N514NC
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 = 'N514NC' 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 = 'N514NC' 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 HYIA20241018001Fitting · corrodedDURING MAINTENANCE 3 SPOTS OF CORROSION WERE VISUALLY IDENTIFIED ON THE OUTBOARD LEFT UPPER AFT WING FITTING (OEM PN: 0822550-45). ALL THREE SPOTS ARE LOCATED ON THE LOWER SURFACE OF THE HORIZONTAL FLANGE OF THIS FITTING, AND ARE CONSISTENT WITH OTHER CORROSIOSDR HYIA20210512001Crossbeam · crackedDURING INSPECTION A CRACK WAS VISUALLY DISCOVERED ON THE INBOARD END OF THE LOWER CHANNEL OF THE RIGHT HAND CROSSOVER BEAM. THIS CRACK IS IN THE AREA OF THE MOUNTING HOLES FOR THE INBOARD EXHAUST ELBOW CLAMP BRACKET, AND MEASURES APPROXIMATELY 2 INCHES LONG ANSDR HYIA20200508001Connecting Rod · damagedDURING ROUTINE INSPECTION AND REPLACEMENT OF THE RIGHT ENGINE CYLINDER #3 IT WAS DISCOVERED THAT THE CONNECTING ROD BUSHING OF THE #3 CYLINDER WAS FOUND TO BE DAMAGED AND LOOSE. THE CONNECTING ROD AND CYLINDER WILL BE REPLACED.SDR HYIA20190117001Beam · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE RIGHT NACELLE INBOARD CROSSOVER BEAM SUPPORT CHANNEL P/N: 5654102-15. AFTER REMOVING THIS CHANNEL IT WAS DISCOVERED THAT THE RIGHT HAND INBOARD BEAM, P/N: 5654109-7 WAS CRACKED UNDERNEATH THE SUPPORT CHANNEL. THSDR HYIA20180926001Engine · making metalPILOT REPORTED RIGHT ENGINE OIL PRESSURE DROPPED TO 20 PSI IN FLIGHT AND TO ZERO PSI AT IDLE ON THE GROUND. MAINTENANCE INSPECTED AND FOUND METAL PARTICLES AT THE OIL PRESSURE RELIEF VALVE, FURTHER INSPECTION FOUND THE STARTER ADAPTER NEEDLE BEARING DAMAGED. TSDR HYIA20170821001Rib · crackedDURING A ROUTINE INSPECTION, A CRACK WAS LOCATED AT RIB RT WS. 106.79. THE CRACK WAS 1.5 INCHES IN LENGTH, REPLACED THE RIB IAW MM.SDR HYIA20170828017Fitting · crackedDURING A ROUTINE INSPECTION, TWO CRACKS WERE FOUND IN THE RT OUTBOARD NACELLE FITTING. THESE CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THEY MEASURED .119 AND .146 IN LENGTH.SDR HYIA20160913157Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160913156Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160913155Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160205002Alternator · failedPILOT REPORTED LOSING BOTH ALTERNATORS IN FLIGHT AFTER A MODERATE JOLT OF TURBULENCE, RETURNED WHEN THEY COULD ONLY RESET ONE ALTERNATOR BY FOLLOWING THE QRH PROCEDURE OF REPLACING FIELD FUSES. INSPECTED & REPAIRED SHORTED F1 WIRE IN RT NACELLE, AS WELL AS RESDR HYIA20150227002Warning System · false activationPILOT REPORTED CABIN DOOR OPEN ON TAKEOFF. INSP THE MAIN CABIN DOOR TOP & BOTTOM WITH NO DISCREPANCY NOTED. REPLACED WORN SPRING ON THE OUTSIDE HANDLE AS PRECAUTION. OPERATIONAL CHECKED OK.SDR HYIA20120528528Gauge · leakingPILOT REPORTED A PREVELENT FUEL ODOR DURING ALL GROUND OPERATIONS AND DURING CLIMBOUT. PILOT NOTED WHAT APPEARED TO BE FUEL IN BOTTOM OF FUEL FLOW INDICATOR. ON INSPECTION, EVIDENCE OF FUEL STAINS AT THE BOTTOM OF FUEL FLOW GAUGE WERE NOTED. BASED ON THIS FISDR HYIA5112FUELODORB-Nut · loosePILOT REPORTED A FUEL ODOR IN THE COCKPIT. ODOR WAS FOUND TO BE CAUSED BY A LEAKING B-NUT ON THE HEATER FUEL PUMP. B-NUT WAS THEN SECURED, AND THE AREA WAS CHECKED WITH NO LEAKS.SDR HYIA20140414005Drag 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 HYIA20140415032Drag 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 HYIA514NC RMLGSeal · leakingCREW REPORTED, ON APPROACH, AFTER GEAR EXTENSION, GEAR UNLOCK LIGHT REMAINED ILLUMINATED WITH NO RT MLG DOWNLOCK INDICATION. PERFORMED EMERGENCY EXTENSION OF LANDING GEAR, AND DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. MX FOUND RT MAIN GEAR DOWNLOCK SWITCSDR N514NCWire · chafedCREW SMELLED BURNING ODOR IN COCKPIT DURING FLIGHT. MX INSPECTED AND FOUND WIRES IN NLG WHEEL WELL CHAFED. MX REPAIRED WIRING AND RELEASED A/C.SDR 1350527514Circuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH, MFG DATE CODE 0527.SDR HYI2003F00008Master Switch · inoperativeAVIONICS MASTER SWITCH INOPERATIVE. MAINTENANCE REPLACED SWITCH AND RETURNED THE AIRCRAFT TO SERVICE.SDR 20010403CW011Strut · dischargedUPON GEAR RETRACT, HYDR PRES LIGHT REMAINED ILLUMINATED. GEAR EXTENSION WAS ATTEMPTED, NOSE GEAR FAILED TO EXTEND. GEAR WAS EXTENDED USING EMERGENCY BLOW DOWN PROCEDURE, ALL GEAR DOWN INDICATORS SHOWED GREEN AND AIRCRAFT LANDED WITHOUT INCIDENT. MECH FOUND
Back to N514NC