N68752
Service difficulty reports · 16
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 = 'N68752' 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 = 'N68752' 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 HYIA20230210001Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE RIGHT HAND CLOSEOUT RIB (P/N: 5122115-56) AT R.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 FORWARD AN APPSDR HYIA20230113001Fitting · damagedDURING MAINTENANCE, A SPOT OF DAMAGE WAS VISUALLY IDENTIFIED ON THE RH FWD WING ATTACH FITTING (PN: 082550-46). THIS DAMAGE IS LOCATED ON THE TOP EDGE OF THE FITTING AS SEEN THROUGH THE WING GAP PANEL 611AT INBOARD OF RWS 58.94. THIS DAMAGE MEASURES APPROXIMASDR HYIA20201112001Fitting · 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 .102 INCHES LONG ON THE OUTBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACSDR HYIA2020090131001Cylinder · damagedPILOT REPORTED MAGNETO ROUGH IN FLIGHT. MAINTENANCE INSPECTED AND FOUND OIL IN THE #5 CYLINDER. UPON REMOVAL OF THE CYLINDER IT WAS FOUND TO HAVE MISSING MATERIAL AT THE VALVE INTAKE GUIDE. THE #5 CYLINDER WAS REPLACED WITH NO FURTHER DEFECTS NOTEDSDR HYIA20190515002Cylinder · failedPILOT REPORTED A ROUGH ENGINE; "MISSING" WHEN PROPS BROUGHT BACK FOR CRUISE AND STRONG VIBRATIONS ON FINAL APPROACH. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINE NR 4 CYLINDER EXHAUST VALVE GUIDE TO HAVE PLAY, THE EXHAUST VALVE CHIPPED, AND THE EXHAUST VALVSDR HYIA20180928001Pushrod · brokenPILOT REPORTED THE LEFT ENGINE RUNNING ROUGH IN FLIGHT AND OIL PRESSURE WENT TO ZERO PSI. PRELIMINARY INSPECTION FOUND METAL CONTAMINATION IN OIL FILTER, #4 CYLINDER INTAKE PUSH ROD BROKEN AND A LARGE GAP AT THE EXHAUST ROCKER ARM. THE ENGINE IS BEING REPLACEDSDR HYIA20180813001Engine · surgesPILOT REPORTED THE ENGINE SURGED TO A POINT OF UNCONTROLLABLE AFTER TAKE-OFF. THE ENGINE WAS INTENTIONALLY SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE ISSUE. OPENSDR HYIA20160323002Nut · crackedDURING INSPECTION, LT ENG SN 1004575, IT WAS DISCOVERED THE UPPER THROUGH BOLT NR 1 MAIN BEARING SADDLE RT NUT FRACTURED, CAUSING THE THROUGH BOLT TO MIGRATE OUT OF POSITION.SDR HYIA20150723002Caliper · failedPILOT REPORTED LT BRAKES INOPERATIVE. R & R THE LT BRAKE CALIPER & BLED BRAKES. OPERATIONAL & LEAK CHECKED GOOD.SDR HYIA20140414026Drag 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 HYIA20140415063Drag 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 HYIA20140415017Drag 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 OSDR HYIA68752RBRK810Master Cylinder · underservicedCREW REPORTED, RT BRAKE FAILED ON TAXI WHICH LEAD TO AFT PROCEEDING INTO GRASS OFF TAXIWAY. MX INSPECTED ACFT BRAKING SYS, SERVICED RT MASTER CYLINDER. ACFT RELEASED BACK TO SERVICE.SDR HYIA68752Master Switch · unserviceableCREW REPORTED AVIONICS MASTER SWITCH INOP. MAINTENANCE REMOVED AND REPLACED CIRCUIT BREAKER SWITCH.SDR HYIA13568752Torque Tube · brokenON APPROACH, RT RUDDER PEDAL WENT TO FLOOR. APPROACH WAS CONTINUED, LANDING UNEVENTFUL. MAINTENANCE FOUND RUDDER PEDAL ATTACH BRACKET HAD FAILED. REMOVED AND REPLACE TORQUE TUBE AND RELEASED AIRCRAFT BACK TO SERVICE.SDR HYI2003F00005Master Switch · failedSWITCH FAILED, MAINTENANCE REPLACED SWITCH AND RETURNED THE AIRCRAFT TO SERVICE.
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