N618CA
Service difficulty reports · 21
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 = 'N618CA' 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 = 'N618CA' 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 HYIA20181031002Spar Cap · corrodedDURING MAINTENANCE CORROSION WAS DISCOVERED ON THE LEFT HAND UPPER AFT SPAR CAP (P/N: 5122041-21). THIS CORROSION IS LOCATED BETWEEN LWS 229.71 AND 224.71, AND MEASURES .032 INCHES DEEP. THIS MEASUREMENT EXCEEDS THE LIMITS FOUND IN MEB95-11R1. THIS CAP WILL BESDR HYIA20181024001Spar Cap · corrodedDURING MAINTENANCE CORROSION WAS DISCOVERED ON THE LEFT HAND LOWER AFT SPAR CAP P/N 5122041-23, AT APPROXIMATE L.W.S. 215.20. THIS CORROSION IS MEASURED TO A DEPTH OF .019 INCHES AND IS BEYOND LIMITS FOUND IN MEB95-11R1. THIS CAP WILL BE REPLACED.SDR HYIA20160913151A/C Pack · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160913150Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA201608003018Ring · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. PISTON SHOWS SIGNS OF DAMAGED RINGS.SDR HYIA201608003017Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20150903001Unknown · odorPILOT REPORTED FUEL SMELL IN CABIN. INSPECTED LT & RT WING FUEL LINES, CABIN FUEL LINE, HEATER FUEL LINES & ENG LT & RT FUEL LINES, NO LEAKS NOTED.SDR HYIA20150729002O-Ring · leakingPILOT REPORTED FUEL ODOR IN CABIN. FOUND THE FUEL SUMP ON LEFT WING LEAKING. R & R O-RING ON SUMP. OPERATIONAL & LEAK CHECK GOOD.SDR HYIA20150102001Caliper · defectiveTHE BRAKES VERY WEAK, LT BRAKE IS NON-EXISTENT. R & R THE LT MLG CALIPER ASSEMBLY IAW MM CH 32-40-00. RT & LT BRAKES SERVICED IAW MM 12-10-05. OPERATIONS CHECKED GOOD.SDR HYIA20140929001Brake Sys · lowVERY POOR BRAKING ALMOST NOTHING. THIS WAS NOTED AFTER DEPARTURE WHICH INDICATES THE PROBLEM WAS FOUND ON LANDING. THE BRAKE SYS WAS THEN SERVICED IAW MM CH 12-10-03 & 32-40-00. OPERATIONS CHECKED TO ADDRESS THE ISSUE.SDR HYIA20140415067Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWSDR HYIA618CARHAXLEAxle · brokenON TAKEOFF ROLL, CREW EXPERIENCED A YAW WHICH CAUSED THE TAKEOFF TO BE DISCONTINUED AT LOW SPEED. CREW TAXIED BACK TO THE RAMP. MX FOUND RT MAIN GEAR AXLE ASSY BROKEN AT LOWER HALF. MX R & R AXLE ASSY, AND RETURNED THE ACFT BACK TO SERVICE.SDR HYIA20100512001Unknown · odorCREW REPORTED, ON CLIMB OUT, CABIN BECAME FILLED WITH SULFURIC / ELECTRICAL BURNING ODOR. CREW ELECTED TO REMAIN IN PATTERN AND RETURNED TO BASE, LANDING WITHOUT INCIDENT. PILOT REPORTED THAT ODOR MAY HAVE EMINATED FROM REAR OF ACFT. MX INSPECTED ACFT. COULD SDR HYIA618CATorque Link · brokenDURING TRAINING FLIGHT, AFTER TOUCH AND GO, DURING GEAR RETRACTION, CREW REPORTED RIGHT MAIN LANDING GEAR DOWNLOCK INDICATION REMAINED ILLUMINATED. PERFORMED "LANDING GEAR WILL NOT EXTEND HYDRAULICALLY" CHECKLIST WHICH RESULTED IN THREE GREEN LIGHTS. ON LANDINSDR HYIA618CAGRDownlock Switch · unserviceableCREW REPORTED NO NOSE GEAR DOWN LOCK INDICATION ON FINAL APPROACH. LIGHT TESTED MORMAL. CREW DECLARED EMERGENCY AND PERFORMED EMERGENCY GEAR EXTENTION. STILL NO NOSE GEAR INDICATION. LANDING WAS UNEVENTFUL. MX REMOVED AND REPLACED DEFECTIVE DOWN LOCK SWITCSDR 1350516N618CACircuit Board · defectiveCREW REPORTED AVIONICS MASTER INOP. MX CHANGED CIRCUIT BREAKER SWITCH.SDR HYI2006F00007Uplock Switch · failedCREW REPORTED RT MAIN GEAR DID NOT FULLY RETRACT WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE RT UPLOCK MICROSWITCH, GEAR SWING CHECKS OK. AIRCRAFT RELEASED FOR SERVICE. (K)SDR HYI2006F00006Uplock Switch · failedCREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE ATTEMPTED TO REMOVE AND REPLACE THE RT UPLOCK MICROSWITCH, 2 SWITCHES FAILED (BAD FROM STOCK) BEFORE INSTALLING A SERVICEABLE UNIT, GEAR SWING CHECKS, OK. AIRCRAFT RELEASSDR HYI2006F00004Uplock Switch · failedCREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE RT UPLOCK SWITCH, GEAR SWING CHECKS OK. AIRCRAFT RELEASED FOR SERVICE. (K)SDR HYI2002F00012Strut · damagedDURING TAXI, RIGHT MAIN LANDING GEAR STRUT ASSEMBLY BROKE AT ACTUATOR ATTACH COLLAR. UPON INSPECTION, FOUND STRUT HAD LOST NITROGEN CHARGE AND HAD BEEN TAXIED IN THE FULLY DEPRESSED POSITION, POSSIBLY DAMAGING THE STRUT INTERNALLY. THE LANDING GEAR DID NOT RSDR 99ZZZX2100Cap · leakingCREW REPORTED FUEL/FUEL PUDDLE ON COCKPIT FLOOR ON THE FIRST OFFICER'S SIDE. DIVERTED TO HYA EN ROUTE FROM BOS TO ACK. MAINTENANCE COULD NOT CONFIRM PUDDLING OF FUEL. FOUND FUEL STAIN (BLUE DYE) ON FUEL FLOW BLEEDER LINE ASSY. TIGHTENED AN 929-2 CAP. C/W
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