N565AS
Service difficulty reports · 509
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 = 'N565AS' 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 = 'N565AS' 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 ASAA0954639Modulating Valve · inoperativeZONE TEMP LIGHT INOP (CONTL CAB) LIGHT GOES OUT WHEN RECALL RESET. FOUND FLT DECK TRIM VALVE LIGHT ON WHILE PERFORMING BITE CHECK. VERIFIED VALVE P/N W 398908 3. INSTALLED THE SERVICEABLE TRIM AIR MODULATING VALVE. PERFORMED BITE CHECK OF BOTH TEMP ZONE COSDR ASAA0954599Filter · faultyWHILE DOING NR 1 ENGINE EGB CHIP DETECTORS FOUND OIL SUPPLY FILTER DELTA P EXTENDED. REMOVED INSPECTED AND REPLACED NR 1 ENGINE OIL SUPPLY FILTER. RESET POP OUT INDICATOR. NO CONTAMINATION FOUND IN FILTER. IDLE LEAK CHECK GOOD. SERVICED ENGINE WITH 2 QTS SDR ASAA0954598Pump · leakingDURING IDLE ENGINE RUN DISCOVERED NR 1 ENGINE LEAKING FUEL FROM FUEL PUMP PAD DRAIN AT A RATE OF 63 DROPS PER MINUTE. REPLACED THE NR 1 ENGINE FUEL PUMP PER MM 73 11 01. ALL LEAK AND OPS CHECKS ARE GOOD.SDR ASAA0954377Circuit Breaker · trippedFOUND STANDBY BUS SECT 2 CIRCUIT BREAKER TRIPPED. GROUNDED YES. RESET STANDBY BUS C/B & PERFORMED STANDBY POWER TEST PER MM 24 34 00 710 800. OPS TEST NORMAL.SDR ASAA0954297Autopilot Sys · malfunctionedDURING THE FLARE THE APCH WARNING CAME ON BOTH THE FO'S PANEL LIGHTS AND THE CAPT'S HUD. THE RWY EDGE LINES ON THE HUD DID NOT ALIGN WITH THE RWY EDGE AND THE A/C VEERED OFF SHARPLY TO THE LT DISCONNECTED THE A/P AND LANDED MANUALLY. GROUNDED YES. DFCS LOGGSDR ASAA0954262Lamp · failedCSD NR 2 DOES NOT HAVE A "DRIVE" LIGHT ILLUMINATED. GROUNDED YES. R&R NR 2 ENG IDG PER MM 24-11-11. OPS/LEAK CK GOOD PER MM 24-11-11. RELAMPED GENERATOR DRIVE LIGHT AND GEN OFF BUSS LIGHT.SDR ASAA0954251Warning System · activatedFAULT LIGHT ILLUMINATED DURING START GROUNDED YES. CK APU BITE NO FLAME 49 41011 SHUT DOWN C/W FIM TASK 49 40 00 810 802 APU STARTED NORMAL. SEAMC TIM NOTIFIED. NO FAULTS NOTED AT START NO HISTORY WITHIN 30 DAYS.SDR ASAA0954241Modulating Valve · malfunctionedAFTER START ZONE TEMP LIGHT ILLUMINATED FOR "CONT CAB". GROUNDED YES. INSTALLED SERVICEABLE TRIM AIR MODULATING VALVE PERFORMED BITE CHECK ON BOTH ZONE TEMP. CONTROLLERS. NO FAULTS LOGGED. PRESSURIZED PNEUMATIC SYSTEM LEAK CK. NORMAL. REF. AMM 21 61 21.SDR ASAA0854108Sensor · faultedAPU FAULT LIGHT ILLUMINATED. GROUNDED YES. VERIFIED DISCREPANCY CURRENT STATUS SHOWS FAULT CODE 49 61223.FOLLOWED FIM 49-60 TASK 812 R&R INLET TEMP SENSOR GROUND VERIFICATION TEST PASSED REF FIM 49-60 TASK 801.
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