Agusta AW119MKII
Service difficulty reports · 71
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'AW119MKII' 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 aircraft_model_key = 'AW119MKII' 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 8LFA20170712003Fitting · crackedDURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT HAND PLATE FITTING CRACKED.SDR 8LFA20170712004Fitting · crackedDURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT HAND PLATE FITTING CRACKED.SDR 8LFA20170524001Damper · crackedFORKED END OF HOUSING HAS A CRACK PROPAGATING FROM ONE SIDE OF THE BUSHING BORE AROUND THE OPPOSITE SIDE OF THE BORE.SDR 8LFA20170712002Fitting · crackedDURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT HAND PLATE FITTING CRACKED.SDR QMLA2017041717039Retainer · crackedFOUND 2 EACH CRACKS AT STA 2049.5, BL 480 LT AND BL 480 RT. RETAINER AND 2 EACH CRACKS AT FASTENER STA 2049.5 LEFT/RIGHT WL 1150.0.SDR QMLA2017041717038Retainer · crackedFOUND 2 EACH CRACKS AT STA 2049.5, BL 480 LT AND BL 480 RT. RETAINER AND 2 EACH CRACKS AT FASTENER STA 2049.5 LEFT/RIGHT WL 1150.0, AND 1 CRACK RIGHT HAND DOOR POST AFT EDGE STA 2049.5 EXTENDING FROM WL 1400.0 TO 1402.0, CRACK IS APPROXIMATELY 1.5 INCHES LONG.SDR QMLA2017041717037Retainer · crackedFOUND 2 EACH CRACKS AT STA 2049.5, BL 480 LT AND BL 480 RT. RETAINER AND 2 EACH CRACKS AT FASTENER STA 2049.5 LEFT/RIGHT WL 1150.0.SDR QMLA2017041717036Retainer · corrodedFOUND 2 EACH CRACKS AT STA 2049.5, BL 480 LT AND BL 480 RT. RETAINER AND 2 EACH CRACKS AT FASTENER STA 2049.5 LEFT/RIGHT WL 1150.0.SDR 8LFA2016100600001Engine · overheatedDURING CRUISE FLIGHT, ABNORMAL ITT INDICATIONS STARTED TO OCCUR. ATTEMPTED TO TROUBLESHOOT, BUT ENGINE ITT WAS EXCEEDING LIMITATIONS ALLOWED. AIRCRAFT DECLARED EMERGENCY AND LANDED WITHOUT FURTHER PROBLEMS.SDR 8LFA2016100600002Door · out of alignmentDURING CLOSING OF THE LEFT HAND PASSENGER SLIDING DOOR, REAR GUIDE PIN WAS PULLED FROM STRUCTURE CAUSING DAMAGE. DAMAGE WAS DUE TO MISALIGNMENT OF DOOR AND WHEN CLOSED DID NOT CONTACT THE AIRCRAFT STRUCTURE IN THE CORRECT MANNER. DOOR POST REPAIRED.SDR QMLA2016061916069Fire Loop · nickedACFT HAD TO MAKE AN EMERGENCY LANDING WITH PATIENT ON BOARD DUE TO A CAUTIONARY FIRE DETECT LIGHT. THE TROUBLESHOOTING PROCEDURES WERE WENT THROUGH AND FOUND HALF WAY THROUGH THE FIRE DETECTION LOOP WERE IT WAS CLIPPED TO THE AIRFRAME THERE WAS NICK. THE NICSDR L2SA2016060700001Bypass Valve · failedPART FAILED, CLOSED, INFLIGHT CAUSING THE ENGINE OIL TEMPERATURE TO RISE 119 DEGREE C. THUS CAUSING A , RED MASTER WARNING LIGHT TO ILLUMINATE. THE PILOT SAFELY LANDED THE ACFT WITH NO ISSUES AND MAINTENANCE WAS CALLED TO TROUBLESHOOT. THE DISCREPANT PART WSDR QMLA2015090415082Bearing · crackedDURING A0521 NT, 100 HR TAIL ROTOR INSPECTION, WAS REMOVING THE TAIL ROTOR CROSS HEAD ASSEMBLY & FOUND THE BLADE END PC LINK BEARING CRACKED WITH A CHUNK MISSING FROM THE FLANGE AREA OF THE BEARING, THE SPHERICAL SURFACE WAS INTACT. R & R PC LINK. EXCESSIVE SDR 8LFA20150813001Blade · crackedDISCOVERED CRACK IN LE CAP OF TAIL ROTOR BLADE, APPROX CRACK IS 7MM IN LENGTH, STARTING 2MM FROM TIP END OF LE CAP, CRACK CONFIRMED USING DYE PENETRANT METHOD. ACFT TAKEN OUT OF SERVICE UNTIL REPLACEMENT PARTS COULD BE INSTALLED. ROTOR BLADE CAME NEW WITH ACSDR CA150413002Skin · cracked(CAN) DURING INSPECTION. TAIL BOOM WAS FOUND CRACKED ON OUTER SKIN, AT STABILIZER ATTACHMENT POINT LT SIDE.SDR 2015F00051Pump · failedAIRFRAME FUEL BOOST PUMP FAILEDSDR QMLA2015012315007Channel · damagedPOST FLIGHT, AFTER ACFT PUSHED INTO HANGAR. PIC DISCOVERED RT SIDE PAX DOOR STRIKER PLATE LOWER SCREW & RIVNUT WAS PULLED THROUGH AIRFRAME STRUCTURE. NOTED DEFORMED & MUSHROOMED HOLE & THREE CRACKS RADIATING FROM RIVNUT HOLE.SDR QMLA2014101014121Skin · crackedNOTICED SKIN CRACK IN LT SIDE OF AFT ENG COWL. FOUND TOTAL OF 5 CRACKS IN COWL SKIN & STRINGER CHANNELS.SDR CA140217007Engine · smoke(CAN) AME OBSERVED EXCESSIVE SMOKE FROM EXHAUST DUCT. ENGINE WAS OPERATING AT GROUND IDLE. NO SMOKE AT FLIGHT IDLE. BORESCOPE INSPECTION SHOWED SUBSTANTIAL CARBON DEPOSITS IN THE DOME AREA OF THE COMBUSTION LINER. BLACK DEPOSITS FOUND ON 2 FUEL NOZZLES TIPSSDR CA140127011Flange · damaged(CAN) AFTER SHUTDOWN, DURING ROTOR BRAKE APPLICATION, CREW REPORTED GRINDING NOISE COMING FROM TRANSMISSION AREA, AND EXCESSIVE VIBRATIONS WERE FELT THROUGH THE AIRFRAME. ACFT WAS INSPECTED BY MAINTENANCE, THE ROTOR BRAKE FLANGE AND OUTPUT SPLINE WERE FOUND TSDR CA130607001Fuel Tank · leaking(CAN) DURING FLIGHT CREW REPORTED ODOR COMING FROM CABIN AREA. ACFT WAS INSPECTED BY MAINTENANCE AND FOUND FUEL IN THE CABIN AREA. UPON REMOVING ALL THE FUEL BAY COVERS, THE RT AUX FUEL CELL WAS "SWEATING" FUEL ON THE ENTIRE FWD FACE OF THE FUEL BLADDER, THE
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