Eurocopter EC120B
Service difficulty reports · 222
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 = 'EC120B' 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 = 'EC120B' 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 HE17107982Cable · bindingCOLLECTIVE BINDING IN FLT FOUND ANTICIPATOR CONTROL CABLE BINDING. REMOVED AND REPLACED CABLE. (K)SDR ALG2006F00009Engine · inoperativePILOT REPORTED T4 EXCEEDANCE. AIRCRAFT DIVERTED FOR MAINTENANCE. FOUND 2 T4 EXCEEDANCES. ONE OF 13 SECONDS AT 998C. REMOVED AND REPLACED ENGINE. (K)SDR CA060124003Spherical Stop · corroded(CAN) ON MONDAY 16 JANUARY 2006, PILOT REPORTED COLLECTIVE WAS ROUGH AT HIGH POWER SETTING. HE WAS UNABLE TO REPLICATE. (TC NR 20060124003)SDR HE17107526Blade · chippedTAIL ROTOR BLADE FAILED INSP. PER AMM 64-21-00,6-9 ZONE ISDR CA051208004O-Ring · deformed(CAN) PRIOR TO THE SECOND FLIGHT OF THE DAY THE PILOT NOTICED HYDRAULIC FLUID ON THE SIDE OF THE FUSELAGE. FURTHER INSPECTION REVEALED LEAK ORIGINATED FROM THE HYDRAULIC COMPACT UNIT. THE O-RING ON THE FILTER SHROUD HAD FAILED. O-RING REPLACED. AIRCRAFT GROUSDR ALG2005F00093Pressure Switch · inoperativeINFLIGHT, THE CAUTION WARNING TONE SOUNDED. WHEN LANDING, THE MGB CHIP LIGHT ILLUMINATED. REMOVED AND REPLACED TRANSMISSION PRESSURE SWITCH IAW MM. CHECKED GOOD. (K)SDR ALG2005F00105Powerpack · malfunctionedBEFORE TAKEOFF, HYDRAULIC CAUTION LIGHT ILLUMINATED AND THE PILOT FELT FEEDBACK IN THE CYCLIC FORE AND AFT. REMOVED AND REPLACED HYDRAULIC POWER PACK. (K)SDR ALGA107785Unknown · wornWORN BEYOND LIMITS IN DROOP AREA. REPLACED UNIT WITH NEW SERVICEABLE PART.SDR ALG2005F00091Wire Harness · failedIN FLIGHT, T4 PORTION OF FLI- INTERMITTENT FLUCTUATION AND T-4 FAILURE. REMOVED HARNESS SN 215B,, INSTALLED HARNESS 279B, OPERATION CHECK GOOD. (K)SDR ALG2005F00115Windshield · crackedDURING PREFLIGHT FOUND 5 SEPARATED, DEBONDED AREAS ON WINDOWS AND A CRACK IN THE WINDSHIELD. INSPECTION BY MAINT REVEALED THE NR 8 TAIL ROTOR DRIVE SHAFT HAD FAILED. A WO WAS OPENED FOR REPAIR OF THIS AC. REMOVED AND REPLACED PILOTS WINDSHIELD. (K)SDR U0GA106525Fuel Cell · leakingPILOT REPORTED SMELL OF FUEL IN COCKPIT FOR 5 - 10 MINUTES DURING CRUISE FLIGHT. UPON LANDING, MAINENANCE DISCOVERED A LEAK IN IN THE UPPER FUEL CELL AT THE AFT R/H SEAM.SDR ALG2005F00086Plate · debondedDURING POST FLIGHT, THE PILOT SUSPECTED THAT M/R DROOP STOP PLATE IS DEBONDED, NOTIFIED MAINTENANCE. THE MECHANIC REMOVED M/R HUB AND BLADE TO GAIN ACCESS TO THE WEAR PLATES AND FOUND BOTH UPPER AND LOWER WEAR PLATED WERE DEBONDED, REMOVED AND REPLACED BOTH WSDR ALG2005F00087Control Rod · out of adjustDURING HOVER, ROTOR RPM WAS LOW, LANDED AND NOTIFIED MAINTENANCE. FUEL CONTROL WAS REPLACED THE NIGHT BEFORE. ADJUSTED GOVERNOR CONTROL ROD IAW MM AND RFM. GROUND RUN AND OPS. CHECK GOOD. (K)SDR ALG2005F00060Fuel Control · failedON THE FIRST HOVER FLIGHT OF THE DAY. IN HOVER FLIGHT, THE ROTOR RPM BLEED OFF AND WOULD NO RECOVER. NOTIFIED MAINTENANCE OF THE PROBLEM. FUEL CONTROL WAS REPLACED IAW MM. AC RETURNED TO SEVICE UPON COMPLETION OF ALL FUNCTIONAL CHECKS. (K)SDR ALG2005F00057Indicator · malfunctionedAT HOVER, A GUST OF WIND HIT THE AC REQUIRING MORE RT PEDAL AS A RESULT THE TORQUE REACHED 111 PERCENT FOR 1 SECOND. THE TAKEOFF WAS ABORTED AND MAINTENANCE WAS NOTIFIED. THE MECHANIC INSPECTED THE T/R GB, T/R DRIVE SHAFT DISC PACKS AND BEARINGS ALSO INPUT DSDR ALGA105168Coupling · crackedCRACKED LAMINATE / REPLACED WITH NEW BY FIELD MAINTENANCE.SDR ALG2005F00055Fuel Control · malfunctionedIN CRUISE FLIGHT, THE TURBINE SURGED WHICH WAS CONFIRMED WITH ENGINE NOISE LEVEL CHANGE. UPON LANDING THE MECHANIC REMOVED AND REPLACED THE FUEL CONTROL AND THE AC WAS RETURNED TO SERVICE UPON COMPLETION OF ALL FUNCTION CHECKS IAW MM. (K)SDR ALGA105148Tail Wheel · crackedCRACKED LAMINATE / REPLACED WITH NEW BY FIELD MAINTENANCE.SDR ALG2005F00036Accumulator · malfunctionedAT HOVER FOR TAKEOFF, PICKED AIRCRAFT UP TO A HOVER 2 TIMES AND BOTH TIMES AT A STEADY HOVER, AIRCRAFT OSCILLATED FORE AND AFT WITH NO PILOT INPUT (NOSE UP AND DOWN). MAINTENANCE INSPECTED SERVO INPUTS FOR WEAR, NO DEFECTS FOUND, SERVICED SERVO CONTROL ACCUMUSDR ALGA104383Scissors · debondedWEAR PLATE DEBONDED / REPLACED WITH NEW OR SERVICEABLE BY FIELD MAINTENANCE.SDR ALG2005F00031Window · separatedWHILE IN FLIGHT, TRAVELING APPROX 105 KNOTS AT 800 FEET THE TOP AFT CORNER OF THE PILOTS WINDOW DELAMINATED AND POPPED OUT APPROX 1 INCH. IMMEDIATELY FOLLOWING (2-3 SECONDS) THE ENTIRE WINDOW DELAMINATED AND SEPARATED FROM THE AIRCRAFT. I SLOWED THE AIRCRAFTSDR ALGA104413Coupling · crackedONE LAMINATE CRACKED. REPLACED WITH NEW BY FIELD MAINTENANCE.SDR ALGA101077Pin · corrodedEXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS, SCRAPPED PINS.SDR ALGA101076Pin · corrodedEXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS, SCRAPPED PINS.SDR ALGA101075Pin · corrodedEXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS, SCRAPPED PINS.SDR ALGA101074Pin · corrodedEXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS, SCRAPPED PINS.SDR ALGA101073Pin · corrodedEXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS. SCRAPPED PINS.SDR ALGA101072Pin · corrodedEXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS. SCRAPPED PINS.SDR TXER104274Servo · leakingSERVO LEAKING.SDR ALGA099803Swashplate · debondedDEBONDED, REPLACED WITH NEW PART IN FIELD.SDR ALGA099525Blade · chippedCHROME MONOXIDE SURFACE CHIPPED BEYOND LIMITS. SEND TO AMERICAN EUROCOPTER FOR WARRANTY CONSIDERATION.SDR CA050216007Rivet · loose(CAN) DURING AME DAILY INSPECTION LT HORIZONTAL STABILIZER FOUND TO HAVE APPROXIMATE 1 INCH VERTICAL DISPLACEMENT AT TIP. RIVETS THAT SECURE THE OUTER SHIM HAD SHEARED ALLOWING BUSHING MOVEMENT. SB 55-001 TO BE INCORPORATED , NOT PREVIOUSLY COMPLIED WITH. TO SDR ALGA099103Bushing · migratedAT 500HR INSP FOUND BUSHING SLID OUT OF PLACE. POSSIBLE MANUFACTURER DEFECT. REPLACED WITH NEW OR SERVICEABLE PART BY O/H SHOP.SDR TXER099450Hub · wornWEAR LIMITS EXCEEDED ON TAIL ROTOR HUB.SDR ALGA098149Scissors · debondedPLATE DEBONDED. REPLACED WITH SERVICEABLE SCISSOR.SDR TXER099765Servo · leakingCYCLIC SERVO LEAKING.SDR CA041014001Magnetic Plug · crackedPILOT REPORTED INTERMITTENT INDICATION OF GEARBOX CHIP DETECTOR. ON INSPECTION NO CHIP FOUND. A LOOSE CONNECTION BETWEEN ELECTRICAL PORTION OF CHIP PLUG & MAGNETIC PART ALLOWED FOR A FALSE INDICATION. THE SWAGGED CONNECTION BETWEEN THE TWO PARTS CRACKED & BRSDR ALGA097671Disc Pack · crackedFOUND CRACKED LAMINATES. REPLACED W/NEW PART.SDR TXER097638Coll Pitch Cntr · bindingCOLLECTIVE BINDING .SDR ALGA097750Disc Pack · crackedCRACKED LAMINATE/REPLACED WITH NEW.SDR ALG2004F00065Warning Light · false activationARRIVED AT E1107A TO PICK UP 1 PASSENGER, LOADED PASSENGER WHILE RUNNING. COMPLETED THE PRE TAKEOFF CHECKS AND BROUGHT AIRCRAFT TO A HOVER. DURING TAKEOFF THE 1.5 SECOND WARNING WENT OFF AND NOTICED THA THE TORQUE ON THE VEMD WAS UNDERLINED AND THE NEEDLE HADSDR CA040914005Windshield · debonded(CAN) WINDOW LT UPPER PN C561S3101202, DEBONDING 11.SDR CA040914003Pump · shortedDURING START SEQUENCE, ELECTRIC BOOST PUMP TRIPPPED CIRCUIT (3A) BREAKER. PUMP REPLACED.AF FUEL SYSTEM FILTER CONTAINED APPROXIMATELY 10 SMALL, NON-FERROUS, METAL SLIVERS. PRESUMED TO BE ALUMINUM. (PRIOR START PUMP CHANGED DUE TO NON-FERROUS METAL GENERATIONSDR TXER100925Tail Rotor · wornTAIL ROTOR, OUT OF LIMITS PER 64-21-00,6-9 ZONE D.SDR TXER100924Tail Rotor · wornTAIL ROTOR, OUT OF LIMITS IAW 64-21-00,6-9 PG. 602 ZONE E.SDR TXER097127Blower · inoperativeBLOWER INOP.SDR ALGA096919Scissors · debondedFOUND WEAR PLATE DEBONDED. REPLACED WITH NEW PART IN FIELD.SDR ALGA096916Disc Pack · crackedFOUND CRACKED LAMINATES ON DISC PACK. REPLACED WITH NEW PART IN FIELD.SDR CA040812008Manifold · chafed(CAN) DURING RECEIVING INSPECTION A 0.010 (DAMAGE TO FUEL MANIFOLD),SDR TXER097126Blower · inoperativeBLOWER INOP.
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