR CONTINUED MEL 21 21C. INSTALLED PLAC VERIFIED FAULT REF MM 21 60 00, FOUND AIR FILTER OBSTRUCTED &SDR ASAA0852914Controller · malfunctionedAUTO FAIL LIGHT AND ALT LIGHT ILLUMINATED ON PRESSURIZATION PANEL. CYCLED TO ALT & BACK TO AUTO, FAULT LIGHT OUT. NR 1 & 2 CABIN PRESSURE CONTROLLERS BITE TEST GOOD.SDR ASAA0852896Filler · cloggedWHILE ACCOMPLISHING TASKCARD 78349013 FOUND APU OIL FILTER EXTENDED. COMPLETED OIL DELTA P INDICATOR SERVICING. REMOVED FILTER ELEMENT. LEAK AND OP CHECKS NORMAL.SDR ASAA0852895Condenser · odiferousAIRCRAFT HAS DIRTY SOCK SMELL FROM PACKS IN FLIGHT. REPLACED CONDENSER AND RE HEATER ASSEMBLIES ON RT AIR CONDITIONING BAY.SDR ASAA0852827Ecu · defectiveAPU GENERATOR INDICATES 15 AMPS WITH APU OFF JUST AS OCCURRED THE DAY BEFORE. REPLACED ECU APU ELECTRONIC CONTROL UNIT AFTER REPLACING GCU THE DAY BEFORE.SDR ASAA0852826Gcu · defectiveDURING CLIMB APU GENERATOR INDICATED 16 AMPS WITH APU NOT RUNNING. REPLACED GCU GENERATOR CONTROL UNIT.SDR ASAA0852820Controller · malfunctionedBOTH AIRCON PACKS ANNUNCIATED AFTER ENGINE START. BITE TESTED EACH TEMPERATURE CONTROLLER PER FIM 21 62 AND RESET.SDR ASAA0852818Modulating Valve · defectiveCABIN ZONE TEMPERATURE ANNUNCIATED ON MASTER CAUTION PANEL. REPLACED TEMPERATURE TRIM MODULATING VALVE.SDR ASAA0852752Fmc · malfunctioned"FMC DISAGREE" ANNUNCIATED ON ND AND FMC SCRATCH PAD. VERIFIED FMC DISAGREE FAULT. RESET FMC NR 1 COMP AND FMC NR 2 COMP C/B'S. FMC SYSTEMS LT AND RT GROUND TEST GOOD.SDR ASAA0852691Fmc · malfunctionedTHE "FMC DISAGREE" DISPLAYED ON FMC. ACCOMPLISHED FIM 34 61 TASK 835 & FMC BITE, OK. NO FURTHER DISCREPANCIES NOTED.SDR ASAA0752381Transceiver · intermittentNO SIDETONE ON HF1 FROM EITHER SEAT. HF1 RECEIVES OK. VOICE & SELCAL OTHER RADIOS WORK OK. ON CAPT'S SIDE VHF & F/O'S SIDE HF2 WORK OK. REPLACED NR 1 HF TRANSCEIVER. GROUND VERIFICATION TEST GOOD, VERIFICATION FLIGHT SATISFACTORY.SDR ASAA0752379Coupler · damagedNR 1 HF FAILED TO TRANSMIT. CONFIRMED FAILURE ON GROUND. REPLACED NR 1 HF ANTENNA COUPLER. OP CHECK & FVF GOOD.SDR ASAA0752272Light · inoperativeMODE CONTROL PANEL BACKGROUND LIGHTING INOP. REPLACED MODE CONTROL PANEL. OP CHECKS GOOD. BITE TEST PASS.SDR ASAA0752196Transceiver · inoperativeHF DATA LINK INOP. CW MM 23-11-00 NORMAL AND MM 23-27-00 NORMAL. UNABLE TO DUPLICATE. AIRCRAFT RELEASED FOR A NON ETOPS VERIFICATION FLIGHT TO CHECK NR 2 HF DATA LINK. NON ETOPS VERIFICATION FLIGHT SATISFACTORY.SDR ASAA0752145Controller · unknownZONE TEMP LIGHT FOR CONTROL CABIN CAME ON AFTER START OF ENGINES. COULD NOT EXTINGUISH. BITE ON NR 1 & 2 CABIN TEMP CONTROLLERS SHOW FAULT FLIGHT DECK CABIN SENSOR. ACCOMPLISHED FIM 21 62 TASK 801. FAULT & ZONE TEMP LIGHT CLEARED. BITE CHECKS GOOD.
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