Aerospatiale AS 355F1
Service difficulty reports · 203
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 = 'AS355F1' 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 = 'AS355F1' 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 96ZZZX4683Pc Board · failedINTERIOR LIGHTS INOPERATIVE. REPLACED P.C. BOARD. LIGHTS OPS CHECKED GOOD.SDR 96ZZZX5534Star · brokenREPAIR IN OVERHAUL SHOP FOUND SWASHPLATE NON-ROTATING STAR BRIDGES (PN 350A37-1 515-20) WORN THROUGH AND BROKEN.SDR CA960916003Crossbeam · cracked lugs(CAN) CRACKS FOUND IN MGB SUSPENSION CROSSBEAM END LUGS AS DESCRIBED IN TELEX SB 05.00.29 AND AD 96-155-053(B).SDR CA960910039Turbine Assy · damaged(CAN) DURING OPERATIONS, THE PILOT HEARD A VIOLENT NOISE FROM HIS RIGHT SIDE. INSTRUMENTS CONFIRMED ENGINE WAS LOST. PILOT PICKED UP AIRSPEED AND WAS ABLE TO CARRY OUT A ONE ENGINE LANDING. PRELIMINARY INVESTIGATION REVEALED SUBSTANTIAL DAMAGE TO THE FIRST SDR 96ZZZX4283Circuit Board · meltedPILOT REPORTED BOOST PUMP INOPERATIVE IN-FLIGHT. FOUND PRINTED CIRCUIT BOARD AND CONNECTOR MELTED AT ONE CORNER. REPLACED CONNECTOR AND PCB. SUBMITTER RECOMMENDS AMENDING STARTING PROCEDURE TO TURN BOOST PUMP SWITCH OF JUST PRIOR TO STARTING ENGINES. SUSPSDR CA960909006Crossbeam · cracked(CAN) CRACKS FOUND IN MGB SUSPENSION CROSSBEAM END LUGS AS DESCRIBED IN TELEX SB 05.00.29 AND AD 96-155-053(B).SDR 96ZZZX4840Circuit Board · failedFORWARD TANK BOOST PUMP QUIT DURING FLIGHT. REPLACED ALPHA 15 CIRCUIT BOARD. OPS CHECK GOOD.SDR HEEA967404Starflex · crackedCRACKED STARFLEX ARM BEYOND LIMITS.SDR KCDA962Connector · wire failedPILOT REPORTED LH FUEL BOOST PUMP INOPERATIVE. FOUND ELECTRICAL CONNECTOR AT 15 ALPHA PANEL TO BE BLACKENED AND DEFORMED DUE TO APPARENT ELECTRICAL SHORT. ONE WIRE IN CONNECTOR HAD BURNED ITSELF WHICH CAUSED PUMP TO GO INOP. FUSE IN CIRCUIT DID NOTOPEN. THIS ISDR 96ZZZX3405Union · crackedREMOVED FOR A FUEL PUMP BYPASS CHECK DUE TO DELAYED LIGHT-OFFS ON A C20F ENGINE. UNION WAS FOUND CRACKED AFTER LOOSENING B-NUT. BYPASS CHECK COMPLETED AND CHECK PASSED, STILL HAD NO RESOLVE TO DELAYED LIGHT-OFFS. INSTALLED UNION AND FUEL TUBE ASSEMBLY AND TSDR 96ZZZX3238Laminated Hinge · bearing failedPREMATURE FAILURE OF LAMINATED TEETERING BEARING. T/R YOKE REMOVED AND REPLACED.SDR HEEA967184Valve · defectiveLEAKING FROM #2 TO #1 ENGINE.SDR HEEA967042Shaft · defectiveUPON INSPECTION OF NEW OUTER PT SHAFT NOTED THE FOLLOWING: ALSEAL COATING FLAKING ON SHAFT O.D. NEW PART INSTALLED.SDR HEEA967030Transceiver · inoperativeTRANSCEIVER INOPERATIVE DISPLAY. DOESN'T TRANSMIT OR RECEIVE. SMELLS BURNT.SDR 96ZZZX2248Switch · failedON 4-14-96 SHORTLY AFTER TAKEOFF, THE OIL PRESSURE DROPPED FROM 7 BARS TO 2.8 BARS. REPLACED NR 1 ENGINE OIL PRESSURE SWITCH. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT HOBBS TIME 142.2. SECOND SWITCH FAILURE IN .7 HRS.SDR 96ZZZX2247Switch · failedON 4-13-96 SEVERAL MINUTES AFTER TAKEOFF, NR 1 ENGINE OIL PRESSURE DROPPED ALMOST TO ZERO. REPLACED NR 1 ENGINE OIL PRESSURE SWITCH. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT HOBBS TIME 141.5.SDR CA960419001Governor · missing(CAN)CIRCLIP AND WASHER SECURING DRIVE GEAR TO GOVERNOR SPLINED DRIVE FOUND MISSING WHEN GOVERNOR REMOVED FOR OVERHAUL. THIS ALLOWS THE DRIVE GEAR TO FLOAT BACK AND FORTH IN THE ENGINE GEARBOX DRIVE.SDR 96ZZZX1809Bolt · brokenFOUR BOLTS THAT SECURE THE MAIN ROTOR STARFLEX TO THE MAIN ROTOR MAST WERE FOUND BROKEN DURING TROUBLESHOOTING OF AN OUT-OF-BALANCE CONDITION WITH THE MAIN ROTOR SYSTEM. THERE ARE A TOTAL OF 12 BOLTS IN THE SYSTEM. AN ADDITIONAL 3 BOLTS FAILED WHEN THE SYSTESDR 96ZZZX1808Bolt · brokenFOUR BOLTS THAT SECURE THE MAIN ROTOR STARFLEX TO THE MAIN ROTOR MAST WERE FOUND BROKEN DURING TROUBLESHOOTING OF AN OUT-OF-BALANCE CONDITION WITH THE MAIN ROTOR SYSTEM. THERE ARE A TOTAL OF 12 BOLTS IN THE SYSTEM. AN ADDITIONAL 3 BOLTS FAILED WHEN THE SYSTESDR HEEA966917Tube Assy. · defectiveENGINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF GEARBOX PARTS NOTED THE FOLLOWING: OIL TRANSFER TUBE FAILED DIMENSIONAL CHECK IN ACCORDANCE WITH CEB1307. INSTALLED A NEW OIL TUBE ASSEMBLY.SDR HEEA966860Wheel · blade erodedENGINE REMOVED DUE TO #1 AND #2 WHEEL CYCLE RETIREMENT. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: 1ST STAGE WHEEL BLADES MINOR SULFIDATION AND ERODED LEADING EDGE. SCRAPPED 1ST STAGE WHEEL.SDR 96ZZZX1803Laminated Hinge · excess wearINSTALLED TEETERING BEARINGS (LAMINATED HINGE) AT ONE-HUNDRED HOUR INSPECTION, 60 HOURS AGO, THEN AT PRE-FLIGHT, NOTICED SEVERE WEAR. REMOVED FROM SERVICE. SUBMITTED TO MANUFACTURE FOR WARRANTY.SDR HEEA966766Transmitter · defectiveCONTACTS OPEN FROM 1.2 TO 1.4 BARS THEN CLOSES.SDR HEEA966700Indicator · erraticT4 INDICATOR NEEDLE HAS A ERRATIC INDICATION. TIME SINCE REPAIR 0:00.SDR CA960306013Mount · cracked(CAN)LEFT HAND FORWARD MOUNT ASSEMBLY FOUND CRACKED.SDR HEEA966654Elec. Box · defectiveR/H GENERATOR WILL NOT COME ON LINE.SDR HEEA966630Transmitter · fluctuatesTRANSMITTER FLUCTUATES AT IDLE SPEED.SDR HEEA966611Indicator · errorCHECKED INDICATOR USING BARFIELD T-1000 AND FOUND INDICATOR 40 DEGREES OFF. INDICATOR COULD NOT BE ADJUSTED. ADJUSTMENT SCREW IS STRIPPED OUT AND PUSHED IN.SDR HEEA966448Sensor Assy · malfunctionAUTO RELIGHT COMES ON IN FLIGHT. REPLACED WITH SERVICEABLE TRANSDUCER.SDR HEEA966422Servo · leakingLEAKING AT PILOT VALVE AND BOTH ENDS OF CYLINDER ALSO OUT OF TIMING. SENT TO AMERICAN EUROCOPTER CORP. ..THEIR PROPERTY BEING RETURNED. (PHI REQUESTS FOR CREDIT)SDR HEEA966330Blade · errosionENGINE REMOVED DUE TO LOW POWER AND OIL LEAKING. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: 50% OF 1ST STAGE WHEEL SULFIDATED AND DELAMINATED ON FORWARD SIDE OF BLADES AND EROSION OF ALL LEADING EDGES AND BLADE TIPS. SCRAPPED 1ST STAGE WHEEL.SDR HEEA956252Indicator · reads lowINDICATOR READS LOW AT 800 DEGREES AND CRACKED SEAL.SDR HEEA956237Elt · inoperativeELT G SWITCH INOPERATIVE.SDR HEEA956235Structure · misinstalledFORWARD UPPER CORNER DOES NOT FIT PROPERLY. MODIFIED LT CARGO DOOR TO FIT AIRCRAFT.SDR 96ZZZX561Thrust Bearing · blisteredTHE MAIN ROTOR SPHERICAL THRUST BEARINGS HAVE BEEN MONITORED IN SERVICE ON THIS AIRCRAFT DUE TO THE WEAR OF THE ELASTOMER MATERIAL. THESE BEARINGS HAVE A HISTORY OF A SHORT LIFE IN RELATIONSHIP TO THEIR PUBLISHED LIFE LIMIT OF 6,400 HOURS.SDR 96ZZZX560Thrust Bearing · blisteredTHE MAIN ROTOR SPHERICAL THRUST BEARINGS HAVE BEEN MONITORED IN SERVICE ON THIS AIRCRAFT DUE TO THE WEAR OF THE ELASTOMER MATERIAL. THESE BEARINGS HAVE A HISTORY OF A SHORT LIFE IN RELATIONSHIP TO THEIR PUBLISHED LIFE LIMIT OF 6,400 HOURS.SDR 96ZZZX559Thrust Bearing · blisteredTHE MAIN ROTOR SPHERICAL THRUST BEARINGS HAVE BEEN MONITORED IN SERVICE ON THIS AIRCRAFT DUE TO THE WEAR OF THE ELASTOMER MATERIAL. THESE BEARINGS HAVE A HISTORY OF A SHORT LIFE IN RELATIONSHIP TO THEIR PUBLISHED LIFE LIMIT OF 6,400 HOURS.SDR 95ZZZX7057Ball End · misinstalledDURING IN-FLIGHT ENGINE TREND CHECK OF ACFT ENGINES, PILOTS DISCOVERED REVERSE OPERATION OF THE NR 2 ENGINE TRIM OR ANTICIPATOR CONTROL AT MID-POINT OF ACTUATION. AFTER RIGGING ACFT PER N.W.C., AND THOROUGH TROUBLESHOOTING, DETERMINED THE ECCENTRIC BALL END LSDR HEEA956114Skynav 5000 · defectivePOWER BUTTON IS SUNK INSIDE UNIT.SDR 96ZZZX744Spring · brokenDURNG CRUISE FLIGHT, NR 2 ENGINE DROPPED TO FLIGHT IDLE. GOVERNOR SPRING ON NR 2 ENGINE WAS FOUND BROKEN.SDR 96ZZZX109Spring · brokenDURING CRUISE FLIGHT, NR 2 ENGINE DROPPED TO FLIGHT IDLE. GOVERNOR SPRING ON NR 2 ENGINE WAS FOUND BROKEN.SDR HEEA955872Stator · leads defectiveBRUSH LEADS ARE TOO SHORT; DOES NOT REACH SCREW HOLE OF BRUSH BOXES.SDR HEEA955833Starflex · bushing wornSTARFLEX THREE ARM BUSHINGS WORN BEYOND LIMITS.SDR HEEA955805Skynav 5000 · defectiveNO FACE LIGHTS AND COULD NOT TURN OFF.SDR HEEA955734Stators · defectiveWHEN INSTALLING ON STARTER GENERATOR TERMINAL THE FIELD LEAD BROKE OFF. REMOVED FROM STARTER GEN. P/N 150SG117Q, S/N 1260.SDR 95ZZZX6090Detector · brokenDURING APPROACH TO LAND, NR 1 ENGINE FIRE LIGHT ILLUMINATED. DURING TROUBLESHOOTING, THE WIRE AT NR 1 ENGINE FORWARD INBOARD FIRE DETECTOR WAS FOUND BROKEN. REPAIRED WIRE.SDR HEEA955624Cell · defectiveTIME. INSPECTED BY ACCESSORY SHOP AND FOUND CELL #2 WOULD NOT ACCEPT A CHARGE. CELL REPLACED WITH ONE GIVEN ON CONSIGNMENT.SDR 95ZZZX5542Starflex · brokenAIRCRAFT SUFFERED SEVERE VIBRATION ON APPLICATION OF POWER AFTER START. AIRCRAFT HAD NOT TAKEN OFF. UPON EXAMINATION, THE YELLOW EAR OF THE STARFLEX WAS FOUND BROKEN OFF AND THE TAIL BOOM WAS BENT DOWNWARDS. CAUSE IS UNDER INVESTIGATION.SDR 95ZZZX5506Transducer · inoperativeIGNITION TRANSDUCER UNIT INOPERATIVE. REPLACED WITH NEW UNIT(S) CORRECTED PROBLEM.SDR HEEA955480Tube Assy · making metalENGINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF GEARBOX PARTS NOTED THE FOLLOWING: BELOW CEB1307 REQUIREMENTS ON TUBE ASSEMBLY. INSTALLED NEW TUBE ASSY. PART RETURNED TO ALLISON FOR CEB1307. REFERENCE: AFA#24405A (PART IS OUT OF CALENDAR DATE AND
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