N6879R
Service difficulty reports · 31
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 = 'N6879R' 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 = 'N6879R' 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 HYIA20241106001Fitting · corrodedDURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE AFT FACE OF THE LEFT HAND UPPER FUSELAGE ATTACH FITTING (OEM PN: 0811350-9). THIS CORROSION MEASURES APPROXIMATELY .400 INCHES LONG .150 WIDE, AND HAS AN APPROXIMATE DEPTH OF .015. THIS CORRSDR HYIA20240718002Axle · brokenDURING TAXI OUT THE PILOT REPORTED THE LEFT MAIN LANDING GEAR AXLE BROKE. MAINTENANCE INSPECTED AND CONFIRMED THE AXLE WAS BROKEN, THE LOWER LEG AND AXLE WERE REPLACED WITH NO FURTHER ISSUES.SDR HYIA20210823001Engine · making metalTHE PILOT REPORTED THE LEFT ENGINE HAD A LOSS OF POWER IN AND THE OIL PRESSURE FELL TO ZERO. MAINTENANCE INSPECTED AND FOUND METAL PARTICLES IN THE OIL FILTER. AN ENGINE HAS BEEN ORDERED TO REPLACE THIS ENGINE. FURTHER DETAILS ARE TO BE PROVIDED UPON ENGINE SDR HYIA202001032001Display · failedPILOT SMELLED SOMETHING BURNING AFTER TURNING WEATHER RADAR ON. SMALL WHIFF OF SMOKE FROM BEHIND INSTRUMENT PANEL WHICH WENT AWAY, BUT SMELL PERSISTED. WEATHER RADAR DISPLAY DOES NOT WORK. MAINTENANCE INSPECTED FOR BURNT WIRES AND COULD NOT FIND DEFECT, SYSTEMSDR HYIA20190806001Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS IDENTIFIED ON THE INBOARD LEG OF THE LEFT HAND OUTBOARD FITTING (P/N 5292029-23.) THIS CRACK MEASURES APPROXIMATELY .100, AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54SDR HYIA20190426001Exhaust Valve · damagedDURING INSPECTION THE #4 CYLINDER OF THE LEFT ENGINE WAS FOUND TO HAVE LOW COMPRESSION. UPON FURTHER INSPECTION THE EXHAUST VALVE HAD FOUR SMALL CHIPS IN THE EDGE OF THE VALVE, AND THE EXHAUST VALVE SPRING HAD PIECES THAT HAD COME APART. NO DAMAGE TO THE ROCKSDR HYIA20190315001Unknown · malfunctionedPILOT REPORTED RUDDER TRIM JAMMED IN FLIGHT. MAINTENANCE INSPECTED AND WAS NOT ABLE TO DUPLICATE THE DISCREPANCY ON THE GROUND. MAINTENANCE INSPECTED RUDDER TRIM SYSTEM CHAIN, CABLE, BLOCKS, LUBED RUDDER TRIM ACTUATOR SCREW ASSEMBLY AS PRECAUTIONARY MEASURES ASDR HYIA20190315002Cylinder · leakingPILOT REPORTED SHAKING FELT IN AIRFRAME DURING CLIMB/CRUISE WITH NO ABNORMAL ENGINE INDICATIONS ON INSTRUMENTATION. MAINTENANCE INSPECTED AND FOUND THE RIGHT ENGINE #6 CYLINDER TO HAVE LOW COMPRESSION. THE CYLINDER WAS REPLACED ALONG WITH THE RIGHT MAGNETO ANSDR HYIA20190208001Cylinder · leakingPILOT REPORTED A SHAKING FELT IN AIRFRAME DURING CLIMB AND CRUISE. MAINTENANCE INSPECTED AND FOUND THE #6 CYLINDER OF THE LEFT ENGINE TO HAVE LOW COMPRESSION. THE LEFT ENGINE RIGHT MAGNETO WAS FOUND TO HAVE INTERNAL OIL AND THE #1 CYLINDER IGNITION CABLE WAS FSDR HYIA20180102001Mount Bolt · missingPILOT REPORTED OIL LEAK IN FLIGHT AND OIL PRESSURE DECREASING ON THE RIGHT ENGINE. UPON INSPECTION MAINTENANCE DISCOVERED ONE STARTER MOUNT BOLT NUT MISSING. STARTER HAD BEEN REMOVED FOR OTHER MAINTENANCE 99.5 HOURS PRIOR. AIRCRAFT HAD GONE THROUGH ROUTINE INSSDR HYIA20180823003Engine · making metalPILOT REPORTED THE LEFT ENGINE OIL PRESSURE DROPPED TO BOTTOM OF GREEN ARC DURING CRUISE. MAINTENANCE INSPECTED AND FOUND METAL PARTICLES IN OIL SYSTEM. THE ENGINE HAS BEEN REPLACED.SDR HYIA20161109201Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160912135Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160825098Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160727001Dimmer · failedPILOT REPORTED SMOKE PRESENT IN FRONT OF THROTTLES, COMING OUT OF THE SIDE OF THE CONSOLE DIMMER SWITCH. MAINTENANCE INSPECTED DIMMER ASSEMBLY AND ASSOCIATED WIRING. FOUND FAILED CIRCUIT IN DIMMER ASSEMBLY. REMOVED AND REPLACED DIMMER ASSEMBLY.SDR HYIA20160323003Link · brokenPILOT REPORTED GEAR DOOR RIPPED OFF UPON EXTENSION. THE DOOR LINK WAS FOUND BROKEN AT THE ADJUSTMENT NUT ON THE DOOR SIDE. REMOVED THE REMAINDER OF GEAR DOOR & INSTALLED REPLACEMENT DOOR.SDR HYIA20140414057Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMESDR HYIA20140415009Drag 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 HYIA6879RHTRIgnition Unit · shortedCREW REPORTED, CABIN HEATER INOPERATIVE DURING FLIGHT. 20 MINUTES PRIOR TO REACHING FINAL DESTINATION, CREW REPORTED ODOR OF SOMETHING MELTING OR SMOLDERING. HEATER WAS TURNED OFF, AND HEATER FUEL SOURCE WAS TURNED OFF ALSO. AFTER A FEW MINUTES, ODOR WENT AWASDR HYIA6879RDEICEDeice System · malfunctionedCREW REPORTED, AT CRUISE ALTITUDE, ACFT BEGAN ENCOUNTERING ICING CONDITIONS. WING AND STABILIZER DEICE BOOTS FAILED TO REMOVE ICE. CREW REPORTED SURFACE DEICE SYS AS INOPERATIVE ALTHOUGH SYS HAD CHECKED NORMAL EARLIER IN THE DAY. SEVERAL ATTEMPTS AT CHANGING SDR HYIA6879RRTENGExhaust Valve · failedCREW REPORTED, DURING INITIAL CLIMB OUT, EXPERIENCED PARTIAL POWER LOSS ON RT ENG, CONSISTENT WITH LOSS OF TURBOCHARGER. CONTINUED CLIMB OUT AT FULL POWER TO CRUISE SETTING AT 7000 FT WHILE DECLARING AN EMERGENCY AND REQUESTING DIVERSION. EXPERIENCED OIL LEAKSDR HYIA6879RSwitch · unserviceableCREW REPORTED ELECTRICAL ODOR PRESENT WHEN INSTRUMENT LIGHT MASTER SWITCH TURNED ON. TURNED SWITCH OFF ODOR WENT AWAY. REMOVED AND REPLACED INTRUMENT LIGHTING MASTER SWITCH.SDR 1356879RAxle · brokenRIGHT MAIN GEAR AXLE BROKE ON TAXI IN.SDR 1356879R0501Axle · brokenRIGHT MAIN GEAR AXLE BROKE ON TAXI IN.SDR HYIA135Engine · failedDURING CRUISE FLIGHT NR 1 ENGINE VIBRATED THEN LOST POWER, ENGINE WAS SHUT DOWN. LEFT ENG HAD A INTERNAL FAILURE, ENG WAS REMOVED AND REPLACED. AIRCRAFT RETURNED TO SERVICE. FAILED ENG HAS BEEN SENT TO MANUFACTURE FOR TEARDOWN AND INVESTIGATION.SDR 1350606N6879RCircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER INOP. MX CHANGED CIRCUIT BREAKER.SDR HYI2002F00006Master Switch · failedON PRE-FLIGHT INSPECTION, AVIONIC MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE.SDR HYI2001F00005Master Switch · failedON PREFLIGHT INSPECTION AVIONIC MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE.(K)SDR HYI2001F00000Case · damagedAIRCRAFT WAS AT CRUISE ALTITUDE, WHEN THE RIGHT ENGINE SHUTTERED, FOLLOWED BY A BANG AND LOSS OF POWER. CREW SECURED THE ENGINE AND LANDED WITHOUT INCIDENT. MECHANIC DETERMINED THE ENGINE EXPERIENCED AN INTERNAL FAILURE, RESULTING IN 2 ONE INCH HOLES IN THE SDR 2001F00039Fuse · blownCREW NOTICED SMELL OF SMOKE, LEFT ALTERNATOR OUT LIGHT ILLUMINATED, FOUND LEFT ALTERNATOR FIELD FUSE BLOWN. MECHANIC REPLACED FUSE, INSPECTED ALTERNATOR WIRING, ALTERNATOR, VOLTAGE REGULATORS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.SDR 98ZZZX3883Uplock Hook · failedTHE LT MAIN GEAR UPLOCK HOOK FAILED ON RETRACTION. FAILURE OCCURRED ACROSS THE UPLOCK HOOK BOSS SEPARATING THE UPLOCK ACTUATOR FROM THE HOOK PORTION OF THE UPLOCK ASSY CAUSING THE GEAR TO REMAIN LOCKED IN WHEEL WELL UPON EXTENSION. EMERGENCY PROCEDURES FAILE
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