N524CA
Service difficulty reports · 20
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 = 'N524CA' 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 = 'N524CA' 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 HYIA20240711002Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CLOSEOUT RIB (P/N: 5122115-55) AT L.W.S. 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE AND TRAVELS VERTICALLY TO ASDR HYIA20240711001Rib · crackedDURING MAINTENANCE THREE CRACKS WERE VISUALLY IDENTIFIED ON THE RIGHT HAND CLOSEOUT RIB (OEM P/N: 5122115-56). ALL CRACKS ARE LOCATED IN THE AREA OF FASTENERS COMMON TO THE FORWARD TRUNNION SUPPORT. THESE CRACKS ARE CONSISTENT WITH OTHERS THAT HAVE BEEN FOUND SDR HYIA20221114001Attach Fitting · corrodedDURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND UPPER AFT OUTBOARD FORWARD WING ATTACH FITTING (P/N: 0822550-45). IT IS LOCATED ON THE BOTTOM FACE OF THE UPPER HORIZONTAL LEG OF THE FITTING AND MEASURES APPROXIMATELY .674 INCHESSDR HYIA20221005001Igniter · burnedTHE PILOT REPORTED AN ELECTRICAL SMELL IN THE COCKPIT DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND THE HEATER IGNITION SYSTEM BURNT. THIS WAS REPLACED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20190424001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE RIGHT HAND OUTBOARD NACELLE FITTING. (P/N: 5292029-24) THIS CRACK MEASURES APPROXIMATELY .100 INCHES LONG ON THE OUTBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKSDR HYIA20180215001Switch · failedPILOT REPORTED CABIN HEATER CIRCUIT BREAKER TRIPPED AND A STRONG ODOR IN THE CABIN. DURING INSPECTION THE HEATER OVERHEAT SWITCH WAS FOUND TO BE DAMAGED AND BURNED.SDR HYIA20170530001Fuel Line · damagedPILOT REPORTED BURNING SMELL IN CABIN, WITH THE ODOR SEEMING TO BE ASSOCIATED WITH THE HEATER. FOUND THE HEATER FUEL LINE DAMAGED. REPLACED THE FUEL LINE.SDR HYIA20161108187Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20161108186Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160803029Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160803028Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA2015072015Alternator · failedPILOT REPORTED LT & RT ALTERNATOR LIGHTS ILLUMINATED IN FLIGHT. R & R THE RT ALTERNATOR & RT VOLTAGE REGULATOR. PERFORMED PARALLELING. OPERATIONAL & LEAK CHECKED GOOD IAW MM CH 24-30-01.SDR HYIA20150529002Door · openPILOT REPORTED THE UPPER CABIN DOOR OPENED IN FLIGHT. INSPECTED THE UPPER CABIN DOOR LATCH WITH NO DEFECTS FOUND IAW MM CHAPTER 52.SDR HYIA20141202001Pump · faultySMELL OF FUEL IN THE CABIN WHEN HEATER TURNED OFF IN FLIGHT. R & R THE HEATER FUEL PUMP. OPERATIONAL & LEAK CHECK WAS SATISFACTORY.SDR HYIA20140414022Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & ASDR HYIA20120904001Hsi · failedDURING CRUISE, THE PILOT NOTED A THE ODOR OF SMOKE IN THE COCKPIT. AN UNSCHEDULED LANDING WAS MADE. THE PROBLEM WAS TROUBLESHOT TO A PICK UP IN THE HSI. THE HSI WAS R & R.SDR HYIA20120817003Exhaust Valve · damagedPILOT REPORTED THAT AFTER TAKEOFF, DURING CLIMB, THE LT ENGINE BEGAN RUNNING ROUGH. PILOT RETURNED TO DEPARTURE. ON MX INSPECTION, A DAMAGED EXHAUST VALVE WAS FOUND ON LT ENGINE NR 5 CYLINDER. CYLINDER WAS R & R. DAMAGE WAS ALSO NOTED TO THE LT ENGINE TURBSDR HYIA20140415001Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE SDR HYIA524CARMLGDownlock Switch · unserviceableCREW REPORTED RT MAIN LANDING DOWNLOCK LIGHT FAILED TO ILLUMINATE ON APPROACH. PERFORMED GEAR EXTENSION, WILL NOT EXTEND HY, LANDING WITH DEFECTIVE GEAR CHECKLIST. PERFORMED EMERGENCY GEAR EXTENSION, STILL NO DOWNLOCK INDICATION. DECLARED EMERGENCY, LANDING WSDR 97ZZZX4003Crankcase · crackedCREW REPORTED OIL LEAK, RIGHT ENGINE. UPON FURTHER INSPECTION, FOUND 1.25 INCH TO 1.5 INCH LONG CRACK IN CRANKCASE JUST AFT OF NR 2 CYLINDER, SEVENTH STUD, LOCATED IN WEB BETWEEN OIL COOLER MOUNTING AREA AND CYLINDER ATTACH AREA.
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